US20010054381A1 - High temperature chemical vapor deposition chamber - Google Patents
High temperature chemical vapor deposition chamber Download PDFInfo
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- US20010054381A1 US20010054381A1 US09/211,998 US21199898A US2001054381A1 US 20010054381 A1 US20010054381 A1 US 20010054381A1 US 21199898 A US21199898 A US 21199898A US 2001054381 A1 US2001054381 A1 US 2001054381A1
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- chamber
- temperature
- pedestal
- liner
- chamber body
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- 238000005229 chemical vapour deposition Methods 0.000 title description 14
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 136
- 238000000034 method Methods 0.000 claims abstract description 108
- 230000008569 process Effects 0.000 claims abstract description 91
- 239000007789 gas Substances 0.000 claims abstract description 90
- 230000008021 deposition Effects 0.000 claims abstract description 35
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 claims abstract description 30
- 238000012545 processing Methods 0.000 claims abstract description 30
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical group [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 claims abstract description 26
- 238000004140 cleaning Methods 0.000 claims abstract description 24
- 238000006243 chemical reaction Methods 0.000 claims abstract description 23
- XJDNKRIXUMDJCW-UHFFFAOYSA-J titanium tetrachloride Chemical compound Cl[Ti](Cl)(Cl)Cl XJDNKRIXUMDJCW-UHFFFAOYSA-J 0.000 claims abstract description 23
- ZAMOUSCENKQFHK-UHFFFAOYSA-N Chlorine atom Chemical compound [Cl] ZAMOUSCENKQFHK-UHFFFAOYSA-N 0.000 claims abstract description 12
- 239000000460 chlorine Substances 0.000 claims abstract description 12
- 229910052801 chlorine Inorganic materials 0.000 claims abstract description 12
- 229910021529 ammonia Inorganic materials 0.000 claims abstract description 5
- 239000000758 substrate Substances 0.000 claims abstract description 4
- 238000000151 deposition Methods 0.000 claims description 37
- 238000010926 purge Methods 0.000 claims description 21
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 14
- 238000010438 heat treatment Methods 0.000 claims description 13
- 238000000137 annealing Methods 0.000 claims description 11
- 229910052759 nickel Inorganic materials 0.000 claims description 7
- 238000002156 mixing Methods 0.000 claims description 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 4
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 4
- KZBUYRJDOAKODT-UHFFFAOYSA-N Chlorine Chemical compound ClCl KZBUYRJDOAKODT-UHFFFAOYSA-N 0.000 claims description 3
- 229910010293 ceramic material Inorganic materials 0.000 claims description 3
- 229910052786 argon Inorganic materials 0.000 claims description 2
- PMHQVHHXPFUNSP-UHFFFAOYSA-M copper(1+);methylsulfanylmethane;bromide Chemical compound Br[Cu].CSC PMHQVHHXPFUNSP-UHFFFAOYSA-M 0.000 claims description 2
- 229910052757 nitrogen Inorganic materials 0.000 claims description 2
- 229910001220 stainless steel Inorganic materials 0.000 claims description 2
- 239000010935 stainless steel Substances 0.000 claims description 2
- 239000006227 byproduct Substances 0.000 abstract description 13
- 238000002955 isolation Methods 0.000 abstract description 12
- 238000011065 in-situ storage Methods 0.000 abstract description 6
- 235000012431 wafers Nutrition 0.000 description 75
- 229910000069 nitrogen hydride Inorganic materials 0.000 description 17
- 238000001816 cooling Methods 0.000 description 11
- 239000000463 material Substances 0.000 description 10
- 229910052782 aluminium Inorganic materials 0.000 description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 7
- 239000002826 coolant Substances 0.000 description 6
- 238000009826 distribution Methods 0.000 description 6
- 230000015572 biosynthetic process Effects 0.000 description 5
- 238000013461 design Methods 0.000 description 5
- 239000012212 insulator Substances 0.000 description 5
- 239000000843 powder Substances 0.000 description 5
- 239000004065 semiconductor Substances 0.000 description 5
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 5
- 239000003638 chemical reducing agent Substances 0.000 description 4
- 230000000875 corresponding effect Effects 0.000 description 4
- 230000007246 mechanism Effects 0.000 description 4
- 239000010453 quartz Substances 0.000 description 4
- 238000012546 transfer Methods 0.000 description 4
- 239000000919 ceramic Substances 0.000 description 3
- 238000005137 deposition process Methods 0.000 description 3
- 238000011068 loading method Methods 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000005086 pumping Methods 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- MHAJPDPJQMAIIY-UHFFFAOYSA-N Hydrogen peroxide Chemical compound OO MHAJPDPJQMAIIY-UHFFFAOYSA-N 0.000 description 2
- 238000009825 accumulation Methods 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 2
- 239000012159 carrier gas Substances 0.000 description 2
- 238000004518 low pressure chemical vapour deposition Methods 0.000 description 2
- 230000000737 periodic effect Effects 0.000 description 2
- 238000007747 plating Methods 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 230000000284 resting effect Effects 0.000 description 2
- -1 ring 290 Chemical compound 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 125000006850 spacer group Chemical group 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- PIGFYZPCRLYGLF-UHFFFAOYSA-N Aluminum nitride Chemical compound [Al]#N PIGFYZPCRLYGLF-UHFFFAOYSA-N 0.000 description 1
- 229920004943 Delrin® Polymers 0.000 description 1
- 229920002449 FKM Polymers 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- BOTDANWDWHJENH-UHFFFAOYSA-N Tetraethyl orthosilicate Chemical compound CCO[Si](OCC)(OCC)OCC BOTDANWDWHJENH-UHFFFAOYSA-N 0.000 description 1
- 230000003466 anti-cipated effect Effects 0.000 description 1
- 230000036760 body temperature Effects 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 239000003990 capacitor Substances 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 239000007795 chemical reaction product Substances 0.000 description 1
- 239000013626 chemical specie Substances 0.000 description 1
- 230000003749 cleanliness Effects 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 239000000498 cooling water Substances 0.000 description 1
- 230000002596 correlated effect Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000005108 dry cleaning Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 229910052736 halogen Inorganic materials 0.000 description 1
- 150000002367 halogens Chemical class 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 238000000623 plasma-assisted chemical vapour deposition Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 239000000376 reactant Substances 0.000 description 1
- 238000005546 reactive sputtering Methods 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- 238000013341 scale-up Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 229910052814 silicon oxide Inorganic materials 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000005382 thermal cycling Methods 0.000 description 1
- 238000005979 thermal decomposition reaction Methods 0.000 description 1
- 238000002207 thermal evaporation Methods 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 238000009827 uniform distribution Methods 0.000 description 1
Images
Classifications
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/455—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating characterised by the method used for introducing gases into reaction chamber or for modifying gas flows in reaction chamber
- C23C16/45563—Gas nozzles
- C23C16/45565—Shower nozzles
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/4401—Means for minimising impurities, e.g. dust, moisture or residual gas, in the reaction chamber
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/4401—Means for minimising impurities, e.g. dust, moisture or residual gas, in the reaction chamber
- C23C16/4405—Cleaning of reactor or parts inside the reactor by using reactive gases
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/4412—Details relating to the exhausts, e.g. pumps, filters, scrubbers, particle traps
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/455—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating characterised by the method used for introducing gases into reaction chamber or for modifying gas flows in reaction chamber
- C23C16/45514—Mixing in close vicinity to the substrate
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/455—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating characterised by the method used for introducing gases into reaction chamber or for modifying gas flows in reaction chamber
- C23C16/45563—Gas nozzles
- C23C16/45574—Nozzles for more than one gas
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/458—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating characterised by the method used for supporting substrates in the reaction chamber
- C23C16/4582—Rigid and flat substrates, e.g. plates or discs
- C23C16/4583—Rigid and flat substrates, e.g. plates or discs the substrate being supported substantially horizontally
- C23C16/4584—Rigid and flat substrates, e.g. plates or discs the substrate being supported substantially horizontally the substrate being rotated
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/50—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating using electric discharges
- C23C16/505—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating using electric discharges using radio frequency discharges
- C23C16/509—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating using electric discharges using radio frequency discharges using internal electrodes
- C23C16/5096—Flat-bed apparatus
Definitions
- the present invention relates to semiconductor wafer processing systems and, more particularly, to a high temperature chemical vapor deposition (CVD) chamber with a heated inside liner, and a temperature-controlled outer chamber body.
- CVD chemical vapor deposition
- Titanium nitride (TiN) film has found wide applications in ultra large-scale integrated circuits (ULSI) as a diffusion barrier and as an adhesion layer for tungsten contacts.
- Low temperature reactive sputtering of Ti in the presence of nitrogen has been used in the past to deposit TiN films upon semiconductor wafers.
- CVD chemical vapor deposition
- TiN film from a titanium tetrachloride based CVD process can be used as a high aspect ratio contact barrier, a capacitor top electrode or in plug fill processes below 0.18 ⁇ m.
- Both cold wall and hot wall low pressure chemical vapor deposition (LPCVD) processes have been used for depositing TiN films using a reaction between titanium tetrachloride (TiCl 4 ) and ammonia (NH 3 ).
- a cold wall reactor contains a wafer that is heated to a temperature above the reaction temperature of the process gases, e.g., over 650° C., by a halogen lamp that is located external to the chamber.
- process by-products such as adduct ammonia salts will detrimentally form on the interior surfaces of the cold chamber walls or other cold surfaces.
- these deposits may flake and fall on a wafer causing contamination and reducing wafer yield. Since these reaction by-products cannot be removed by in-situ chamber cleaning processes, frequent chamber disassembly and cleaning is required. This necessitates the opening of the chamber to the atmosphere, and results in considerable down time for the chamber.
- quartz hot wall reactors have been used to form high quality TiN films.
- the heated walls of these reactors help reduce accumulation of undesirable deposits, such as adduct ammonia salts, on the interior chamber walls.
- hot wall chambers can be dangerous to operate because of the high temperature of the walls, e.g., 150-200° C.
- the heated liner lies against the inner surface of the cold reactor wall, and, as such, is only partially insulated from the reactor wall. Not only does this contact promote excessive thermal conduction to the reactor wall resulting in the chamber wall becoming dangerously hot, but additional heating of the liner will be needed to compensate for the heat lost to the wall.
- an apparatus for processing a wafer having a chamber body that encloses a chamber liner, where the liner is maintains a spaced apart distance from the chamber body such that the liner is maintained at a higher temperature than the chamber body.
- the liner can be maintained at a temperature that reduces the amount of deposition on the liner while maintaining a safe temperature for the chamber body.
- the present invention relates to a process chamber system for high temperature film deposition, e.g., using a reaction between titanium tetrachloride (TiCl 4 ) and ammonia (NH 3 ) to deposit titanium nitride (TiN).
- the system comprises a process chamber and an exhaust assembly.
- the process chamber has an inside liner which is maintained at a temperature of approximately 150-250° C., while the chamber body is maintained at a temperature of approximately 60-65° C. or below.
- the liner can either be heated directly by a resistive heater embedded in the liner, or indirectly by a heated wafer support pedestal.
- the liner which is substantially cylindrical, is enclosed within the bucket-shaped chamber body having a cylindrical wall and a base.
- Isolating pins are located between the bottom of the liner and the inside surface of the chamber base such that a spacing is maintained between the liner and the chamber body, i.e., the liner only contacts the chamber body through the isolating pins. Excellent thermal isolation is achieved between the liner and the chamber body because of the low thermal conductivity resulting from the small contact area between the isolating pins and the liner.
- the process chamber further comprises a heated wafer support pedestal for supporting and heating a semiconductor wafer and a showerhead for separately introducing TiCl 4 and NH 3 into the process chamber into a space above the wafer.
- the wafer is maintained at a temperature of approximately 600-700° C. such that a thermal reaction occurs at the surface of the wafer between TiCl 4 and NH 3 , resulting in the formation of a TiN film upon the wafer.
- the exhaust assembly is connected to the process chamber to allow for continuous pumping of gases away from the process chamber.
- a substantial portion of the exhaust assembly is maintained at approximately 150° C.-200° C. by the use of several heaters disposed on the outside walls of the exhaust assembly. Such heating reduces reaction by-product accumulation within the exhaust assembly.
- FIG. 1 is a partial cross-sectional perspective view of the high temperature CVD chamber system of the present invention, showing a process chamber and an exhaust assembly;
- FIG. 2 a is a cross-sectional view of the process chamber, showing details of various components inside the process chamber of FIG. 1;
- FIG. 2 b shows an enlarged cross-sectional view around the area of the inside liner, the isolating pin and the chamber body of FIG. 2 a;
- FIG. 3 a shows a cross-sectional view of the showerhead assembly
- FIG. 3 b shows a cross-sectional view of the dual-gas faceplate of the showerhead assembly of FIG. 3 a;
- FIG. 4 a is a top view of the cooling plate
- FIG. 4 b is a cross-sectional view showing the channel inside the cooling plate of FIG. 4 a;
- FIG. 4 c is a side view of the cooling plate of FIG. 4 a;
- FIG. 5 a is a cross-sectional view of the process chamber showing the bottom purge arrangement
- FIG. 5 b is a perspective view of another embodiment of an edge ring
- FIG. 5 c is a partial cross-sectional view of the edge ring (line 5 c in FIG. 5 b ) resting atop of the liner;
- FIG. 5 d is a partial cross-sectional view of the edge ring (line 5 d in FIG. 5 b ) resting atop of the liner;
- FIG. 6 shows a partial cross-sectional view of the exhaust assembly
- FIG. 7 a shows a conceptual design of a process chamber modified for plasma application
- FIG. 7 b is a cross-sectional view illustrating the RF connections to the chamber of FIG. 7 a.
- FIG. 1 shows a partial cross-sectional perspective view of a high temperature chemical vapor deposition (HT CVD) system, including a process chamber 100 and an exhaust assembly 600 .
- a chamber mounting plate 110 is provided for mounting this process chamber 100 onto a wafer transfer chamber (not shown) which interfaces the process chamber 100 to the rest of a complete wafer processing system, such as a Centura 5200 system (not shown) manufactured by Applied Materials, Inc. of Santa Clara, Calif.
- Cross-sectional views illustrating various components in the process chamber 100 are shown in FIGS. 2 - 5 . To best understand the process chamber 100 of the present invention and its operation, the reader should simultaneously refer to all these figures.
- the process chamber 100 of the present invention performs, for example, high temperature deposition of titanium nitride upon a semiconductor wafer using a TiCl 4 +NH 3 chemistry. Since the thermal decomposition of TiCl 4 and NH 3 occurs at high temperature, the wafer should preferably be maintained at a temperature range of 600-700° C. to facilitate deposition upon the wafer.
- the process chamber 100 comprises a chamber body 250 , a liner 200 , a pedestal assembly 160 and a showerhead assembly 300 .
- the pedestal assembly 160 contains a pedestal 180 that supports the wafer in the chamber 100 .
- the dual-gas showerhead assembly 300 is positioned in a parallel, spaced apart relation with respect to the pedestal 180 such that the wafer support surface of the pedestal 180 and a faceplate 330 of the showerhead assembly 300 define a reaction zone.
- the wafer is heated by a heated pedestal 180 while the showerhead assembly 300 introduces the two reactant gases (TiCl 4 and NH 3 ) into the process chamber 100 such that reaction occurs only above the wafer, resulting in TiN deposition onto the wafer.
- the interior wall of the chamber i.e., the chamber liner 200
- the chamber liner 200 is maintained at a temperature between 150° C. to 250° C.
- An improved bottom purge arrangement is also provided to reduce undesirable adduct reaction by-products which may form on cold areas of the chamber.
- the heated exhaust assembly 600 also prevents the formation of powder deposits on the interior walls of the exhaust assembly 600 .
- This powder deposit is a reaction by-product between TiCl 4 and NH 3 which forms at a temperature below 150° C.
- minimal amounts of TiN is deposited on interior chamber components.
- the TiN film that is inadvertently deposited on chamber components can readily be removed by an in-situ thermal chlorine cleaning process performed within chamber 100 of the present invention.
- the chamber body 250 is substantially bucket-shaped, with a cylindrical side 254 and a base 252 . There is an opening 256 at one portion of the cylindrical side 254 , which is connected to the exhaust assembly 600 for the removal of process and product gases.
- the chamber base 252 has a centrally-located opening 258 , which is provided to accommodate a pedestal assembly 160 , as well as a gas purging arrangement to be described below.
- An inside liner 200 which is substantially cylindrical, is located on the inside, but spaced apart from the chamber body 250 .
- the chamber body 250 which substantially encloses this inside liner 200 , is made of nickel-plated aluminum.
- nickel plating is needed to protect the aluminum components from corrosion by chlorine gas, which is used in an in-situ chamber cleaning process to be described below.
- alternative metal-plating may be used as long as it is compatible with the chemical species used in the reaction or cleaning processes.
- the chamber body temperature is maintained at approximately 60° C.-65° C. or less by thermally isolating the chamber body 250 from the inside heated liner 200 .
- the inside liner 200 which is also made of nickel-plated aluminum, has an embedded resistive heater 215 for establishing a fixed liner temperature.
- a thermal conductive paste is applied to the resistive heater 215 and enclosed within a cover plate 207 which is welded to the liner 200 to ensure good thermal conductivity between the heater 215 and the liner 200 .
- An AC voltage is coupled to the heater 215 using AC connectors inside a feedthrough portion 214 of the liner 200 .
- This heater 215 can optionally be used to dynamically control the temperature of the liner 200 .
- the heater 215 may be used to maintain the liner temperature at approximately 150 to 250° C. to avoid the formation of adduct ammonia salt or other process by-products on the interior surface of liner 200 .
- a Type K thermocouple 212 is removably inserted in the liner 200 approximately half the distance along its cylindrical wall 204 .
- the liner temperature can be measured at approximately half way from the bottom 202 of the liner 200 .
- Connectors (not shown) for the thermocouple 212 and the resistive heater 215 are located inside the feedthrough portion 214 of the liner 200 .
- a clamping plate 216 seats an O-ring 201 against the chamber base 252 and the feedthrough portion 214 to seal the interior of the chamber 100 from the outside atmosphere.
- independent heating by the resistive heater 215 is not always necessary to achieve an appropriate liner temperature since the operation of the heated pedestal 180 (see FIG. 2 a ) alone is generally sufficient to maintain the temperature of the liner 200 within the desired range of 150-250° C.
- this heater 215 may be used, alone or in conjunction with the heated pedestal 180 , for other processes with different temperature requirements.
- the inside liner 200 and the chamber body 250 are substantially isolated from each other by means of three dowel pins 220 , one of which is shown in the cross-sectional view in FIG. 2 a .
- These isolating pins 220 are located between the bottom 202 of the inside liner 200 and the inside surface 253 of the chamber base 252 .
- the area around the inside liner 200 , dowel pin 220 and the chamber base 252 is shown in an enlarged cross-sectional view in FIG. 2 b .
- the three pins 220 are arranged to lie equidistant from each other on the circumference of a circle, subtending angles of 120 degrees at the center of the circle.
- Each dowel pin 220 has a central portion 221 having a diameter d 1 and two smaller ends 222 and 223 , each having a diameter d 2 , where d 2 is less than d 1 .
- a drilled-through hole 225 is provided along the longitudinal axis of the pin 220 to allow for pump-out of any trapped gases.
- the pins 220 are press-fit into corresponding receiving holes 224 in the bottom 202 of the liner 200 , such that the liner 200 rests against one side of the larger central portion 221 of each pin 220 .
- One of these holes 226 is round, and the other two are slotted (not shown) to provide for additional assembly tolerance.
- the pins 220 serve to maintain a proper spacing (s) between the liner 200 and the chamber base 252 .
- This spacing (s) corresponds to the thickness of the larger central portion 221 of the pin 220 , which is about 0.135′′ (3.4 mm).
- Four 1 ⁇ 4-20 nickel screws (not shown), which also lie on the circumference of the same diameter circle as the dowel pins 220 , are used to secure the liner 200 in place by screwing into corresponding tapped holes (not shown) on the inside surface 253 of the chamber base 252 .
- the small contact areas of the nickel pins 220 and screws ensure very good thermal isolation between the heated liner 200 and the chamber body 250 , and allows the chamber body 250 to be kept at around 65° C. while maintaining the heated liner at 150-250° C.
- dowel pins 220 can be made of a variety of materials that can withstand high temperatures and have a relatively high thermal resistivity (low thermal conductivity), such as stainless steel or nickel.
- the choice of material depends on the specific processing applications.
- nickel (200 or 201 grade) is the preferred material because of its chemical resistance to chlorine and high thermal resistance.
- the dimensions and specific layouts for the various components are for illustrative purpose only.
- the liner 200 could be spaced from the body 250 by intermittently spaced ribs formed in the bottom 252 of chamber body 250 , a continuous annular ridge formed in the bottom 252 of the chamber body 250 , a spacer ring positioned on the bottom 252 of the chamber body 250 and the like.
- the present invention encompasses many other chamber/liner/spacer combinations that facilitate thermal isolation between the liner 200 and the chamber body 250 . Such isolation enables separate temperature control of these components.
- FIG. 3 a shows a cross-sectional view of the dual-gas showerhead assembly 300 , comprising a nickel-plated aluminum lid/gas box (manifold assembly 310 ) and a faceplate 330 .
- the showerhead assembly 300 provides a dual-gas separate entry for TiCl 4 and NH 3 into the process chamber 100 without premixing of the gases.
- the gas manifold assembly 310 also serves as the lid of the chamber 100 .
- the faceplate 330 is described in a commonly-assigned patent application by Umotoy et al. entitled “Dual Gas Faceplate for a showerhead in a Semiconductor Wafer Processing System,” Ser. No. 09/098,969, filed Jun. 16, 1998; which is herein incorporated by reference.
- the showerhead assembly 300 allows two gases, for example, NH 3 and TiCl 4 , to be separately introduced into the reaction region, or processing zone 515 .
- the processing zone 515 is roughly defined by the space between the bottom 332 of the faceplate 330 and the heated pedestal 180 , which is the top portion of a pedestal assembly 160 to be described below. (See FIG. 5 a .)
- separate flow paths or passageways are established through different channels 320 or chambers 322 inside the showerhead assembly 300 . These channels 320 and chambers 322 prevent mixing of the two gases prior to reaching the process zone 515 .
- the gas manifold or lid 310 comprises three plates—bottom 312 , middle 314 and top 316 , which have been fused together by vacuum brazing their mating surfaces 334 and 336 using a silicon-rich aluminum film, clamping the entire assembly and placing the assembly in a furnace at a temperature of approximately 550° C. to form a unitary manifold assembly 310 .
- no O-rings are necessary to provide isolation between the process gases as they flow through the manifold assembly 310 .
- These plates 312 , 314 and 316 contain a combination of channels 320 and chambers 322 , such that when the faceplate 330 is bolted to the manifold assembly 310 , the myriad of channels 320 and chambers 322 provide proper passageways, or flow paths, for introducing two gases separately from their supply sources (not shown) outside the chamber 100 into the process zone 515 without pre-mixing of the gases.
- the faceplate 330 further comprises a lower gas distribution plate 340 and a upper gas distribution plate 350 , as shown in FIG. 3 b .
- the specific arrangement of channels 343 and holes ( 351 , 352 , 341 , 342 and 344 ) that together define distinct passageways or flow paths for the two process gases are described in detail in the above-referenced patent application Ser. No. 09/098,969. Suffice to say that when the two plates, 340 and 350 , are fused together using the same technique as previously described for the gas manifold plates 312 , 314 and 316 , the resulting unitary faceplate 330 provides separate passageways, or flow paths, for uniformly introducing two gases into the processing zone 515 without pre-mixing of the gases.
- holes 341 and 342 there are two sets of holes, 341 and 342 , in the lower plate 340 , one for each gas.
- one set of holes 341 aligns with holes 351 in the upper plate to form one flow path (from 351 , via 344 to 341 ) for one gas, e.g., TiCl 4 .
- the other set of holes 342 are connected to channels 343 within the lower plate 340 . These channels 343 are in turn connected to a circumferential plenum 390 , which is formed between the upper and lower plates, 350 and 340 , when they are fused together.
- the plenum 390 is further connected to another hole 352 in the upper plate 350 , which provides an inlet for a second gas, e.g., NH 3 .
- a second gas e.g., NH 3 .
- This configuration allows the first gas to pass through the first passageway (e.g., from 351 , via 344 to 341 ) and the second gas to pass through the second passageway (e.g., from 352 , via 390 to 343 and 342 ) within the faceplate 330 without mixing until the gases enter the process zone 515 after exiting from these holes 341 and 342 at the bottom 332 of the faceplate 330 .
- the choice of hole size for each gas and hole distribution are functions of process conditions. For example, the hole size will vary depending upon gas flow rate, gas pressure, gas type, chamber pressure and the faceplate 330 such that gas flow rates through the holes are correlated with the locations of the holes in the faceplate 330 .
- the showerhead assembly 300 is formed by affixing the faceplate 330 directly to the bottom of the gas distribution manifold 310 using a plurality of bolts (not shown) through the mounting holes (hole 396 is shown in FIG. 3 b ) in the faceplate 330 .
- An O-ring groove 325 (see FIG. 3 a ) is provided in the gas manifold 310 to accommodate an O-ring 326 which is used to provide sealing between the gas manifold 310 and the faceplate 330 .
- Different types of O-ring materials, such as Viton may be used, as long the material is compatible with the operating temperature and chemically resistant to the gases used in the process.
- Both the faceplate 330 and the gas distribution manifold 310 are made of nickel-plated aluminum or some other thermally conductive and chlorine compatible materials such as nickel. Of course, other material choices are possible as long as they provide the thermal conductivity and/or chemical compatibility which are necessary for the specific process.
- the showerhead assembly 300 can be coupled to a cold plate assembly 400 or other cooling apparatus that will maintain the entire lid/gas box 310 at a uniform and constant temperature.
- the showerhead assembly 300 is heated by the heated pedestal 180 through thermal radiation in the reaction zone 515 . Therefore, to avert deposition of TiN or by-products of the TiN deposition process upon and/or within the showerhead, a cold plate assembly 400 is necessary to maintain the faceplate temperature within a range of 150-250° C.
- the cold plate assembly 400 serves a dual-purpose of preventing the showerhead assembly 300 from temperature drift, as well as keeping the areas around the O-ring seal to within specification for proper sealing.
- FIG. 4 a is a schematic illustration of the top view of the cold plate assembly 400 .
- This cold plate assembly 400 is substantially annular in shape, except for a rectangular protruded portion 402 .
- FIG. 4 b shows a cross-sectional view of the cold plate assembly 400 , comprising a top plate 440 and a bottom plate 420 , which are brazed together and then nickel-plated as an assembly.
- the top plate 440 has a coil-shaped channel 410 passing through the plate 440 for circulating coolant, as illustrated in FIG. 4 a .
- the two ends, 412 and 414 , of the coil-shaped channel 410 are located at the rectangular protruded portion 402 , and serve as the inlet and outlet for the coolant.
- the channel 410 has a rectangular cross-section and is open on its bottom side 415 . This is illustrated in the cross-sectional view shown in FIG. 4 b and the side view shown in FIG. 4 c .
- the top surface 425 of the bottom plate 420 when brazed together with the top plate 440 , defines a closed channel 445 through which a coolant can circulate.
- the bottom plate 420 has two apertures 422 and 424 , close to the end of the rectangular protruded portion 402 . These apertures 422 and 424 are aligned respectively with the two ends 412 and 414 of the top plate channel 410 to provide for coolant inlet and outlet.
- the coolant typically water, is connected in series with the coolant for the chamber 100 .
- the cold plate assembly 400 is attached onto the top of the lid/gas box ( 310 in FIG. 3 a ) using screws at locations 430 around the circumference of the cold plate assembly 400 .
- one annular portion 421 of the bottom plate 420 is recessed such that only an inner 426 and an outer 428 portion of the bottom plate 420 actually come into physical contact with the chamber lid 310 .
- the cooling plate assembly 400 , lid/gas box 310 and the faceplate 330 are sometimes collectively referred to as a lid assembly. With an inlet water temperature of about 45-55° C., the lid/gas box 310 can readily be maintained within a temperature range of 60-65° C.
- this cold plate assembly 400 is a cost-effective design feature which allows for ease of maintenance as well as design and process flexibility. For example, different temperature control scenarios for the faceplate 330 may be achieved by a suitable interchange with a different cooling (or heating) plate that provide more or less heating or cooling. To most effectively process a wafer or wafers, the cold plate assembly 400 that is best suited for a particular process can be easily installed onto the chamber lid.
- FIG. 5 a illustrates a pedestal assembly 160 in a cross-sectional view within the process chamber 100 .
- the pedestal assembly 160 comprises a flat circular portion 180 at the top, sometimes referred to as a susceptor or pedestal; and a bottom cylindrical shaft-like portion 560 which extends downwards through the centrally-located opening 258 at the bottom 252 of the chamber body 250 .
- the upper surface 185 of the pedestal 180 has a wafer pocket 563 to support a wafer 564 (shown in phantom in FIG. 5 a ), and four clearance holes to accommodate wafer lift pins 285 .
- These wafer lift pins 285 are made of ceramic, and are used for wafer-handling and transport.
- the current pedestal assembly 160 and chamber design can accommodate wafer diameters of 125 mm, 150 mm and 200 mm, respectively. Those skilled in the art can perform proper design scale-up to encompass applications to larger wafer diameters such as 300 mm as well.
- the pedestal 180 preferably made of a ceramic material such as aluminum nitride (AlN), is further equipped with two embedded electrodes 571 and 572 .
- these electrodes 571 and 572 made of different types of conducting materials, can be of various thicknesses and shapes.
- one of these electrodes is a radio-frequency (RF) grid 571 for performing plasma clean and other plasma processes such as plasma annealing of the wafer.
- the mesh-type grid 571 made of molybdenum, is located slightly below the pedestal's top surface 185 . Slightly below the RF electrode is an alternating current (AC) grid 572 for heating purpose.
- AC alternating current
- the pedestal 180 currently in use is made of a dark gray, high resistivity AlN of 99.9% purity. Of course, other similar heaters may also be used, depending on the specific process requirements.
- This heated pedestal 180 allows the wafer temperature to be controlled within a range of approximately 600-800° C.
- TiN film deposition can also be performed between 200-600° C., the resulting TiN film tends to have an undesirably high chlorine content. Therefore, the wafer temperature is preferably maintained within a range of 600-700° C. for optimal deposition results.
- the pedestal assembly 160 moves vertically within the chamber cavity by a lift mechanism (not shown) between a first (top) position 501 and a second (bottom) position 502 .
- This second position 502 of the pedestal assembly 160 is illustrated in phantom in FIG. 5 a .
- the pedestal assembly 160 is placed in the first position 501 .
- a reaction zone, or process zone 515 , within the chamber cavity 280 can be defined roughly as the space between the bottom 332 of the faceplate 330 and the pedestal top surface 185 , and confined on the side by the edge ring 290 .
- a wafer substrate 564 is positioned in the wafer pocket 563 during wafer processing, and the distance between the wafer and the bottom of the faceplate 330 is approximately 0.360′′ (9.1 mm). Note that this distance is for illustrative purpose only, and it may be different for other process applications.
- the spacing 530 between the outside edge 186 of the pedestal 180 to the inside surface 286 of the liner 200 is about 0.125′′ (3.2 mm). The choice of this spacing 530 is determined both by the specified temperature of the liner 200 and the need to prevent purge gas from entering the process zone 515 .
- the pedestal assembly 160 Before and after film deposition for each wafer, the pedestal assembly 160 is moved to a second position 502 for wafer loading or unloading. In this second position 502 , the pedestal top surface 185 is slightly below a slit valve opening 260 , which is located on the side, or cylindrical wall, 204 of the chamber liner 200 and the cylindrical side 254 of the chamber body 250 .
- a wafer can be transported in and out of the process chamber 100 through the slit valve opening 260 to an adjacent transfer chamber and/or load-lock chamber (not shown), or another chamber within a cluster tool.
- a cluster tool of a type that can be coupled to the process chamber 100 is described in a commonly assigned U.S. Pat. No. 5,186,718, entitled “Staged-Vacuum Wafer Processing System and Method”, issued Feb. 16, 1993, and is herein incorporated by reference.
- Wafer-handling and transport is accomplished by the wafer lift pins 285 in the pedestal 180 in conjunction with a robotic transfer assembly (not shown) which has been described in a commonly assigned U.S. Pat. No. 4,951,601, entitled “Multi-chamber Integrated Process System,” issued Aug. 28, 1990; the complete disclosure of which is incorporated herein by reference.
- the sequence for wafer loading involves the pedestal being placed in position 502 , and a robotic arm transporting a wafer through the slit valve opening 260 into the process chamber 100 .
- the wafer lift ring 580 rises to engage pin bottoms such that the wafer lift pins 285 are raised above the pedestal top surface 185 to lift the wafer 564 off the robotic arm.
- the pedestal assembly 160 is raised to receive the wafer 564 in the wafer pocket 563 , and the lift ring 580 lowers to its original position.
- the pedestal assembly 160 is subsequently moved into its first position 501 for wafer processing.
- the wafer unloading sequence is a reverse of the loading sequence.
- the self-adjusting mechanism for the vertical movement of the pedestal assembly 160 has also been described in a commonly assigned U.S. patent application Ser. No. 08/738,240, filed on Oct. 25, 1996, and entitled “Self-Aligning Lift Mechanism,” the disclosure of which is herein incorporated by reference.
- FIG. 5 a also illustrates details of an edge ring 290 and a backside gas purge arrangement.
- the edge ring 290 is disposed around the outer perimeter 187 of the pedestal 180 of the pedestal assembly 160 .
- This edge ring 290 is substantially annular, with a protruding portion 292 at the bottom 294 of the ring 290 .
- this protruding portion 292 essentially divides the bottom 294 of the ring 290 into an inside bottom surface 297 and an outside bottom surface 298 .
- the edge ring 290 rests on top of the heated pedestal 180 , such that its inside bottom surface 297 covers part of the top pedestal surface 185 .
- the protruded portion 292 of the edge ring 290 covers part of the side, or outside edge 186 of the pedestal 180 .
- a space 531 is then defined between the outside bottom portion 298 of the edge ring 290 and a protruded portion 203 of the heated liner 200 .
- This gap 531 provides a choke for the bottom, or backside, purge gas flow (to be described below) and ensures uniform distribution of the purge gas about the edge of the pedestal 180 .
- the edge ring 290 rests on top of the protruded portion 203 of the heated liner 200 . As such, the edge ring does not interfere with access of the robotic transfer mechanism as it places and/or retrieves the wafer to/from the pedestal 180 .
- the edge ring 290 can be made of a variety of materials such as ceramic, quartz, aluminum and steel, among others. The exact choice of material depends, of course, on the specific process applications. For example, quartz can be used for TiN deposition using TiCl 4 +NH 3 chemistry.
- this edge ring 290 is two-fold: 1) to act as a choke such that uniform pumping can be established for the gases and/or by-products during processing; and 2) to prevent process gases from entering behind the pedestal assembly 160 , which may cause undesirable deposits in the lower portions of the chamber 100 .
- the pedestal assembly 160 is in the first (top) position 501 , such that the gap 520 between the top 295 of the edge ring 290 and the bottom 332 of the faceplate 330 is about 0.05′′ (1.3 mm).
- a backside purge is established by flowing argon through a liner purge inlet 505 into the gap 599 between the liner 200 and chamber body 250 to prevent powder deposition on the cold wall surfaces of the chamber body 250 .
- This gap 599 is about 0.06′′ (1.5 mm) wide.
- a set of holes 595 is also provided through the shaft portion 590 of the wafer lift ring 580 located around the pedestal shaft 560 at the bottom opening 258 .
- Undesirable deposition behind the pedestal 180 is prevented by establishing a purge gas flow through these holes 595 into the chamber cavity 280 , as illustrated by the arrows.
- various spaces such as 520 , 530 , and 531 are defined by different portions of the showerhead 330 , pedestal 180 , edge ring 290 , and liner 200 . It is to be understood that dimensions quoted for these spaces, like those quoted for other components, are for illustrative purpose only. In general, the choice of these dimensions depend on the desired results of a specific process being performed in the chamber. For example, spaces 530 and 531 are selected to ensure uniformity in the purge gas distribution around the edge of the pedestal 180 .
- the space 520 may be a variable parameter affecting uniformity or deposition rate in the film deposition step itself. Suffice to say that one skilled in the art of wafer processing would be able to arrive at optimal combinations of these dimensions to achieve desirable wafer processing results such as deposition uniformity.
- FIG. 5 b shows a perspective view of an alternative embodiment of an edge ring 550
- FIGS. 5 c and 5 d show partial cross-sectional views of the edge ring 550 being supported by a horizontal surface 522 of the liner 200
- FIG. 5 c illustrates the edge ring 550 with a top surface 551 , a bottom surface 552 , an inside surface 556 , an outside surface 557 , and a protruded inside portion 559 .
- the edge ring 550 is supported entirely by the liner 200 , i.e., the edge ring 550 does not contact the pedestal 180 or wafer 564 .
- a step 523 is provided on a horizontal surface 522 of the liner 200 to keep the edge ring 550 in place.
- a key stop portion 554 located on the outside surface 557 of the edge ring 550 interfits with the step 523 of the liner 200 to facilitate secure mounting of the edge ring 550 .
- three grooves or slots 565 are provided on the bottom surface 552 of the edge ring 550 (see FIG. 5 d ), and are located equidistant from each other.
- Three pins 526 are press fit into corresponding recessed holes 525 in the horizontal surface 522 of the liner 200 .
- a portion 527 of the pin 526 protrudes above the horizontal surface 522 of the liner 200 and engages the slot 565 at the bottom surface 552 of the edge ring 550 . As such, the edge ring 550 is prevented from rotating with respect to the liner 200 .
- mounting screws (not shown) can also be used to secure the edge ring 550 to the liner 200 .
- the dimensions disclosed for the pin and slot arrangement are for illustrative purpose only, and do not represent limitations pertaining to the practice of this invention. Suffice to say that in the present arrangement, the edge ring 550 is heated by thermal radiation from the pedestal 180 , and expands before the liner 200 reaches the same final temperature. This results in a uniform expansion of the edge ring 550 with respect to its centerline O-O′.
- the protruded inside portion 559 of the edge ring 550 is disposed over the outer perimeter 187 of the pedestal 180 , such that the outer perimeter 187 and the outside edge 186 of the pedestal 180 are in close proximity to and substantially surrounded by the edge ring 550 .
- undesirable deposition over the perimeter 187 and outer edge 186 of the pedestal 180 can be avoided. In this embodiment, however, there is no direct physical contact between the pedestal 180 and the edge ring 550 .
- a gap or space 568 is maintained between the top 185 of the pedestal 180 and the bottom 553 of the protruded portion 559 of the edge ring 550 .
- Another space 566 is defined between the pedestal edge 186 and the inside surface 556 of the edge ring 550 .
- a number of openings 555 are provided around the circumference of the edge ring 550 close to the bottom surface 552 . These openings 555 extend horizontally from the inside surface 556 to the outside surface 557 of the edge ring 550 . Through these openings 555 , a purge gas is pumped from the space 566 , into the space 567 between the outside surface 557 of the edge ring 550 and the inside surface 524 of the liner 200 .
- the gap 568 acts as a choke to prevent any purge gas from flowing towards the top 185 of the pedestal 180 , which may otherwise dilute the process gases and affect the deposition process. Similar to the other edge ring 290 shown in FIG.
- the top surface 551 of this edge ring 550 and the bottom 332 of the showerhead 330 defines the space 520 through which process gases and/or by-products are pumped out from the reaction zone 515 (see FIG. 5 a ).
- the dimensions of these spaces 520 , 566 , 567 and 568 are process-dependent, and are typically designed to suit the needs of a particular process. For example, one skilled in the art would seek to adjust these spacings to optimize or achieve desired results such as deposition uniformity.
- this particular configuration (the liner 200 supporting the edge ring 550 ) allows the temperature of the edge ring 550 to be maintained within a range of approximately 200-250° C., and undesirable deposition on the edge ring 550 is further minimized. Note that the use of an edge ring, while highly desirable, is not absolutely necessary for the practice of this invention.
- TiCl 4 in a He carrier gas and NH 3 in a H 2 carrier gas are introduced into the processing zone 515 via the showerhead assembly 300 and a chemical reaction between TiCl 4 and NH 3 takes place at close proximity above the wafer 564 that is supported by the heated pedestal 180 .
- the reaction results in the deposition of TiN film onto the wafer 564 .
- a continuous gas flow is maintained by the pumping system that is attached to the exhaust assembly 600 such that gases, including any volatile reaction products, are pumped out of the processing zone 515 and other areas of the chamber cavity 280 , past the space 520 between the top 295 of the quartz edge ring 290 and the bottom 332 of the faceplate 330 , through a slot 205 (see FIG. 2 a ) in the inside liner 200 , into the exhaust chamber 600 which is connected to the process chamber 100 by various vacuum adapter and connector components. While the exhaust assembly 600 removes gases, the showerhead 330 replaces the process gases and the purge gas is continuously flowed past the outer edge 186 of the pedestal 180 . This ensures a steady fresh supply of process and purge gases within the chamber 100 during wafer processing.
- FIG. 6 shows a cross-sectional view of one embodiment of the exhaust assembly 600 and vacuum components connecting it to the process chamber 100 .
- These vacuum components comprise: an adapter plate 601 , a thermal insulator 602 , an exhaust tubing 603 , a band heater 605 , a cover 604 , a 20-torr Baratron 606 , and a reducer 607 .
- the annular adapter plate 601 mates directly to the chamber body 250 around the side opening 256 , and fits around the outside of an exhaust tubing 603 which extends partly into the process chamber 100 side opening 256 .
- a thermal insulator 602 is fitted adjacent to the adapter 601 on the side away from the process chamber 100 .
- This thermal insulator 602 provides insulation between the heated exhaust assembly 600 , which is maintained at a temperature of about 150° C., and the chamber body 250 , which is maintained at a temperature of about 60-65° C.
- a band heater 605 is located around a substantial portion of the outside wall of the exhaust tubing 603 .
- An annular cover 604 fits over the outside of the insulator 602 , the band heater 605 and the remaining exhaust tubing portion 603 .
- a reducer 607 At the far end 613 of the exhaust tubing (away from the process chamber 100 ) is a reducer 607 , which has a larger diameter opening 617 on one end to mate with the exhaust tubing 603 , and a smaller diameter opening 627 at the other end to mate to additional components of the exhaust assembly 600 .
- a 20-torr Baratron pressure gauge 606 is connected to the reducer 607 via a side port.
- Numerous heaters are installed to maintain the exhaust assembly 600 at a temperature of approximately 150-200° C. so as reduce undesirable deposits from coating the interior walls of the exhaust assembly 600 and the associated vacuum components.
- a series of flexible heaters 625 , 645 , 655 , 665 and 675 are installed around the outside walls of the exhaust assembly 600 , a 2′′ manual angle valve 620 , a 1′′ manual valve 640 , cold trap 650 , isolation valve 660 , and throttle valve 670 .
- heater jackets 609 , 629 , 619 a , 619 b , 619 c and 619 d are provided around the reducer 607 , the 2′′ manual angle valve 620 and various parts of the exhaust assembly 600 .
- the cold trap 650 is connected between the manual valve 620 and the isolation valve 660 .
- a heater 655 is provided around the inlet 651 of the cold trap 650 to keep the temperature in the range of 150-200° C. This prevents undesirable deposits from forming on the interior of the inlet 651 of the cold trap 650 .
- a baffle plate 659 is provided close to the top 650 T of the cold trap 650 .
- a multi-loop cooling coil 656 is brazed to the bottom 650 B of the cold trap 650 , and cooling water at a temperature of about 20-25° C. is circulated inside the cooling coil 656 .
- the exhaust gases When the exhaust gases enter the cold trap 650 through the inlet 651 , they are diverted by the baffle plate 659 to flow radially outwards. Some of the condensibles, such as HCl and other by-products from the TiCl 4 /NH 3 reaction, are trapped onto the baffle plate 659 , but most are trapped onto the cooling coil 656 , which offers a relatively large trapping surface area.
- the remaining exhaust gases exit the cold trap 650 through an axially located channel 658 which is connected to the outlet 652 of the cold trap 650 , and pass through the isolation valve 660 and the throttle valve 670 before being exhausted into the exhaust line 690 .
- a chlorine-based chamber cleaning process provides efficient dry cleaning of the interior of the exhaust assembly 600
- powder deposits tend to accumulate after an extended period of wafer processing—e.g., 5000 wafers. These deposits can readily be removed by cleaning with water or hydrogen peroxide during periodic maintenance.
- the use of the heated exhaust assembly 600 contributes to equipment uptime by facilitating chamber maintenance and extending the time between chamber cleanings.
- Chlorine gas is introduced into the chamber 100 via the same flow path as for TiCl 4 inside the showerhead assembly 300 .
- Typical process conditions include a chlorine flow rate in the range of 500 sccm, a pressure in the range of 10-20 torr, and a temperature range of 600-700° C. for the heater 180 , and 150-250° C. for the interior walls of chamber 100 .
- the process parameters may be adjusted to suit specific needs, depending on the actual cleaning process conditions employed.
- the chamber 100 can also be adapted for use with other cleaning techniques such a plasma-based or remote microwave chlorine processes.
- adaptation for plasma-based cleaning processes would require a modification of the chamber lid 310 to accommodate RF biasing, as well as to allow for electrical isolation from ground.
- RF power would be applied between the showerhead assembly 300 and the chamber body 250 and liner 200 (ground).
- the hardware modifications necessary to implement plasma cleaning are described below in the section on plasma generation.
- an annealing step can be used to improve the film properties.
- Film annealing is performed by thermal annealing the wafer at a relatively high temperature, e.g., 750° C., which is readily attainable using the existing heated pedestal 180 .
- Annealing reduces traces of chlorine in the TiN film, which may otherwise result in undesirably high film resistivity.
- plasma annealing may also be used, in which case, the showerhead 330 acts as a top RF electrode while the pedestal 180 serves as a bottom ground electrode. The hardware modifications necessary for plasma annealing are described below.
- the existing chamber 100 described above is suitable only for non-plasma application, the chamber can readily be modified for plasma-enhanced applications such as deposition, cleaning or annealing.
- the entire lid assembly i.e., cooling plate assembly 400 , lid/gas box 310 and showerhead 330
- the entire lid assembly i.e., cooling plate assembly 400 , lid/gas box 310 and showerhead 330
- the showerhead 330 is coupled to the grounded chamber body 250 and liner 200 .
- RF power is applied to the showerhead 330 .
- Electrical isolation is therefore required between the showerhead 330 and the chamber body 250 .
- FIG. 7 a illustrates one embodiment of a modified configuration for plasma application.
- the RF lids used for existing CVD chambers such as CVD Ti, W, Al and dielectric chamber lids (configured for plasma application) are suitable for adaptation to the high temperature CVD chamber of the present invention.
- both the showerhead 330 and the gas box 710 are electrically insulated from the chamber lid 720 by a ceramic isolator 780 .
- the chamber lid 720 and the chamber body 250 remain at ground.
- FIG. 7 b shows an RF module 750 , which supplies RF power to the showerhead 330 .
- the RF module 750 can either be chamber installed or remotely installed, and provides RF power to the showerhead 330 through a RF connecting rod 752 , a RF plunger connector 754 and a RF strap connector 756 .
- Several delrin insulators 770 insulate these RF connectors 752 , 754 and 756 from the chamber body 250 and the chamber lid 720 .
- process gases enter the process chamber 100 via separate gas inlets 711 and 712 of the gas box 710 , which is connected to the dual-gas showerhead 330 .
- a voltage gradient assembly 790 is installed over the gas box 710 around the gas inlets 711 and 712 .
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Abstract
An apparatus for wafer processing, which comprises a chamber body and a heated liner which are thermally isolated from each other by isolating pins. During wafer processing, e.g., deposition of titanium nitride film by thermal reaction between titanium tetrachloride and ammonia, a wafer substrate is heated to a reaction temperature in the range of 600-700° C. by a heated support pedestal. The chamber liner and the interior chamber walls are maintained at a temperature between 150-250° C. to prevent deposition of undesirable by-products inside the chamber. This facilitates the chamber cleaning procedure, which can be performed using an in-situ chlorine-based process. The excellent thermal isolation between the heated liner and the chamber body allows the chamber exterior to be maintained at a safe operating temperature of 60-65° C. A heated exhaust assembly is also used in conjunction with the process chamber to remove exhaust gases and reaction by-products. External heaters are used to maintain the exhaust assembly at a temperature of about 150-200° C. to minimize undesirable deposits on the interior surfaces of the exhaust assembly.
Description
- 1. Field of the Invention
- The present invention relates to semiconductor wafer processing systems and, more particularly, to a high temperature chemical vapor deposition (CVD) chamber with a heated inside liner, and a temperature-controlled outer chamber body.
- 2. Description of the Background Art
- Titanium nitride (TiN) film has found wide applications in ultra large-scale integrated circuits (ULSI) as a diffusion barrier and as an adhesion layer for tungsten contacts. Low temperature reactive sputtering of Ti in the presence of nitrogen has been used in the past to deposit TiN films upon semiconductor wafers. However, as device geometries become increasingly smaller, the resulting step coverage from a sputtered TiN film is no longer adequate. Therefore, chemical vapor deposition (CVD) techniques have become the methods of choice in ULSI applications. For example, TiN film from a titanium tetrachloride based CVD process can be used as a high aspect ratio contact barrier, a capacitor top electrode or in plug fill processes below 0.18 μm.
- Both cold wall and hot wall low pressure chemical vapor deposition (LPCVD) processes have been used for depositing TiN films using a reaction between titanium tetrachloride (TiCl4) and ammonia (NH3). A cold wall reactor contains a wafer that is heated to a temperature above the reaction temperature of the process gases, e.g., over 650° C., by a halogen lamp that is located external to the chamber. However, since the chamber walls are cold (unheated), process by-products such as adduct ammonia salts will detrimentally form on the interior surfaces of the cold chamber walls or other cold surfaces. During thermal cycling of the chamber, these deposits may flake and fall on a wafer causing contamination and reducing wafer yield. Since these reaction by-products cannot be removed by in-situ chamber cleaning processes, frequent chamber disassembly and cleaning is required. This necessitates the opening of the chamber to the atmosphere, and results in considerable down time for the chamber.
- Alternatively, quartz hot wall reactors have been used to form high quality TiN films. The heated walls of these reactors help reduce accumulation of undesirable deposits, such as adduct ammonia salts, on the interior chamber walls. However, hot wall chambers can be dangerous to operate because of the high temperature of the walls, e.g., 150-200° C. Furthermore, it is difficult to achieve uniform heating of the chamber walls and other interior surfaces such that no undesirable deposits form.
- One possible solution is the use of a chamber liner, such as that disclosed in U.S. Pat. No. 5,348,587, issued on Sep. 20, 1994, to Eichman et al., entitled “Apparatus for Elimination of Low Temperature Ammonia Salts in TiCl4 NH3 CVD Reaction,” which is a continuation of U.S. Pat. No. 5,271,963, issued on Dec. 21, 1993. Both patents are herein incorporated by reference. Eichman et al. discloses an inside liner which is partly heated by lamps external to the chamber, and partly heated by a secondary plasma. This heated liner is located within a cold reactor wall enclosure. The heated liner lies against the inner surface of the cold reactor wall, and, as such, is only partially insulated from the reactor wall. Not only does this contact promote excessive thermal conduction to the reactor wall resulting in the chamber wall becoming dangerously hot, but additional heating of the liner will be needed to compensate for the heat lost to the wall.
- Therefore, a need exists in the art for a CVD chamber having a heated liner which substantially defines a chamber cavity and is thermally isolated from the external chamber body.
- The disadvantages of the prior art are overcome by an apparatus for processing a wafer having a chamber body that encloses a chamber liner, where the liner is maintains a spaced apart distance from the chamber body such that the liner is maintained at a higher temperature than the chamber body. As such, the liner can be maintained at a temperature that reduces the amount of deposition on the liner while maintaining a safe temperature for the chamber body.
- More specifically, the present invention relates to a process chamber system for high temperature film deposition, e.g., using a reaction between titanium tetrachloride (TiCl4) and ammonia (NH3) to deposit titanium nitride (TiN). The system comprises a process chamber and an exhaust assembly. The process chamber has an inside liner which is maintained at a temperature of approximately 150-250° C., while the chamber body is maintained at a temperature of approximately 60-65° C. or below. The liner can either be heated directly by a resistive heater embedded in the liner, or indirectly by a heated wafer support pedestal. The liner, which is substantially cylindrical, is enclosed within the bucket-shaped chamber body having a cylindrical wall and a base. Isolating pins are located between the bottom of the liner and the inside surface of the chamber base such that a spacing is maintained between the liner and the chamber body, i.e., the liner only contacts the chamber body through the isolating pins. Excellent thermal isolation is achieved between the liner and the chamber body because of the low thermal conductivity resulting from the small contact area between the isolating pins and the liner.
- The process chamber further comprises a heated wafer support pedestal for supporting and heating a semiconductor wafer and a showerhead for separately introducing TiCl4 and NH3 into the process chamber into a space above the wafer. The wafer is maintained at a temperature of approximately 600-700° C. such that a thermal reaction occurs at the surface of the wafer between TiCl4 and NH3, resulting in the formation of a TiN film upon the wafer.
- The exhaust assembly is connected to the process chamber to allow for continuous pumping of gases away from the process chamber. In one embodiment, a substantial portion of the exhaust assembly is maintained at approximately 150° C.-200° C. by the use of several heaters disposed on the outside walls of the exhaust assembly. Such heating reduces reaction by-product accumulation within the exhaust assembly.
- The teachings of the present invention can be readily understood by considering the following detailed description in conjunction with the accompanying drawings, in which:
- FIG. 1 is a partial cross-sectional perspective view of the high temperature CVD chamber system of the present invention, showing a process chamber and an exhaust assembly;
- FIG. 2a is a cross-sectional view of the process chamber, showing details of various components inside the process chamber of FIG. 1;
- FIG. 2b shows an enlarged cross-sectional view around the area of the inside liner, the isolating pin and the chamber body of FIG. 2a;
- FIG. 3a shows a cross-sectional view of the showerhead assembly;
- FIG. 3b shows a cross-sectional view of the dual-gas faceplate of the showerhead assembly of FIG. 3a;
- FIG. 4a is a top view of the cooling plate;
- FIG. 4b is a cross-sectional view showing the channel inside the cooling plate of FIG. 4a;
- FIG. 4c is a side view of the cooling plate of FIG. 4a;
- FIG. 5a is a cross-sectional view of the process chamber showing the bottom purge arrangement;
- FIG. 5b is a perspective view of another embodiment of an edge ring;
- FIG. 5c is a partial cross-sectional view of the edge ring (
line 5 c in FIG. 5b) resting atop of the liner; - FIG. 5d is a partial cross-sectional view of the edge ring (
line 5 d in FIG. 5b) resting atop of the liner; - FIG. 6 shows a partial cross-sectional view of the exhaust assembly; and
- FIG. 7a shows a conceptual design of a process chamber modified for plasma application; and
- FIG. 7b is a cross-sectional view illustrating the RF connections to the chamber of FIG. 7a.
- To facilitate understanding, identical reference numerals have been used, where possible, to designate identical elements that are common to the figures.
- FIG. 1 shows a partial cross-sectional perspective view of a high temperature chemical vapor deposition (HT CVD) system, including a
process chamber 100 and anexhaust assembly 600. Achamber mounting plate 110 is provided for mounting thisprocess chamber 100 onto a wafer transfer chamber (not shown) which interfaces theprocess chamber 100 to the rest of a complete wafer processing system, such as a Centura 5200 system (not shown) manufactured by Applied Materials, Inc. of Santa Clara, Calif. Cross-sectional views illustrating various components in theprocess chamber 100 are shown in FIGS. 2-5. To best understand theprocess chamber 100 of the present invention and its operation, the reader should simultaneously refer to all these figures. - The
process chamber 100 of the present invention performs, for example, high temperature deposition of titanium nitride upon a semiconductor wafer using a TiCl4+NH3 chemistry. Since the thermal decomposition of TiCl4 and NH3 occurs at high temperature, the wafer should preferably be maintained at a temperature range of 600-700° C. to facilitate deposition upon the wafer. - The
process chamber 100 comprises achamber body 250, aliner 200, apedestal assembly 160 and ashowerhead assembly 300. Thepedestal assembly 160 contains apedestal 180 that supports the wafer in thechamber 100. The dual-gas showerhead assembly 300 is positioned in a parallel, spaced apart relation with respect to thepedestal 180 such that the wafer support surface of thepedestal 180 and afaceplate 330 of theshowerhead assembly 300 define a reaction zone. To achieve deposition, the wafer is heated by aheated pedestal 180 while theshowerhead assembly 300 introduces the two reactant gases (TiCl4 and NH3) into theprocess chamber 100 such that reaction occurs only above the wafer, resulting in TiN deposition onto the wafer. In order to minimize unwanted TiN deposition on the inside surface of the chamber, the interior wall of the chamber, i.e., thechamber liner 200, is maintained at a temperature between 150° C. to 250° C. An improved bottom purge arrangement is also provided to reduce undesirable adduct reaction by-products which may form on cold areas of the chamber. Theheated exhaust assembly 600 also prevents the formation of powder deposits on the interior walls of theexhaust assembly 600. This powder deposit is a reaction by-product between TiCl4 and NH3 which forms at a temperature below 150° C. At a temperature above 150° C. but below 600° C., minimal amounts of TiN is deposited on interior chamber components. The TiN film that is inadvertently deposited on chamber components can readily be removed by an in-situ thermal chlorine cleaning process performed withinchamber 100 of the present invention. - As shown in FIG. 2a, the
chamber body 250 is substantially bucket-shaped, with acylindrical side 254 and abase 252. There is anopening 256 at one portion of thecylindrical side 254, which is connected to theexhaust assembly 600 for the removal of process and product gases. Thechamber base 252 has a centrally-locatedopening 258, which is provided to accommodate apedestal assembly 160, as well as a gas purging arrangement to be described below. Aninside liner 200, which is substantially cylindrical, is located on the inside, but spaced apart from thechamber body 250. Thechamber body 250, which substantially encloses thisinside liner 200, is made of nickel-plated aluminum. In this particular application, nickel plating is needed to protect the aluminum components from corrosion by chlorine gas, which is used in an in-situ chamber cleaning process to be described below. Of course, for other applications with different cleaning processes, alternative metal-plating may be used as long as it is compatible with the chemical species used in the reaction or cleaning processes. - To avoid an exterior temperature of the
chamber body 250 that may harm a user/operator, the chamber body temperature is maintained at approximately 60° C.-65° C. or less by thermally isolating thechamber body 250 from the insideheated liner 200. Theinside liner 200, which is also made of nickel-plated aluminum, has an embeddedresistive heater 215 for establishing a fixed liner temperature. A thermal conductive paste is applied to theresistive heater 215 and enclosed within acover plate 207 which is welded to theliner 200 to ensure good thermal conductivity between theheater 215 and theliner 200. An AC voltage is coupled to theheater 215 using AC connectors inside afeedthrough portion 214 of theliner 200. Thisheater 215 can optionally be used to dynamically control the temperature of theliner 200. For example, theheater 215 may be used to maintain the liner temperature at approximately 150 to 250° C. to avoid the formation of adduct ammonia salt or other process by-products on the interior surface ofliner 200. To facilitate dynamic thermal control of theliner 200, aType K thermocouple 212 is removably inserted in theliner 200 approximately half the distance along itscylindrical wall 204. Thus, the liner temperature can be measured at approximately half way from thebottom 202 of theliner 200. Connectors (not shown) for thethermocouple 212 and theresistive heater 215 are located inside thefeedthrough portion 214 of theliner 200. A clampingplate 216 seats an O-ring 201 against thechamber base 252 and thefeedthrough portion 214 to seal the interior of thechamber 100 from the outside atmosphere. - In practice, independent heating by the
resistive heater 215 is not always necessary to achieve an appropriate liner temperature since the operation of the heated pedestal 180 (see FIG. 2a) alone is generally sufficient to maintain the temperature of theliner 200 within the desired range of 150-250° C. Of course, thisheater 215 may be used, alone or in conjunction with theheated pedestal 180, for other processes with different temperature requirements. - The
inside liner 200 and thechamber body 250 are substantially isolated from each other by means of threedowel pins 220, one of which is shown in the cross-sectional view in FIG. 2a. These isolatingpins 220 are located between the bottom 202 of theinside liner 200 and theinside surface 253 of thechamber base 252. The area around theinside liner 200,dowel pin 220 and thechamber base 252 is shown in an enlarged cross-sectional view in FIG. 2b. The threepins 220 are arranged to lie equidistant from each other on the circumference of a circle, subtending angles of 120 degrees at the center of the circle. Eachdowel pin 220 has acentral portion 221 having a diameter d1 and twosmaller ends hole 225 is provided along the longitudinal axis of thepin 220 to allow for pump-out of any trapped gases. Thepins 220 are press-fit into corresponding receivingholes 224 in thebottom 202 of theliner 200, such that theliner 200 rests against one side of the largercentral portion 221 of eachpin 220. There are also threecorresponding holes 226 on theinside surface 253 of thechamber base 252 to accommodate thesepins 220. One of theseholes 226 is round, and the other two are slotted (not shown) to provide for additional assembly tolerance. - When the
liner 200, with the dowel pins 220 in place, is set to rest in theseholes 226 inside thechamber base 252, thepins 220 serve to maintain a proper spacing (s) between theliner 200 and thechamber base 252. This spacing (s) corresponds to the thickness of the largercentral portion 221 of thepin 220, which is about 0.135″ (3.4 mm). Four ¼-20 nickel screws (not shown), which also lie on the circumference of the same diameter circle as the dowel pins 220, are used to secure theliner 200 in place by screwing into corresponding tapped holes (not shown) on theinside surface 253 of thechamber base 252. The small contact areas of the nickel pins 220 and screws ensure very good thermal isolation between theheated liner 200 and thechamber body 250, and allows thechamber body 250 to be kept at around 65° C. while maintaining the heated liner at 150-250° C. - These dowel pins220 can be made of a variety of materials that can withstand high temperatures and have a relatively high thermal resistivity (low thermal conductivity), such as stainless steel or nickel. The choice of material depends on the specific processing applications. For example, nickel (200 or 201 grade), is the preferred material because of its chemical resistance to chlorine and high thermal resistance. It is understood that the dimensions and specific layouts for the various components are for illustrative purpose only. For example, the
liner 200 could be spaced from thebody 250 by intermittently spaced ribs formed in thebottom 252 ofchamber body 250, a continuous annular ridge formed in thebottom 252 of thechamber body 250, a spacer ring positioned on thebottom 252 of thechamber body 250 and the like. As such, the present invention encompasses many other chamber/liner/spacer combinations that facilitate thermal isolation between theliner 200 and thechamber body 250. Such isolation enables separate temperature control of these components. - FIG. 3a shows a cross-sectional view of the dual-
gas showerhead assembly 300, comprising a nickel-plated aluminum lid/gas box (manifold assembly 310) and afaceplate 330. Theshowerhead assembly 300 provides a dual-gas separate entry for TiCl4 and NH3 into theprocess chamber 100 without premixing of the gases. Thegas manifold assembly 310 also serves as the lid of thechamber 100. Thefaceplate 330 is described in a commonly-assigned patent application by Umotoy et al. entitled “Dual Gas Faceplate for a Showerhead in a Semiconductor Wafer Processing System,” Ser. No. 09/098,969, filed Jun. 16, 1998; which is herein incorporated by reference. Theshowerhead assembly 300 allows two gases, for example, NH3 and TiCl4, to be separately introduced into the reaction region, orprocessing zone 515. Theprocessing zone 515 is roughly defined by the space between the bottom 332 of thefaceplate 330 and theheated pedestal 180, which is the top portion of apedestal assembly 160 to be described below. (See FIG. 5a.) In order to avoid the formation of undesirable deposits inside theshowerhead assembly 300, separate flow paths or passageways are established throughdifferent channels 320 orchambers 322 inside theshowerhead assembly 300. Thesechannels 320 andchambers 322 prevent mixing of the two gases prior to reaching theprocess zone 515. Briefly, the gas manifold orlid 310 comprises three plates—bottom 312, middle 314 and top 316, which have been fused together by vacuum brazing theirmating surfaces unitary manifold assembly 310. As such, no O-rings are necessary to provide isolation between the process gases as they flow through themanifold assembly 310. Theseplates channels 320 andchambers 322, such that when thefaceplate 330 is bolted to themanifold assembly 310, the myriad ofchannels 320 andchambers 322 provide proper passageways, or flow paths, for introducing two gases separately from their supply sources (not shown) outside thechamber 100 into theprocess zone 515 without pre-mixing of the gases. - The
faceplate 330 further comprises a lowergas distribution plate 340 and a uppergas distribution plate 350, as shown in FIG. 3b. The specific arrangement ofchannels 343 and holes (351, 352, 341, 342 and 344) that together define distinct passageways or flow paths for the two process gases are described in detail in the above-referenced patent application Ser. No. 09/098,969. Suffice to say that when the two plates, 340 and 350, are fused together using the same technique as previously described for thegas manifold plates unitary faceplate 330 provides separate passageways, or flow paths, for uniformly introducing two gases into theprocessing zone 515 without pre-mixing of the gases. - For example, there are two sets of holes,341 and 342, in the
lower plate 340, one for each gas. As shown in FIG. 3b, one set ofholes 341 aligns withholes 351 in the upper plate to form one flow path (from 351, via 344 to 341) for one gas, e.g., TiCl4. The other set ofholes 342 are connected tochannels 343 within thelower plate 340. Thesechannels 343 are in turn connected to acircumferential plenum 390, which is formed between the upper and lower plates, 350 and 340, when they are fused together. Theplenum 390 is further connected to anotherhole 352 in theupper plate 350, which provides an inlet for a second gas, e.g., NH3. This configuration allows the first gas to pass through the first passageway (e.g., from 351, via 344 to 341) and the second gas to pass through the second passageway (e.g., from 352, via 390 to 343 and 342) within thefaceplate 330 without mixing until the gases enter theprocess zone 515 after exiting from theseholes faceplate 330. It should be noted that the choice of hole size for each gas and hole distribution are functions of process conditions. For example, the hole size will vary depending upon gas flow rate, gas pressure, gas type, chamber pressure and thefaceplate 330 such that gas flow rates through the holes are correlated with the locations of the holes in thefaceplate 330. - The
showerhead assembly 300 is formed by affixing thefaceplate 330 directly to the bottom of thegas distribution manifold 310 using a plurality of bolts (not shown) through the mounting holes (hole 396 is shown in FIG. 3b) in thefaceplate 330. An O-ring groove 325 (see FIG. 3a) is provided in thegas manifold 310 to accommodate an O-ring 326 which is used to provide sealing between thegas manifold 310 and thefaceplate 330. Different types of O-ring materials, such as Viton, may be used, as long the material is compatible with the operating temperature and chemically resistant to the gases used in the process. Both thefaceplate 330 and thegas distribution manifold 310 are made of nickel-plated aluminum or some other thermally conductive and chlorine compatible materials such as nickel. Of course, other material choices are possible as long as they provide the thermal conductivity and/or chemical compatibility which are necessary for the specific process. - The
showerhead assembly 300 can be coupled to acold plate assembly 400 or other cooling apparatus that will maintain the entire lid/gas box 310 at a uniform and constant temperature. During wafer processing, theshowerhead assembly 300 is heated by theheated pedestal 180 through thermal radiation in thereaction zone 515. Therefore, to avert deposition of TiN or by-products of the TiN deposition process upon and/or within the showerhead, acold plate assembly 400 is necessary to maintain the faceplate temperature within a range of 150-250° C. Thecold plate assembly 400 serves a dual-purpose of preventing theshowerhead assembly 300 from temperature drift, as well as keeping the areas around the O-ring seal to within specification for proper sealing. - A detachable
cold plate assembly 400 is designed to maintain temperature of the lid/gas box 310 to prevent it from temperature drift. FIG. 4a is a schematic illustration of the top view of thecold plate assembly 400. Thiscold plate assembly 400 is substantially annular in shape, except for a rectangular protrudedportion 402. FIG. 4b shows a cross-sectional view of thecold plate assembly 400, comprising atop plate 440 and abottom plate 420, which are brazed together and then nickel-plated as an assembly. Thetop plate 440 has a coil-shapedchannel 410 passing through theplate 440 for circulating coolant, as illustrated in FIG. 4a. The two ends, 412 and 414, of the coil-shapedchannel 410 are located at the rectangular protrudedportion 402, and serve as the inlet and outlet for the coolant. Thechannel 410 has a rectangular cross-section and is open on itsbottom side 415. This is illustrated in the cross-sectional view shown in FIG. 4b and the side view shown in FIG. 4c. Thetop surface 425 of thebottom plate 420, when brazed together with thetop plate 440, defines aclosed channel 445 through which a coolant can circulate. Thebottom plate 420 has twoapertures 422 and 424, close to the end of the rectangular protrudedportion 402. Theseapertures 422 and 424 are aligned respectively with the two ends 412 and 414 of thetop plate channel 410 to provide for coolant inlet and outlet. The coolant, typically water, is connected in series with the coolant for thechamber 100. - The
cold plate assembly 400 is attached onto the top of the lid/gas box (310 in FIG. 3a) using screws atlocations 430 around the circumference of thecold plate assembly 400. Note that oneannular portion 421 of thebottom plate 420 is recessed such that only an inner 426 and an outer 428 portion of thebottom plate 420 actually come into physical contact with thechamber lid 310. The coolingplate assembly 400, lid/gas box 310 and thefaceplate 330 are sometimes collectively referred to as a lid assembly. With an inlet water temperature of about 45-55° C., the lid/gas box 310 can readily be maintained within a temperature range of 60-65° C. - As a detachable component, this
cold plate assembly 400 is a cost-effective design feature which allows for ease of maintenance as well as design and process flexibility. For example, different temperature control scenarios for thefaceplate 330 may be achieved by a suitable interchange with a different cooling (or heating) plate that provide more or less heating or cooling. To most effectively process a wafer or wafers, thecold plate assembly 400 that is best suited for a particular process can be easily installed onto the chamber lid. - FIG. 5a illustrates a
pedestal assembly 160 in a cross-sectional view within theprocess chamber 100. Thepedestal assembly 160 comprises a flatcircular portion 180 at the top, sometimes referred to as a susceptor or pedestal; and a bottom cylindrical shaft-like portion 560 which extends downwards through the centrally-locatedopening 258 at the bottom 252 of thechamber body 250. Theupper surface 185 of thepedestal 180 has awafer pocket 563 to support a wafer 564 (shown in phantom in FIG. 5a), and four clearance holes to accommodate wafer lift pins 285. These wafer lift pins 285 are made of ceramic, and are used for wafer-handling and transport. They are slidably mounted within bores in thepedestal 180 and can be lifted above the pedestal'supper surface 185 by engaging awafer lift ring 580, in order to raise and lower the wafer with respect to thesupport surface 185 of thepedestal 180. These lift pins 285 are kept from falling out from thepedestal 180 byconical heads 585 located on their upper ends. Thecurrent pedestal assembly 160 and chamber design can accommodate wafer diameters of 125 mm, 150 mm and 200 mm, respectively. Those skilled in the art can perform proper design scale-up to encompass applications to larger wafer diameters such as 300 mm as well. - The
pedestal 180, preferably made of a ceramic material such as aluminum nitride (AlN), is further equipped with two embedded electrodes 571 and 572. In general, these electrodes 571 and 572, made of different types of conducting materials, can be of various thicknesses and shapes. In the present invention, one of these electrodes is a radio-frequency (RF) grid 571 for performing plasma clean and other plasma processes such as plasma annealing of the wafer. The mesh-type grid 571, made of molybdenum, is located slightly below the pedestal'stop surface 185. Slightly below the RF electrode is an alternating current (AC) grid 572 for heating purpose. Thepedestal 180 currently in use is made of a dark gray, high resistivity AlN of 99.9% purity. Of course, other similar heaters may also be used, depending on the specific process requirements. Thisheated pedestal 180 allows the wafer temperature to be controlled within a range of approximately 600-800° C. Although TiN film deposition can also be performed between 200-600° C., the resulting TiN film tends to have an undesirably high chlorine content. Therefore, the wafer temperature is preferably maintained within a range of 600-700° C. for optimal deposition results. During wafer processing, there is also a center-to-edge temperature difference in thepedestal 180 of about 10° C., with theedge 186 being cooler because of a purge gas flow around the pedestal'sedge 186. - The
pedestal assembly 160 moves vertically within the chamber cavity by a lift mechanism (not shown) between a first (top)position 501 and a second (bottom)position 502. Thissecond position 502 of thepedestal assembly 160 is illustrated in phantom in FIG. 5a. During wafer processing, e.g., for film deposition onto thewafer substrate 564, thepedestal assembly 160 is placed in thefirst position 501. A reaction zone, orprocess zone 515, within thechamber cavity 280 can be defined roughly as the space between the bottom 332 of thefaceplate 330 and the pedestaltop surface 185, and confined on the side by theedge ring 290. Awafer substrate 564 is positioned in thewafer pocket 563 during wafer processing, and the distance between the wafer and the bottom of thefaceplate 330 is approximately 0.360″ (9.1 mm). Note that this distance is for illustrative purpose only, and it may be different for other process applications. The spacing 530 between theoutside edge 186 of thepedestal 180 to theinside surface 286 of theliner 200 is about 0.125″ (3.2 mm). The choice of thisspacing 530 is determined both by the specified temperature of theliner 200 and the need to prevent purge gas from entering theprocess zone 515. - Before and after film deposition for each wafer, the
pedestal assembly 160 is moved to asecond position 502 for wafer loading or unloading. In thissecond position 502, the pedestaltop surface 185 is slightly below aslit valve opening 260, which is located on the side, or cylindrical wall, 204 of thechamber liner 200 and thecylindrical side 254 of thechamber body 250. A wafer can be transported in and out of theprocess chamber 100 through the slit valve opening 260 to an adjacent transfer chamber and/or load-lock chamber (not shown), or another chamber within a cluster tool. A cluster tool of a type that can be coupled to theprocess chamber 100 is described in a commonly assigned U.S. Pat. No. 5,186,718, entitled “Staged-Vacuum Wafer Processing System and Method”, issued Feb. 16, 1993, and is herein incorporated by reference. - Wafer-handling and transport is accomplished by the wafer lift pins285 in the
pedestal 180 in conjunction with a robotic transfer assembly (not shown) which has been described in a commonly assigned U.S. Pat. No. 4,951,601, entitled “Multi-chamber Integrated Process System,” issued Aug. 28, 1990; the complete disclosure of which is incorporated herein by reference. Briefly, the sequence for wafer loading involves the pedestal being placed inposition 502, and a robotic arm transporting a wafer through the slit valve opening 260 into theprocess chamber 100. With thewafer 564 poised above thepedestal surface 185, thewafer lift ring 580 rises to engage pin bottoms such that the wafer lift pins 285 are raised above the pedestaltop surface 185 to lift thewafer 564 off the robotic arm. After the retraction of the robotic arm away from thepedestal surface 185, thepedestal assembly 160 is raised to receive thewafer 564 in thewafer pocket 563, and thelift ring 580 lowers to its original position. Thepedestal assembly 160 is subsequently moved into itsfirst position 501 for wafer processing. The wafer unloading sequence is a reverse of the loading sequence. The self-adjusting mechanism for the vertical movement of thepedestal assembly 160 has also been described in a commonly assigned U.S. patent application Ser. No. 08/738,240, filed on Oct. 25, 1996, and entitled “Self-Aligning Lift Mechanism,” the disclosure of which is herein incorporated by reference. - FIG. 5a also illustrates details of an
edge ring 290 and a backside gas purge arrangement. Theedge ring 290 is disposed around theouter perimeter 187 of thepedestal 180 of thepedestal assembly 160. Thisedge ring 290 is substantially annular, with a protrudingportion 292 at the bottom 294 of thering 290. As such, this protrudingportion 292 essentially divides thebottom 294 of thering 290 into aninside bottom surface 297 and anoutside bottom surface 298. When thepedestal assembly 160 is in itsfirst position 501, theedge ring 290 rests on top of theheated pedestal 180, such that itsinside bottom surface 297 covers part of thetop pedestal surface 185. Also, in this position, the protrudedportion 292 of theedge ring 290 covers part of the side, oroutside edge 186 of thepedestal 180. Aspace 531 is then defined between theoutside bottom portion 298 of theedge ring 290 and a protrudedportion 203 of theheated liner 200. Thisgap 531 provides a choke for the bottom, or backside, purge gas flow (to be described below) and ensures uniform distribution of the purge gas about the edge of thepedestal 180. - When the
pedestal assembly 160 is in itssecond position 502, theedge ring 290 rests on top of the protrudedportion 203 of theheated liner 200. As such, the edge ring does not interfere with access of the robotic transfer mechanism as it places and/or retrieves the wafer to/from thepedestal 180. - The
edge ring 290 can be made of a variety of materials such as ceramic, quartz, aluminum and steel, among others. The exact choice of material depends, of course, on the specific process applications. For example, quartz can be used for TiN deposition using TiCl4+NH3 chemistry. - The purpose of this
edge ring 290 is two-fold: 1) to act as a choke such that uniform pumping can be established for the gases and/or by-products during processing; and 2) to prevent process gases from entering behind thepedestal assembly 160, which may cause undesirable deposits in the lower portions of thechamber 100. - During wafer processing, the
pedestal assembly 160 is in the first (top)position 501, such that thegap 520 between the top 295 of theedge ring 290 and thebottom 332 of thefaceplate 330 is about 0.05″ (1.3 mm). A backside purge is established by flowing argon through aliner purge inlet 505 into thegap 599 between theliner 200 andchamber body 250 to prevent powder deposition on the cold wall surfaces of thechamber body 250. Thisgap 599 is about 0.06″ (1.5 mm) wide. To facilitate purge gas flow, a set ofholes 595 is also provided through theshaft portion 590 of thewafer lift ring 580 located around thepedestal shaft 560 at thebottom opening 258. Undesirable deposition behind thepedestal 180 is prevented by establishing a purge gas flow through theseholes 595 into thechamber cavity 280, as illustrated by the arrows. As previously mentioned, various spaces such as 520, 530, and 531 are defined by different portions of theshowerhead 330,pedestal 180,edge ring 290, andliner 200. It is to be understood that dimensions quoted for these spaces, like those quoted for other components, are for illustrative purpose only. In general, the choice of these dimensions depend on the desired results of a specific process being performed in the chamber. For example,spaces pedestal 180. Thespace 520 may be a variable parameter affecting uniformity or deposition rate in the film deposition step itself. Suffice to say that one skilled in the art of wafer processing would be able to arrive at optimal combinations of these dimensions to achieve desirable wafer processing results such as deposition uniformity. - FIG. 5b shows a perspective view of an alternative embodiment of an
edge ring 550, and FIGS. 5c and 5 d show partial cross-sectional views of theedge ring 550 being supported by ahorizontal surface 522 of theliner 200. FIG. 5c illustrates theedge ring 550 with atop surface 551, abottom surface 552, aninside surface 556, anoutside surface 557, and a protruded insideportion 559. In this embodiment, theedge ring 550 is supported entirely by theliner 200, i.e., theedge ring 550 does not contact thepedestal 180 orwafer 564. Astep 523 is provided on ahorizontal surface 522 of theliner 200 to keep theedge ring 550 in place. Akey stop portion 554 located on theoutside surface 557 of theedge ring 550 interfits with thestep 523 of theliner 200 to facilitate secure mounting of theedge ring 550. Additionally, three grooves orslots 565 are provided on thebottom surface 552 of the edge ring 550 (see FIG. 5d), and are located equidistant from each other. Threepins 526 are press fit into corresponding recessedholes 525 in thehorizontal surface 522 of theliner 200. Aportion 527 of thepin 526 protrudes above thehorizontal surface 522 of theliner 200 and engages theslot 565 at thebottom surface 552 of theedge ring 550. As such, theedge ring 550 is prevented from rotating with respect to theliner 200. Optionally, mounting screws (not shown) can also be used to secure theedge ring 550 to theliner 200. Again, the dimensions disclosed for the pin and slot arrangement are for illustrative purpose only, and do not represent limitations pertaining to the practice of this invention. Suffice to say that in the present arrangement, theedge ring 550 is heated by thermal radiation from thepedestal 180, and expands before theliner 200 reaches the same final temperature. This results in a uniform expansion of theedge ring 550 with respect to its centerline O-O′. - During wafer processing, when the pedestal180 (shown in phantom in FIG. 5c) is in the
first position 501, the protruded insideportion 559 of theedge ring 550 is disposed over theouter perimeter 187 of thepedestal 180, such that theouter perimeter 187 and theoutside edge 186 of thepedestal 180 are in close proximity to and substantially surrounded by theedge ring 550. Thus, undesirable deposition over theperimeter 187 andouter edge 186 of thepedestal 180 can be avoided. In this embodiment, however, there is no direct physical contact between thepedestal 180 and theedge ring 550. Instead, a gap orspace 568 is maintained between the top 185 of thepedestal 180 and thebottom 553 of the protrudedportion 559 of theedge ring 550. Anotherspace 566 is defined between thepedestal edge 186 and theinside surface 556 of theedge ring 550. - A number of
openings 555, e.g., about 30 in this particular embodiment, are provided around the circumference of theedge ring 550 close to thebottom surface 552. Theseopenings 555 extend horizontally from theinside surface 556 to theoutside surface 557 of theedge ring 550. Through theseopenings 555, a purge gas is pumped from thespace 566, into thespace 567 between theoutside surface 557 of theedge ring 550 and theinside surface 524 of theliner 200. Thegap 568 acts as a choke to prevent any purge gas from flowing towards the top 185 of thepedestal 180, which may otherwise dilute the process gases and affect the deposition process. Similar to theother edge ring 290 shown in FIG. 5a, thetop surface 551 of thisedge ring 550 and thebottom 332 of theshowerhead 330 defines thespace 520 through which process gases and/or by-products are pumped out from the reaction zone 515 (see FIG. 5a). The dimensions of thesespaces liner 200 supporting the edge ring 550) allows the temperature of theedge ring 550 to be maintained within a range of approximately 200-250° C., and undesirable deposition on theedge ring 550 is further minimized. Note that the use of an edge ring, while highly desirable, is not absolutely necessary for the practice of this invention. - Returning to FIG. 5a, during wafer deposition, TiCl4 in a He carrier gas and NH3 in a H2 carrier gas are introduced into the
processing zone 515 via theshowerhead assembly 300 and a chemical reaction between TiCl4 and NH3 takes place at close proximity above thewafer 564 that is supported by theheated pedestal 180. The reaction results in the deposition of TiN film onto thewafer 564. A continuous gas flow is maintained by the pumping system that is attached to theexhaust assembly 600 such that gases, including any volatile reaction products, are pumped out of theprocessing zone 515 and other areas of thechamber cavity 280, past thespace 520 between the top 295 of thequartz edge ring 290 and thebottom 332 of thefaceplate 330, through a slot 205 (see FIG. 2a) in theinside liner 200, into theexhaust chamber 600 which is connected to theprocess chamber 100 by various vacuum adapter and connector components. While theexhaust assembly 600 removes gases, theshowerhead 330 replaces the process gases and the purge gas is continuously flowed past theouter edge 186 of thepedestal 180. This ensures a steady fresh supply of process and purge gases within thechamber 100 during wafer processing. - FIG. 6 shows a cross-sectional view of one embodiment of the
exhaust assembly 600 and vacuum components connecting it to theprocess chamber 100. These vacuum components comprise: anadapter plate 601, athermal insulator 602, anexhaust tubing 603, aband heater 605, acover 604, a 20-torr Baratron 606, and areducer 607. Theannular adapter plate 601 mates directly to thechamber body 250 around theside opening 256, and fits around the outside of anexhaust tubing 603 which extends partly into theprocess chamber 100side opening 256. Athermal insulator 602 is fitted adjacent to theadapter 601 on the side away from theprocess chamber 100. Thisthermal insulator 602 provides insulation between theheated exhaust assembly 600, which is maintained at a temperature of about 150° C., and thechamber body 250, which is maintained at a temperature of about 60-65° C.A band heater 605 is located around a substantial portion of the outside wall of theexhaust tubing 603. Anannular cover 604 fits over the outside of theinsulator 602, theband heater 605 and the remainingexhaust tubing portion 603. At thefar end 613 of the exhaust tubing (away from the process chamber 100) is areducer 607, which has a larger diameter opening 617 on one end to mate with theexhaust tubing 603, and a smaller diameter opening 627 at the other end to mate to additional components of theexhaust assembly 600. A 20-torrBaratron pressure gauge 606 is connected to thereducer 607 via a side port. Numerous heaters are installed to maintain theexhaust assembly 600 at a temperature of approximately 150-200° C. so as reduce undesirable deposits from coating the interior walls of theexhaust assembly 600 and the associated vacuum components. For example, a series offlexible heaters exhaust assembly 600, a 2″manual angle valve 620, a 1″manual valve 640,cold trap 650,isolation valve 660, andthrottle valve 670. Note that heating is necessary even for theisolation valve 660 and thethrottle valve 670 which are located beyond thecold trap 650 in order to prevent the formation of undesirable deposit inside these vacuum components. Additionally, to minimize heat loss and to provide a safe operating environment,heater jackets reducer 607, the 2″manual angle valve 620 and various parts of theexhaust assembly 600. - The
cold trap 650 is connected between themanual valve 620 and theisolation valve 660. Aheater 655 is provided around theinlet 651 of thecold trap 650 to keep the temperature in the range of 150-200° C. This prevents undesirable deposits from forming on the interior of theinlet 651 of thecold trap 650. Abaffle plate 659 is provided close to the top 650T of thecold trap 650. Amulti-loop cooling coil 656 is brazed to the bottom 650B of thecold trap 650, and cooling water at a temperature of about 20-25° C. is circulated inside the coolingcoil 656. When the exhaust gases enter thecold trap 650 through theinlet 651, they are diverted by thebaffle plate 659 to flow radially outwards. Some of the condensibles, such as HCl and other by-products from the TiCl4/NH3 reaction, are trapped onto thebaffle plate 659, but most are trapped onto the coolingcoil 656, which offers a relatively large trapping surface area. The remaining exhaust gases exit thecold trap 650 through an axially locatedchannel 658 which is connected to theoutlet 652 of thecold trap 650, and pass through theisolation valve 660 and thethrottle valve 670 before being exhausted into theexhaust line 690. - Although a chlorine-based chamber cleaning process (to be described below) provides efficient dry cleaning of the interior of the
exhaust assembly 600, powder deposits tend to accumulate after an extended period of wafer processing—e.g., 5000 wafers. These deposits can readily be removed by cleaning with water or hydrogen peroxide during periodic maintenance. The use of theheated exhaust assembly 600 contributes to equipment uptime by facilitating chamber maintenance and extending the time between chamber cleanings. - As with most processing equipment, periodic chamber cleaning is necessary to ensure cleanliness of the processed wafers. An in-situ chlorine-based thermal cleaning process has been developed for this purpose. When TiN deposition is accomplished using TiCl4 and NH3, a TiN film deposit is formed on the chamber interior (as opposed to a powder deposit of adduct ammonia salt), as long as the wall temperature is kept at around 150-250° C. This film can be effectively removed (etched) by the use of an in-situ thermal chlorine process. This thermal cleaning process is described in a commonly assigned U.S. patent application Ser. No. 09/163,711, filed on Sep. 30, 1998 by Vasudev et al., and is hereby incorporated by reference. Chlorine gas is introduced into the
chamber 100 via the same flow path as for TiCl4 inside theshowerhead assembly 300. Typical process conditions include a chlorine flow rate in the range of 500 sccm, a pressure in the range of 10-20 torr, and a temperature range of 600-700° C. for theheater 180, and 150-250° C. for the interior walls ofchamber 100. Of course, the process parameters may be adjusted to suit specific needs, depending on the actual cleaning process conditions employed. In addition to thermal cleaning, it is anticipated that thechamber 100 can also be adapted for use with other cleaning techniques such a plasma-based or remote microwave chlorine processes. For example, adaptation for plasma-based cleaning processes would require a modification of thechamber lid 310 to accommodate RF biasing, as well as to allow for electrical isolation from ground. To ignite a cleaning plasma, RF power would be applied between theshowerhead assembly 300 and thechamber body 250 and liner 200 (ground). The hardware modifications necessary to implement plasma cleaning are described below in the section on plasma generation. - After TiN film deposition, an annealing step can be used to improve the film properties. Film annealing is performed by thermal annealing the wafer at a relatively high temperature, e.g., 750° C., which is readily attainable using the existing
heated pedestal 180. Annealing reduces traces of chlorine in the TiN film, which may otherwise result in undesirably high film resistivity. Alternatively, plasma annealing may also be used, in which case, theshowerhead 330 acts as a top RF electrode while thepedestal 180 serves as a bottom ground electrode. The hardware modifications necessary for plasma annealing are described below. - Although the existing
chamber 100 described above is suitable only for non-plasma application, the chamber can readily be modified for plasma-enhanced applications such as deposition, cleaning or annealing. For thermal deposition process, the entire lid assembly (i.e., coolingplate assembly 400, lid/gas box 310 and showerhead 330) is coupled to the groundedchamber body 250 andliner 200. In plasma applications, however, RF power is applied to theshowerhead 330. Electrical isolation is therefore required between theshowerhead 330 and thechamber body 250. FIG. 7a illustrates one embodiment of a modified configuration for plasma application. For example, the RF lids used for existing CVD chambers, such as CVD Ti, W, Al and dielectric chamber lids (configured for plasma application) are suitable for adaptation to the high temperature CVD chamber of the present invention. As shown in FIG. 7a, both theshowerhead 330 and thegas box 710 are electrically insulated from thechamber lid 720 by aceramic isolator 780. Thechamber lid 720 and thechamber body 250 remain at ground. FIG. 7b shows anRF module 750, which supplies RF power to theshowerhead 330. TheRF module 750 can either be chamber installed or remotely installed, and provides RF power to theshowerhead 330 through aRF connecting rod 752, aRF plunger connector 754 and a RF strap connector 756. Severaldelrin insulators 770 insulate theseRF connectors chamber body 250 and thechamber lid 720. During deposition, process gases enter theprocess chamber 100 viaseparate gas inlets gas box 710, which is connected to the dual-gas showerhead 330. To prevent electrical breakdown of process gases inside the gas delivery lines, avoltage gradient assembly 790 is installed over thegas box 710 around thegas inlets voltage gradient assembly 790 is provided in a commonly-assigned U.S. Pat. No. 5,362,526 entitled “Plasma-Enhanced CVD Process Using TEOS for Depositing Silicon Oxide”, filed on Jan. 23, 1991. This patent is herein incorporated by reference. - It should be emphasized that there is no inherent limitation restricting the use of this high temperature chamber to TiN film deposition. In general, other CVD film deposition can also be performed using this high temperature chamber. Furthermore, it is possible to extend the use of this chamber to facilitate other process applications. The dual-gas showerhead arrangement will be useful in any application where there is a need to separately introduce processing gases without premixing, and the heated liner may also find applications in various etch and deposition processes where deposition of by-products of the process are reduced by heating chamber surfaces.
- Although a preferred embodiment which incorporates the teachings of the present invention has been shown and described in detail, those skilled in the art can readily devise many other varied embodiments that still incorporate these teachings.
Claims (34)
1. Apparatus for wafer processing, comprising:
a chamber body; and
a liner being substantially enclosed in said chamber body, where said liner is maintained at a first temperature T1, and said chamber body is maintained at a second temperature T2, where said second temperature T2 is lower than said first temperature T1.
2. The apparatus as in , wherein said liner and said chamber body are spaced apart from one another.
claim 1
3. The apparatus as in , wherein said liner and said chamber body are separated from one another by an isolating member.
claim 2
4. The apparatus as in , wherein said isolating member is a plurality of pins.
claim 3
5. The apparatus as in , wherein said pins are made of stainless steel or nickel.
claim 4
6. The apparatus as in , wherein said wafer processing comprises depositing titanium nitride film from a reaction of titanium tetrachloride and ammonia.
claim 1
7. The apparatus as in , wherein said first temperature T1 is approximately between 150° C. and 250° C.; and said second temperature T2 is approximately between 60° C. and 65° C.
claim 1
8. The apparatus as in , wherein said liner further comprises a heater embedded therein.
claim 1
9. The apparatus as in , further comprising:
claim 1
a pedestal positioned centrally within said liner to support a substrate within the chamber, where said pedestal is maintained at a third temperature T3 approximately between 600° C. and 800° C.
10. The apparatus as in , wherein said pedestal further comprises a heating element disposed inside said pedestal.
claim 9
11. The apparatus as in , wherein said pedestal is made of a ceramic material.
claim 9
12. The apparatus as in , wherein said ceramic material is aluminum nitride.
claim 11
13. The apparatus as in , wherein said pedestal further comprises an electrode disposed inside said pedestal, and said electrode is capable of imparting radio frequency power to a volume proximate said pedestal.
claim 9
14. The apparatus as in , further comprising:
claim 1
an exhaust assembly connected to said chamber body; and at least one heater element positioned proximate said exhaust assembly to maintain said exhaust assembly at a temperature T4.
15. The apparatus as in , where said temperature T4 is approximately between 150° C. and 200° C.
claim 14
16. The apparatus as in , where said at least one heater element is disposed around an exterior surface of said exhaust assembly.
claim 14
17. The apparatus as in , further comprising:
claim 1
a pedestal having a top surface, a bottom surface, an outer perimeter and an outside edge;
a substantially annular edge ring having a top surface, a bottom surface, an inside surface, an outside surface, and a protruded portion; and
said bottom surface, said inside surface and said protruded portion of said edge ring are disposed adjacent to and in close proximity to said outer perimeter and outside edge of said pedestal.
18. Apparatus for wafer processing, comprising:
a substantially bucket-shaped chamber body having a chamber side and a substantially annular-shaped chamber base having an inside bottom surface and defining a bottom opening in said chamber body, said chamber body capable of being maintained at a temperature T2;
a liner being substantially enclosed by said chamber body having a top end and a bottom end, an inside surface and an outside surface; where said liner is maintained at a temperature T1 which is higher than said temperature T2 of said chamber body;
an isolating member disposed between said bottom end of said liner and said inside surface of said chamber base that maintains said liner and said chamber base in a spaced apart relation;
a pedestal assembly positioned centrally within said bottom opening of said chamber body and within said liner; said pedestal assembly comprising:
a pedestal with a top surface, a bottom surface and a circumferential edge having a heater and at least one electrode embedded therein, said pedestal capable of being maintained at a temperature T3 which is higher than temperatures T1 and T2;
a shaft-like portion connected to said bottom surface of said pedestal;
a showerhead disposed above said pedestal having a top surface and a bottom surface;
an edge ring disposed at said circumferential edge of said pedestal; and
an exhaust assembly connected to said chamber body having an interior surface and an exterior surface, with at least one heater element disposed around said exterior surface to maintain said exhaust assembly at a temperature T4.
19. The apparatus as in , where said liner has a heater embedded therein.
claim 18
20. The apparatus as in , where said isolating member is a plurality of pins.
claim 18
21. The apparatus as in , wherein said temperature T1 is approximately between 150° C. and 250° C.; said temperature T2 is approximately between 60° C. and 65° C.; said temperature T3 is approximately between 600° C. and 800° C.; and said temperature T4 is approximately between 150° C. and 200° C.
claim 18
22. The apparatus as in , wherein said showerhead is capable of being coupled to a radio-frequency source for imparting radio-frequency to said showerhead.
claim 18
23. A method of wafer processing comprising the steps of:
a) heating a pedestal to temperature T3;
b) maintaining a liner at temperature T1 and a chamber at temperature T2; and
c) injecting process gases into said chamber for film deposition, where T3>T1>T2.
24. The method as in , where said temperature T1 is approximately between 150° C. and 250° C., said temperature T2 is approximately between 60° C. to 65° C., and said temperature T3 is approximately between 600° C. to 800° C.
claim 23
25. The method as in , further comprising the step of introducing a first purge gas to flow past said bottom surface of said pedestal and a second purge gas to flow between said liner and an inside surface of said chamber.
claim 24
26. The method as in , wherein said purge gas is nitrogen or argon.
claim 25
27. The method as in , further comprising the step of annealing said wafer after film deposition.
claim 23
28. The method as in , wherein said annealing step comprises heating said wafer to a temperature higher than T3.
claim 27
29. The method as in , wherein said annealing step comprises subjecting said wafer to a plasma inside said chamber.
claim 27
30. The method as in , wherein said injecting step comprises introducing at least two process gases without pre-mixing the process gases prior to entry into said chamber.
claim 23
31. The method as in , wherein said liner is heated to said temperature T1 by a heater embedded in said liner.
claim 23
32. The method as in , further comprising the step of cleaning said chamber after said film deposition.
claim 23
33. The method as in , wherein said cleaning step comprises the steps of:
claim 32
maintaining said pedestal at a temperature between 600-700° C.;
maintaining said chamber at a temperature between 150-250° C.; and
introducing chlorine gas into said chamber.
34. The method as in , wherein said cleaning step comprises creating a plasma containing chlorine species inside said chamber.
claim 33
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
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US09/211,998 US6364954B2 (en) | 1998-12-14 | 1998-12-14 | High temperature chemical vapor deposition chamber |
TW088120548A TW447014B (en) | 1998-12-14 | 1999-11-24 | High temperature chemical vapor deposition chamber |
PCT/US1999/029115 WO2000036179A2 (en) | 1998-12-14 | 1999-12-07 | High temperature chemical vapor deposition chamber |
KR1020017007351A KR20010080758A (en) | 1998-12-14 | 1999-12-07 | High temperature chemical vapor deposition chamber |
JP2000588423A JP2003524703A (en) | 1998-12-14 | 1999-12-07 | High temperature chemical vapor deposition chamber |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US09/211,998 US6364954B2 (en) | 1998-12-14 | 1998-12-14 | High temperature chemical vapor deposition chamber |
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US09/047,146 Continuation-In-Part US6360947B1 (en) | 1995-12-18 | 1998-03-24 | Automated holographic-based tunnel-type laser scanning system for omni-directional scanning of bar code symbols on package surfaces facing any direction or orientation within a three-dimensional scanning volume disposed above a conveyor belt |
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US09/157,778 Continuation-In-Part US6517004B2 (en) | 1995-12-18 | 1998-09-21 | Automated system for identifying and dimensioning packages transported through a laser scanning tunnel using laser scanning beam indexing techniques |
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US09/211,998 Expired - Lifetime US6364954B2 (en) | 1998-12-14 | 1998-12-14 | High temperature chemical vapor deposition chamber |
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JP (1) | JP2003524703A (en) |
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KR20010080758A (en) | 2001-08-22 |
JP2003524703A (en) | 2003-08-19 |
US6364954B2 (en) | 2002-04-02 |
WO2000036179A3 (en) | 2002-10-17 |
TW447014B (en) | 2001-07-21 |
WO2000036179A2 (en) | 2000-06-22 |
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