JPS5582757A - Preparing complex crystal structure within nickel based superalloy material member - Google Patents

Preparing complex crystal structure within nickel based superalloy material member

Info

Publication number
JPS5582757A
JPS5582757A JP16170579A JP16170579A JPS5582757A JP S5582757 A JPS5582757 A JP S5582757A JP 16170579 A JP16170579 A JP 16170579A JP 16170579 A JP16170579 A JP 16170579A JP S5582757 A JPS5582757 A JP S5582757A
Authority
JP
Japan
Prior art keywords
crystal structure
material member
based superalloy
nickel based
complex crystal
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP16170579A
Other languages
Japanese (ja)
Other versions
JPS6344816B2 (en
Inventor
Arufuretsudo Kuromubii Edouin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of JPS5582757A publication Critical patent/JPS5582757A/en
Publication of JPS6344816B2 publication Critical patent/JPS6344816B2/ja
Granted legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/10Changing 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
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C8/04Treatment of selected surface areas, e.g. using masks
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/005Selecting particular materials
JP16170579A 1978-12-15 1979-12-14 Preparing complex crystal structure within nickel based superalloy material member Granted JPS5582757A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US97004778A 1978-12-15 1978-12-15

Publications (2)

Publication Number Publication Date
JPS5582757A true JPS5582757A (en) 1980-06-21
JPS6344816B2 JPS6344816B2 (en) 1988-09-07

Family

ID=25516358

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16170579A Granted JPS5582757A (en) 1978-12-15 1979-12-14 Preparing complex crystal structure within nickel based superalloy material member

Country Status (9)

Country Link
JP (1) JPS5582757A (en)
BE (1) BE880645A (en)
CA (1) CA1133366A (en)
CH (1) CH648866A5 (en)
DE (1) DE2949673A1 (en)
FR (1) FR2444086A1 (en)
GB (1) GB2043116A (en)
IT (1) IT1126062B (en)
NL (1) NL7908902A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0196447B1 (en) * 1985-03-15 1989-08-09 BBC Brown Boveri AG Process for enhancing the oxidation and corrosion resistance of a component made from a dispersion-hardened superalloy by means of a surface treatment
EP0214080A3 (en) * 1985-08-16 1987-11-25 United Technologies Corporation Reduction of twinning in directional recrystallization of nickel base superalloys
JP6685800B2 (en) 2016-03-31 2020-04-22 三菱重工業株式会社 Turbine blade design method, turbine blade manufacturing method, and turbine blade

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1127157A (en) * 1966-06-13 1968-09-11 Orenda Ltd Method for improving the fatigue resistance of turbine blades
FR1528328A (en) * 1966-06-21 1968-06-07 Int Nickel Ltd Refining of metal grain
US3597286A (en) * 1968-02-23 1971-08-03 Westinghouse Electric Corp Method of treating a high strength high ductility iron-cobalt alloy
US3741821A (en) * 1971-05-10 1973-06-26 United Aircraft Corp Processing for integral gas turbine disc/blade component
US4078951A (en) * 1976-03-31 1978-03-14 University Patents, Inc. Method of improving fatigue life of cast nickel based superalloys and composition
US4093476A (en) * 1976-12-22 1978-06-06 Special Metals Corporation Nickel base alloy

Also Published As

Publication number Publication date
BE880645A (en) 1980-06-16
FR2444086A1 (en) 1980-07-11
DE2949673C2 (en) 1989-06-22
NL7908902A (en) 1980-06-17
IT7941681A0 (en) 1979-12-14
JPS6344816B2 (en) 1988-09-07
GB2043116A (en) 1980-10-01
IT1126062B (en) 1986-05-14
CH648866A5 (en) 1985-04-15
DE2949673A1 (en) 1980-06-26
CA1133366A (en) 1982-10-12

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