US3502549A - Method for the protection of zirconium and zirconium-base alloys - Google Patents
Method for the protection of zirconium and zirconium-base alloys Download PDFInfo
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- US3502549A US3502549A US721935A US3502549DA US3502549A US 3502549 A US3502549 A US 3502549A US 721935 A US721935 A US 721935A US 3502549D A US3502549D A US 3502549DA US 3502549 A US3502549 A US 3502549A
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- zirconium
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- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 title description 24
- 229910052726 zirconium Inorganic materials 0.000 title description 24
- 229910045601 alloy Inorganic materials 0.000 title description 16
- 239000000956 alloy Substances 0.000 title description 16
- 238000000034 method Methods 0.000 title description 13
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical group [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 27
- 238000000576 coating method Methods 0.000 description 27
- 229910052804 chromium Inorganic materials 0.000 description 23
- 239000011651 chromium Substances 0.000 description 23
- 239000011248 coating agent Substances 0.000 description 21
- 239000003795 chemical substances by application Substances 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 238000000151 deposition Methods 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 239000010949 copper Substances 0.000 description 4
- 230000007547 defect Effects 0.000 description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 3
- 239000007864 aqueous solution Substances 0.000 description 3
- 229910052802 copper Inorganic materials 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- 238000005868 electrolysis reaction Methods 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000010791 quenching Methods 0.000 description 3
- 238000011282 treatment Methods 0.000 description 3
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- 229910019580 Cr Zr Inorganic materials 0.000 description 2
- 229910019817 Cr—Zr Inorganic materials 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 229910001257 Nb alloy Inorganic materials 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 239000002826 coolant Substances 0.000 description 2
- 230000008021 deposition Effects 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 229910000765 intermetallic Inorganic materials 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 2
- 238000007747 plating Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000000171 quenching effect Effects 0.000 description 2
- 238000007669 thermal treatment Methods 0.000 description 2
- 230000009466 transformation Effects 0.000 description 2
- 238000009489 vacuum treatment Methods 0.000 description 2
- 230000004584 weight gain Effects 0.000 description 2
- 235000019786 weight gain Nutrition 0.000 description 2
- 229910001928 zirconium oxide Inorganic materials 0.000 description 2
- YJTKZCDBKVTVBY-UHFFFAOYSA-N 1,3-Diphenylbenzene Chemical group C1=CC=CC=C1C1=CC=CC(C=2C=CC=CC=2)=C1 YJTKZCDBKVTVBY-UHFFFAOYSA-N 0.000 description 1
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical class [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- 241000136406 Comones Species 0.000 description 1
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- 229910020220 Pb—Sn Inorganic materials 0.000 description 1
- 229910001245 Sb alloy Inorganic materials 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 239000003570 air Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000010953 base metal Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- UBAZGMLMVVQSCD-UHFFFAOYSA-N carbon dioxide;molecular oxygen Chemical compound O=O.O=C=O UBAZGMLMVVQSCD-UHFFFAOYSA-N 0.000 description 1
- 229910002090 carbon oxide Inorganic materials 0.000 description 1
- 238000005253 cladding Methods 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- XTYUEDCPRIMJNG-UHFFFAOYSA-N copper zirconium Chemical compound [Cu].[Zr] XTYUEDCPRIMJNG-UHFFFAOYSA-N 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- ZXKXJHAOUFHNAS-UHFFFAOYSA-N fenfluramine hydrochloride Chemical compound [Cl-].CC[NH2+]C(C)CC1=CC=CC(C(F)(F)F)=C1 ZXKXJHAOUFHNAS-UHFFFAOYSA-N 0.000 description 1
- 230000004992 fission Effects 0.000 description 1
- 229910000743 fusible alloy Inorganic materials 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 150000001911 terphenyls Chemical class 0.000 description 1
- 230000008719 thickening Effects 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/34—Pretreatment of metallic surfaces to be electroplated
- C25D5/38—Pretreatment of metallic surfaces to be electroplated of refractory metals or nickel
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C11/00—Alloys based on lead
- C22C11/08—Alloys based on lead with antimony or bismuth as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C16/00—Alloys based on zirconium
-
- 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
- C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
- C22F1/18—High-melting or refractory metals or alloys based thereon
- C22F1/186—High-melting or refractory metals or alloys based thereon of zirconium or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23F—NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
- C23F15/00—Other methods of preventing corrosion or incrustation
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23F—NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
- C23F17/00—Multi-step processes for surface treatment of metallic material involving at least one process provided for in class C23 and at least one process covered by subclass C21D or C22F or class C25
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D3/00—Electroplating: Baths therefor
- C25D3/02—Electroplating: Baths therefor from solutions
- C25D3/04—Electroplating: Baths therefor from solutions of chromium
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D3/00—Electroplating: Baths therefor
- C25D3/02—Electroplating: Baths therefor from solutions
- C25D3/56—Electroplating: Baths therefor from solutions of alloys
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/48—After-treatment of electroplated surfaces
- C25D5/50—After-treatment of electroplated surfaces by heat-treatment
-
- G—PHYSICS
- G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
- G21C—NUCLEAR REACTORS
- G21C17/00—Monitoring; Testing ; Maintaining
- G21C17/06—Devices or arrangements for monitoring or testing fuel or fuel elements outside the reactor core, e.g. for burn-up, for contamination
-
- 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
Definitions
- My invention relates to the protection of zirconium and zirconium-base alloys [hereinafter generically called zirconium] against corrosion by external agents at high temperatures.
- zirconium and zirconium-base alloys and particularly those alloys used in nuclear reac tors as cladding materials or in the fabrication of pressure or calandria tubes, have limited applications due to thecorroding action of the coolants, generally, presurized water, carbon dioxide, terphenyl or steam. Furthermore, the fabrication and transformation of the same alloys are diflicult and costly because of the rapid corrosion in air at temperatures above 800 to 900 C.
- zirconium oxide film of 10W ductility is formed on the surface of zirconium. This film has a tendency to thicken and to eventually scale off. Simultaneously with the thickening and scaling off of the zirconium oxide film, oxygen penetrates into the subjacent metal and causes these areas to become brittle. This phenomena is even more pronounced as the temperature increases.
- chromium has shown the greatest advantages. Chromium oxidizes very slowly, is hard, and is resistant to abrasion. It has practically no diffusion into zirconium up to a temperature of approximately 800 C., and only slowly above this temperature. Furthermore, it reacts with zirconium to form a fusible alloy only at approximately 1300 C. Also of importance, is the fact that chromium has a coefficient of expansion very close to that of zirconium.
- the electrolytic bath of my invention comprises an aqueous solution containing:
- the temperature at the bath is maintained near room temperature, for example, between 10 and 30 C.
- the current density is maintained between 5 and 40 A./dm. preferably near 20 A./dm and the bath is stirred.
- the anode is a lead-base alloy anode, preferably a PbSb alloy containing 6-8 percent by weight Sb, and the interpolar distance is preferably between 3 and 200 millimeters.
- my method it is possible to obtain a continuous deposit with a minimum thickness of about 2 microns. For best results, a thickness of from 5 to 15 microns is placed on the zirconium, and it is possible to realize even thicker coatings with my process. Furthermore, my coatings have excellent adhesion.
- the coatings protect zirconium against most of the usual agents brought into contact with it at high temperature and especially against organic coolants. In particular, the coating protects against terphenyls up to around 400-450 C., against air, oxygen, carbon dioxide, up to 700-800 C. for long periods of time.
- the chromium coating applied on the zirconium with my method also protects for short periods of time against air, oxygen, carbon oxides and molten salt baths which have temperatures as high as 1000 to 1200 C. In fact, the coating may protect at these high temperatures up to several hours, Moreover, it is possible to quench the coating in oil or water without any fission or cracking.
- the coatings of the invention protect zirconium and zirconium-base alloys when used at high temperatures, during hot deformations and during thermal treatments in air. In the latter case, the coating deposited according to my invention may be removed after thermal or quenching treatment.
- the electrolysis was carried out at C. with a 20 A./dm. current density.
- the anode was a cylindrical Pb-Sb tube with 6 percent Sb.
- the interpolar distance was between and mm.
- the coated samples were placed in an autoclave containing CO under atmospheric pressure at 700 C. After 3 days, their weight gain was ten times lower than that of identical noncoated cylinders placed under the same conditions.
- EXAMPLE 2 A Zr-Nb sheet with 2.5 percent Nb, and having a dimension of 500 x x 1.5 mm. was used as a cathode in a stirred electrolytic bath of the same composition as that of Example 1.
- the electrolysis was carried out at 15 C. with a 15 A./dm. current density.
- the anode was a Pb-Sn slab with 6 percent Sb.
- the interploar distance was 30 to 40 mm.
- the chromium film was deposited in 25 minutes and was approximately 12 thick.
- the coated sheets were placed in a furnace at 1000 C. in air for 15 minutes, then quenched in water at 25 C. Despite the thermal shock, the chromium coating neither blistered nor scaled, and the coating efficiently protected the alloy during the air treatment at 1000 C.
- EXAMPLE 3 A Zr-Cu tube portion with 2.5 percent copper and being 500 mm. in length, about 13 mm. in outer diameter and about 11 mm. in inner diameter, was utilized. Under conditions similar to those in the previous examples, a chromium film of 10 was deposited by electrolysis on both the inside and outside of the tube.
- the tube was maintained under vacuum for 30 hours at 800 C., then submitted to 40 successive thermal cycles of one hour each, comprising 20 minutes of heating.
- the heating temperature in air was 700 C.
- the cooling temperature was 40 C.
- the strips were placed into an atuoclave containing CO under atmospheric pressure at 700 C. In 6 days, their weight gain was ten times lower than that of noncoated samples of the same alloy placed under similar conditions.
- these tubes were heated in air at 1000 C., in a high frequency induction furnace. After 2 minutes at 1000 C., they were quenched in cold water. Under such conditions the chromium film was neither blistered nor scaled.
- EXAMPLE 6 Tube portions of Zr-Nb alloy with 2.5 percent Nb having a 600 mm. length, a 92 mm. inner diameter and a 98 mm. outer diameter were plated. After the chrome plating, the tubes were immediately introduced into a metal furnace at 900 C., and maintained for 30 minutes at 900 C. and quenched in water at the end of the furnace. It was found that after quenching, the chrome deposited according to the invention was always present, and after a chemical removing of the chrome, the metal was free of oxide pits or defects.
- EXAMPLE 7 A large piece of Zr-Nb (250 x 400 x 75 mm.) having a chromium film of 15 thickness deposited thereon according to the invention, was maintained for 1 hour, in air, at a temperature of 1200" C., prior to being rolled at a high temperature. It was found that the film had protected the piece against oxidation.
- a method for the protection of zirconium and zirconium-base alloys by electrolytic deposition of chromium comprising:
- said bath comprises 500 g./l. CrO 20 to 25 g./l. SrSO and 60 to 65 g./l. K SiF with a current density of 20 A./dm.
- the method of claim 1 including subjecting the coated metal to a vacuum-heat treatment from between 700 and 850 C. to form an intermetallic Cr-Zr compound of up to 5 thick between said coating and zirconium.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Plasma & Fusion (AREA)
- General Engineering & Computer Science (AREA)
- High Energy & Nuclear Physics (AREA)
- Electroplating Methods And Accessories (AREA)
- Electroplating And Plating Baths Therefor (AREA)
Description
United States Patent Int. Cl. c236 /06, 5/52 US. Cl. 204-37 5 Claims ABSTRACT OF THE DISCLOSURE The method of protecting zirconium and its alloys by the electrolytic deposition of chrome thereon, utilizing an electrolytic bath comprising an aqueous solution of from 400 to 550 g./l. CrO to 40 g./l. SrSO and 30 to 80 g./l. K SiF maintained at a temperature between 10 and 30 C. and at a current density of 5 to 40 A./dm.
My invention relates to the protection of zirconium and zirconium-base alloys [hereinafter generically called zirconium] against corrosion by external agents at high temperatures.
It is well-known that zirconium and zirconium-base alloys and particularly those alloys used in nuclear reac tors as cladding materials or in the fabrication of pressure or calandria tubes, have limited applications due to thecorroding action of the coolants, generally, presurized water, carbon dioxide, terphenyl or steam. Furthermore, the fabrication and transformation of the same alloys are diflicult and costly because of the rapid corrosion in air at temperatures above 800 to 900 C.
Due to external agents, a zirconium oxide film of 10W ductility is formed on the surface of zirconium. This film has a tendency to thicken and to eventually scale off. Simultaneously with the thickening and scaling off of the zirconium oxide film, oxygen penetrates into the subjacent metal and causes these areas to become brittle. This phenomena is even more pronounced as the temperature increases.
To protect zirconium against such corrosion, it has been proposed that it be separated from the external agents by coatings for which various coating processes have been developed. Different metals have been tried as a coating material including aluminum, copper, nickel, and iron. However, the deposition techniques have been inefficient particularly, where the metals are submitted to a high temperature during either utilization or transformation. The primary defects of the prior deposition techniques include unevenness or great thickness of the coating and its lack of adherence or adhesion, particularly, when hot. The maximum temperature at which the coating may be used is in adequate and limited because of the inner diffusion between the zirconium and the coating itself and/or to the formation of fusible eutectics. The specificity of the agent against which the coating was efficient has been too high. Finally, the prior processes are complex in nature, high in cost, and/or irregular in result. Not all of the prior techniques manifested all of these defects simultaneously, but at least one of them was present and generally several. 7
Of all the protective materials proposed for the protection of zirconium, chromium has shown the greatest advantages. Chromium oxidizes very slowly, is hard, and is resistant to abrasion. It has practically no diffusion into zirconium up to a temperature of approximately 800 C., and only slowly above this temperature. Furthermore, it reacts with zirconium to form a fusible alloy only at approximately 1300 C. Also of importance, is the fact that chromium has a coefficient of expansion very close to that of zirconium.
3,502,549 Patented Mar. 24, 1970 Prior to my invention, the depositing of chromium electrolytically on zirconium pieces had been tried but without success. The usual chromium plating baths contain ponderal ratios of CrO /H SO of approximately 100. The chromium deposits comprise spaced apart nodules which require the coating to be thick if it is to be continuous due to the progressive surface increase of the nodules and their bonding, Moreover, even when a contlnuous outer coating was obtained, thick coating had inherent defects of adhesion particularly at high temperatures. Accordingly, these electrolytically plated zirconium pieces have a tendency to blister and thus fail to protect the zirconium, particularly during deformation to which it is submitted.
I have invented a method for placing a tight and perfectly adhesive chromium coating upon zirconium and zirconium-base alloys. The electrolytic bath of my invention comprises an aqueous solution containing:
400 to 550 g./l. CrO preferably close to 500 g./l. 10 to 40 g./l. SrSO preferably between 20 and 25 g./l. 30 to g./l. K SiF preferably 60 to 65 g./l.
The temperature at the bath is maintained near room temperature, for example, between 10 and 30 C. The current density is maintained between 5 and 40 A./dm. preferably near 20 A./dm and the bath is stirred. The anode is a lead-base alloy anode, preferably a PbSb alloy containing 6-8 percent by weight Sb, and the interpolar distance is preferably between 3 and 200 millimeters.
Utilizing my method it is possible to obtain a continuous deposit with a minimum thickness of about 2 microns. For best results, a thickness of from 5 to 15 microns is placed on the zirconium, and it is possible to realize even thicker coatings with my process. Furthermore, my coatings have excellent adhesion. The coatings protect zirconium against most of the usual agents brought into contact with it at high temperature and especially against organic coolants. In particular, the coating protects against terphenyls up to around 400-450 C., against air, oxygen, carbon dioxide, up to 700-800 C. for long periods of time. The chromium coating applied on the zirconium with my method also protects for short periods of time against air, oxygen, carbon oxides and molten salt baths which have temperatures as high as 1000 to 1200 C. In fact, the coating may protect at these high temperatures up to several hours, Moreover, it is possible to quench the coating in oil or water without any fission or cracking.
It is also possible to obtain a coating which is both more adhesive and more ductile by subjecting the coating obtained to a vacuum-treatment between 700 and 850 C. This complementary treatment provides a greater margin of safety during hot deformations in air. During this thermal treatment a film of Cr-Zr intermetallic compound, usually below 1 micron but never above 5 microns is formed between the chromium and zirconium. This intermetallic compound insures a strong adhesion between the base metal and the coating. Interestingly, this vacuum-treatment considerably improved the ductility of the chromium deposit due to the elimination of the gaseous impurities contained therein.
The coatings of the invention protect zirconium and zirconium-base alloys when used at high temperatures, during hot deformations and during thermal treatments in air. In the latter case, the coating deposited according to my invention may be removed after thermal or quenching treatment.
The following nonlimitative examples illustrate the results obtained with a coating of this invention as against comon external agents.
3 EXAMPLE 1 Bulk cylindrical samples of zirconium-copper alloy with 1.6 percent copper, 50 mm. in length and mm. in diameter, were chromium plated by being used as a cathode in a stirred aqueous solution of:
CI'O3 K SiF 60 S1'S0 22 which constituted the electrolytic bath.
The electrolysis was carried out at C. with a 20 A./dm. current density. The anode was a cylindrical Pb-Sb tube with 6 percent Sb. The interpolar distance was between and mm. A chrominum film of about 10; was deposited within 20 minutes.
The coated samples were placed in an autoclave containing CO under atmospheric pressure at 700 C. After 3 days, their weight gain was ten times lower than that of identical noncoated cylinders placed under the same conditions.
EXAMPLE 2 A Zr-Nb sheet with 2.5 percent Nb, and having a dimension of 500 x x 1.5 mm. was used as a cathode in a stirred electrolytic bath of the same composition as that of Example 1.
The electrolysis was carried out at 15 C. with a 15 A./dm. current density. The anode was a Pb-Sn slab with 6 percent Sb. The interploar distance was 30 to 40 mm. The chromium film was deposited in 25 minutes and was approximately 12 thick. The coated sheets were placed in a furnace at 1000 C. in air for 15 minutes, then quenched in water at 25 C. Despite the thermal shock, the chromium coating neither blistered nor scaled, and the coating efficiently protected the alloy during the air treatment at 1000 C.
EXAMPLE 3 A Zr-Cu tube portion with 2.5 percent copper and being 500 mm. in length, about 13 mm. in outer diameter and about 11 mm. in inner diameter, was utilized. Under conditions similar to those in the previous examples, a chromium film of 10 was deposited by electrolysis on both the inside and outside of the tube.
After this electrolytic operation, the tube was maintained under vacuum for 30 hours at 800 C., then submitted to 40 successive thermal cycles of one hour each, comprising 20 minutes of heating. The heating temperature in air was 700 C. The cooling temperature was 40 C.
After examination, the chromium film was neither blistered nor scaled.
EXAMPLE 4 Strips of zirconium-base alloy containing:
Zr, remainder.
were coated electrolytically under conditions similar to those in the previous examples, but the deposit time was 40 minutes instead of 20 minutes, which permitted obtainment of a 20 micron chromium film.
The examination of a section of the strips showed the apparition between base alloy and chromium of an intermetallic film of about 0.5 1 in thickness.
The strips were placed into an atuoclave containing CO under atmospheric pressure at 700 C. In 6 days, their weight gain was ten times lower than that of noncoated samples of the same alloy placed under similar conditions.
The examination of the strips also showed that the chromium film was neither blistered nor scaled.
4 EXAMPLE 5 Tube portions of Zr-Nb alloy with 2.5 percent Nb having an mm. length, a 20 mm. outer diameter and an 0.5 mm. thickness were chromium plated electrolytically under the same conditions as those of Example 1, which permitted obtainment of a chromium film, about 10a thick both inside and outside.
After this operation, these tubes were heated in air at 1000 C., in a high frequency induction furnace. After 2 minutes at 1000 C., they were quenched in cold water. Under such conditions the chromium film was neither blistered nor scaled.
EXAMPLE 6 Tube portions of Zr-Nb alloy with 2.5 percent Nb having a 600 mm. length, a 92 mm. inner diameter and a 98 mm. outer diameter were plated. After the chrome plating, the tubes were immediately introduced into a metal furnace at 900 C., and maintained for 30 minutes at 900 C. and quenched in water at the end of the furnace. It was found that after quenching, the chrome deposited according to the invention was always present, and after a chemical removing of the chrome, the metal was free of oxide pits or defects.
EXAMPLE 7 A large piece of Zr-Nb (250 x 400 x 75 mm.) having a chromium film of 15 thickness deposited thereon according to the invention, was maintained for 1 hour, in air, at a temperature of 1200" C., prior to being rolled at a high temperature. It was found that the film had protected the piece against oxidation.
I claim:
1. A method for the protection of zirconium and zirconium-base alloys by electrolytic deposition of chromium, comprising:
(A) electrolyzing said zirconium in an aqueous electrolytic bath of from 400 to 550 g./l. CrO 10 to 40 g./l. SrSO, and 30 to 80 g./l. K SiF with a current density of from 5 to 40 A./dm. utilizing a lead-base alloy anode;
(B) stirring said bath; and
(C) maintaining the temperature of said bath between 10 and 30 C.
2. The method as set forth in claim 1 wherein said bath comprises 500 g./l. CrO 20 to 25 g./l. SrSO and 60 to 65 g./l. K SiF with a current density of 20 A./dm.
3. The method as set forth in claim 1 wherein said anode is a Pb-Sb alloy having 6 to 8 percent by weight Sb.
4. The method of claim 1 wherein the interpolar distance is from 3 to 200 mm.
5. The method of claim 1 including subjecting the coated metal to a vacuum-heat treatment from between 700 and 850 C. to form an intermetallic Cr-Zr compound of up to 5 thick between said coating and zirconium.
References Cited UNITED STATES PATENTS 1,608,694 11/1926 Cain 204-37 XR 1,745,912 2/ 1930 Richardson 20437 XR 1,838,273 12/1931 McBride 204--37 2,640,021 5/1953 Passal 204-51 3,041,257 6/1962 Cope et al. 2045l JOHN H. MACK, Primary Examiner G. L. KAPLAN, Assistant Examiner U.S. Cl. X.R. 2045l
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR102932A FR1527055A (en) | 1967-04-17 | 1967-04-17 | Improvements relating to the protection of zirconium and its alloys |
Publications (1)
Publication Number | Publication Date |
---|---|
US3502549A true US3502549A (en) | 1970-03-24 |
Family
ID=8628973
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US721935A Expired - Lifetime US3502549A (en) | 1967-04-17 | 1968-04-17 | Method for the protection of zirconium and zirconium-base alloys |
Country Status (8)
Country | Link |
---|---|
US (1) | US3502549A (en) |
BE (1) | BE711125A (en) |
CH (1) | CH492029A (en) |
DE (1) | DE1771162B1 (en) |
FR (1) | FR1527055A (en) |
GB (1) | GB1203700A (en) |
LU (1) | LU55872A1 (en) |
NL (1) | NL159729B (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3627650A (en) * | 1969-07-15 | 1971-12-14 | Atomic Energy Commission | Method for producing a chromium-tungsten coating on tungsten for protection against oxidation at elevated temperatures |
FR2290736A1 (en) * | 1974-11-11 | 1976-06-04 | Gen Electric | PERFECTED NUCLEAR FUEL ELEMENT |
JPS5169794A (en) * | 1974-11-11 | 1976-06-16 | Gen Electric | |
US5264109A (en) * | 1991-09-16 | 1993-11-23 | Siemens Power Corporation | Zirconium and zirconium alloy passivation process |
US5383228A (en) * | 1993-07-14 | 1995-01-17 | General Electric Company | Method for making fuel cladding having zirconium barrier layers and inner liners |
US5469481A (en) * | 1993-07-14 | 1995-11-21 | General Electric Company | Method of preparing fuel cladding having an alloyed zirconium barrier layer |
US5524032A (en) * | 1993-07-14 | 1996-06-04 | General Electric Company | Nuclear fuel cladding having an alloyed zirconium barrier layer |
US20130302639A1 (en) * | 2012-05-10 | 2013-11-14 | Korea Hydro And Nuclear Power Co., Ltd. | Zirconium alloy for improving resistance to oxidation at very high temperature and fabrication method thereof |
US9721676B2 (en) | 2014-05-27 | 2017-08-01 | Westinghouse Electric Company, Llc | Deposition of a protective coating including metal-containing and chromium-containing layers on zirconium alloy for nuclear power applications |
EP3502321A1 (en) | 2017-12-20 | 2019-06-26 | Westinghouse Electric Sweden AB | Method of forming a coated component made of zirconium or zirconium-based alloy |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2989923B1 (en) * | 2012-04-26 | 2014-05-16 | Commissariat Energie Atomique | MULTILAYER MATERIAL RESISTANT TO OXIDATION IN NUCLEAR MEDIA. |
FR3025929B1 (en) | 2014-09-17 | 2016-10-21 | Commissariat Energie Atomique | NUCLEAR FUEL TANKS, METHODS OF MANUFACTURE AND USE AGAINST OXIDATION. |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
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US1608694A (en) * | 1925-08-10 | 1926-11-30 | John R Cain | Corrosion-resistant article and method of making the same |
US1745912A (en) * | 1923-05-03 | 1930-02-04 | Westinghouse Lamp Co | Chromium-coated wire and method of manufacture |
US1838273A (en) * | 1927-12-24 | 1931-12-29 | Westinghouse Electric & Mfg Co | Method of producing chromium plated tools |
US2640021A (en) * | 1949-11-23 | 1953-05-26 | United Chromium Inc | Composition, bath, and process for chromium plating |
US3041257A (en) * | 1960-08-25 | 1962-06-26 | Westinghouse Electric Corp | Chromium electroplating |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2555372A (en) * | 1944-10-02 | 1951-06-05 | Westinghouse Electric Corp | Method of coating refractory readily oxidizable metals |
US3065154A (en) * | 1959-06-29 | 1962-11-20 | Bendix Corp | Method of plating chromium and the like to titanium, its alloys, and the like |
FR1493040A (en) * | 1966-07-12 | 1967-08-25 | Commissariat Energie Atomique | Process for protecting zirconium and its alloys with a chromium coating |
-
1967
- 1967-04-17 FR FR102932A patent/FR1527055A/en not_active Expired
-
1968
- 1968-02-22 BE BE711125D patent/BE711125A/xx not_active IP Right Cessation
- 1968-04-10 LU LU55872D patent/LU55872A1/xx unknown
- 1968-04-13 DE DE19681771162 patent/DE1771162B1/en not_active Withdrawn
- 1968-04-16 CH CH554068A patent/CH492029A/en not_active IP Right Cessation
- 1968-04-16 GB GB07951/68A patent/GB1203700A/en not_active Expired
- 1968-04-17 NL NL6805383.A patent/NL159729B/en not_active IP Right Cessation
- 1968-04-17 US US721935A patent/US3502549A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1745912A (en) * | 1923-05-03 | 1930-02-04 | Westinghouse Lamp Co | Chromium-coated wire and method of manufacture |
US1608694A (en) * | 1925-08-10 | 1926-11-30 | John R Cain | Corrosion-resistant article and method of making the same |
US1838273A (en) * | 1927-12-24 | 1931-12-29 | Westinghouse Electric & Mfg Co | Method of producing chromium plated tools |
US2640021A (en) * | 1949-11-23 | 1953-05-26 | United Chromium Inc | Composition, bath, and process for chromium plating |
US3041257A (en) * | 1960-08-25 | 1962-06-26 | Westinghouse Electric Corp | Chromium electroplating |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3627650A (en) * | 1969-07-15 | 1971-12-14 | Atomic Energy Commission | Method for producing a chromium-tungsten coating on tungsten for protection against oxidation at elevated temperatures |
FR2290736A1 (en) * | 1974-11-11 | 1976-06-04 | Gen Electric | PERFECTED NUCLEAR FUEL ELEMENT |
JPS5169794A (en) * | 1974-11-11 | 1976-06-16 | Gen Electric | |
JPS5712115B2 (en) * | 1974-11-11 | 1982-03-09 | ||
US5264109A (en) * | 1991-09-16 | 1993-11-23 | Siemens Power Corporation | Zirconium and zirconium alloy passivation process |
US5383228A (en) * | 1993-07-14 | 1995-01-17 | General Electric Company | Method for making fuel cladding having zirconium barrier layers and inner liners |
US5469481A (en) * | 1993-07-14 | 1995-11-21 | General Electric Company | Method of preparing fuel cladding having an alloyed zirconium barrier layer |
US5524032A (en) * | 1993-07-14 | 1996-06-04 | General Electric Company | Nuclear fuel cladding having an alloyed zirconium barrier layer |
US20130302639A1 (en) * | 2012-05-10 | 2013-11-14 | Korea Hydro And Nuclear Power Co., Ltd. | Zirconium alloy for improving resistance to oxidation at very high temperature and fabrication method thereof |
US9421740B2 (en) * | 2012-05-10 | 2016-08-23 | Korea Atomic Energy Research Institute | Zirconium alloy for improving resistance to oxidation at very high temperature and fabrication method thereof |
US9721676B2 (en) | 2014-05-27 | 2017-08-01 | Westinghouse Electric Company, Llc | Deposition of a protective coating including metal-containing and chromium-containing layers on zirconium alloy for nuclear power applications |
EP3502321A1 (en) | 2017-12-20 | 2019-06-26 | Westinghouse Electric Sweden AB | Method of forming a coated component made of zirconium or zirconium-based alloy |
Also Published As
Publication number | Publication date |
---|---|
NL159729B (en) | 1979-03-15 |
NL6805383A (en) | 1968-10-18 |
FR1527055A (en) | 1968-05-31 |
BE711125A (en) | 1968-07-01 |
GB1203700A (en) | 1970-09-03 |
LU55872A1 (en) | 1968-07-09 |
CH492029A (en) | 1970-06-15 |
DE1771162B1 (en) | 1971-04-08 |
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