CA1209726A - Zirconium alloy barrier having improved corrosion resistance - Google Patents
Zirconium alloy barrier having improved corrosion resistanceInfo
- Publication number
- CA1209726A CA1209726A CA000427055A CA427055A CA1209726A CA 1209726 A CA1209726 A CA 1209726A CA 000427055 A CA000427055 A CA 000427055A CA 427055 A CA427055 A CA 427055A CA 1209726 A CA1209726 A CA 1209726A
- Authority
- CA
- Canada
- Prior art keywords
- zirconium
- chromium
- iron
- weight
- zirconium alloy
- 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.)
- Expired
Links
- 229910001093 Zr alloy Inorganic materials 0.000 title claims abstract description 116
- 238000005260 corrosion Methods 0.000 title abstract description 17
- 230000007797 corrosion Effects 0.000 title abstract description 17
- 230000004888 barrier function Effects 0.000 title abstract description 14
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 156
- 238000005253 cladding Methods 0.000 claims abstract description 128
- 229910052742 iron Inorganic materials 0.000 claims abstract description 78
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 76
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims abstract description 76
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 76
- 239000011651 chromium Substances 0.000 claims abstract description 76
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 74
- 239000003758 nuclear fuel Substances 0.000 claims abstract description 71
- 239000002131 composite material Substances 0.000 claims abstract description 59
- 239000000758 substrate Substances 0.000 claims abstract description 46
- 239000000463 material Substances 0.000 claims abstract description 37
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 32
- 229910052802 copper Inorganic materials 0.000 claims abstract description 31
- 239000010949 copper Substances 0.000 claims abstract description 31
- 229910052751 metal Inorganic materials 0.000 claims abstract description 31
- 239000002184 metal Substances 0.000 claims abstract description 31
- 229910045601 alloy Inorganic materials 0.000 claims description 21
- 239000000956 alloy Substances 0.000 claims description 21
- 239000000203 mixture Substances 0.000 claims description 7
- 230000006872 improvement Effects 0.000 claims description 4
- ZSLUVFAKFWKJRC-IGMARMGPSA-N 232Th Chemical compound [232Th] ZSLUVFAKFWKJRC-IGMARMGPSA-N 0.000 claims 2
- 229910052778 Plutonium Inorganic materials 0.000 claims 2
- 229910052776 Thorium Inorganic materials 0.000 claims 2
- 229910052770 Uranium Inorganic materials 0.000 claims 2
- 150000001875 compounds Chemical class 0.000 claims 2
- OYEHPCDNVJXUIW-UHFFFAOYSA-N plutonium atom Chemical compound [Pu] OYEHPCDNVJXUIW-UHFFFAOYSA-N 0.000 claims 2
- DNYWZCXLKNTFFI-UHFFFAOYSA-N uranium Chemical compound [U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U] DNYWZCXLKNTFFI-UHFFFAOYSA-N 0.000 claims 2
- 230000004992 fission Effects 0.000 abstract description 19
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 12
- 239000012535 impurity Substances 0.000 abstract description 6
- 230000003647 oxidation Effects 0.000 abstract description 6
- 238000007254 oxidation reaction Methods 0.000 abstract description 6
- 238000005336 cracking Methods 0.000 abstract description 5
- 239000000446 fuel Substances 0.000 description 41
- 239000002826 coolant Substances 0.000 description 13
- 239000007789 gas Substances 0.000 description 13
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 10
- 238000006243 chemical reaction Methods 0.000 description 9
- 238000000034 method Methods 0.000 description 9
- 239000010935 stainless steel Substances 0.000 description 9
- 229910001220 stainless steel Inorganic materials 0.000 description 8
- 239000008188 pellet Substances 0.000 description 7
- 238000000576 coating method Methods 0.000 description 6
- 238000009792 diffusion process Methods 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 6
- 238000007792 addition Methods 0.000 description 5
- 239000010410 layer Substances 0.000 description 5
- 229910052759 nickel Inorganic materials 0.000 description 5
- 230000009467 reduction Effects 0.000 description 5
- FCTBKIHDJGHPPO-UHFFFAOYSA-N uranium dioxide Inorganic materials O=[U]=O FCTBKIHDJGHPPO-UHFFFAOYSA-N 0.000 description 5
- 238000013459 approach Methods 0.000 description 4
- 230000008901 benefit Effects 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 4
- 239000001257 hydrogen Substances 0.000 description 4
- 229910052739 hydrogen Inorganic materials 0.000 description 4
- 230000003993 interaction Effects 0.000 description 4
- 229910001338 liquidmetal Inorganic materials 0.000 description 4
- 239000010955 niobium Substances 0.000 description 4
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 4
- OOAWCECZEHPMBX-UHFFFAOYSA-N oxygen(2-);uranium(4+) Chemical compound [O-2].[O-2].[U+4] OOAWCECZEHPMBX-UHFFFAOYSA-N 0.000 description 4
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 3
- 238000010521 absorption reaction Methods 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 230000008021 deposition Effects 0.000 description 3
- 239000011888 foil Substances 0.000 description 3
- 150000002431 hydrogen Chemical class 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 229910052758 niobium Inorganic materials 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- 238000012546 transfer Methods 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000000919 ceramic Substances 0.000 description 2
- 230000006866 deterioration Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000009713 electroplating Methods 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 230000002285 radioactive effect Effects 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- BHMLFPOTZYRDKA-IRXDYDNUSA-N (2s)-2-[(s)-(2-iodophenoxy)-phenylmethyl]morpholine Chemical compound IC1=CC=CC=C1O[C@@H](C=1C=CC=CC=1)[C@H]1OCCNC1 BHMLFPOTZYRDKA-IRXDYDNUSA-N 0.000 description 1
- 229910018125 Al-Si Inorganic materials 0.000 description 1
- 229910018520 Al—Si Inorganic materials 0.000 description 1
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- 229910000861 Mg alloy Inorganic materials 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 241001611408 Nebo Species 0.000 description 1
- 229910001128 Sn alloy Inorganic materials 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- XNFDWBSCUUZWCI-UHFFFAOYSA-N [Zr].[Sn] Chemical compound [Zr].[Sn] XNFDWBSCUUZWCI-UHFFFAOYSA-N 0.000 description 1
- 239000006096 absorbing agent Substances 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 239000011889 copper foil Substances 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000004845 hydriding Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 238000009659 non-destructive testing Methods 0.000 description 1
- 230000003071 parasitic effect Effects 0.000 description 1
- 150000003061 plutonium compounds Chemical class 0.000 description 1
- UTDLAEPMVCFGRJ-UHFFFAOYSA-N plutonium dihydrate Chemical compound O.O.[Pu] UTDLAEPMVCFGRJ-UHFFFAOYSA-N 0.000 description 1
- FLDALJIYKQCYHH-UHFFFAOYSA-N plutonium(IV) oxide Inorganic materials [O-2].[O-2].[Pu+4] FLDALJIYKQCYHH-UHFFFAOYSA-N 0.000 description 1
- 239000002574 poison Substances 0.000 description 1
- 231100000614 poison Toxicity 0.000 description 1
- 229920000136 polysorbate Polymers 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000036647 reaction Effects 0.000 description 1
- 239000003870 refractory metal Substances 0.000 description 1
- 229910052702 rhenium Inorganic materials 0.000 description 1
- WUAPFZMCVAUBPE-UHFFFAOYSA-N rhenium atom Chemical compound [Re] WUAPFZMCVAUBPE-UHFFFAOYSA-N 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 229910001256 stainless steel alloy Inorganic materials 0.000 description 1
- 230000008961 swelling Effects 0.000 description 1
- 150000003586 thorium compounds Chemical class 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 150000003671 uranium compounds Chemical class 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
-
- G—PHYSICS
- G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
- G21C—NUCLEAR REACTORS
- G21C3/00—Reactor fuel elements and their assemblies; Selection of substances for use as reactor fuel elements
- G21C3/02—Fuel elements
- G21C3/04—Constructional details
- G21C3/16—Details of the construction within the casing
- G21C3/20—Details of the construction within the casing with coating on fuel or on inside of casing; with non-active interlayer between casing and active material with multiple casings or multiple active layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/013—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E30/00—Energy generation of nuclear origin
- Y02E30/30—Nuclear fission reactors
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- General Engineering & Computer Science (AREA)
- High Energy & Nuclear Physics (AREA)
- Monitoring And Testing Of Nuclear Reactors (AREA)
- Laminated Bodies (AREA)
- Details Of Rigid Or Semi-Rigid Containers (AREA)
- Physical Vapour Deposition (AREA)
- Powder Metallurgy (AREA)
Abstract
ZIRCONIUM ALLOY BARRIER HAVING
IMPROVED CORROSION RESISTANCE
ABSTRACT OF THE DISCLOSURE
A nuclear fuel element for use in the core of a nuclear reactor has a composite cladding container having a substrate and a dilute zirconium alloy liner bonded to the inside surface of the substrate.
The dilute zirconium alloy liner forms about 1 to about 20 percent of the thickness of the cladding and is comprised of zirconium and a metal selected from the group consisting of iron, chromium, iron plus chromium, and copper. The dilute zirconium alloy liner shields the substrate from impurities or fission products from the nuclear fuel material and protects the substrate from stress corrosion and stress cracking. The dilute zirconium alloy liner displays greater corrosion resistance, especially to oxidation by hot water or steam than unalloyed zirconium. The substrate material is selected from conventional cladding materials, and preferably is a zirconium alloy.
IMPROVED CORROSION RESISTANCE
ABSTRACT OF THE DISCLOSURE
A nuclear fuel element for use in the core of a nuclear reactor has a composite cladding container having a substrate and a dilute zirconium alloy liner bonded to the inside surface of the substrate.
The dilute zirconium alloy liner forms about 1 to about 20 percent of the thickness of the cladding and is comprised of zirconium and a metal selected from the group consisting of iron, chromium, iron plus chromium, and copper. The dilute zirconium alloy liner shields the substrate from impurities or fission products from the nuclear fuel material and protects the substrate from stress corrosion and stress cracking. The dilute zirconium alloy liner displays greater corrosion resistance, especially to oxidation by hot water or steam than unalloyed zirconium. The substrate material is selected from conventional cladding materials, and preferably is a zirconium alloy.
Description
~2`~ 72~
Z IRCONIUM ALLOY BARRIER HAVING
.
IMPROVED CORROSION RESISTANCE
EIELD OF TXE INVENTION
This invention relates broadly to an improvement in nuclear fuel elements for use in the core of nuclear fission reactors and, more particularly, to an improved nuclear fuel element having a composite cladding container having a metal liner of dilute zirconium alloy consisting of zirconium and a metal selected from the group consisting of iron, chromium, iron plus chromiuml and copper bonded to the inside surface of the zirconium alloy cladding substrate.
~ACKGROUND OF T~IE INVENTION
Nuclear reactors are presently being designed, constructed, and operated in which the nuclear fuel is contained in fuel elements which can have various geometric shapes, such as plates, tubes, or rods.
The fuel material is usually enclosed in a corroslon-resistant, non-reactive, heat conductive container or cladding. The fuel elements are assembled together in a lattice at fixed distances from each other in a coolant flow channel or region forming a fuel assembly, and sufficient fuel assemblies are combined to orm the nuclear fission chain reacting assembly or reactor core capabIe of a sel-f-sustained fission reaction.
The corel in turn, is enclosed within a reactor vessel through which a coolant ls passed.
~ ;
~J ~'2~i The cladding serves several purposes and two primary purposes are: first, to prevent contact and chemical reactions between the nuelear fuel and the coolant or the moderator if a moderator is present, or both if both the coolant and the moderator are present; and second, to prevent the radioactive fission products, some o:E which are gases, from being released from the fuel into the coolant or the moderator or both if both the coolant and the moderator are present. Common cladding materials are stainless steel, aluminum and its alloys~ zirconium and its alloys~ niobium (columbium), certain magnesium alloys, and others. The failure of the cladding, i.e.~ a loss of the leak tightness~ can contaminate the coolant or moderator and the associated systems with long-lived radioactive products to a degree which interferes with plant operation.
Problems have been encountered in the manufacture and in the operation of nuclear fuel elements which employ certain metals and alloys as the cladding material due to mechanical or chemical reactions of these cladding materials under certain circumstances.
Zirconium and its alloys, under normal circumstances, make excellent nuclear fuel claddings since they have low neutron absorption cross-sections and at temperatures below about 750 F (about 398 C) are strong, ductile, extremely stable and relatively non-reactive in the presence of demineralized water or steam which are commonly used as reactor coolants and moderators.
However, fuel element performance has revealed a problem with the brittle splitting of the cladding due to the eombined interactions between the nuelear fuel, the cladding and the fission products produced during nuclear fission reac-tions. It has been discovered that this undesirable performance is promoted by localized mechanical stress due to differential expansion of fuel and cladding (stresses ~9~
24--NT-044 ~1 in the cladding are concentrated at cracks in the nuclear fuel). Corrosive fission products are released from the nuclear fuel and are present at the intersection of the fuel cracks with the cladding surface. Such fission products are created in the nuclear fuel during the fission chain reaction during operation of a nuclear reactor. The localized stress is exaggerated ~y high friction between the fuel and the cladding.
Within the confines of a sealed fuel element, hydrogen gas can be generated by the slow reaction between the cladding and residual water inside the cladding. This hydrogen gas may build up to levels which, under certain conditions; can result in localized hydriding of the cladding with concurrent local deterioration in the mechanical properties of the cladding. The cladding is also adversely affected by such gases as oxygen, nitrogen, carbon monoxide, and carbon dioxide over a wide range of temperatures.
The zirconium cladding of a nuclear fuel element is exposed to one or more of the gases listed above and fission products during irradiation in a nuclear reactor and this occurs in spite of the fact that these gases may not be present in the reactor coolant or moderator, and further may have been excluded as far as possible from the ambient atmosphere during manufacture of the cladding and the fuel element.
Sintered refractory and ceramic compositions, such as uranium dioxide and other compositions used as nuclear fuel, release measurable quantities of the aforementioned gases upon heatingl such as during fuel element manufacture and urther release ~ission products during irradiation. Particulate refractory and ceramic compositions~ such as uranium dioxide powder and other powders used as nuclear fuel, have been known to reIease even larger quantities of the a-forementioned gases during irradiation. These ~2~
- 4 - 24-NF-044~1 released gases are capable of reacting with the zirconium cladding containing the nuclear fuel.
Thus, in light of the foregoing, it has been found desirable to minimize attack of the cladding from water, water vapor and other gases, especially hydrogen, which are reactive with the cladding from inside the fuel element throughout the time the fuel element is used in the operation of nuclear power plants. One such approach has been to find materials which will chemically react rapidly with the water, water vapor and other gases to eliminate these from the interior of the cladding. Such materials are called getters.
Another approach has been to coat the nuclear fuel material with any of a variety of materials to prevent moisture coming in contact with the nuclear fuel material.
The coating of nuclear fuel material introduces reliability problems in that achieving uniform coatings free of faults is difficult. Further, the deterioration of the coating can introduce problems with the long-lived performance of the nuclear fuel material.
General Electric Atomic Power Document 4555 of February 1964, at GE NEBO Library, 175 Curtner Ave., San Jose, Calif. 95125, discloses a composite cladding of a zirconium alloy with an inner lining of stainless steel metallurgically bonded to the zirconium alloy, and the composite cladding is fabricated by extrusion of a hollow billet of the zirconium alloy having an inner lining of stainless steel. This cladding has the disadvantage that the stainless steel develops brittle phases, and the stainless steel layer involves a neutron absorption penalty of about -ten to fifteen times the penalty for a zirconium alloy of the same thickness.
U~S. Patent No. 3,502,5~9, issued March 24, 1970 to Charveriat, discloses a method for protecting zirconium and its alloys by the electrolytic deposition of chromium to provide a composite material useful for nuclear reactors. A method for electrolytic ~2~97~ 24-NT-0~481 deposition of copper on Zircaloy-2 surfaces and subsequent heat treatment for the purpose of obtaining surface diffusion of the electrolytically deposited metal is presented in Energia Nuclearer ~olume 11~
No. 9 ~September, 1964) at pages 505-508. In Stability and Compatibility of Hydrogen Barriers Applied to zirconium Alloys, by F. Brossa et al (~uropean Atomic Energy Community, Joint Nuclear Research Center, EUR 4098e~ 1969), methods of deposition of different coatings and their efficiency as hydrogen diffusion barriers are described along with an Al-Si coating as the most promising barrier against hydrogen diffusion.
Methods for electroplating nickel on zirconium and zirconium-tin alloys and heat treating these alloys to produce alloy-diffusion bonds are disclosed in Electroplating on Zirconium and Zirconium-Tln, by W.C. Schickner et al (BMI-757/ Technical Information Service, 1952~.
U.S. Patent No. 3,625,821, issued December 7l 1971 to Ricks, presents a fuel element for a nuclear reactor having a fuel cladding tube with the inner surface of the tube being coated with a metal of low neutron capture cross-section such as nickel and having finely dispersed particles of a burnable poison disposed therein. Reactor Development Program - ~ of August, 1973 (ANL-RDP-l9) discloses a chemical getter arrangement of a sacrificial layer of chromium on the inner surface of a stainless steel cladding.
Another approach has been to introduce a barrie~ between the nuclear fuel material and the cladding holding the nuclear fuel material as disclosed in U.S. Patent No. 3,230,150, issued ~anuary 18, 1966 to Martin et al (copper foil); German Patent Publication DAS lr238,115 (titanium layer); U.S. Patent No. 3,212,988, issued October 19, 1965 to Ringot et al (sheath of ~2~Z~
zirconium, aluminum, aluminum or beryllium); U.S. Patent No. 3,018,238, issued January ?3~ 1962 to Layer et al (barrier of crystalline carbon between the U02 and the zirconium alloy cladding); and U.S. Patent No. 3,088,893, issued May 7, 1963 to Spalaris, (stainless steel foil).
While the barrier concept proves promising, some of the foregoing references involve incompatible ma-terials with either the nuclear fuel (e.g., carbon can combine with oxygen from the nuclear fuel), or the cladding (e.g., copper and other metals can react with the cladding, altering the properties of the cladding), or the nuclear fission reaction (e.g., by acting as neutron absorbers). None of the listed references disclose solutions to the problem of localized chemical-mechanical interactions between the nuclear fuel andthe cladding.
Further approaches to the barrier concept are disclosed in U~S. Patent No. 3,969,186t issued July 13, 1976 to Thompson, (refractory metal such as molybdenum~ tungsten, rhenium, niobium and alloys thereof in the form of a tube or foil of single or multiple layers or a coa~ing on the internal surface of the cladding), and U.5. Patent No. 3,925,151, issued December 9, 1975 to Klepfer, (liner of zirconium, niobium~ or alloys thereof between the nuclear fuel and the cladding with a coating of a high lubricity material between liner and the cladding).
U.S. Patent No. 4rO45,288, issued August 30, 1977~ to Armijo, discloses a composite cladding of a zirconium alloy substrate with a metal barrier metallurgically bonded to the substrate and an inner layer of zirconium alloy metallurgically bonded to the metal barrier. The barrier i5 selected from a group of niobiumr aluminuml copper, nickel, stainless steel, and iron. The buried metal barrier reduces corrosion due to fission products and corrosive gases, but is subject to stress corrosion cracking , ~ ~ 24-NT-04~81 and liquid metal embrittlement.
U.S. Patent No. 4,200,492~ issued April 29, 1980, to Armijo, discloses a composite cladding of a zirconium alloy substrate with a sponge zirconium liner. The soft zirconium liner minimizes localized strain, and reduces stress corrosion cracking and liquid metal embrittlement, but is subject to loss due to honing and the like during fabrication and due to oxidation. Furthermore, if a breach in the cladding should occur, allowing water and/or steam to enter the fuel rod, the zirconium liner tends to oxidize rapidly.
Accordingly, it has remained desirable to develop nuclear fuel elements minimizing the problems discussed above.
SU~ARY OF THE INVENTION
A particularly effective nuclear fuel elemen-t for use in -the core of a nuclear reactor has a composite cladding having a metal liner of dilute zirconium alloy metallurgically bonded to the inside surface of the substrate. The dilute zirconium alloy comprises zirconium and a metal selected from the group consisting of iron, chromium, iron plus chromium and copper, wherein the amount of iron alloyed with the zirconium is from about 0.2% to about 0.3% by weight, the amount of chromium is from about 0.05% to about 0.3% by weight; the total amount of iron plus chromium is from about 0.15% to about 0.3% by weight and wherein the ratio of the weights of iron to chromium is in the range of from about 1:1 to about 4:1; and wherein the amount of copper is from about 0.002% to about 0.2% by weight.
The substrate of the cladding is completely unchanged in design and function from previous practice for a nuclear reactor and is selected from conventional cladding materials such as zirconium alloys. A
zirconium alloy cladding substrate has a higher alloy content than the dilute zirconium alloy liner. The ~ 7~ 24-NT-04481 dilute zirconium alloy liner forms a continuous shield between the substrate and the nuclear fuel material held in the cladding, as well as shielding -the zirconium alloy or other substrate cladding from fission products and gases.
The dilute zirconium alloy liner forms from about 1 to about 20 percent of the thickness of the cladding. The liner remains soft, relative to the substrate, during irradiation and minimizes localized stress inside the nuclear fuel element, thus serving to protect the cladding from stress corrosion cracking or liquid metal embrittlement. The dilute zirconium alloy liner shields the substrate from reaction with volatile impurities or fission products present inside the nuclear fuel element and, in this mannerJ serves to protect the cladding substrate from attack by the volatile impurities or fission products~
This invention has a striking advantage that the substrate of the cladding is protected from stress corrosion cracking and liquid metal embrittlement, in addition to contact with fission products, corrosive gases, etc., by the dilute zirconium alloy liner and the liner does not introduce any appreciable neutron capture penalties~ heat transfer penalties, or fuel/
liner incompatibility problems. In addition, the liner provides superior resistance to steam or hot water oxidation as compared to unalloyed zirconium in the event of a breach in the cladding.
DESCRIPTION OF THE DRA~INGS
The foregoing and other objects of this invention will become apparent to persons skilled in the art from reading the following specification and the appended claims with reference to the accompanying drawings described hereinafter.
FIG. 1 is a partial cutaway sectional view of a nuclear fuel assembly containing nuclear fuel . .
37;~6 24-NT-04481 g elements constructed according to the teaching of this invention; and FIG. 2 is an enlarged transverse cross-sectional view of the nuclear fuel element in FIG. 2 illustrating the teaching of this invention.
DESCRIPTION OF THE INVENTION
Referring now more particularly to FIG. 1, there is shown a partially cutaway sectional view of a nuclear fuel assembly 10. This fuel assembly 10 consists of a tubular flow channel 11 of generally square cross section provided at its upper end with a lifting bail 12 and at its lower end with a nose piece (not shown due to the lower portion of assembly 10 being omitted). The upper end of channel 11 is open at outlet 13 and the lower end of the nose piece is provided with coolant flow openings. An array of fuel elements or rods 14 is enclosed in the channel 11 and suppor-ted -therein by means of an upper end plate 15 and a lower end plate (not shown due to the lower portion being omitted). The liquid coolant ordinarily enters through the openings in the lower end of the nose piece, passes upwardly around fuel elements 14, and discharges through -the upper outlet 13 at an elevated temperature in a partially vaporized condition for boiling reactors or in an unvaporized condition for pressurized reactors.
The nuclear fuel elements or rods 14 are sealed at their ends by means of end plugs 18 welded to the cladding 17, which may include studs 19 to facilitate the mounting of the fuel rod in the assembly.
A void space or plenum 20 is provided at one end of the element to permit longitudinal expansion of the fuel material and accumulation of gases released from the fuel material~ ~ nuclear fuel material retainer means 24 in the form of a helical member is positioned within space 20 to provide restraint against the axial movement of the pellet column, especially during handling and transportation of the fuel element.
7;~
The fuel element is designed to provide an excellent thermal contact between the cladding and the fuel material, a minimum of parasitic neutron absorption and resistance to bowing and vibration which is occasionally caused by flow of the coolant at high velocity.
A nuclear fuel element or rod 14 constructed according to the teachings of this invention is shown in a partial section in FIG~ 1. The fuel element includes a core or central cylindrical portion of nuclear fuel material 16, here shown as a plurality of fuel pellets of fissionable and/or fertile material positioned within a structural cladding or container 17. In some cases, the fuel pellets may be of various shapes such as cylindrical pellets or spheres and, in other cases, different fuel forms such as a particulate fuel may be used. The physical form of the fuel is immaterial to this invention.
Various nuclear fuel materials may be used including uranium compounds, plutonium compounds, thorium compounds, and mixtures thereo. A preferred fuel is uranium dioxide or a mixture comprising uranium dioxide and plutonium dioxide.
Referring now to FIG. 2, the nuclear fuel material 16 forming the central core of the fuel element 14 is surrounded by a cladding 17 which, in this invention, is also referred to as a composite cladding container.
The composite cladding container encloses the fissile core so as to leave a gap 23 be-tween the core and the cladding during use in a nuclear reactor. The composite cladding container has an external substrate 21 selected from conventional cladding materials such as a stainless steel and zirconium alloys and, in a preferred embodiment of this invention, the substrate is a zirconium alloy such as Zircaloy-2.
35The substrate 2I has metallurgically bonded on the inside circumference thereof a dilute zirconium 24-NT-0~81 alloy liner 22 so that the dilute zirconium alloy liner forms a shield of the substrate from the nuclear fuel material 16 inside the composite cladding The dilute zirconium alloy liner preferably forms about 1 to about 20% of the thickness of the cladding. A dilute zirconium alloy liner forming less than about 1% of the thickness of the cladding would be difficult to achieve in commercial production, and a dilute zirconium alloy liner forming more than 20% of the thickness of the cladding provides no additional benefit for the added thickness. Further, a liner more than about 20% of the thickness of the cladding means a concomitant reduction in thickness of the substrate and possible weakening of the cladding.
The dilute zirconium alloy is comprised of zirconium and an alloy addition selected from the group consisting of: iron, chromium, iron pIus chromium and copper. As used herein, dilute zirconium alloy means a zirconium alloy with an alloy content sufficiently low to display greater ductility and higher strain rate than does the substrate material under equivalent conditions of stress.
The amount of iron alloyed with zirconium is from about 0.2% to about 0.3% by weight, and preferably from about 0.2% to about 0.25% by weight.
Chromium is in the range of from about 0.05%
to about 0.3% by weight and preferably from about 0.15%
to about 0.25~ by weight.
Iron plus chomium may be included so that the total amount of both components is from about 0.15% to about 0.3% by weight and preferably from about 0.2% to about 0.25% by weight and wherein the ratio of the weights of iron to chromium is from about 1:1 to about ~:1 and preferably about 2:1.
Copper is used in the amount of from about 0.02% to about 0.2% by weight and preferably from about 0.05~ to about 0.15% by weight.
..
7~
` 24-NT-04481 The dilute zirconium alloy liner shields the substrate from gaseous impurities and fission products and protects the substrate portion of the cladding from contact and reaction with such impurities and fission products and prevents the occurrence of localized stress.
The addition to zirconium of small amounts of a metal selected from the group of iron, chromium, iron plus chromium and copper improves corrosion resistance, especially resistance to oxidation by hot water or steam if the addition is within the stated range for that metal. The lower limit of the amount of each metal alloyed with zirconium provides su~ficient quantity of that metal to signiEicantly improve the corrosion resistance as compared to unalloyed zirconium.
The upper limit of the amount of each metal alloyed with zirconium is generally set at the maximum amount of the metal which significantly improves the corrosion resistance as compared with sponge zirconium.
Additions of the metal exceeding the upper limit fail to significantly enhance the corrosion resistance properties of zirconium and may have a detrimental effect in reducing the softness and ductility of the liner.
The additions of each metal to zirconium that impart the greatest improvement in corrosion resistance are stated as the preferred ranges.
Iron, chromium and copper are sparingly soluble in zirconium. Dilute zirconium alloys involving one or more of these metals can be heat treated to provide a material with a fine dispersion of intermetallic particles which ar~ noble with respect to the zirconium matrix. Because the alloy constituents are sparingly soluble, little solid solution strengthening of the zirconium occurs. The strengthening effect is sufficiently low to maintain the softness required 7;~j
Z IRCONIUM ALLOY BARRIER HAVING
.
IMPROVED CORROSION RESISTANCE
EIELD OF TXE INVENTION
This invention relates broadly to an improvement in nuclear fuel elements for use in the core of nuclear fission reactors and, more particularly, to an improved nuclear fuel element having a composite cladding container having a metal liner of dilute zirconium alloy consisting of zirconium and a metal selected from the group consisting of iron, chromium, iron plus chromiuml and copper bonded to the inside surface of the zirconium alloy cladding substrate.
~ACKGROUND OF T~IE INVENTION
Nuclear reactors are presently being designed, constructed, and operated in which the nuclear fuel is contained in fuel elements which can have various geometric shapes, such as plates, tubes, or rods.
The fuel material is usually enclosed in a corroslon-resistant, non-reactive, heat conductive container or cladding. The fuel elements are assembled together in a lattice at fixed distances from each other in a coolant flow channel or region forming a fuel assembly, and sufficient fuel assemblies are combined to orm the nuclear fission chain reacting assembly or reactor core capabIe of a sel-f-sustained fission reaction.
The corel in turn, is enclosed within a reactor vessel through which a coolant ls passed.
~ ;
~J ~'2~i The cladding serves several purposes and two primary purposes are: first, to prevent contact and chemical reactions between the nuelear fuel and the coolant or the moderator if a moderator is present, or both if both the coolant and the moderator are present; and second, to prevent the radioactive fission products, some o:E which are gases, from being released from the fuel into the coolant or the moderator or both if both the coolant and the moderator are present. Common cladding materials are stainless steel, aluminum and its alloys~ zirconium and its alloys~ niobium (columbium), certain magnesium alloys, and others. The failure of the cladding, i.e.~ a loss of the leak tightness~ can contaminate the coolant or moderator and the associated systems with long-lived radioactive products to a degree which interferes with plant operation.
Problems have been encountered in the manufacture and in the operation of nuclear fuel elements which employ certain metals and alloys as the cladding material due to mechanical or chemical reactions of these cladding materials under certain circumstances.
Zirconium and its alloys, under normal circumstances, make excellent nuclear fuel claddings since they have low neutron absorption cross-sections and at temperatures below about 750 F (about 398 C) are strong, ductile, extremely stable and relatively non-reactive in the presence of demineralized water or steam which are commonly used as reactor coolants and moderators.
However, fuel element performance has revealed a problem with the brittle splitting of the cladding due to the eombined interactions between the nuelear fuel, the cladding and the fission products produced during nuclear fission reac-tions. It has been discovered that this undesirable performance is promoted by localized mechanical stress due to differential expansion of fuel and cladding (stresses ~9~
24--NT-044 ~1 in the cladding are concentrated at cracks in the nuclear fuel). Corrosive fission products are released from the nuclear fuel and are present at the intersection of the fuel cracks with the cladding surface. Such fission products are created in the nuclear fuel during the fission chain reaction during operation of a nuclear reactor. The localized stress is exaggerated ~y high friction between the fuel and the cladding.
Within the confines of a sealed fuel element, hydrogen gas can be generated by the slow reaction between the cladding and residual water inside the cladding. This hydrogen gas may build up to levels which, under certain conditions; can result in localized hydriding of the cladding with concurrent local deterioration in the mechanical properties of the cladding. The cladding is also adversely affected by such gases as oxygen, nitrogen, carbon monoxide, and carbon dioxide over a wide range of temperatures.
The zirconium cladding of a nuclear fuel element is exposed to one or more of the gases listed above and fission products during irradiation in a nuclear reactor and this occurs in spite of the fact that these gases may not be present in the reactor coolant or moderator, and further may have been excluded as far as possible from the ambient atmosphere during manufacture of the cladding and the fuel element.
Sintered refractory and ceramic compositions, such as uranium dioxide and other compositions used as nuclear fuel, release measurable quantities of the aforementioned gases upon heatingl such as during fuel element manufacture and urther release ~ission products during irradiation. Particulate refractory and ceramic compositions~ such as uranium dioxide powder and other powders used as nuclear fuel, have been known to reIease even larger quantities of the a-forementioned gases during irradiation. These ~2~
- 4 - 24-NF-044~1 released gases are capable of reacting with the zirconium cladding containing the nuclear fuel.
Thus, in light of the foregoing, it has been found desirable to minimize attack of the cladding from water, water vapor and other gases, especially hydrogen, which are reactive with the cladding from inside the fuel element throughout the time the fuel element is used in the operation of nuclear power plants. One such approach has been to find materials which will chemically react rapidly with the water, water vapor and other gases to eliminate these from the interior of the cladding. Such materials are called getters.
Another approach has been to coat the nuclear fuel material with any of a variety of materials to prevent moisture coming in contact with the nuclear fuel material.
The coating of nuclear fuel material introduces reliability problems in that achieving uniform coatings free of faults is difficult. Further, the deterioration of the coating can introduce problems with the long-lived performance of the nuclear fuel material.
General Electric Atomic Power Document 4555 of February 1964, at GE NEBO Library, 175 Curtner Ave., San Jose, Calif. 95125, discloses a composite cladding of a zirconium alloy with an inner lining of stainless steel metallurgically bonded to the zirconium alloy, and the composite cladding is fabricated by extrusion of a hollow billet of the zirconium alloy having an inner lining of stainless steel. This cladding has the disadvantage that the stainless steel develops brittle phases, and the stainless steel layer involves a neutron absorption penalty of about -ten to fifteen times the penalty for a zirconium alloy of the same thickness.
U~S. Patent No. 3,502,5~9, issued March 24, 1970 to Charveriat, discloses a method for protecting zirconium and its alloys by the electrolytic deposition of chromium to provide a composite material useful for nuclear reactors. A method for electrolytic ~2~97~ 24-NT-0~481 deposition of copper on Zircaloy-2 surfaces and subsequent heat treatment for the purpose of obtaining surface diffusion of the electrolytically deposited metal is presented in Energia Nuclearer ~olume 11~
No. 9 ~September, 1964) at pages 505-508. In Stability and Compatibility of Hydrogen Barriers Applied to zirconium Alloys, by F. Brossa et al (~uropean Atomic Energy Community, Joint Nuclear Research Center, EUR 4098e~ 1969), methods of deposition of different coatings and their efficiency as hydrogen diffusion barriers are described along with an Al-Si coating as the most promising barrier against hydrogen diffusion.
Methods for electroplating nickel on zirconium and zirconium-tin alloys and heat treating these alloys to produce alloy-diffusion bonds are disclosed in Electroplating on Zirconium and Zirconium-Tln, by W.C. Schickner et al (BMI-757/ Technical Information Service, 1952~.
U.S. Patent No. 3,625,821, issued December 7l 1971 to Ricks, presents a fuel element for a nuclear reactor having a fuel cladding tube with the inner surface of the tube being coated with a metal of low neutron capture cross-section such as nickel and having finely dispersed particles of a burnable poison disposed therein. Reactor Development Program - ~ of August, 1973 (ANL-RDP-l9) discloses a chemical getter arrangement of a sacrificial layer of chromium on the inner surface of a stainless steel cladding.
Another approach has been to introduce a barrie~ between the nuclear fuel material and the cladding holding the nuclear fuel material as disclosed in U.S. Patent No. 3,230,150, issued ~anuary 18, 1966 to Martin et al (copper foil); German Patent Publication DAS lr238,115 (titanium layer); U.S. Patent No. 3,212,988, issued October 19, 1965 to Ringot et al (sheath of ~2~Z~
zirconium, aluminum, aluminum or beryllium); U.S. Patent No. 3,018,238, issued January ?3~ 1962 to Layer et al (barrier of crystalline carbon between the U02 and the zirconium alloy cladding); and U.S. Patent No. 3,088,893, issued May 7, 1963 to Spalaris, (stainless steel foil).
While the barrier concept proves promising, some of the foregoing references involve incompatible ma-terials with either the nuclear fuel (e.g., carbon can combine with oxygen from the nuclear fuel), or the cladding (e.g., copper and other metals can react with the cladding, altering the properties of the cladding), or the nuclear fission reaction (e.g., by acting as neutron absorbers). None of the listed references disclose solutions to the problem of localized chemical-mechanical interactions between the nuclear fuel andthe cladding.
Further approaches to the barrier concept are disclosed in U~S. Patent No. 3,969,186t issued July 13, 1976 to Thompson, (refractory metal such as molybdenum~ tungsten, rhenium, niobium and alloys thereof in the form of a tube or foil of single or multiple layers or a coa~ing on the internal surface of the cladding), and U.5. Patent No. 3,925,151, issued December 9, 1975 to Klepfer, (liner of zirconium, niobium~ or alloys thereof between the nuclear fuel and the cladding with a coating of a high lubricity material between liner and the cladding).
U.S. Patent No. 4rO45,288, issued August 30, 1977~ to Armijo, discloses a composite cladding of a zirconium alloy substrate with a metal barrier metallurgically bonded to the substrate and an inner layer of zirconium alloy metallurgically bonded to the metal barrier. The barrier i5 selected from a group of niobiumr aluminuml copper, nickel, stainless steel, and iron. The buried metal barrier reduces corrosion due to fission products and corrosive gases, but is subject to stress corrosion cracking , ~ ~ 24-NT-04~81 and liquid metal embrittlement.
U.S. Patent No. 4,200,492~ issued April 29, 1980, to Armijo, discloses a composite cladding of a zirconium alloy substrate with a sponge zirconium liner. The soft zirconium liner minimizes localized strain, and reduces stress corrosion cracking and liquid metal embrittlement, but is subject to loss due to honing and the like during fabrication and due to oxidation. Furthermore, if a breach in the cladding should occur, allowing water and/or steam to enter the fuel rod, the zirconium liner tends to oxidize rapidly.
Accordingly, it has remained desirable to develop nuclear fuel elements minimizing the problems discussed above.
SU~ARY OF THE INVENTION
A particularly effective nuclear fuel elemen-t for use in -the core of a nuclear reactor has a composite cladding having a metal liner of dilute zirconium alloy metallurgically bonded to the inside surface of the substrate. The dilute zirconium alloy comprises zirconium and a metal selected from the group consisting of iron, chromium, iron plus chromium and copper, wherein the amount of iron alloyed with the zirconium is from about 0.2% to about 0.3% by weight, the amount of chromium is from about 0.05% to about 0.3% by weight; the total amount of iron plus chromium is from about 0.15% to about 0.3% by weight and wherein the ratio of the weights of iron to chromium is in the range of from about 1:1 to about 4:1; and wherein the amount of copper is from about 0.002% to about 0.2% by weight.
The substrate of the cladding is completely unchanged in design and function from previous practice for a nuclear reactor and is selected from conventional cladding materials such as zirconium alloys. A
zirconium alloy cladding substrate has a higher alloy content than the dilute zirconium alloy liner. The ~ 7~ 24-NT-04481 dilute zirconium alloy liner forms a continuous shield between the substrate and the nuclear fuel material held in the cladding, as well as shielding -the zirconium alloy or other substrate cladding from fission products and gases.
The dilute zirconium alloy liner forms from about 1 to about 20 percent of the thickness of the cladding. The liner remains soft, relative to the substrate, during irradiation and minimizes localized stress inside the nuclear fuel element, thus serving to protect the cladding from stress corrosion cracking or liquid metal embrittlement. The dilute zirconium alloy liner shields the substrate from reaction with volatile impurities or fission products present inside the nuclear fuel element and, in this mannerJ serves to protect the cladding substrate from attack by the volatile impurities or fission products~
This invention has a striking advantage that the substrate of the cladding is protected from stress corrosion cracking and liquid metal embrittlement, in addition to contact with fission products, corrosive gases, etc., by the dilute zirconium alloy liner and the liner does not introduce any appreciable neutron capture penalties~ heat transfer penalties, or fuel/
liner incompatibility problems. In addition, the liner provides superior resistance to steam or hot water oxidation as compared to unalloyed zirconium in the event of a breach in the cladding.
DESCRIPTION OF THE DRA~INGS
The foregoing and other objects of this invention will become apparent to persons skilled in the art from reading the following specification and the appended claims with reference to the accompanying drawings described hereinafter.
FIG. 1 is a partial cutaway sectional view of a nuclear fuel assembly containing nuclear fuel . .
37;~6 24-NT-04481 g elements constructed according to the teaching of this invention; and FIG. 2 is an enlarged transverse cross-sectional view of the nuclear fuel element in FIG. 2 illustrating the teaching of this invention.
DESCRIPTION OF THE INVENTION
Referring now more particularly to FIG. 1, there is shown a partially cutaway sectional view of a nuclear fuel assembly 10. This fuel assembly 10 consists of a tubular flow channel 11 of generally square cross section provided at its upper end with a lifting bail 12 and at its lower end with a nose piece (not shown due to the lower portion of assembly 10 being omitted). The upper end of channel 11 is open at outlet 13 and the lower end of the nose piece is provided with coolant flow openings. An array of fuel elements or rods 14 is enclosed in the channel 11 and suppor-ted -therein by means of an upper end plate 15 and a lower end plate (not shown due to the lower portion being omitted). The liquid coolant ordinarily enters through the openings in the lower end of the nose piece, passes upwardly around fuel elements 14, and discharges through -the upper outlet 13 at an elevated temperature in a partially vaporized condition for boiling reactors or in an unvaporized condition for pressurized reactors.
The nuclear fuel elements or rods 14 are sealed at their ends by means of end plugs 18 welded to the cladding 17, which may include studs 19 to facilitate the mounting of the fuel rod in the assembly.
A void space or plenum 20 is provided at one end of the element to permit longitudinal expansion of the fuel material and accumulation of gases released from the fuel material~ ~ nuclear fuel material retainer means 24 in the form of a helical member is positioned within space 20 to provide restraint against the axial movement of the pellet column, especially during handling and transportation of the fuel element.
7;~
The fuel element is designed to provide an excellent thermal contact between the cladding and the fuel material, a minimum of parasitic neutron absorption and resistance to bowing and vibration which is occasionally caused by flow of the coolant at high velocity.
A nuclear fuel element or rod 14 constructed according to the teachings of this invention is shown in a partial section in FIG~ 1. The fuel element includes a core or central cylindrical portion of nuclear fuel material 16, here shown as a plurality of fuel pellets of fissionable and/or fertile material positioned within a structural cladding or container 17. In some cases, the fuel pellets may be of various shapes such as cylindrical pellets or spheres and, in other cases, different fuel forms such as a particulate fuel may be used. The physical form of the fuel is immaterial to this invention.
Various nuclear fuel materials may be used including uranium compounds, plutonium compounds, thorium compounds, and mixtures thereo. A preferred fuel is uranium dioxide or a mixture comprising uranium dioxide and plutonium dioxide.
Referring now to FIG. 2, the nuclear fuel material 16 forming the central core of the fuel element 14 is surrounded by a cladding 17 which, in this invention, is also referred to as a composite cladding container.
The composite cladding container encloses the fissile core so as to leave a gap 23 be-tween the core and the cladding during use in a nuclear reactor. The composite cladding container has an external substrate 21 selected from conventional cladding materials such as a stainless steel and zirconium alloys and, in a preferred embodiment of this invention, the substrate is a zirconium alloy such as Zircaloy-2.
35The substrate 2I has metallurgically bonded on the inside circumference thereof a dilute zirconium 24-NT-0~81 alloy liner 22 so that the dilute zirconium alloy liner forms a shield of the substrate from the nuclear fuel material 16 inside the composite cladding The dilute zirconium alloy liner preferably forms about 1 to about 20% of the thickness of the cladding. A dilute zirconium alloy liner forming less than about 1% of the thickness of the cladding would be difficult to achieve in commercial production, and a dilute zirconium alloy liner forming more than 20% of the thickness of the cladding provides no additional benefit for the added thickness. Further, a liner more than about 20% of the thickness of the cladding means a concomitant reduction in thickness of the substrate and possible weakening of the cladding.
The dilute zirconium alloy is comprised of zirconium and an alloy addition selected from the group consisting of: iron, chromium, iron pIus chromium and copper. As used herein, dilute zirconium alloy means a zirconium alloy with an alloy content sufficiently low to display greater ductility and higher strain rate than does the substrate material under equivalent conditions of stress.
The amount of iron alloyed with zirconium is from about 0.2% to about 0.3% by weight, and preferably from about 0.2% to about 0.25% by weight.
Chromium is in the range of from about 0.05%
to about 0.3% by weight and preferably from about 0.15%
to about 0.25~ by weight.
Iron plus chomium may be included so that the total amount of both components is from about 0.15% to about 0.3% by weight and preferably from about 0.2% to about 0.25% by weight and wherein the ratio of the weights of iron to chromium is from about 1:1 to about ~:1 and preferably about 2:1.
Copper is used in the amount of from about 0.02% to about 0.2% by weight and preferably from about 0.05~ to about 0.15% by weight.
..
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` 24-NT-04481 The dilute zirconium alloy liner shields the substrate from gaseous impurities and fission products and protects the substrate portion of the cladding from contact and reaction with such impurities and fission products and prevents the occurrence of localized stress.
The addition to zirconium of small amounts of a metal selected from the group of iron, chromium, iron plus chromium and copper improves corrosion resistance, especially resistance to oxidation by hot water or steam if the addition is within the stated range for that metal. The lower limit of the amount of each metal alloyed with zirconium provides su~ficient quantity of that metal to signiEicantly improve the corrosion resistance as compared to unalloyed zirconium.
The upper limit of the amount of each metal alloyed with zirconium is generally set at the maximum amount of the metal which significantly improves the corrosion resistance as compared with sponge zirconium.
Additions of the metal exceeding the upper limit fail to significantly enhance the corrosion resistance properties of zirconium and may have a detrimental effect in reducing the softness and ductility of the liner.
The additions of each metal to zirconium that impart the greatest improvement in corrosion resistance are stated as the preferred ranges.
Iron, chromium and copper are sparingly soluble in zirconium. Dilute zirconium alloys involving one or more of these metals can be heat treated to provide a material with a fine dispersion of intermetallic particles which ar~ noble with respect to the zirconium matrix. Because the alloy constituents are sparingly soluble, little solid solution strengthening of the zirconium occurs. The strengthening effect is sufficiently low to maintain the softness required 7;~j
2~-NT-04~81 for the dilute zirconium alloy liner to preven-t or mitigate fuel failure by pellet-cladding interaction.
The dilute zirconium alloy liner in the composite cladding resists irradiation hardening relative to Zircoloy or other conventional zirconium alloys, and this enables the dilute zirconium alloy liner, after prolonged irradiation, to .naintain desirable structural properties such as yield strength and hardness at levels considerably lower than those of conventional zirconium alloys. In effect, the dilute zirconium alloy ]iner does not harden as much as conventional zirconium alloys when subjected to irradiation and this, thogether with its initially low yield strength, enables the dilute zirconium alloy liner to deform plastically and relieve pellet-induced stresses in the fuel element that can be broughtabout, for example, by swelling of the pellets of nuclear fuel a-t reactor operating -temperatures (300 C to 350C) so that the pellet comes into contact with the cladding.
A dilute zirconium alloy liner comprising zirconium and a metal selected from the group comprising iron, chromium, iron plus chromium, and copper and preferably about 5 to 15 percent of the thickness of the cladding bonded to a conventional z.irconium alloy substrate provides stress reduction sufficient to prevent or mitigate failures in the composite claddiny.
The purity of the zirconium metal that is alloyed with iron, chromium, iron plus chromium or copper is important and serves to impart special properties to the dilute zirconium alloy liner.
Generally, there is less than 5000 ppm impurities in the zirconium metal. Of these oxygen should be as low as practical but may vary up to about 1000 ppm ~, 7Z~i ~14-The composite cladding of the nuclear fuel element of this invention has a dilute zirconium alloy liner metallurgically bonded to the substrate.
Metallographic examination shows that there is sufficient cross-diffusion between the substrate and the dilute zirconium alloy liner to form metallurgical bonds, but insufficient cross-diffusion to alloy siynificantly with the dilute zirconium alloy liner itself.
Among the conventional zirconium alloys serviny as suitable substrates are Zircaloy-2 and Zircaloy-4.
Zircaloy-2 has on a weight basis about 1.5 percent tin; 0.12 percent iron; 0.09 percent chromium and 0.005 percent nickel and is extensively employed in water-cooled reactors. Zircaloy-4 has less nickel than Zircaloy-2, but contains slightly more iron than Zircaloy-2. The composite cladding used in the nuclear fuel elements of this invention can be fabricated by any of the following methods~
In one method, a tube of the dilute zirconium alloy liner material is inserted into a hollow billet of the material selected to be the substrate, and then the assembly is subjected to explGsive bonding of the tube to the billet. The composite is extruded using conventional tube shell extrusion at elevated temperatures of about 1000 F to 1400 F ~about 538 C
to 760C~. Then the extruded composite is subjected to a process involving conventional tube reduction until the desired size o~ cladding is achieved. The relative wall thickness of the hollow billet and the dilute zirconium alloy liner tube are selected to give the desired thickness ratios in the finished cladding tube.
In another method, a tube of the dilute zirconium alloy liner material is inserted into a hollow billet of the material selected to be the substrate, and , ~2~ 6 2~-NT-04~81 The present invention offers several advantages promoting a long operating life for a nuclear fuel element, lncluding the reduction of chemical interaction of the cladding, the minimization of localized stress on the zirconium alloy substrate portion of the cladding, the minimization of stress corroslon on the zirconium alloy substrate portion of the cladding, and the reduction o~ the probability of a splitting failure occurring in the zirconium alloy substrate.
l~ In addition to minimizing stress and stress corrosion on the substrate~ the dilute ~irconium alloy liner is resistant to oxidation by steam and hot water in the event that the cladding is breached, whereas unalloyed zirconium oxidizes rapidly under -these conditions. The dilute zirconium alloy exhibi-ts plasticity similar to unalloyed zirconium and provides the benefits thereof while also providing increased resistance to corrosion~ especially to oxidation by hot water and steam.
2~ An important property of the composite cladding of this invention is that the foregoing improvements are achieved with no substantial additional neutron penalty. Such a cladding is readily accepted in nuclear reactors since the cladding would have no eutectic formation during a loss-of-coolant accident or an accident involving the dropping of a nuclear control rod. Further, the composite cladding has a very small heat transfer penalty in that there is no thermal barrier to transfer of heat such as results in the situation where a separate foil or liner is inser-ted in a fuel element. Also, the composite cladding of this invention is inspectable by conventional non-destructive testing methods during various stage of fabrication and operation.
~s will be apparent to those skilled in the art, various modifications and changes may be made in the ' ;
12~972~ 24-NT-04481 invention described herei.n. It is accordingly the intenti~n that the invention be construed in the broadestmanner within the spirit and scope as set forth in the accompanying claims.
~2~72~ 2~-NT-04481 invention described herein. It is accordingly the intention that the invention be construed in the broadest manner within the spirit and scope as set forth in the accompanying claims.
The dilute zirconium alloy liner in the composite cladding resists irradiation hardening relative to Zircoloy or other conventional zirconium alloys, and this enables the dilute zirconium alloy liner, after prolonged irradiation, to .naintain desirable structural properties such as yield strength and hardness at levels considerably lower than those of conventional zirconium alloys. In effect, the dilute zirconium alloy ]iner does not harden as much as conventional zirconium alloys when subjected to irradiation and this, thogether with its initially low yield strength, enables the dilute zirconium alloy liner to deform plastically and relieve pellet-induced stresses in the fuel element that can be broughtabout, for example, by swelling of the pellets of nuclear fuel a-t reactor operating -temperatures (300 C to 350C) so that the pellet comes into contact with the cladding.
A dilute zirconium alloy liner comprising zirconium and a metal selected from the group comprising iron, chromium, iron plus chromium, and copper and preferably about 5 to 15 percent of the thickness of the cladding bonded to a conventional z.irconium alloy substrate provides stress reduction sufficient to prevent or mitigate failures in the composite claddiny.
The purity of the zirconium metal that is alloyed with iron, chromium, iron plus chromium or copper is important and serves to impart special properties to the dilute zirconium alloy liner.
Generally, there is less than 5000 ppm impurities in the zirconium metal. Of these oxygen should be as low as practical but may vary up to about 1000 ppm ~, 7Z~i ~14-The composite cladding of the nuclear fuel element of this invention has a dilute zirconium alloy liner metallurgically bonded to the substrate.
Metallographic examination shows that there is sufficient cross-diffusion between the substrate and the dilute zirconium alloy liner to form metallurgical bonds, but insufficient cross-diffusion to alloy siynificantly with the dilute zirconium alloy liner itself.
Among the conventional zirconium alloys serviny as suitable substrates are Zircaloy-2 and Zircaloy-4.
Zircaloy-2 has on a weight basis about 1.5 percent tin; 0.12 percent iron; 0.09 percent chromium and 0.005 percent nickel and is extensively employed in water-cooled reactors. Zircaloy-4 has less nickel than Zircaloy-2, but contains slightly more iron than Zircaloy-2. The composite cladding used in the nuclear fuel elements of this invention can be fabricated by any of the following methods~
In one method, a tube of the dilute zirconium alloy liner material is inserted into a hollow billet of the material selected to be the substrate, and then the assembly is subjected to explGsive bonding of the tube to the billet. The composite is extruded using conventional tube shell extrusion at elevated temperatures of about 1000 F to 1400 F ~about 538 C
to 760C~. Then the extruded composite is subjected to a process involving conventional tube reduction until the desired size o~ cladding is achieved. The relative wall thickness of the hollow billet and the dilute zirconium alloy liner tube are selected to give the desired thickness ratios in the finished cladding tube.
In another method, a tube of the dilute zirconium alloy liner material is inserted into a hollow billet of the material selected to be the substrate, and , ~2~ 6 2~-NT-04~81 The present invention offers several advantages promoting a long operating life for a nuclear fuel element, lncluding the reduction of chemical interaction of the cladding, the minimization of localized stress on the zirconium alloy substrate portion of the cladding, the minimization of stress corroslon on the zirconium alloy substrate portion of the cladding, and the reduction o~ the probability of a splitting failure occurring in the zirconium alloy substrate.
l~ In addition to minimizing stress and stress corrosion on the substrate~ the dilute ~irconium alloy liner is resistant to oxidation by steam and hot water in the event that the cladding is breached, whereas unalloyed zirconium oxidizes rapidly under -these conditions. The dilute zirconium alloy exhibi-ts plasticity similar to unalloyed zirconium and provides the benefits thereof while also providing increased resistance to corrosion~ especially to oxidation by hot water and steam.
2~ An important property of the composite cladding of this invention is that the foregoing improvements are achieved with no substantial additional neutron penalty. Such a cladding is readily accepted in nuclear reactors since the cladding would have no eutectic formation during a loss-of-coolant accident or an accident involving the dropping of a nuclear control rod. Further, the composite cladding has a very small heat transfer penalty in that there is no thermal barrier to transfer of heat such as results in the situation where a separate foil or liner is inser-ted in a fuel element. Also, the composite cladding of this invention is inspectable by conventional non-destructive testing methods during various stage of fabrication and operation.
~s will be apparent to those skilled in the art, various modifications and changes may be made in the ' ;
12~972~ 24-NT-04481 invention described herei.n. It is accordingly the intenti~n that the invention be construed in the broadestmanner within the spirit and scope as set forth in the accompanying claims.
~2~72~ 2~-NT-04481 invention described herein. It is accordingly the intention that the invention be construed in the broadest manner within the spirit and scope as set forth in the accompanying claims.
Claims (51)
1. A nuclear fuel element comprising:
a central core of a body of nuclear fuel material selected from the group consisting of compounds or uranium, plutonium, thorium, and mixtures thereof; and an elongated composite cladding container enclosing said core including an outer portion forming a substrate, and a dilute zirconium alloy liner formed of zircinoum and a metal selected from the group consisting of iron, chromium, iron plus chromium, and copper metallurgically bonded on the inside surface of the substrate, said ilute zirconium alloy liner comprising from about 1 to about 20 percent of the thickness of the composite cladding container, the concentra-tion of said selected metal being greater than: 0.015 percent iron; 0.002 percent chromium or 0.0005 percent copper, by weight, of said liner alloy.
a central core of a body of nuclear fuel material selected from the group consisting of compounds or uranium, plutonium, thorium, and mixtures thereof; and an elongated composite cladding container enclosing said core including an outer portion forming a substrate, and a dilute zirconium alloy liner formed of zircinoum and a metal selected from the group consisting of iron, chromium, iron plus chromium, and copper metallurgically bonded on the inside surface of the substrate, said ilute zirconium alloy liner comprising from about 1 to about 20 percent of the thickness of the composite cladding container, the concentra-tion of said selected metal being greater than: 0.015 percent iron; 0.002 percent chromium or 0.0005 percent copper, by weight, of said liner alloy.
2. The nuclear fuel element of claim 1 in which the dilute zirconium alloy liner comprises from about 0.2%
to about 0.3% by weight iron, the balance being zirconium.
to about 0.3% by weight iron, the balance being zirconium.
3. The nuclear fuel element of claim 1 in which the dilute zirconium alloy liner comprises from about 0.2%
to about 0.25% by weight iron, the balance being zirconium.
to about 0.25% by weight iron, the balance being zirconium.
4. A nuclear fuel element of claim 1 in which the dilute zirconium alloy liner comprises from about 0.05%
to about 0.3% by weight chromium, the balance being zirconium.
to about 0.3% by weight chromium, the balance being zirconium.
5. A nuclear fuel element of claim 1 in which the dilute zirconium alloy liner comprises from about 0.15% to about 0.25% by weight chromium, the balance being zirconium.
6. A nuclear fuel element of claim 1 in which the dilute zirconium alloy liner comprises iron and chromium wherein the total amount of iron plus chromium is from about 0.15% to about 0.3% by weight, the balance being zirconium and wherein the weight ratio of iron to chromium is from about 1:1 to about 4:1.
7. A nuclear fuel element of claim 6 wherein the weight ratio of iron to chromium is about 2:1.
8. A nuclear fuel element of claim 1 in which the dilute zirconium alloy liner comprises iron and chromium wherein the total amount of iron plus chromium is from about 0.2% to about 0.25% by weight, the balance being zirconium and wherein the weight ratio of iron to chromium is from about 1:1 to about 4:1.
9. A nuclear fuel element of claim 8 wherein the weight ratio of iron to chromium is about 2:1.
10. The nuclear fuel element of claim 1 in which the dilute zirconium alloy liner comprises about 0.02% to about 0.2% by weight copper, the balance being zirconium.
11. The nuclear fuel element of claim 1 in which the dilute zirconium alloy liner comprises about 0.05% to about 0.15% by weight copper, the balance being zirconium.
12. The nuclear fuel element of claim 1 in which the dilute zirconium alloy liner comprises from about 5 to about 15 percent of the thickness of the composite cladding container.
13. A composite cladding container for nuclear reactors comprising a zirconium alloy outer portion forming a substrate and a dilute zirconium alloy liner formed of zirconium and a metal selected from the group consisting of iron, chromium, iron plus chromium, and copper metallurgically bonded on the inside surface of the substrate, said zirconium alloy liner comprising from about 5 to about 15 percent of thickness of the composite cladding container, the concentration of said selected metal being greater than:
0.015 percent iron, 0.002 percent chromium or 0.0005 percent copper, by weight, of said liner alloy.
0.015 percent iron, 0.002 percent chromium or 0.0005 percent copper, by weight, of said liner alloy.
14. A composite cladding container as claimed in Claim 13 in which the dilute zirconium alloy liner comprises from about 0.02% to about 0.3% by weight iron, the balance being zirconium.
15. A composite cladding container as claimed in Claim 13 in which the dilute zirconium alloy liner comprises from about 0.2% to about 0.25% by weight iron, the balance being zirconium.
16. A composite cladding container as claimed in Claim 13 in which the dilute zirconium alloy liner comprises from about 0.05% to about 0.3% by weight chromium, the balance being zirconium.
17. A composite cladding container as claimed in Claim 13 in which the dilute zirconium alloy liner comprises from about 0.15% to about 0.25% by weight chromium, the balance being zirconium.
18. A composite cladding container as claimed in Claim 13 in which the dilute zirconium alloy liner comprises iron and chromium wherein the total amount of iron plus chromium is from about 0.15% to about 0.3% by weight, the balance being zirconium and wherein the weight ratio of iron to chromium is from about 1:1 to about 4:1.
19. A composite cladding container as claimed in Claim 13 in which the dilute zirconium alloy liner comprises iron and chromium wherein the total amount of iron plus chromium is from about 0.2% to about 0.25% by weight, the balance being zirconium and wherein the weight ratio of iron to chromium is from about 1:1 to about 4:1.
20. A composite cladding container as claimed in Claim 13 in which the dilute zirconium alloy liner comprises about 0.02% to about 0.2% by weight copper, the balance being zirconium.
21. A composite cladding container as claimed in Claim 13 in which the dilute zirconium alloy liner comprises about 0.05% to about 0.15% by weight copper, the balance being zirconium.
22. A hollow composite cladding container comprising an outer portion formed of a zirconium alloy forming a substrate and a continuous dilute zirconium alloy liner formed of zirconium and a metal selected from the group consisting of iron, in the range of from about 0.2% to about 0.3% by weight; chromium in the range of from about 0.05% to about 0.3% by weight;
iron plus chromium in the range of from about 0.15% to about 0.3% by weight wherein the weight ratio of iron to chromium is from about 1:1 to about 4:1; and copper in the range of from about 0.02% to about 0.2% by weight.
iron plus chromium in the range of from about 0.15% to about 0.3% by weight wherein the weight ratio of iron to chromium is from about 1:1 to about 4:1; and copper in the range of from about 0.02% to about 0.2% by weight.
23. A composite cladding container as claimed in Claim 22 in which the dilute zirconium alloy liner comprises from about 0.2% to about 0.25% by weight iron, the balance being zirconium.
24. A composite cladding container as claimed in Claim 22 in which the dilute zirconium alloy liner comprises from about 0.15% to about 0.25% by weight chromium, the balance being zirconium.
25. A composite cladding container as claimed in Claim 22 in which the dilute zirconium alloy liner comprises iron and chromium wherein the total amount of iron plus chromium is from about 0.2% to about 0.25%
by weight, the balance being zirconium.
by weight, the balance being zirconium.
26. A composite cladding container as claimed in Claim 22 in which the dilute zirconium alloy liner comprises about 0.05% to about 0.15% by weight copper, the balance being zirconium.
27. A composite cladding container as claimed in Claim 22 in which the dilute zirconium alloy liner comprises from about 1 to about 20 percent of the thickness of the composite cladding container.
28. A composite cladding container as claimed in Claim 22 in which the dilute zirconium alloy liner comprises from about 5 to 15 percent of the thickness of the composite cladding container.
29. In a hollow composite cladding container for nuclear fuel for use in a nuclear reactor comprising an outer substrate of zirconium alloy and an inner liner metallurgically bonded to the zirconium alloy substrate, the improvement comprising forming the liner of a dilute zirconium alloy consisting essentially of zirconium and a metal selected from the group consisting of iron, chromium, iron plus chromium, and copper, the concentration of said selected metal being greater than: 0.015 percent iron, 0.002 percent chromium, or 0.0005 percent copper, by weight, of said dilute zirconium alloy.
30. A composite cladding container as claimed in claim 29 in which the dilute zirconium alloy liner comprises from about 0.2% to about 0.3% by weight iron, the balance being zirconium.
31. A composite cladding container as claimed in claim 29 in which the dilute zirconium alloy liner comprises from about 0.2% to about 0.25% by weight iron, the balance being zirconium.
32. A composite cladding container as claimed in claim 29 in which the dilute zirconium alloy liner comprises from about 0.05% to about 0.3% by weight chromium, the balance being zirconium.
33. A composite cladding container as claimed in claim 29 in which the dilute zirconium alloy liner comprises from about 0.15% to about 0.25% by weight chromium, the balance being zirconium.
34. A composite cladding container as claimed in claim 29 wherein the dilute zirconium alloy liner comprises iron and chromium wherein the total amount of iron plus chromium is from about 0.15% to about 0.3% by weight, the balance being zirconium and wherein the weight ratio of iron to chromium is from about 1:1 to about 4:1.
35. A composite cladding container as claimed in claim 29 wherein the dilute zirconium alloy liner comprises iron and chromium wherein the total amount or iron plus chromium is from about 0.2% to about 0.25% by weight, the balance being zirconium and wherein the weight ratio of iron to chromium is from about 1:1 to about 4:1.
36. A composite cladding container as claimed in claim 29 in which the dilute zirconium alloy liner comprises from about 0.02% to about 0.2% by weight copper, the balance being zirconium.
37. A composite cladding container as claimed in claim 29 in which the dilute zirconium alloy liner comprises from about 0.05% to about 0.15% by weight copper, the balance being zirconium.
38. A composite cladding container as recited in claim 29 wherein the dilute zirconium alloy liner has a thickness in the range of from about 1 to about 20 percent of the thickness of the composite cladding container.
39. A composite cladding container as claimed in claim 29 wherein the dilute zirconium alloy liner has a thickness in the range of from about 5 to about 15 percent of the thickness of the composite cladding container.
40. A nuclear fuel element comprising:
a central core of a body of nuclear fuel material selected from the group consisting of compounds of uranium, plutonium, thorium, and mixtures thereof, and an elongated composite cladding container enclosing said core including an outer portion of zirconium alloy forming a substrate, and a zirconium alloy liner having a lower alloy content than the substrate formed of zirconium and a metal selected from the group consisting of iron, chromium, iron plus chromium, and copper metallurgically bonded on the inside surface of the substrate, said zirconium alloy liner comprising from about 1 to about 20 percent of the thickness of the composite cladding container, the concentration of said selected metal being greater than: 0.015 percent iron, 0.002 percent chromium or 0.005 percent copper, by weight, of said liner alloy.
a central core of a body of nuclear fuel material selected from the group consisting of compounds of uranium, plutonium, thorium, and mixtures thereof, and an elongated composite cladding container enclosing said core including an outer portion of zirconium alloy forming a substrate, and a zirconium alloy liner having a lower alloy content than the substrate formed of zirconium and a metal selected from the group consisting of iron, chromium, iron plus chromium, and copper metallurgically bonded on the inside surface of the substrate, said zirconium alloy liner comprising from about 1 to about 20 percent of the thickness of the composite cladding container, the concentration of said selected metal being greater than: 0.015 percent iron, 0.002 percent chromium or 0.005 percent copper, by weight, of said liner alloy.
41. The nuclear fuel element of Claim 40 in which the zirconium alloy liner comprises from about 0.2% to about 0.3% by weight iron, the balance being zirconium.
42. The nuclear fuel element of Claim 40 in which the zirconium alloy liner comprises from about 0.2% by about 0.25% by weight iron, the balance being zirconium.
43. A nuclear fuel element of Claim 40 in which the zirconium alloy liner comprises from about 0.05% to about 0.3%° by weight chromium, the balance being zirconium.
44. A nuclear fuel element of Claim 40 in which the zirconium alloy liner comprises from about 0.15% to about 0.25% by weight chromium, the balance being zirconium
45. A nuclear fuel element of Claim 40 in which the zirconium alloy liner comprises iron and chromium wherein the total amount of iron plus chromium is from about 0.15% to about 0.3% by weight, the balance being zirconium and wherein the weight ratio of iron to chromium is from about 1:1 to about 4:1.
46. A nuclear fuel element of Claim 45 wherein the weight ratio of iron to chromium is about 2:1.
47. A nuclear fuel element of Claim 1 in which the zirconium alloy liner comprises iron and chromium wherein the total amount of iron plus chromium is from about 0.2% to about 0.25% by weight, the balance being zirconium and wherein the weight ratio of iron to chromium is from about 1:1 to about 4:1.
48. A nuclear fuel element of claim 47 wherein the weight ratio of iron to chromium is about 2:1.
49. The nuclear fuel element of claim 40 in which the zirconium alloy liner comprises from about 0.02% to about 0.2% by weight copper, the balance being zirconium.
50. The nuclear fuel element of claim 40 in which the zirconium alloy liner comprises about 0.05%
to about 0.15% by weight copper, the balance being zirconium.
to about 0.15% by weight copper, the balance being zirconium.
51. The nuclear fuel element of claim 40 in which the zirconium alloy liner comprises from about 5 to about 15 percent of the thickness of the composite cladding container.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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US37405282A | 1982-05-03 | 1982-05-03 | |
US374,052 | 1982-05-03 |
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CA1209726A true CA1209726A (en) | 1986-08-12 |
Family
ID=23475064
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CA000427055A Expired CA1209726A (en) | 1982-05-03 | 1983-04-29 | Zirconium alloy barrier having improved corrosion resistance |
Country Status (10)
Country | Link |
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JP (1) | JPS58199836A (en) |
KR (1) | KR910003286B1 (en) |
BE (1) | BE895526A (en) |
CA (1) | CA1209726A (en) |
DE (1) | DE3248235A1 (en) |
ES (1) | ES8506926A1 (en) |
FR (1) | FR2526213B1 (en) |
GB (1) | GB2119559B (en) |
IT (1) | IT1153911B (en) |
SE (1) | SE459101B (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3571096D1 (en) * | 1984-03-09 | 1989-07-20 | Nippon Nuclear Fuel Dev Co | Cladding tube for nuclear fuel and nuclear fuel element having this cladding tube |
US4664881A (en) * | 1984-03-14 | 1987-05-12 | Westinghouse Electric Corp. | Zirconium base fuel cladding resistant to PCI crack propagation |
US4675153A (en) * | 1984-03-14 | 1987-06-23 | Westinghouse Electric Corp. | Zirconium alloy fuel cladding resistant to PCI crack propagation |
JPS6224182A (en) * | 1985-03-08 | 1987-02-02 | ウエスチングハウス・エレクトリック・コ−ポレ−ション | Nuclear fuel coated tube |
US4933136A (en) * | 1985-03-08 | 1990-06-12 | Westinghouse Electric Corp. | Water reactor fuel cladding |
CN86101123A (en) * | 1985-03-08 | 1987-01-21 | 西屋电气公司 | Vessel of water reactor fuel |
US4775508A (en) * | 1985-03-08 | 1988-10-04 | Westinghouse Electric Corp. | Zirconium alloy fuel cladding resistant to PCI crack propagation |
JPS61217793A (en) * | 1985-03-08 | 1986-09-27 | ウエスチングハウス・エレクトリック・コ−ポレ−ション | Nuclear fuel coated tube |
US4894203A (en) * | 1988-02-05 | 1990-01-16 | General Electric Company | Nuclear fuel element having oxidation resistant cladding |
US6243433B1 (en) | 1999-05-14 | 2001-06-05 | General Electic Co. | Cladding for use in nuclear reactors having improved resistance to stress corrosion cracking and corrosion |
CA2666651C (en) * | 2006-10-16 | 2016-01-26 | Commissariat A L'energie Atomique - Cea | Erbium-containing zirconium alloy, method for preparing and shaping the same, and structural part containing said alloy |
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BE571786A (en) * | 1957-10-16 | |||
US3925151A (en) * | 1974-02-11 | 1975-12-09 | Gen Electric | Nuclear fuel element |
GB1507487A (en) * | 1974-06-24 | 1978-04-12 | Gen Electric | Nuclear fuel element |
US4045288A (en) * | 1974-11-11 | 1977-08-30 | General Electric Company | Nuclear fuel element |
GB1525717A (en) * | 1974-11-11 | 1978-09-20 | Gen Electric | Nuclear fuel elements |
FR2404898B2 (en) * | 1974-11-11 | 1986-05-02 | Gen Electric | COMPOSITE SHEATH FOR A NUCLEAR FUEL ELEMENT |
US4029545A (en) * | 1974-11-11 | 1977-06-14 | General Electric Company | Nuclear fuel elements having a composite cladding |
GB1569078A (en) * | 1977-09-30 | 1980-06-11 | Gen Electric | Nuclear fuel element |
CA1139023A (en) * | 1979-06-04 | 1983-01-04 | John H. Davies | Thermal-mechanical treatment of composite nuclear fuel element cladding |
-
1982
- 1982-12-21 IT IT24877/82A patent/IT1153911B/en active
- 1982-12-22 GB GB08236441A patent/GB2119559B/en not_active Expired
- 1982-12-28 DE DE19823248235 patent/DE3248235A1/en not_active Ceased
- 1982-12-28 FR FR8221912A patent/FR2526213B1/en not_active Expired
- 1982-12-28 JP JP57227826A patent/JPS58199836A/en active Pending
- 1982-12-29 ES ES518638A patent/ES8506926A1/en not_active Expired
- 1982-12-30 BE BE0/209838A patent/BE895526A/en not_active IP Right Cessation
- 1982-12-31 KR KR8205904A patent/KR910003286B1/en active
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1983
- 1983-01-03 SE SE8300016A patent/SE459101B/en not_active IP Right Cessation
- 1983-04-29 CA CA000427055A patent/CA1209726A/en not_active Expired
Also Published As
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IT8224877A0 (en) | 1982-12-21 |
ES518638A0 (en) | 1985-07-16 |
FR2526213A1 (en) | 1983-11-04 |
GB2119559B (en) | 1986-02-26 |
KR840003119A (en) | 1984-08-13 |
DE3248235A1 (en) | 1983-11-03 |
SE8300016L (en) | 1983-11-04 |
IT1153911B (en) | 1987-01-21 |
GB2119559A (en) | 1983-11-16 |
KR910003286B1 (en) | 1991-05-25 |
JPS58199836A (en) | 1983-11-21 |
SE459101B (en) | 1989-06-05 |
SE8300016D0 (en) | 1983-01-03 |
ES8506926A1 (en) | 1985-07-16 |
BE895526A (en) | 1983-06-30 |
IT8224877A1 (en) | 1984-06-21 |
FR2526213B1 (en) | 1986-10-31 |
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