EP2932102A2 - Chemise d'entrefer pour pompes à couplage magnétique et procédé de fabrication de ladite chemise - Google Patents
Chemise d'entrefer pour pompes à couplage magnétique et procédé de fabrication de ladite chemiseInfo
- Publication number
- EP2932102A2 EP2932102A2 EP13820745.1A EP13820745A EP2932102A2 EP 2932102 A2 EP2932102 A2 EP 2932102A2 EP 13820745 A EP13820745 A EP 13820745A EP 2932102 A2 EP2932102 A2 EP 2932102A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- weight percent
- percent
- nickel
- side wall
- containment shell
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000004519 manufacturing process Methods 0.000 title claims description 8
- 239000000463 material Substances 0.000 claims abstract description 55
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 43
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 18
- 239000011651 chromium Substances 0.000 claims abstract description 13
- 238000010438 heat treatment Methods 0.000 claims abstract description 13
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 12
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 11
- 229910000623 nickel–chromium alloy Inorganic materials 0.000 claims abstract description 6
- 239000010955 niobium Substances 0.000 claims description 28
- 229910052758 niobium Inorganic materials 0.000 claims description 25
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 20
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 18
- 229910052782 aluminium Inorganic materials 0.000 claims description 16
- 239000010936 titanium Substances 0.000 claims description 14
- 229910052719 titanium Inorganic materials 0.000 claims description 14
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 10
- 238000000137 annealing Methods 0.000 claims description 10
- 229910052750 molybdenum Inorganic materials 0.000 claims description 10
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 9
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 9
- 229910052742 iron Inorganic materials 0.000 claims description 9
- 239000011733 molybdenum Substances 0.000 claims description 9
- 229910052715 tantalum Inorganic materials 0.000 claims description 8
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 8
- 229910000640 Fe alloy Inorganic materials 0.000 claims description 7
- BIJOYKCOMBZXAE-UHFFFAOYSA-N chromium iron nickel Chemical compound [Cr].[Fe].[Ni] BIJOYKCOMBZXAE-UHFFFAOYSA-N 0.000 claims description 7
- 238000000034 method Methods 0.000 claims description 6
- 229910001182 Mo alloy Inorganic materials 0.000 claims description 5
- OGSYQYXYGXIQFH-UHFFFAOYSA-N chromium molybdenum nickel Chemical compound [Cr].[Ni].[Mo] OGSYQYXYGXIQFH-UHFFFAOYSA-N 0.000 claims description 5
- 230000007797 corrosion Effects 0.000 abstract description 11
- 238000005260 corrosion Methods 0.000 abstract description 11
- 235000019589 hardness Nutrition 0.000 description 20
- 229910045601 alloy Inorganic materials 0.000 description 16
- 239000000956 alloy Substances 0.000 description 16
- 229910052799 carbon Inorganic materials 0.000 description 9
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- 239000000470 constituent Substances 0.000 description 4
- RKTYLMNFRDHKIL-UHFFFAOYSA-N copper;5,10,15,20-tetraphenylporphyrin-22,24-diide Chemical compound [Cu+2].C1=CC(C(=C2C=CC([N-]2)=C(C=2C=CC=CC=2)C=2C=CC(N=2)=C(C=2C=CC=CC=2)C2=CC=C3[N-]2)C=2C=CC=CC=2)=NC1=C3C1=CC=CC=C1 RKTYLMNFRDHKIL-UHFFFAOYSA-N 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 3
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 3
- 238000005275 alloying Methods 0.000 description 3
- 229910052796 boron Inorganic materials 0.000 description 3
- 239000010941 cobalt Substances 0.000 description 3
- 229910017052 cobalt Inorganic materials 0.000 description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 239000001257 hydrogen Substances 0.000 description 3
- 239000011572 manganese Substances 0.000 description 3
- 230000035882 stress Effects 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- 229910000990 Ni alloy Inorganic materials 0.000 description 2
- 230000032683 aging Effects 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 230000000171 quenching effect Effects 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 101100298222 Caenorhabditis elegans pot-1 gene Proteins 0.000 description 1
- RWSOTUBLDIXVET-UHFFFAOYSA-N Dihydrogen sulfide Chemical compound S RWSOTUBLDIXVET-UHFFFAOYSA-N 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 238000003483 aging Methods 0.000 description 1
- 239000000356 contaminant Substances 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000004519 grease Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 238000007542 hardness measurement Methods 0.000 description 1
- 229910000856 hastalloy Inorganic materials 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 238000010327 methods by industry Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 238000012805 post-processing Methods 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 239000011573 trace mineral Substances 0.000 description 1
- 235000013619 trace mineral Nutrition 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D13/00—Pumping installations or systems
- F04D13/02—Units comprising pumps and their driving means
- F04D13/021—Units comprising pumps and their driving means containing a coupling
- F04D13/024—Units comprising pumps and their driving means containing a coupling a magnetic coupling
- F04D13/025—Details of the can separating the pump and drive area
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/055—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/10—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D13/00—Pumping installations or systems
- F04D13/02—Units comprising pumps and their driving means
- F04D13/06—Units comprising pumps and their driving means the pump being electrically driven
- F04D13/0606—Canned motor pumps
- F04D13/0626—Details of the can
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/02—Selection of particular materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/02—Selection of particular materials
- F04D29/026—Selection of particular materials especially adapted for liquid pumps
Definitions
- the invention relates to a containment shell for arrangement in a gap between a driver and a rotor of a magnetically coupled pump, and to a method for producing the containment shell.
- Magnetically coupled pumps can be statically sealed by placing a stationary containment shell between a drive side driver and a magnetically driven output side rotor and surrounding the rotor.
- the containment shell is arranged in the magnetic field between the driver and the rotor, and the magnetic forces are transmitted through the containment shell.
- a pump impeller can be coupled.
- Drivers and rotors are provided with permanent magnets and arranged as close to each other as possible in order to provide an efficient drive.
- the wall thickness of the side wall of the containment shell specifies how large the gap or gap between driver and runner must be at least.
- a narrow gap or a very brief interpretation of the wall thickness of the split pot with respect to a minimum width the gap provides advantages in efficiency, in particular with regard to minimizing drive losses, but at the same time reduces a safety factor and possibly also the service life of the can, depending on which fluids are to be conveyed.
- the corrosion resistance is just in terms of the lowest possible wall thickness of the side wall of importance.
- the containment shell is also to be reworked, in particular cold-formed, in order to be able to adjust the geometry of the side wall by forming processes.
- Nickel-based alloys have proven to be suitable material for containment pots.
- the object is to provide a containment shell in which, in addition to good structural material properties, a high corrosion resistance can be ensured. It is also an object to design the containment shell so that it can be easily brought into a desired geometry. Last but not least, it is the task to design a containment shell in such a way that it can easily be given a high material hardness. At least one of these objects is achieved by a containment shell according to claim 1 and by a method according to claim 9. Advantageous developments of the invention are the subject of the dependent claims.
- An inventive containment shell e.g. can be used for arrangement in a gap between a driver and a rotor of a magnetically coupled pump or in a canned motor pump, has:
- a flange part e.g. for connecting the containment shell to the pump or the motor;
- the material is a nickel-chromium alloy which has at least 50 percent by weight nickel and 17 to 21 percent by weight chromium.
- a particularly resistant containment can be provided.
- the side wall of the material is made uniformly from the material, in particular when the side wall is designed with a view to a minimum material thickness.
- the entire containment shell made of the material although in particular for the flange and deviating, especially less expensive materials can be selected.
- the material has cobalt (Co), and the cobalt content is at most 1 percent by weight. More preferably, the material boron (B), and the boron content is at most 0.006 weight percent.
- a bottom of the split pot is preferably a section to understand, which closes the gap pot pot-shaped at one end and thereby merges into the side wall.
- a flange part of the containment shell is preferably a section which is designed to arrange and to fix the containment pot in a defined position and orientation in the pump.
- the material is a nickel-chromium-iron alloy, in particular a nickel alloy called Alloy 718 (Nicofer 5219 Nb), wherein the nickel content is at most 55 weight percent and the iron content is between 10 and 25 weight percent.
- the invention relates to the use of a suitable nickel-chromium-iron alloy for a split pot, which is designed for arrangement in a gap between a driver and a rotor of a magnetically coupled pump.
- Such a material may be a nickel-chromium-iron alloy, which has high strength and is therefore particularly useful for splitters used in pumps operating at high pressures. At the same time it is well deformable in certain conditions, especially in one solution annealed condition, and therefore can be easily reworked, for example by spin forming. It is also advantageous that hydrogen embrittlement does not occur in this material, so that hydrogen-containing media can also be delivered by means of a pump with such a containment shell.
- Such a material also provides the advantage that it is curable without deformations occur. In this way, a high-strength containment can be provided in a simple manner, which has a high dimensional accuracy, so that an air gap in the pump can be made very narrow.
- the hardening can take place in that a heat treatment takes place over a predefined period of time and at a predefined temperature at at least one predefined temperature level.
- a preliminary solution annealing is useful. The solution annealing can preferably take place with the following parameters:
- ⁇ produce in a furnace a temperature in the range of 960 ° C, especially 960 ° C + 15 ° C, preferably exactly 960 ° C;
- a hardness measurement is preferably carried out before and after the heat treatment.
- the containment shell be kept free of grease, oils, lubricants or other contaminants before it is heat treated.
- the adjustment of the hardness of the material can preferably take place with the following parameters:
- the material has a greater hardness compared to titanium. Furthermore, the material provides the advantage of high temperature resistance, in particular up to 600 ° C.
- the split pot according to the invention preferably obtains its desired geometry by spin forming the side wall as a special type of cold deformation.
- the cup part can be provided with a relatively thin side wall, for example in the range of 1 mm, wherein the wall thickness of the side wall can also lie in a narrow tolerance range, in particular with deviations smaller 1/10.
- the thin wall thickness, but also the narrow tolerance range offer the advantage of high drive efficiency in a magnetically coupled pump, because driver and rotor of the pump can be arranged very close together.
- the manufacturing costs can be kept low because rework on the side wall of the split pot are not required.
- the sidewall can be made with such high accuracy and tolerance that a face turning or grinding or any other molding process is no longer required.
- the term "spinning rolls" preferably refers to a cold forming process in which the side wall of the split pot is brought to a defined thickness and receives a defined orientation, in particular a cylindrical geometry with a high dimensional stability, ie a small deviation from the cylindrical shape in the radial direction (accuracy better 1/10). In this case, the pressure-rolling can lead to an extension of the cylindrical side wall in the axial direction, without changing the diameter of the gap pot.
- a desired geometry is to be understood as a geometry which the containment shell is to assume at the end of the production process, in particular in the region of the side wall and the bottom.
- the desired geometry is preferably defined by the respective wall thickness of the side wall and the bottom, an outer diameter and tolerance ranges for the respective dimensions.
- the mechanical properties of the hot- or cold-formed material of the split can of the invention at room temperature in solution annealed condition and after curing can be determined by the tensile strength (Rm) in N / mm 2 , the yield strength (Rp0.2) in N / mm 2 , the elongation at break (A5) and constriction (Z) in percent, the Brinell hardness in HB and the particle size in ⁇ define:
- Grain size in ⁇ preferably ⁇ 127.
- the modulus of elasticity may be, for example, in the range of 205 kN per mm 2 for room temperature and, for example, in the range of 199 kN per mm 2 for 100 ° C.
- the material of the can of the invention can (by suitable heat treatment) have an elongation at break of> 14% and a notch impact of> 20 joules, preferably> 27 joules.
- the can according to the invention meets the requirements of the Pressure Equipment Directive (Directive 97/23 / EC on pressure equipment). This makes the containment shell suitable for use in pumps that operate with an internal overpressure of more than 0.5 bar.
- the alloy contains a substantial content of niobium and molybdenum and a low content of aluminum and titanium.
- the percentages by weight are preferably in the following ranges, with the values given in parentheses referring to a variant of the alloy that can be used in corrosive media, especially media having H 2 S, C0 2 or Cl ,
- the change in composition relates in particular to the alloying constituents carbon and niobium, but also to aluminum and titanium, with higher carbon and niobium fractions providing advantages in high-temperature applications and lower carbon and niobium levels for corrosive media applications are:
- Chromium between 17 and 21 percent
- Niobium between 4.75 and 5.5 percent (niobium and tantalum together between 4.87 and 5.2 percent);
- Aluminum between 0.2 and 0.8 percent (0.4 and 0.6 percent); Titanium between 0.65 and 1, 15 percent (0.8 and 1, 1 5 percent);
- the remainder of iron is preferably in a range from 1 1 to 24.6 weight percent (12 to 24.13 weight percent).
- the alloy may have other trace elements, in particular up to 0.08 percent (0.045 percent) C, and / or up to 0.35 percent Mn, and / or up to 0.35 percent Si, and / or up to 0.3 Percent (0.23 percent) Cu, and / or up to 1.0 percent Co, and / or up to 0.05 percent Ta, and / or up to 0.006 percent B, and / or up to 0.015 percent (0, 01 percent) P, and / or up to 0.0015 percent (0.01 percent) S, and / or up to 5 ppm (10 ppm) Pb, and / or up to 3 ppm (5 ppm) S, and / or up to 0.3 ppm (0.5 ppm) Bi.
- trace elements in particular up to 0.08 percent (0.045 percent) C, and / or up to 0.35 percent Mn, and / or up to 0.35 percent Si, and / or up to 0.3 Percent (0.23 percent) Cu, and / or up to 1.0 percent Co, and
- the carbon content is exactly 0.08 wt% (0.045 wt%) or in a range of 75-100% of 0.08 wt% (0.045 wt%), ie between 0.06 and 0.08 weight percent (0.03375 and 0.045 weight percent).
- the niobium content is exactly 5.5 weight percent (5.2 weight percent niobium and tantalum together) or in a range of 5.25 to 5.5 weight percent (5.1 to 5.2 weight percent niobium and tantalum together).
- the carbon content is 0.00 wt% (0.00 wt%) or in the range 0-25% of 0.08 wt% (0.045 wt%), ie between 0.00 and 0.02 wt% (0 , 00 and 0.01 1 weight percent).
- the niobium content is exactly 4.75 weight percent (4.87 weight percent) or in the range of 4.75 to 5.0 weight percent (4.87 to 4.98 weight percent niobium and tantalum together).
- Such an alloy provides the advantage of high temperature resistance up to 700 ° C with good strength even in the high temperature range. Furthermore, these alloys have a high fatigue strength, a good creep strength up to 700 ° C and a good oxidation resistance up to 1000 ° C. They also provide good low temperature mechanical properties, good corrosion resistance at high and low temperatures, and good resistance to stress corrosion cracking and pitting. The corrosion resistance, especially against stress cracks, can be ensured in particular by the chromium content. The alloy can therefore also be used in media that are used in petroleum production and oil processing, in H 2 S-containing sour gas environments or in the field of marine technology.
- the density of the alloy is for example in the range of 8 g / cm 3 , in particular it is 8.2 g / cm 3 .
- the structure of the alloy is austenitic with several phases, in particular the phases carbides, laves ([Fe, Cr] 2Nb), ⁇ (Ni3Nb) orthorhombic, ⁇ "(Ni3Nb, Al, Ti) centered tetragonal, and / or ⁇ '( ⁇ 3 ⁇
- the phase ⁇ "(Ni 3 Nb, Al, Ti) is preferably tetragonally centered in space, which can be adjusted by precipitation hardening.
- the phase ⁇ "(Ni 3 Nb, Al, Ti) tetragonal body centered provides good resistance to aging deformation cracking
- the alloy can be made by melting in a vacuum induction furnace followed by electroslag remelting. The remelting can also be done by a vacuum arc process.
- the material has molybdenum, wherein the molybdenum content is between 2.8 and 3.3 percent by weight. In this way, a good corrosion resistance can be achieved, in particular independently of the temperature range in which the containment shell is used.
- the material comprises niobium, wherein the niobium content is 4.75 to 5.5 percent by weight, or the material comprises niobium and tantalum, the proportion of niobium and tantalum together being 4.87 to 5.2 percent by weight.
- a good temperature resistance can be set.
- the niobium content thereby ensures the formation of at least one of the following phases of an austenitic microstructure, whereby the advantageous strength values of the material can be adjusted: phase ⁇ (Ni 3 Nb) orthorhombic, phase ⁇ "(Ni 3 Nb, Al, Ti) tetragonal body-centered, and / or phase ⁇ '(Ni3AI, Nb) face centered cubic.
- the material comprises aluminum and titanium, wherein the aluminum content is between 0.2 and 0.8, preferably 0.4 and 0.6 weight percent and / or the titanium content between 0.65 and 1, 15, preferably 0 , 8 and 1, 15 weight percent.
- aluminum and titanium can ensure the formation of at least one of the following phases of an austenitic structure: phase ⁇ "(Ni 3 Nb, Al, Ti) tetragonal body-centered, and / or phase ⁇ '(Ni 3 Al, Nb ) Cubic area-centered.
- the material is a nickel-chromium-molybdenum alloy, in particular the nickel alloy Hastelloy C-22HS or one of the variants of this alloy, wherein the chromium content is 21 percent by weight and the nickel content is at least 56 percent by weight, especially 56.6 percent by weight, and Molybdenum content is 17 percent by weight.
- the invention relates to the use of a suitable nickel-chromium-molybdenum alloy for a split pot, for example for arrangement in a gap between a driver and a Rotor of a magnetically coupled or for a canned motor pump.
- a material is a nickel-chromium-molybdenum alloy, which has a high corrosion resistance and a high ductility with high rigidity and thus also dimensional stability in relation to a generated desired geometry.
- the alloying ingredients are preferably in the following percentages by weight:
- Nickel as the main constituent in a percentage depending on the percentages of the other constituents, but at least 56.6 percent;
- Co Cobalt (Co): maximum 1 percent
- Such a material can be cured in a simple manner after a preliminary forming. It is highly hardening by age hardening after cold working, especially without intermediate solution heat treatment.
- the achievable hardness is a function of the degree of deformation.
- This provides the advantage that, for example, a spin forming of the side wall of the split pot can be done to set a defined wall thickness, and that after the spin forming hardening of the side wall takes place.
- Cold forming, in particular spin forming preferably takes place after solution heat treatment.
- the material is also of high acid resistance, which makes its use for pumps in the chemical industry (chemical pumps) particularly interesting.
- the material has tungsten, which distinguishes it from the nickel-chromium-iron alloy described above.
- the strength of the material can be adjusted by a heat treatment in which Ni 2 (Mo, Cr) particles are formed, and the heat treatment is preferably carried out in a temperature range of 605 to 705 ° C.
- the good corrosion resistance of the alloy can also already be achieved by annealing alone.
- the heat treatment is performed to set a higher hardness under the following parameters:
- the density is preferably in the range of 8.6 g / cm 3 in the solution-annealed condition or 8.64 g / cm 3 in the cured state.
- the modulus of elasticity is for example in the range of 223 GPa (or kN / mm 2 ) for room temperature and for example in the range of 218 GPa (or kN / mm 2 ) for 100 ° C.
- the mechanical properties of the formed material at room temperature in solution annealed condition can be determined by the tensile strength (Rm) in N / mm 2 , the yield strength (Rp0.2) in N / mm 2 , the elongation at break (A5) and constriction (Z) in percent , which define Brinell hardness in HB and the grain size in ⁇ , the first values being cold-formed Refer to components and the second values in brackets to thermoformed components:
- the achievable hardnesses are in the following ranges, depending on the duration of a solution annealing before hardening, the hardness values were determined according to Rockwell, either by scale B (hardness values in the unit Rb) or C (hardness values in the unit Rc) ,
- the following hardness values of the side wall can be set by aging-hardening:
- the achievable hardness depends on the degree of deformation. The higher the degree of deformation, the higher the achievable hardness.
- the material comprises iron, wherein the iron content is at most 2 percent by weight.
- the side wall is a side wall brought into a desired geometry by a forming step, which has a degree of deformation of more than 10 percent, preferably between 20 and 50 percent, more preferably between 30 and 40 percent, in particular 35 percent.
- a forming step which has a degree of deformation of more than 10 percent, preferably between 20 and 50 percent, more preferably between 30 and 40 percent, in particular 35 percent.
- the invention also relates to a method for producing a split pot for arrangement in a gap between a driver and a rotor of a magnetically coupled pump, comprising the steps of:
- a side wall which can be arranged in the gap in the assembled state of the can, at least partially made of a material having a nickel component, wherein the side wall is brought into a desired geometry by a forming step, in particular by spin forming.
- the material selected is a nickel-chromium alloy in a solution-annealed state, which has at least 50 percent nickel by weight and 17 to 21 percent chromium by weight, hardening being effected by heat treatment after forming.
- the curing can be done either directly or after an intermediate solution annealing.
- the curing is preferably carried out by a heat treatment in the temperature range of 605 to 728 ° C, in particular over a period of 18 to 48 hours, wherein the heat treatment is in any case two-stage with respect to the selected temperature and a respective stage is maintained for at least 8 hours.
- the forming is a cold forming, wherein after the cold forming a paging hardening takes place, in particular in a temperature range of 605 to 728 ° C and without intermediate solution annealing after the cold forming.
- the cold forming is preferably a spin forming.
- Paging hardening can be done either directly after cold forming or after an intermediate step for solution annealing.
- aging is preferably carried out without solution annealing intermediate step.
- increasing hardness can be achieved with increasing hardening times, wherein the hardening times are e.g. be selected in the range of 1, 4, 10, 24 or 32 hours, preferably 32 hours at 605 ° C, since the longer duration, the hardness Rc to Rockwell scale C can be increased by over 10 percent.
- FIG. 1 is a diagram of typical
- FIG. 2 is a diagram of typical
- FIG. 3 in a schematic representation of a
- FIG. 1 shows typical short-term properties of a nickel-chromium-iron alloy in a solution-annealed and cured state as a function of temperature in ° C.
- FIG. It can be seen from the diagram that quite constant mechanical properties are present in a temperature range from room temperature to 600 ° C., which applies in particular to the breaking elongation (A5) and the constriction (Z), which provides advantages with regard to good dimensional accuracy of the containment shell.
- FIG. 2 shows typical creep ruptures of the nickel-chromium-iron alloy in a solution-annealed and cured state as a function of time in hours, with time plotted on a logarithmic scale, and with creep ruptures indicated on the y-axis in N / mm 2 are. It can be seen from the diagram that even over a period of 10 5 hours corresponding to just over 1 1 years at temperatures below 500 ° C., a loss of mechanical strengths is hardly noticeable. 3, a split pot 1 is shown, which is formed symmetrically with respect to a symmetry axis S and a bottom 2, a side wall 3 and a flange 4 has.
- the containment shell 1 has a nickel-chromium alloy, so it is partially or completely made of a material which can be formed from nickel and chromium and other alloying constituents.
- a partial embodiment of the split pot in the material may, for example, relate only to the side wall 3.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Heat Treatment Of Articles (AREA)
- Pressure Vessels And Lids Thereof (AREA)
Abstract
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102012024130.5A DE102012024130B4 (de) | 2012-12-11 | 2012-12-11 | Spalttopf für magnetgekuppelte Pumpen sowie Herstellungsverfahren |
PCT/EP2013/076195 WO2014090863A2 (fr) | 2012-12-11 | 2013-12-11 | Chemise d'entrefer pour pompes à couplage magnétique et procédé de fabrication de ladite chemise |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2932102A2 true EP2932102A2 (fr) | 2015-10-21 |
EP2932102B1 EP2932102B1 (fr) | 2017-03-01 |
Family
ID=50777749
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13820745.1A Revoked EP2932102B1 (fr) | 2012-12-11 | 2013-12-11 | Chemise d'entrefer pour pompes à couplage magnétique et procédé de fabrication de ladite chemise |
Country Status (10)
Country | Link |
---|---|
US (2) | US10167870B2 (fr) |
EP (1) | EP2932102B1 (fr) |
JP (3) | JP2016509125A (fr) |
KR (1) | KR102125592B1 (fr) |
CN (1) | CN104937277B (fr) |
DE (2) | DE102012024130B4 (fr) |
ES (1) | ES2627097T3 (fr) |
PL (1) | PL2932102T3 (fr) |
RU (1) | RU2640306C2 (fr) |
WO (1) | WO2014090863A2 (fr) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
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DE102012024130B4 (de) | 2012-12-11 | 2014-09-11 | Klaus Union Gmbh & Co. Kg | Spalttopf für magnetgekuppelte Pumpen sowie Herstellungsverfahren |
DE102013018159A1 (de) * | 2013-12-05 | 2015-06-11 | Klaus Union Gmbh & Co. Kg | Spalttopf und Verfahren zur Herstellung desselben |
US9771938B2 (en) * | 2014-03-11 | 2017-09-26 | Peopleflo Manufacturing, Inc. | Rotary device having a radial magnetic coupling |
EP3239534A4 (fr) * | 2015-01-27 | 2018-01-10 | Mitsubishi Heavy Industries Compressor Corporation | Carter de compresseur centrifuge et compresseur centrifuge |
US9920764B2 (en) | 2015-09-30 | 2018-03-20 | Peopleflo Manufacturing, Inc. | Pump devices |
CN105526190B (zh) * | 2016-01-21 | 2018-09-28 | 盐城海纳汽车零部件有限公司 | 一种汽车发动机冷却水泵合金结构钢模锻轮毂 |
DE102018130946B4 (de) * | 2017-12-14 | 2024-06-20 | Vdm Metals International Gmbh | Verfahren zur herstellung von halbzeugen aus einer nickel-basislegierung |
WO2020004286A1 (fr) * | 2018-06-28 | 2020-01-02 | 株式会社東亜鍛工所 | Procédé de fabrication de soupape de moteur creuse |
GB2581339A (en) * | 2019-02-08 | 2020-08-19 | Hmd Seal/Less Pumps Ltd | Containment shell for a magnetic pump |
EP4024675B1 (fr) | 2020-12-28 | 2024-07-10 | Tomas Pink | Rotor à usage unique pourvu de cage en court-circuit |
RU2764491C1 (ru) * | 2021-03-16 | 2022-01-17 | Александр Анатольевич Изюков | Разделительный стакан магнитной муфты |
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DE3413930A1 (de) * | 1984-04-13 | 1985-10-31 | Friedrichsfeld Gmbh, Steinzeug- Und Kunststoffwerke, 6800 Mannheim | Kreiselpumpe |
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JPH03134144A (ja) * | 1989-10-19 | 1991-06-07 | Toshiba Corp | ニッケル基合金部材およびその製造方法 |
DE9100515U1 (de) * | 1991-01-17 | 1991-04-04 | Friatec-Rheinhütte GmbH & Co, 65203 Wiesbaden | Magnetgekuppelte Kreiselpumpe |
EP0769076B1 (fr) * | 1994-06-24 | 2002-05-15 | Teledyne Industries, Inc | Alliage a base de nickel et procede |
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DE50202923D1 (de) * | 2002-09-06 | 2005-06-02 | Grundfos As | Nasslaufkreiselpumpenaggregat |
TW200514914A (en) * | 2003-09-19 | 2005-05-01 | Chrysalis Tech Inc | Threaded sealing flange for use in an external combustion engine and method of sealing a pressure vessel |
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DE202004013080U1 (de) | 2004-08-20 | 2006-01-05 | Speck-Pumpen Walter Speck Gmbh & Co. Kg | Magnetkupplungspumpe |
RU2290540C1 (ru) * | 2005-05-13 | 2006-12-27 | Федеральное государственное унитарное предприятие "Научно-производственное объединение прикладной механики им. акад. М.Ф. Решетнева" | Электронасосный агрегат |
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CA2588626A1 (fr) * | 2007-05-15 | 2008-11-15 | Benoit Julien | Procede de fabbrication d'elements statiques pour turbines a gaz |
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US7789288B1 (en) * | 2009-07-31 | 2010-09-07 | General Electric Company | Brazing process and material for repairing a component |
DE202009017996U1 (de) * | 2009-10-12 | 2010-10-28 | Deutsche Vortex Gmbh & Co. Kg | Trennwand für einen Elektromotor und Pumpe mit Elektromotor |
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CN201934335U (zh) * | 2010-12-29 | 2011-08-17 | 四川红华实业有限公司 | 无级变频气体增压机 |
DE202012006480U1 (de) * | 2012-07-06 | 2012-08-06 | Ruhrpumpen Gmbh | Doppelwandiger Spalttopf einer Magnetkupplung, insbesondere einer Magnetkupplungspumpe |
DE102012024130B4 (de) | 2012-12-11 | 2014-09-11 | Klaus Union Gmbh & Co. Kg | Spalttopf für magnetgekuppelte Pumpen sowie Herstellungsverfahren |
JP6857428B1 (ja) * | 2020-02-12 | 2021-04-14 | 株式会社アースクリエイト | 積層体及び食品用容器包装 |
-
2012
- 2012-12-11 DE DE102012024130.5A patent/DE102012024130B4/de not_active Withdrawn - After Issue
-
2013
- 2013-12-11 DE DE202013012787.2U patent/DE202013012787U1/de not_active Expired - Lifetime
- 2013-12-11 WO PCT/EP2013/076195 patent/WO2014090863A2/fr active Application Filing
- 2013-12-11 CN CN201380071200.XA patent/CN104937277B/zh active Active
- 2013-12-11 RU RU2015128080A patent/RU2640306C2/ru active
- 2013-12-11 KR KR1020157018663A patent/KR102125592B1/ko active IP Right Grant
- 2013-12-11 US US14/650,823 patent/US10167870B2/en active Active
- 2013-12-11 ES ES13820745.1T patent/ES2627097T3/es active Active
- 2013-12-11 PL PL13820745T patent/PL2932102T3/pl unknown
- 2013-12-11 JP JP2015546996A patent/JP2016509125A/ja active Pending
- 2013-12-11 EP EP13820745.1A patent/EP2932102B1/fr not_active Revoked
-
2018
- 2018-07-06 US US16/029,018 patent/US10253776B2/en active Active
-
2019
- 2019-02-12 JP JP2019022806A patent/JP7185551B2/ja active Active
-
2021
- 2021-08-02 JP JP2021126789A patent/JP2021191896A/ja not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
US10253776B2 (en) | 2019-04-09 |
CN104937277B (zh) | 2018-07-13 |
JP2021191896A (ja) | 2021-12-16 |
EP2932102B1 (fr) | 2017-03-01 |
WO2014090863A2 (fr) | 2014-06-19 |
WO2014090863A3 (fr) | 2015-02-26 |
KR20150094754A (ko) | 2015-08-19 |
ES2627097T3 (es) | 2017-07-26 |
US20150337844A1 (en) | 2015-11-26 |
RU2640306C2 (ru) | 2017-12-27 |
KR102125592B1 (ko) | 2020-07-08 |
US10167870B2 (en) | 2019-01-01 |
DE202013012787U1 (de) | 2019-08-26 |
DE102012024130B4 (de) | 2014-09-11 |
CN104937277A (zh) | 2015-09-23 |
RU2015128080A (ru) | 2017-01-18 |
JP2019116686A (ja) | 2019-07-18 |
JP7185551B2 (ja) | 2022-12-07 |
JP2016509125A (ja) | 2016-03-24 |
PL2932102T3 (pl) | 2017-09-29 |
US20180313353A1 (en) | 2018-11-01 |
DE102012024130A1 (de) | 2014-06-12 |
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