US3276903A - Heat treatment of metals - Google Patents
Heat treatment of metals Download PDFInfo
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- US3276903A US3276903A US438788A US43878865A US3276903A US 3276903 A US3276903 A US 3276903A US 438788 A US438788 A US 438788A US 43878865 A US43878865 A US 43878865A US 3276903 A US3276903 A US 3276903A
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- United States
- Prior art keywords
- fluoride
- nickel
- treatment
- articles
- metal
- Prior art date
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- Expired - Lifetime
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- 238000010438 heat treatment Methods 0.000 title claims description 27
- 229910052751 metal Inorganic materials 0.000 title description 31
- 239000002184 metal Substances 0.000 title description 31
- 150000002739 metals Chemical class 0.000 title description 7
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 69
- 229910045601 alloy Inorganic materials 0.000 claims description 37
- 239000000956 alloy Substances 0.000 claims description 37
- 239000011651 chromium Substances 0.000 claims description 28
- 229910052759 nickel Inorganic materials 0.000 claims description 28
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 27
- KRHYYFGTRYWZRS-UHFFFAOYSA-M Fluoride anion Chemical compound [F-] KRHYYFGTRYWZRS-UHFFFAOYSA-M 0.000 claims description 27
- 229910052804 chromium Inorganic materials 0.000 claims description 26
- 238000000034 method Methods 0.000 claims description 16
- 239000001257 hydrogen Substances 0.000 claims description 14
- 229910052739 hydrogen Inorganic materials 0.000 claims description 14
- DBJLJFTWODWSOF-UHFFFAOYSA-L nickel(ii) fluoride Chemical compound F[Ni]F DBJLJFTWODWSOF-UHFFFAOYSA-L 0.000 claims description 14
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 12
- 239000007787 solid Substances 0.000 claims description 12
- 239000010941 cobalt Substances 0.000 claims description 11
- 229910017052 cobalt Inorganic materials 0.000 claims description 11
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical class [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 10
- 229910001220 stainless steel Inorganic materials 0.000 claims description 9
- YCYBZKSMUPTWEE-UHFFFAOYSA-L cobalt(ii) fluoride Chemical compound F[Co]F YCYBZKSMUPTWEE-UHFFFAOYSA-L 0.000 claims description 7
- 229910021583 Cobalt(III) fluoride Inorganic materials 0.000 claims description 6
- VNNRSPGTAMTISX-UHFFFAOYSA-N chromium nickel Chemical compound [Cr].[Ni] VNNRSPGTAMTISX-UHFFFAOYSA-N 0.000 claims description 5
- 238000011282 treatment Methods 0.000 description 47
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 27
- DDFHBQSCUXNBSA-UHFFFAOYSA-N 5-(5-carboxythiophen-2-yl)thiophene-2-carboxylic acid Chemical compound S1C(C(=O)O)=CC=C1C1=CC=C(C(O)=O)S1 DDFHBQSCUXNBSA-UHFFFAOYSA-N 0.000 description 23
- 238000000137 annealing Methods 0.000 description 20
- 150000002222 fluorine compounds Chemical group 0.000 description 16
- 239000000203 mixture Substances 0.000 description 16
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical class F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 description 15
- 239000010410 layer Substances 0.000 description 13
- 229910052742 iron Inorganic materials 0.000 description 12
- 229910001512 metal fluoride Inorganic materials 0.000 description 11
- 229910001235 nimonic Inorganic materials 0.000 description 11
- 239000000047 product Substances 0.000 description 11
- 238000009792 diffusion process Methods 0.000 description 9
- 230000001681 protective effect Effects 0.000 description 9
- 230000015572 biosynthetic process Effects 0.000 description 7
- 238000009835 boiling Methods 0.000 description 7
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 6
- 229910052782 aluminium Inorganic materials 0.000 description 6
- 238000001816 cooling Methods 0.000 description 6
- 230000007935 neutral effect Effects 0.000 description 5
- 230000003647 oxidation Effects 0.000 description 5
- 238000007254 oxidation reaction Methods 0.000 description 5
- 238000007669 thermal treatment Methods 0.000 description 5
- QGZKDVFQNNGYKY-UHFFFAOYSA-O Ammonium Chemical compound [NH4+] QGZKDVFQNNGYKY-UHFFFAOYSA-O 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 238000007865 diluting Methods 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 150000002431 hydrogen Chemical class 0.000 description 4
- 230000001590 oxidative effect Effects 0.000 description 4
- 238000007493 shaping process Methods 0.000 description 4
- 229910052719 titanium Inorganic materials 0.000 description 4
- 239000010936 titanium Substances 0.000 description 4
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 3
- 239000002253 acid Substances 0.000 description 3
- 229910021529 ammonia Inorganic materials 0.000 description 3
- 238000005282 brightening Methods 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 229910000753 refractory alloy Inorganic materials 0.000 description 3
- 239000010935 stainless steel Substances 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- ZSLUVFAKFWKJRC-IGMARMGPSA-N 232Th Chemical compound [232Th] ZSLUVFAKFWKJRC-IGMARMGPSA-N 0.000 description 2
- 238000012935 Averaging Methods 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 2
- LDDQLRUQCUTJBB-UHFFFAOYSA-N ammonium fluoride Chemical compound [NH4+].[F-] LDDQLRUQCUTJBB-UHFFFAOYSA-N 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 229910021563 chromium fluoride Inorganic materials 0.000 description 2
- 238000005242 forging Methods 0.000 description 2
- SHXXPRJOPFJRHA-UHFFFAOYSA-K iron(iii) fluoride Chemical compound F[Fe](F)F SHXXPRJOPFJRHA-UHFFFAOYSA-K 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 229910001507 metal halide Inorganic materials 0.000 description 2
- 150000005309 metal halides Chemical group 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 239000011733 molybdenum 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
- 238000005498 polishing Methods 0.000 description 2
- 238000001556 precipitation Methods 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 238000009991 scouring Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229910003452 thorium oxide Inorganic materials 0.000 description 2
- FTBATIJJKIIOTP-UHFFFAOYSA-K trifluorochromium Chemical compound F[Cr](F)F FTBATIJJKIIOTP-UHFFFAOYSA-K 0.000 description 2
- 229910001928 zirconium oxide Inorganic materials 0.000 description 2
- IRPGOXJVTQTAAN-UHFFFAOYSA-N 2,2,3,3,3-pentafluoropropanal Chemical compound FC(F)(F)C(F)(F)C=O IRPGOXJVTQTAAN-UHFFFAOYSA-N 0.000 description 1
- KLZUFWVZNOTSEM-UHFFFAOYSA-K Aluminum fluoride Inorganic materials F[Al](F)F KLZUFWVZNOTSEM-UHFFFAOYSA-K 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910052684 Cerium Inorganic materials 0.000 description 1
- 229910000599 Cr alloy Inorganic materials 0.000 description 1
- 229910000640 Fe alloy Inorganic materials 0.000 description 1
- 229910000604 Ferrochrome Inorganic materials 0.000 description 1
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 description 1
- -1 Ni TiAl Chemical class 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 240000007594 Oryza sativa Species 0.000 description 1
- 235000007164 Oryza sativa Nutrition 0.000 description 1
- 229910052776 Thorium Inorganic materials 0.000 description 1
- 229910010038 TiAl Inorganic materials 0.000 description 1
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical group O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 150000001638 boron Chemical class 0.000 description 1
- WTEOIRVLGSZEPR-UHFFFAOYSA-N boron trifluoride Chemical class FB(F)F WTEOIRVLGSZEPR-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- ZMIGMASIKSOYAM-UHFFFAOYSA-N cerium Chemical compound [Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce] ZMIGMASIKSOYAM-UHFFFAOYSA-N 0.000 description 1
- 229910000423 chromium oxide Inorganic materials 0.000 description 1
- 238000005254 chromizing Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 229910001610 cryolite Inorganic materials 0.000 description 1
- JKWMSGQKBLHBQQ-UHFFFAOYSA-N diboron trioxide Chemical compound O=BOB=O JKWMSGQKBLHBQQ-UHFFFAOYSA-N 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 239000011737 fluorine Substances 0.000 description 1
- 229910052731 fluorine Inorganic materials 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 239000007792 gaseous phase Substances 0.000 description 1
- 150000004820 halides Chemical class 0.000 description 1
- 229910000040 hydrogen fluoride Inorganic materials 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- FZGIHSNZYGFUGM-UHFFFAOYSA-L iron(ii) fluoride Chemical class [F-].[F-].[Fe+2] FZGIHSNZYGFUGM-UHFFFAOYSA-L 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- FUJCRWPEOMXPAD-UHFFFAOYSA-N lithium oxide Chemical compound [Li+].[Li+].[O-2] FUJCRWPEOMXPAD-UHFFFAOYSA-N 0.000 description 1
- 229910001947 lithium oxide Inorganic materials 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- 150000002815 nickel Chemical class 0.000 description 1
- 229910000480 nickel oxide Inorganic materials 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 230000001473 noxious effect Effects 0.000 description 1
- GNRSAWUEBMWBQH-UHFFFAOYSA-N oxonickel Chemical compound [Ni]=O GNRSAWUEBMWBQH-UHFFFAOYSA-N 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 230000009993 protective function Effects 0.000 description 1
- 239000011241 protective layer Substances 0.000 description 1
- 230000002829 reductive effect Effects 0.000 description 1
- 239000003870 refractory metal Substances 0.000 description 1
- 230000001172 regenerating effect Effects 0.000 description 1
- 230000008929 regeneration Effects 0.000 description 1
- 238000011069 regeneration method Methods 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 235000009566 rice Nutrition 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000002689 soil Substances 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 229910052623 talc Inorganic materials 0.000 description 1
- 235000012222 talc Nutrition 0.000 description 1
- 239000000454 talc Substances 0.000 description 1
- ZCUFMDLYAMJYST-UHFFFAOYSA-N thorium dioxide Chemical compound O=[Th]=O ZCUFMDLYAMJYST-UHFFFAOYSA-N 0.000 description 1
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 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
- 229910052720 vanadium Inorganic materials 0.000 description 1
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/28—Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes
- C23C10/34—Embedding in a powder mixture, i.e. pack cementation
-
- 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
- C22F1/02—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working in inert or controlled atmosphere or vacuum
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/10—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/06—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of metallic material
- C23C16/08—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of metallic material from metal halides
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
- F24S70/00—Details of absorbing elements
- F24S70/10—Details of absorbing elements characterised by the absorbing material
-
- 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
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/40—Solar thermal energy, e.g. solar towers
Definitions
- Patent 1,060,225 Feb. 4,- 1953, 642,305, Patent 1,074,096; Mar. 12, 1953, 644,414, Patent 1,075,620; Feb. 16, 1955, 54,951, Patent 1,060,225; May 13, 1955, 691,668, Patent 1,134,763
- the present invention relates to methods for the heat treatment, at temperatures higher than 700 C., of articles made of alloys containing chromium and at least one metal of the group consisting of nickel and cobalt and which may also contain iron.
- the object of this invention is to permit of carrying out the heat treatment without any oxidizing of the article being treated.
- the essential feature of my invention consists in conducting said heat treatment in a non-oxidizing atmosphere essentially constituted by at least one fluoride having a boiling point greater than 700 C. under conditions preventing difiusion of chromium into said article.
- a first embodiment of my invention is concerned with the treatment of ferrous pieces made of stainless steels (i.e., of chromium, nickel and iron alloys) for brightening the surface thereof.
- ferrous pieces made of stainless steels (i.e., of chromium, nickel and iron alloys) for brightening the surface thereof.
- such pieces are heated, at temperatures above 700 C. in a fluorine containing atmosphere.
- a brightening reheating of these ferrous pieces is performed in a particularly easy way by placing the pieces of bulk in a diluting body such as talcum containing ammonium fluoride.
- the brightening of ferrous pieces which have been initially oxidized may be explained by the volatilizing of the oxide in the state of iron fluoride at temperatures averaging 900 C. with formation of water which is gradually eliminated. Subsequently, the fluoride vapor thus formed is reduced and the metal deposits on the piece which is thus covered with an iron film.
- a second embodiment of my invention is concerned with the treatment of metal articles made of refractory alloys having as main component, or components, nickel or/ and cobalt, and further containing chromium and possibly at least one of the following components, to wit: titanium, aluminum, molybdenum, tungsten, zirconium, iron, manganese, cerium and thorium.
- chromium possibly at least one of the following components, to wit: titanium, aluminum, molybdenum, tungsten, zirconium, iron, manganese, cerium and thorium.
- Such alloys are known in the art under the name of Nimonics (Nimonic 80, Nirnonic 90, Nimonic 95), Waspalloys, etc.
- the treatment of such articles generally requires a shaping in the hot state, such as forging, stamping, rolling, extruding, etc., which is generally carried out in the presence of air.
- This treatment involves a considerable superficial oxidizing of the alloys which reduces the percentage of protective elements in the superficial layers of the article and which necessitates costly scouring operations. If the articles are to be machined after this shaping operation, this drawback is less important, but however the formation of oxides between the successive steps of the shaping operation involves risks of producing undesirable inclusions in the articles if special precautions are 3,276,903 Patented Oct. 4, 1966 not taken.
- the articles are again heated at a temperature equal, or close to, the above mentioned initial thermal treatment temperature, but for a very short time, for instance averaging from 8 to 10 minutes at 1080 C. in a bath of boric anhydride containing a small amount of cryolite, or in an atmosphere of hydrogen as pure as possible.
- This short complementary homogenizing treatment after a machining or other cold working operation is called skin-annealing.
- Articles having undergone the skin-annealing operation may become particularly sensitive to the type of corrosion which produces cracks in the metal of the articles, this kind of corrosion constituting a danger even for articles working at temperatures where there is only a negligible corrosion by oxidation and scaling.
- Articles having undergone a skin-annealing treatment generally have an unsatisfactory surface, even after cleaning thereof.
- My invention relates to treatments including at least one operation during which the metalarticle (as defined hereinbefore) is treated at temperatures higher than 700 C. in a neutral or reducing atmosphere containing at least one fluoride of a metal component of the alloy of which the article is made having a boiling point higher than 700 C., and according to my invention, the conditions in which the operation is carried out and the composition of said atmosphere are so chosen as practically to prevent any superficial metal diffusion into the article.
- treatment operations during which the article is heated at temperatures higher than 700 C.” includes, for instance, shaping treatments for refractory and stainless alloys, thermal treatments and, in particular, skin-annealing operations of refractory alloys.
- inert fluoride any fluoride which, in the conditions of the treatment operation, does not cause the formation of a superficial diffusion alloy into the article in treatment. Therefore the term ine fluoride: applies to the fluorides of the main components of the alloy, that is to say nickel and/ or cobalt, and also to ammonium and hydrogen fluorides.
- an active fluoride is a metal fluoride which, in the conditions of the operation, causes its metal to diffuse to a substantial degree into the article to form in the superficial layers thereof, an alloy with the metal of the article.
- My invention is concerned with the case where it sutfices to add to the neutral or reducing protective atmosphere in the treatment container one or several inert fluorides. As a matter of fact, it was found that some gaS turbine elements working at relatively moderate tem perature, but subjected ,to very'strong vibrations, give.
- the protective atmosphere may be mainly constituted, for temperatures above 700 C., by one or several inert metal fluorides, and it must not include any metal fluoride capable of producing a diffusion of its metal into the article.
- aluminum fluoride causes diifusion of aluminum into the superficial layers of a refractory metal article, but to such a low degree that this fluoride may be classified either as an active fluoride or as an inert one.
- the fluoride vapors which are to form the protective atmosphere in the treatment container are advantageously obtained by placing in said container elements which will be called sources of such a fluoride and which are located out of contact with the articles to be treated (said articles being, for instance, separated by grids from said sources).
- the desired metal fluoride vapors may be constituted either by a so-called cementation product, requiring only the action of heat thereon to give off said metal fluoride vapors, or by a metal mass or a compound capable of giving 05 said metal fluoride vapors under the combined actions of heat and of other fluoride vapors evolved in another region of the container.
- this metal is that of the fluoride to be obtained and the fluoride vapors acting thereon may be vapors of hydrofluoric acid.
- a metal is for instance used in addition to a cementation product located in another region of the treatment container- When said container is heated, the cementation product gives off vapors of the desired fluoride; .
- These vapors upon coming into contact with the metal article, decompose into the Inetalof the fluoride, which diifuses steps taking place at different temperatures.
- the metal mass is called regeneration mass.
- a cementation product may be constituted by the metal fluoride itself in the solid state (which disengages vapors under the efi'ect of heat), or by a mixture of components which, under the 'elfect of heat, react upon each other to produce such vapors.
- I may also make use of metal powders. which, when attacked by an ammonium fluoride or a hydrogen fluoride (or hydrofluoric acid), give 0d the desired fluoride vapors.
- I may also use a metal mass placed in the treatment container in the vicinity of the article, but out of contact therewith, and which is attacked by suitably formed fluoride vapors whereby the desired metalfluoride is formed on the surface of said mass, this metal halide being vaporized by the action of heat to give oif the fluoride vapors of the protective atmosphere.
- a certain amount of ammonium fluoride, introduced in the container, may serve to sweep the atmosphere thereof at the beginning of the treatment.
- the treatment operation during which the article is treated at temperatures higher than 700 C. may be a skin-annealing treatment.
- this treatment is preferably. performed in a purely gaseous phase, that is to say. without direct contact of the article with the source or sources of fluoride or fluorides.
- the article is separated from said sources by grids of a shape conforming as much as possible to that of the article and advantageously made of a metal (or of an alloy containing ametal) which is a main component of the alloy of the article.
- this operation is advantageously carried out in two successive
- the temperature of the first step is higher than that at which skin-annealing is generally conducted, so as to permit of more efliciently bringing into solution some compounds which contribute to the structural hardening of the alloy, such as carbides and nitrides (temperature ranging from 1150 to 1200 C. for Nimonic and Nimonic alloys).
- the temperature during the second step is lower than that during the first step by about one hundred degrees, so as to obtain a dispersed precipitation of said components (temperature ranging from 1050 to 1100 C. for the above mentioned alloys), while maintaining in solution other purely metallic structural hardening compounds, such as Ni TiAl, which precipitate in controlled fashion during the final annealing.
- the skin-annealing treatment is preferably performed in boxes which are small or at least one dimension of which is small (flat boxes or boxes limiting a volume in the form of an annular cylindrical space).
- This heating is advantageously performed in powerful furnaces in an atmosphere of hydrogen so as to obtain a conductivity of heat as high as possible.
- cooling of the boxes is accelerated by circulation of air or by immersion in a liquid.
- thermal treatments which are considered require temperatures higher than 1200 C.
- I may make use of other fluorides having a higher boiling point, such as cobalt fluoride (boiling point 1300 C.).
- Nimonic articles in the presence of nickel fluoride (which may be formed by heating a fine nickel powder with ammonium fluoride) with a small amount of ammonium fluoride which drives off the air in the container at the beginning of the heating operation, or with ammonium fluoride alone if itsvapors are made to form nickel fluoride by attacking a mass of nickel placed in the treatment container close to the article but out of contact therewith.
- This mass may be constituted by small lumps of nickel of suitable size or by nickel grids surrounding the articles.
- This formation of nickel fluoride during the skin-annealing operation may even be obtained by reaction of ammonium fluoride or hydrofluoric acid on the metal of the Nimonic article itself, which forms on said article a protective layer of nickel fluoride which volatilizes at high temperature.
- I may reduce the proportion of titanium and aluminum from the superficial layers of Nimonic articles, before the skin-annealing operation, by performing a controlled oxidation for some hours at 700-750 C., without subsequent scouring.
- the efliect of this operation is superficially to soften the alloy by lowering the proportion of titanium and aluminum therein.
- undesirable fluorides are fluorides of metals which are not included in the composition of the alloy and which might give rise to the formation of undesirable superficial diffusion alloys.
- the treatment container will be preferably made of the main component metal or one of the main component metals of the alloy of which the article is made, with the exception of chromium, or, alternately, this container will be coated or lined with such a metal or metals. If for some reasons, for instance of economy or mechanical resistance, it is however desired to use containers or accessories which contain iron, any noxious effects on the alloy may be avoided by surrounding the iron parts or the article to be treated with means (such as nickel grids for instance) through which the iron fluoride vapors must pass before reaching the articles to be treated.
- means such as nickel grids for instance
- Example 1 Turbine blades made of Nimonic were skin-annealed with the use of a cementation substance consisting of nickel fluoride and ammonium fluoride obtained by preliminary heating of ammonium fluoride and nickel powder. The articles were placed without separation in the boxes and treated for 1 hour at 1060 C. After this treatment, the articles were of a very bright light grey.
- Example 2 Two turbine blades made of Nimonic 95 were skinannealed by being placed in a diluting mass consisting of thorium or zirconium oxide.
- the metal fluoride to be formed in the container was obtained from acid fluoride of ammonium to which may be added a small amount of nickel fluoride.
- the duration of the heating at the temperature of 1080 C. was 40 minutes,
- Example 3 A turbine wheel made of Nimonic 80 was skin-annealed under conditions similar to those of the preceding example, with the exception that the diluting substance is titanium oxide. Due to the size of the article, and therefore of the treatment box (350 mm. of diameter and mm. of height), the thermal treatment was carried out as follows:
- Heating up from 700 to 1050 C 1 h. 30 minutes. Heating at 1050 C 40 minutes. Cooling, from 1050 to 700 C 35 minutes.
- the box was placed under a hood fed with hydrogen, and cooled by atomized water.
- Example 4 Gas turbine blades of an alloy of nickel-cobalt-chrornium-titanium-aluminum and molybdenum were skin-annealed for 20 minutes at a temperature of 1080 C. without any material chromiziug in a reducing atmosphere consisting of directly cracked ammonia in a closed partly gastight box of ordinary steel which contains at the bottom thereof a mixture of chromium or fe'rrochromium (in granular form) with ammonium fluoride either acid or neutral, the amount of this fluoride being about 2 grams per liter.
- the articles in the box are kept out of contact with the above mentioned mixture by a nickel grid.
- said pieces are surrounded by an envelope of nickel wire gauze (mesh of about 1.2 mm.; thickness of wire 0.3 'mm.; two layers of gauze).
- Example 1 The pieces to be treated are the same as in the preceding example and the conditions of treatment are similar but, in this case, in order to prevent diffusion of chromium into the pieces, instead of enveloping these pieces in a nickel wire gauze, the mixture intended to produce the fluoride vapors, instead of consisting of ammonium fluoride and chromium is a mixture of neutral ammonium fluoride with nickel powder and iron powder.
- Example 6 Turbine combustion chambers made of stainless steel containing 20% nickel and 25% chromium had been assembled by welding individual elements. To eliminate stresses in the assembly and to deoxidize the welded zones, the chambers were placed in a closed partly gastight box of ordinary steel'which contained, at the bottom thereof, amixture of chromium or ferrochromium (in granular form) with ammonium fluoride (either acid or neutral), the amount of this fluoride being about 2 grams per liter, the chambers being separated from the mixture by a nickel grid. The box was heated in a reducing atmosphere.
- Example 7 Similar stainless steel articles were treated as in Example 6 except diffusion of chromium into the articles was prevented without nickel wire gauze but by producing the fluoride vapors from a mixture of neutral ammonium fluoride with nickel powder and iron powders. The articles after treatment have not the appearance of polished chromium but a light gray bright silvered appearance.
- Example 8 Sheets of stainless steel containing 25% of chromium and 20% of nickel were annealed between two rolling operations to improve the aptitude of the sheets to being stamped either in the hot or cold states.
- the sheets were placed in a partly gastight closed box of ordinary steel which contains, at the bottom thereof, a mixture of nickel and iron (in powder form) with ammonium fluoride, the amount of this fluoride being about 2.5 grams per liter.
- the sheets are placed vertically in the boxwith small amounts of ammonium fluoride placed in the intervals between said sheets, these sheets resting upon a nickel grid which keeps them out of contact with the above mentioned mixture.
- the box was heated in a reducing atmosphere consisting of directly cracked ammonium for about half'an hour at a temperature of 10801100 C., after which the boxes were cooled on the, outside of the annealing oven in a reducing gas atmosphere.
- the sheets obtained after this treatment have an exceptional aptitude to being stamped either in the cold or hot state. This is due to the fact that the annealing operation has been performed without any possibility of oxidizing and also that the surface of the sheet has been softened (elimination of any inclusion or of carbon in this surface over a depth of some tenths of a micron).
- the method which comprises placing in one chamber of a box divided into two chambersby a grid, a solid body of an alloy of the group consisting of cobalt and a temperature of 700-1100 C. for a time ranging from five minutes to five hours.
- the method which comprises placing in one chamber of a box divided into two chambers by a grid, a solid body of an alloy of the group consisting of cobalt and nickel base chromium containing heat resisting alloys, placing in the other of said chambers a cementation prod- -uct containing ammonium fluoride and cobalt powder, closing said box while permitting hydrogen to enter it, and heating said box to a temperature of 700-1100 C. for a time ranging from five minutes to five hours.
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Description
United States Patent 3,276,903 HEAT TREATMENT OF METALS Philippe Galmiche, Paris, France, assignor to Ofiice National dEtudes et de Recherches Aerospatiales, called O.N.E.R.A., Chatillon-sur-Bagneux (Seine), France, a society of France No Drawing. Continuation of application Ser. No. 42,200, July 12, 1960. This application Mar. 10, 1965, Ser. No. 438,788
Claims priority, application France, July 11, 1952,
631,962, Patent 1,060,225; Feb. 4,- 1953, 642,305, Patent 1,074,096; Mar. 12, 1953, 644,414, Patent 1,075,620; Feb. 16, 1955, 54,951, Patent 1,060,225; May 13, 1955, 691,668, Patent 1,134,763
14 Claims. (Cl. 117-107.2)
This application is a continuation of my copending application Serial No. 42,200, filed July 12, 1960, now abandoned, which was itself a continuation-in-part of my copending applications Serial Nos. 367,286, filed July 10, 1953, now abandoned, and 565,286, filed February 13, 1956, now abandoned.
The present invention relates to methods for the heat treatment, at temperatures higher than 700 C., of articles made of alloys containing chromium and at least one metal of the group consisting of nickel and cobalt and which may also contain iron.
The object of this invention is to permit of carrying out the heat treatment without any oxidizing of the article being treated.
The essential feature of my invention consists in conducting said heat treatment in a non-oxidizing atmosphere essentially constituted by at least one fluoride having a boiling point greater than 700 C. under conditions preventing difiusion of chromium into said article.
A first embodiment of my invention is concerned with the treatment of ferrous pieces made of stainless steels (i.e., of chromium, nickel and iron alloys) for brightening the surface thereof. For this purpose, according to my invention, such pieces are heated, at temperatures above 700 C. in a fluorine containing atmosphere. Such a brightening reheating of these ferrous pieces is performed in a particularly easy way by placing the pieces of bulk in a diluting body such as talcum containing ammonium fluoride. The brightening of ferrous pieces which have been initially oxidized may be explained by the volatilizing of the oxide in the state of iron fluoride at temperatures averaging 900 C. with formation of water which is gradually eliminated. Subsequently, the fluoride vapor thus formed is reduced and the metal deposits on the piece which is thus covered with an iron film.
A second embodiment of my invention is concerned with the treatment of metal articles made of refractory alloys having as main component, or components, nickel or/ and cobalt, and further containing chromium and possibly at least one of the following components, to wit: titanium, aluminum, molybdenum, tungsten, zirconium, iron, manganese, cerium and thorium. Such alloys are known in the art under the name of Nimonics (Nimonic 80, Nirnonic 90, Nimonic 95), Waspalloys, etc.
The treatment of such articles generally requires a shaping in the hot state, such as forging, stamping, rolling, extruding, etc., which is generally carried out in the presence of air. This treatment involves a considerable superficial oxidizing of the alloys which reduces the percentage of protective elements in the superficial layers of the article and which necessitates costly scouring operations. If the articles are to be machined after this shaping operation, this drawback is less important, but however the formation of oxides between the successive steps of the shaping operation involves risks of producing undesirable inclusions in the articles if special precautions are 3,276,903 Patented Oct. 4, 1966 not taken. In order to limit these drawbacks, it has already been suggested to perform these operations in an atmosphere of hydrogen, but, despite this precaution, superficial oxidation remains important because a stream of hydrogen, even purified, always contains traces of oxygen which are dangerous because they combine with some highly oxidizable elements contained in the alloy in treatment (Ti, Al, Cr, etc.).
In particular it has already been proposed to treat turbine blades made of refractory alloys of compositions such as above stated, by taking the rough-shaped articles obtained after forging and subjecting them to a thermal treatment for bringing into solution some components thereof at a temperature ranging from 900 to 1300 C., and preferably from 1050 to 1100 C., for instance for ten hours at 1080 C. Then the articles are subjected to a controlled cooling after which they are machined.
In order to remedy the structural modification resulting from the machining operation, the articles are again heated at a temperature equal, or close to, the above mentioned initial thermal treatment temperature, but for a very short time, for instance averaging from 8 to 10 minutes at 1080 C. in a bath of boric anhydride containing a small amount of cryolite, or in an atmosphere of hydrogen as pure as possible. This short complementary homogenizing treatment after a machining or other cold working operation is called skin-annealing.
Skin-annealing, in the above specified conditions, involves some drawbacks, such as the following ones:
(a) The results obtained by such a treatment are not uniform and, without any prior indications, often the articles are partly covered at the end of the treatment with a layer of oxide (chromium and/or nickel oxide) which can be eliminated only by a mechanical treatment which reintroduces the structural modifications which were intended to be eliminated by the skin-annealing operation.
(b) The articles are subjected to an electrolytic polishing intended to permit of eliminating those which have undesirable inclusions; indirectly, this polishing operation permits of eliminating the new layer where undesirable structural modifications have taken place, but on the other hand it has the very serious drawback of weakening the surface protection of the articles.
(c) The fact that the skin-annealing operation is carried out in a bath of boron salt causes boron to be introduced into the surface layers of the article, and this small amount of boron acts as a flux on the metal oxides, which is particularly undesirable.
(d) Articles having undergone the skin-annealing operation may become particularly sensitive to the type of corrosion which produces cracks in the metal of the articles, this kind of corrosion constituting a danger even for articles working at temperatures where there is only a negligible corrosion by oxidation and scaling.
(e) Articles having undergone a skin-annealing treatment generally have an unsatisfactory surface, even after cleaning thereof.
It is proposed elsewhere to perform such heating treatments of refractory articles at high temperatures (for instance 1050-1100 C.) in a neutral or reducing atmosphere containing at least one metal halide of high boiling point the metal of which diffuses into the article in treatment at this temperature. But such metal diffusions caused differences between the composition of the superficial layers of the article and that of the mass thereof and there are cases where such difierences are objectionable.
My invention relates to treatments including at least one operation during which the metalarticle (as defined hereinbefore) is treated at temperatures higher than 700 C. in a neutral or reducing atmosphere containing at least one fluoride of a metal component of the alloy of which the article is made having a boiling point higher than 700 C., and according to my invention, the conditions in which the operation is carried out and the composition of said atmosphere are so chosen as practically to prevent any superficial metal diffusion into the article.
The expression treatment operations during which the article is heated at temperatures higher than 700 C." includes, for instance, shaping treatments for refractory and stainless alloys, thermal treatments and, in particular, skin-annealing operations of refractory alloys.
For the sake of clarity, in the following description, I will call inert fluoride any fluoride which, in the conditions of the treatment operation, does not cause the formation of a superficial diffusion alloy into the article in treatment. Therefore the term ine fluoride: applies to the fluorides of the main components of the alloy, that is to say nickel and/ or cobalt, and also to ammonium and hydrogen fluorides. In opposition with this, an active fluoride is a metal fluoride which, in the conditions of the operation, causes its metal to diffuse to a substantial degree into the article to form in the superficial layers thereof, an alloy with the metal of the article.
My invention is concerned with the case where it sutfices to add to the neutral or reducing protective atmosphere in the treatment container one or several inert fluorides. As a matter of fact, it was found that some gaS turbine elements working at relatively moderate tem perature, but subjected ,to very'strong vibrations, give.
much more satisfactory results if no difference of composition and/ or of structure is created betweenthe mass of the element and the superficial layers thereof. The only condition to be complied with in this caseis that the treatment, for instance the skin-annealing treatment, must not result in a loss of chromium in the superficial layers of the elements.
In such cases, the protective atmosphere may be mainly constituted, for temperatures above 700 C., by one or several inert metal fluorides, and it must not include any metal fluoride capable of producing a diffusion of its metal into the article. As above stated, the metals=of said inert fluorides must be metals entering into the composition of the alloy, and in particular nickel and cobalt.
By way of indication, it is pointed out that aluminum fluoride causes diifusion of aluminum into the superficial layers of a refractory metal article, but to such a low degree that this fluoride may be classified either as an active fluoride or as an inert one.
The fluoride vapors which are to form the protective atmosphere in the treatment container are advantageously obtained by placing in said container elements which will be called sources of such a fluoride and which are located out of contact with the articles to be treated (said articles being, for instance, separated by grids from said sources).
When the container is heated, such a source gives off,
either directly or indirectly, the desired metal fluoride vapors. It may be constituted either by a so-called cementation product, requiring only the action of heat thereon to give off said metal fluoride vapors, or by a metal mass or a compound capable of giving 05 said metal fluoride vapors under the combined actions of heat and of other fluoride vapors evolved in another region of the container.
In the case of a metal mass, this metal is that of the fluoride to be obtained and the fluoride vapors acting thereon may be vapors of hydrofluoric acid. Such a metal is for instance used in addition toa cementation product located in another region of the treatment container- When said container is heated, the cementation product gives off vapors of the desired fluoride; .These vapors, upon coming into contact with the metal article, decompose into the Inetalof the fluoride, which diifuses steps taking place at different temperatures.
into the superficial layers of the article, and vapors of hydrofluoric acid, which come to attack the metal of the above mentioned mass, thus regenerating vapors of the metal fluoride. These vapors in turn come into contact with the article and decompose as above stated, and so on. In view of this operation, the metal mass is called regeneration mass.
By way of example, a cementation product may be constituted by the metal fluoride itself in the solid state (which disengages vapors under the efi'ect of heat), or by a mixture of components which, under the 'elfect of heat, react upon each other to produce such vapors. I may also make use of metal powders. which, when attacked by an ammonium fluoride or a hydrogen fluoride (or hydrofluoric acid), give 0d the desired fluoride vapors.
I may also use a metal mass placed in the treatment container in the vicinity of the article, but out of contact therewith, and which is attacked by suitably formed fluoride vapors whereby the desired metalfluoride is formed on the surface of said mass, this metal halide being vaporized by the action of heat to give oif the fluoride vapors of the protective atmosphere.
A certain amount of ammonium fluoride, introduced in the container, may serve to sweep the atmosphere thereof at the beginning of the treatment.
As above stated, the treatment operation during which the article is treated at temperatures higher than 700 C. may be a skin-annealing treatment. According to my invention, this treatment is preferably. performed in a purely gaseous phase, that is to say. without direct contact of the article with the source or sources of fluoride or fluorides. Advantageously, the article is separated from said sources by grids of a shape conforming as much as possible to that of the article and advantageously made of a metal (or of an alloy containing ametal) which is a main component of the alloy of the article.
In view of the good protection of the article against oxidation during the skin-annealing operation, this operation is advantageously carried out in two successive The temperature of the first step is higher than that at which skin-annealing is generally conducted, so as to permit of more efliciently bringing into solution some compounds which contribute to the structural hardening of the alloy, such as carbides and nitrides (temperature ranging from 1150 to 1200 C. for Nimonic and Nimonic alloys). The temperature during the second step is lower than that during the first step by about one hundred degrees, so as to obtain a dispersed precipitation of said components (temperature ranging from 1050 to 1100 C. for the above mentioned alloys), while maintaining in solution other purely metallic structural hardening compounds, such as Ni TiAl, which precipitate in controlled fashion during the final annealing.
As a .rule, it is advantageous to heat up as quickly as possible the treatment container and the parts present therein (at least for temperatures higher than that.
at which precipitation can begin) so that the heating at homogenizing temperature takes place after not too long a period during which the conditions are not well defined and dangerous from a structural point of view. Also, all the portions of the .article must be constantly at the same temperature, or approximately so.
For this purpose, the skin-annealing treatment ispreferably performed in boxes which are small or at least one dimension of which is small (flat boxes or boxes limiting a volume in the form of an annular cylindrical space).
This heating is advantageously performed in powerful furnaces in an atmosphere of hydrogen so as to obtain a conductivity of heat as high as possible.
According to the nature of. the alloy and to the shape and mass of the articles, cooling of the boxes is accelerated by circulation of air or by immersion in a liquid. In
any case, it is advantageous to cool down the bottom of the container so as to trap the fluoride vapors and to prevent their condensation on the articles in treatment.
When, according to my invention, skin-annealing is conducted in an inert protective atmosphere, it is advantageous to provide in this atmosphere one or several of the following fluoride compounds: nickel fluoride, cobalt fluoride, ammonium fluoride, hydrofluoric acid. However, precautions must be taken to obtain a protective atmosphere which lasts during the whole time of the treatment. As a matter of fact, due to their high volatility, ammonium fluoride and hydrofluoric acid can exert their protective function only if they are being evolved continuously or if they are accompanied by a halide having a high boiling point and of a substantial vapor tension. This is the case in particular of nickel fluoride (boiling point 1025 C.) which may be obtained from the corresponding ammonium or hydrogen fluorides.
If the thermal treatments which are considered require temperatures higher than 1200 C., I may make use of other fluorides having a higher boiling point, such as cobalt fluoride (boiling point 1300 C.).
I obtain very good results by performing the skinannealing treatment of Nimonic articles in the presence of nickel fluoride (which may be formed by heating a fine nickel powder with ammonium fluoride) with a small amount of ammonium fluoride which drives off the air in the container at the beginning of the heating operation, or with ammonium fluoride alone if itsvapors are made to form nickel fluoride by attacking a mass of nickel placed in the treatment container close to the article but out of contact therewith. This mass may be constituted by small lumps of nickel of suitable size or by nickel grids surrounding the articles. This formation of nickel fluoride during the skin-annealing operation may even be obtained by reaction of ammonium fluoride or hydrofluoric acid on the metal of the Nimonic article itself, which forms on said article a protective layer of nickel fluoride which volatilizes at high temperature.
In the course of a special operation, I may reduce the proportion of titanium and aluminum from the superficial layers of Nimonic articles, before the skin-annealing operation, by performing a controlled oxidation for some hours at 700-750 C., without subsequent scouring. The efliect of this operation is superficially to soften the alloy by lowering the proportion of titanium and aluminum therein.
When the atmosphere does not contain ammonium fluoride, the slight oxidation which takes place during the period before the vaporizing of the nickel automatically produces such a superficial softening. According to my invention, it is necessary to avoid the formation of undesirable fluorides inside the treatment container. As a rule, such undesirable fluorides are fluorides of metals which are not included in the composition of the alloy and which might give rise to the formation of undesirable superficial diffusion alloys.
Thus, it is necessary to prevent the introduction or the formation of iron, vanadium, and boron fluorides, Such fluorides diffuse superficially into nickel and/ or cobalt in a fluoride vapor atmosphere, in the same manner as chromium diffuses into iron articles. It is therefore preferable to avoid the presence, inside the treatment container, of iron or any alloy incorporating iron, because the protective nickel or cobalt fluorides which are normally included in the atmosphere of the container might give, by reaction with iron, corresponding iron fluorides which would soil the superficial layers of the article. Therefore the treatment container will be preferably made of the main component metal or one of the main component metals of the alloy of which the article is made, with the exception of chromium, or, alternately, this container will be coated or lined with such a metal or metals. If for some reasons, for instance of economy or mechanical resistance, it is however desired to use containers or accessories which contain iron, any noxious effects on the alloy may be avoided by surrounding the iron parts or the article to be treated with means (such as nickel grids for instance) through which the iron fluoride vapors must pass before reaching the articles to be treated.
I will now describe some examples of treatments made, according to my invention, in cementation boxes provided with partly gastight covers, said boxes being heated in an electric furnace, preferably in an atmosphere of hydrogen or containing hydrogen, for instance of cracked ammonia. Heating up is conducted as quickly as possible, and in the case of a furnace where the temperature would rise slowly from 700 to 1000 C., it would be necessary to increase the duration of the skin-annealing operation. The treatment boxes I used were made of iron but their inner walls were lined with nickel sheets. When the boxes were withdrawn from the furnace, their bottom was placed in a vessel containing water so as to condense any fluorides carried along by them and they were covered with a hood into which a stream of hydrogen was supplied so as to prevent the inflow of air during the cooling period. Finally the whole box was placed under a fan in order to obtain a quick cooling of the treatment container, at least down to the temperature of 700 C.
Example 1 Turbine blades made of Nimonic were skin-annealed with the use of a cementation substance consisting of nickel fluoride and ammonium fluoride obtained by preliminary heating of ammonium fluoride and nickel powder. The articles were placed without separation in the boxes and treated for 1 hour at 1060 C. After this treatment, the articles were of a very bright light grey.
Analogous results were obtained by placing in the boxes a certain amount of ammonium fluoride, the articles being placed in nickel grids surrounding them, whereby the protective nickel fluoride was formed by the vapors of ammonium fluoride acting on said grids.
Example 2 Two turbine blades made of Nimonic 95 were skinannealed by being placed in a diluting mass consisting of thorium or zirconium oxide. The metal fluoride to be formed in the container was obtained from acid fluoride of ammonium to which may be added a small amount of nickel fluoride. In order to compensate for the relatively slow heating in this case, the duration of the heating at the temperature of 1080 C. was 40 minutes,
Example 3 A turbine wheel made of Nimonic 80 was skin-annealed under conditions similar to those of the preceding example, with the exception that the diluting substance is titanium oxide. Due to the size of the article, and therefore of the treatment box (350 mm. of diameter and mm. of height), the thermal treatment was carried out as follows:
Heating up, from 700 to 1050 C 1 h. 30 minutes. Heating at 1050 C 40 minutes. Cooling, from 1050 to 700 C 35 minutes.
During the cooling operation, the box was placed under a hood fed with hydrogen, and cooled by atomized water.
Example 4 Gas turbine blades of an alloy of nickel-cobalt-chrornium-titanium-aluminum and molybdenum were skin-annealed for 20 minutes at a temperature of 1080 C. without any material chromiziug in a reducing atmosphere consisting of directly cracked ammonia in a closed partly gastight box of ordinary steel which contains at the bottom thereof a mixture of chromium or fe'rrochromium (in granular form) with ammonium fluoride either acid or neutral, the amount of this fluoride being about 2 grams per liter. The articles in the box are kept out of contact with the above mentioned mixture by a nickel grid. In
7 order to prevent diffusion of chromium into the pieces, said pieces are surrounded by an envelope of nickel wire gauze (mesh of about 1.2 mm.; thickness of wire 0.3 'mm.; two layers of gauze).
Example The pieces to be treated are the same as in the preceding example and the conditions of treatment are similar but, in this case, in order to prevent diffusion of chromium into the pieces, instead of enveloping these pieces in a nickel wire gauze, the mixture intended to produce the fluoride vapors, instead of consisting of ammonium fluoride and chromium is a mixture of neutral ammonium fluoride with nickel powder and iron powder.
Example 6 Turbine combustion chambers made of stainless steel containing 20% nickel and 25% chromium had been assembled by welding individual elements. To eliminate stresses in the assembly and to deoxidize the welded zones, the chambers were placed in a closed partly gastight box of ordinary steel'which contained, at the bottom thereof, amixture of chromium or ferrochromium (in granular form) with ammonium fluoride (either acid or neutral), the amount of this fluoride being about 2 grams per liter, the chambers being separated from the mixture by a nickel grid. The box was heated in a reducing atmosphere. consisting of directly cracked ammonia, for about one hour at a temperature of 1100-1120" C., during which the mixture of chromium and ammonium fluoride evolved chromium fluoride vapors. In order to prevent diffusion of chromium from these vapors into the articles in treatment, said articles were surrounded, either individually. oras a whole, by an envelope of nickelwire gauze (mesh of about 1.2 mm.; thickness of wire 0.3 mm.; two layers of gauze). This nickel envelope serves, by causing chromium to diffuse into its surface, to prevent chromizing of the articles in treatment. After the annealing operation, the box is cooled outside of the treatment oven in an atmosphere of reducing gas.
Example 7 Similar stainless steel articles were treated as in Example 6 except diffusion of chromium into the articles was prevented without nickel wire gauze but by producing the fluoride vapors from a mixture of neutral ammonium fluoride with nickel powder and iron powders. The articles after treatment have not the appearance of polished chromium but a light gray bright silvered appearance.
Example 8 Sheets of stainless steel containing 25% of chromium and 20% of nickel were annealed between two rolling operations to improve the aptitude of the sheets to being stamped either in the hot or cold states. The sheets were placed in a partly gastight closed box of ordinary steel which contains, at the bottom thereof, a mixture of nickel and iron (in powder form) with ammonium fluoride, the amount of this fluoride being about 2.5 grams per liter. The sheets are placed vertically in the boxwith small amounts of ammonium fluoride placed in the intervals between said sheets, these sheets resting upon a nickel grid which keeps them out of contact with the above mentioned mixture. The box ,was heated in a reducing atmosphere consisting of directly cracked ammonium for about half'an hour at a temperature of 10801100 C., after which the boxes were cooled on the, outside of the annealing oven in a reducing gas atmosphere. The sheets obtained after this treatment have an exceptional aptitude to being stamped either in the cold or hot state. This is due to the fact that the annealing operation has been performed without any possibility of oxidizing and also that the surface of the sheet has been softened (elimination of any inclusion or of carbon in this surface over a depth of some tenths of a micron).
What I claim is:
1. The method which comprises heating for a time ranging from five minutes to five hours, in a closed vessel, at a temperature between 700 C. and 1100", C., a solid body of an alloy of the group consisting of chromiumnickel stainless steels, of nickel basechromium containing heat resisting alloys, and of cobalt base chromium containing heat resisting alloys, in the presence of hydrogen andvapors of a fluoride of the group consisting of nickel fluoride and cobalt fluoride, said fluoride ,being nickel fluoride when said solid body contains nickel and cobalt fluoride when said solid body contains cobalt.
2. The method according to claim-1 wherein the heating takes place for a time ranging from half an hour to one hour.
3. The method which-comprises placing in. a box, on the one hand, a solid body of an alloy ofthe group consisting of chromium-nickel stainless steels and nickel base chromiumcontaining heat resisting alloys, and, on the other hand, a cementation product capable, upon heating, of producing nickel fiuoride,'said body and said cementation product being out of contact with each other, closing said box while permitting hydrogen to enter it and heating the whole to a temperature of 7001100 C. for a time ranging from five minutes to five hours.
4. The method according to claim 3 wherein the heat ing takes place .for a time ranging from half an hour to one hour. a
5. The method which comprises placing in one chamber of a box divided into two chambers by a grid, a solid body of an alloy of the group consisting of chromium-nickel stainless steels and nickel base chromium containing heat resisting alloys, placing in the other of said chambers acementation productcontaining ammonium fluoride and nickel powder, closing said box while permitting hydrogen to enter it, and heating said box to a temperature of 700- 1100 C. for a time ranging from five minutes to five hours.
6. The method according to claim 5 wherein the heating takes place for a time ranging from half an hour to one hour.
7. The method of claim 5 wherein said cementation product further contains iron powder. r
8. The method according to claim 5 wherein said article is placedin said first mentioned chamber in a diluting mass of at least one body of the group consisting of thorium oxide, zirconium oxide and lithium oxide.
9. The method which comprises placing in one chamber of a box divided into two chambers by a grid, a solid body of an alloy of the group consisting of chromium nickel stainless steels and nickel base chromium containing heat-resisting alloys, said body being surrounded by a nickel wire gauze, placing in the other of said chambers a cementation product containing a cementation product capable, when heated at a temperature of 700-1100 C., of giving off metal fluoride vapors little volatile at this temperature, closing said box while permitting hydrogen to enter it, and heating said box to a temperature of 700- 1100" C. for a time ranging from five minutes to five hours.
10. The method according to claim 9 wherein said cementation productcontains chromiumso as to give off chromium fluoride vapors which are transformed'by said nickel wire gauze into nickel fluoride.
11. The method according to claim 9 wherein said cementation product consists chiefly of chromium and ammonium fluoride. v
12. The method which comprises placing in one chamber of a box divided into two chambersby a grid, a solid body of an alloy of the group consisting of cobalt and a temperature of 700-1100 C. for a time ranging from five minutes to five hours.
13. The method which comprises placing in one chamber of a box divided into two chambers by a grid, a solid body of an alloy of the group consisting of cobalt and nickel base chromium containing heat resisting alloys, placing in the other of said chambers a cementation prod- -uct containing ammonium fluoride and cobalt powder, closing said box while permitting hydrogen to enter it, and heating said box to a temperature of 700-1100 C. for a time ranging from five minutes to five hours.
14. The method according to claim 13 wherein the heating takes place for a time ranging from half an hour to one hour.
References Cited by the Examiner UNITED STATES PATENTS 1,497,417 6/ 1924 Weber 117107.2 1,642,348 9/ 1927 Williams et al 75-224 X 1,770,177 7/ 1930 Martin 117-1072 1,902,503 3/1933 Howe 117-107 2,046,638 7/ 1936 Lauenstein ct a1. 117-130 2,181,095 11/1939 Ness 148-16.7 X 2,199,418 5/ 1940 Redmond l486 2,257,668 9/1941 Becker et a1 117-107 Daeves 117-130 Schlesinger et a1 148-16 Rice et a1 148-16.7 X Edson et a1 148-167 X Moore et a1. 148-26 X Wainer 75-222 X Gonser et a1 75-84 Goetzel 75-208 X Roush 148-27 X Spence 158-14 Spendelow et al 148-16 Wainer et a1 75-845 Galmiche 148-16 Benski 252-1816 FOREIGN PATENTS Great Britain.
OTHER REFERENCES Revue de Metallurgie, vol. 51, No. 7, July 1954, pp.
ALFRED L. LEAVITT, Primary Examiner.
RICHARD D. NEVIUS, A. GOLIAN,
Assistant Examiners.
Claims (1)
1. THE METHOD WHICH COMPRISES HEATING, FOR A TIME RANGING FROM A FIVE MINUTES TO FIVE HOURS, IN A CLOSED VESSEL, AT A TEMPERATURE BETWEEN 700*C. AND 1100*C., A SOLID BODY OF AN ALLOY OF THE GROUP CONSISTING OF CHROMIUMNICKEL STAINLESS STEELS, OF NICKEL BASE CHROMIUM CONTAINING HEAT RESISTING ALLOYS, AND OF COBALT BASE CHROMIUM CONTAINING HEAT RESISTING ALLOYS, IN THE PRESENCE OF HYDROGEN AND VAPORS OF A FLUORIDE OF THE GROUP CONSISTING OF NICKEL FLUORIDE AND COBALT FLUORIDE, SAID FLUORIDE BEING NICKEL FLUORIDE WHEN SAID SOLID BODY CONTAINS NICKEL AND COBALT FLUORIDE WHEN SAID SOLID CONTAINS COBALT.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR642305 | 1953-02-04 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3276903A true US3276903A (en) | 1966-10-04 |
Family
ID=8697335
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US438788A Expired - Lifetime US3276903A (en) | 1953-02-04 | 1965-03-10 | Heat treatment of metals |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3276903A (en) |
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|---|---|---|---|---|
| US3753758A (en) * | 1970-09-15 | 1973-08-21 | Nat Steel Corp | Open pack heat treatment of metal sheet material using sized particles as spacing means |
| US4005698A (en) * | 1974-10-18 | 1977-02-01 | International Business Machines Corporation | Photon energy converter |
| US4698244A (en) * | 1985-10-31 | 1987-10-06 | Air Products And Chemicals, Inc. | Deposition of titanium aluminides |
| US4835010A (en) * | 1987-06-08 | 1989-05-30 | Exxon Research And Engineering Company | Aluminide dispersed ferrite diffusion coating on austenitic stainless steel substrates |
| US4965095A (en) * | 1979-03-30 | 1990-10-23 | Alloy Surfaces Company, Inc. | Method for refurbishing used jet engine hot section airfoils |
| US5217757A (en) * | 1986-11-03 | 1993-06-08 | United Technologies Corporation | Method for applying aluminide coatings to superalloys |
| US6361836B1 (en) * | 1999-12-09 | 2002-03-26 | Johns Manville International, Inc. | Method of making spinner discs for rotary fiberization processes |
| US7146990B1 (en) * | 2005-07-26 | 2006-12-12 | Chromalloy Gas Turbine Corporation | Process for repairing sulfidation damaged turbine components |
| US20140076470A1 (en) * | 2011-05-12 | 2014-03-20 | Kangying Zhu | Method for the production of very high strength martensitic steel and sheet or part thus obtained |
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| US4698244A (en) * | 1985-10-31 | 1987-10-06 | Air Products And Chemicals, Inc. | Deposition of titanium aluminides |
| US5217757A (en) * | 1986-11-03 | 1993-06-08 | United Technologies Corporation | Method for applying aluminide coatings to superalloys |
| US4835010A (en) * | 1987-06-08 | 1989-05-30 | Exxon Research And Engineering Company | Aluminide dispersed ferrite diffusion coating on austenitic stainless steel substrates |
| US6361836B1 (en) * | 1999-12-09 | 2002-03-26 | Johns Manville International, Inc. | Method of making spinner discs for rotary fiberization processes |
| US7146990B1 (en) * | 2005-07-26 | 2006-12-12 | Chromalloy Gas Turbine Corporation | Process for repairing sulfidation damaged turbine components |
| US20140076470A1 (en) * | 2011-05-12 | 2014-03-20 | Kangying Zhu | Method for the production of very high strength martensitic steel and sheet or part thus obtained |
| US10337090B2 (en) * | 2011-05-12 | 2019-07-02 | Arcelormittal Investigaciòn Y Desarrollo, S.L. | Method for the production of very high strength martensitic steel and sheet or part thus obtained |
| US10895003B2 (en) | 2011-05-12 | 2021-01-19 | Arcelormittal | Very high strength martensitic steel or part and method of fabrication |
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