BE901250A - Procede de forgeage de matiere en superalliage a base de nickel de haute resistance, en particulier sous forme moulee. - Google Patents

Procede de forgeage de matiere en superalliage a base de nickel de haute resistance, en particulier sous forme moulee.

Info

Publication number
BE901250A
BE901250A BE0/214146A BE214146A BE901250A BE 901250 A BE901250 A BE 901250A BE 0/214146 A BE0/214146 A BE 0/214146A BE 214146 A BE214146 A BE 214146A BE 901250 A BE901250 A BE 901250A
Authority
BE
Belgium
Prior art keywords
forging process
based superalloy
molded form
superalloy material
strength nickel
Prior art date
Application number
BE0/214146A
Other languages
English (en)
Inventor
D F Paulonis
D R Malley
E E Brown
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Publication of BE901250A publication Critical patent/BE901250A/fr

Links

Classifications

    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K1/00—Making machine elements
    • B21K1/28—Making machine elements wheels; discs
    • B21K1/32—Making machine elements wheels; discs discs, e.g. disc wheels

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Forging (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Inorganic Compounds Of Heavy Metals (AREA)

Abstract

Le procédé consiste à survieillir la matière pour produire une répartition de phase gamma prime à gros grains et sousmettre l'alliage à un forgeage isothermique de la matière survieillie. L'invention est, par exemple, utilisable pour la farication de disques de moteurs à turbine à gaz.
BE0/214146A 1983-12-27 1984-12-11 Procede de forgeage de matiere en superalliage a base de nickel de haute resistance, en particulier sous forme moulee. BE901250A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/565,487 US4579602A (en) 1983-12-27 1983-12-27 Forging process for superalloys

Publications (1)

Publication Number Publication Date
BE901250A true BE901250A (fr) 1985-03-29

Family

ID=24258825

Family Applications (1)

Application Number Title Priority Date Filing Date
BE0/214146A BE901250A (fr) 1983-12-27 1984-12-11 Procede de forgeage de matiere en superalliage a base de nickel de haute resistance, en particulier sous forme moulee.

Country Status (14)

Country Link
US (1) US4579602A (fr)
JP (1) JPS60170548A (fr)
BE (1) BE901250A (fr)
CA (1) CA1229004A (fr)
CH (1) CH665145A5 (fr)
DE (1) DE3445768A1 (fr)
DK (1) DK162942C (fr)
FR (1) FR2557147B1 (fr)
GB (1) GB2151951B (fr)
IL (1) IL73865A (fr)
IT (1) IT1181942B (fr)
NL (1) NL8403732A (fr)
NO (1) NO165930C (fr)
SE (1) SE462103B (fr)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5328659A (en) * 1982-10-15 1994-07-12 United Technologies Corporation Superalloy heat treatment for promoting crack growth resistance
US4608094A (en) * 1984-12-18 1986-08-26 United Technologies Corporation Method of producing turbine disks
US4769087A (en) * 1986-06-02 1988-09-06 United Technologies Corporation Nickel base superalloy articles and method for making
US5169463A (en) * 1987-10-19 1992-12-08 Sps Technologies, Inc. Alloys containing gamma prime phase and particles and process for forming same
US4908069A (en) * 1987-10-19 1990-03-13 Sps Technologies, Inc. Alloys containing gamma prime phase and process for forming same
US4803880A (en) * 1987-12-21 1989-02-14 United Technologies Corporation Hollow article forging process
US4820356A (en) * 1987-12-24 1989-04-11 United Technologies Corporation Heat treatment for improving fatigue properties of superalloy articles
US4877461A (en) * 1988-09-09 1989-10-31 Inco Alloys International, Inc. Nickel-base alloy
US5100050A (en) * 1989-10-04 1992-03-31 General Electric Company Method of manufacturing dual alloy turbine disks
US5161950A (en) * 1989-10-04 1992-11-10 General Electric Company Dual alloy turbine disk
US5693159A (en) * 1991-04-15 1997-12-02 United Technologies Corporation Superalloy forging process
EP0533914B1 (fr) * 1991-04-15 1997-03-12 United Technologies Corporation Procede de forgeage de superalliages et composition connexe
US5120373A (en) * 1991-04-15 1992-06-09 United Technologies Corporation Superalloy forging process
GB9217194D0 (en) * 1992-08-13 1992-09-23 Univ Reading The Forming of workpieces
US5328530A (en) * 1993-06-07 1994-07-12 The United States Of America As Represented By The Secretary Of The Air Force Hot forging of coarse grain alloys
US5593519A (en) * 1994-07-07 1997-01-14 General Electric Company Supersolvus forging of ni-base superalloys
US5547523A (en) * 1995-01-03 1996-08-20 General Electric Company Retained strain forging of ni-base superalloys
US6059904A (en) * 1995-04-27 2000-05-09 General Electric Company Isothermal and high retained strain forging of Ni-base superalloys
EP1390167B1 (fr) 2001-05-15 2006-09-27 Santoku Corporation Procede de coulee d'alliages dans des moules en graphite isotrope
US6705385B2 (en) 2001-05-23 2004-03-16 Santoku America, Inc. Castings of metallic alloys with improved surface quality, structural integrity and mechanical properties fabricated in anisotropic pyrolytic graphite molds under vacuum
EP1414604B1 (fr) 2001-06-11 2007-04-25 Santoku America, Inc. Coulee par centrifugation de superalliages a base de nickel a qualite de surface, integrite et proprietes mecaniques ameliorees dans des modules en graphite isotropes sous vide
US6755239B2 (en) 2001-06-11 2004-06-29 Santoku America, Inc. Centrifugal casting of titanium alloys with improved surface quality, structural integrity and mechanical properties in isotropic graphite molds under vacuum
US6799627B2 (en) 2002-06-10 2004-10-05 Santoku America, Inc. Castings of metallic alloys with improved surface quality, structural integrity and mechanical properties fabricated in titanium carbide coated graphite molds under vacuum
EP1428897A1 (fr) * 2002-12-10 2004-06-16 Siemens Aktiengesellschaft Méthode de fabrication d'un composant en alliage à soudabilité et/ou formabilité améliorée
US6986381B2 (en) * 2003-07-23 2006-01-17 Santoku America, Inc. Castings of metallic alloys with improved surface quality, structural integrity and mechanical properties fabricated in refractory metals and refractory metal carbides coated graphite molds under vacuum
US7449075B2 (en) * 2004-06-28 2008-11-11 General Electric Company Method for producing a beta-processed alpha-beta titanium-alloy article
US7553384B2 (en) * 2006-01-25 2009-06-30 General Electric Company Local heat treatment for improved fatigue resistance in turbine components
US20100037994A1 (en) * 2008-08-14 2010-02-18 Gopal Das Method of processing maraging steel
US8313593B2 (en) * 2009-09-15 2012-11-20 General Electric Company Method of heat treating a Ni-based superalloy article and article made thereby
US20120051919A1 (en) * 2010-08-31 2012-03-01 General Electric Company Powder compact rotor forging preform and forged powder compact turbine rotor and methods of making the same
WO2012063879A1 (fr) * 2010-11-10 2012-05-18 本田技研工業株式会社 Alliage de nickel
US10309232B2 (en) * 2012-02-29 2019-06-04 United Technologies Corporation Gas turbine engine with stage dependent material selection for blades and disk
US10718041B2 (en) 2017-06-26 2020-07-21 Raytheon Technologies Corporation Solid-state welding of coarse grain powder metallurgy nickel-based superalloys

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2798827A (en) * 1956-05-07 1957-07-09 Gen Motors Corp Method of casting and heat treating nickel base alloys
GB1253755A (en) * 1968-07-19 1971-11-17 United Aircraft Corp Method to improve the weldability and formability of nickel-base superalloys by heat treatment
US3649379A (en) * 1969-06-20 1972-03-14 Cabot Corp Co-precipitation-strengthened nickel base alloys and method for producing same
BE756653A (fr) * 1969-09-26 1971-03-01 United Aircraft Corp Accroissement thermo-mecanique de la resistance des superalliages (
BE756652A (fr) * 1969-09-26 1971-03-01 United Aircraft Corp Superalliages contenant des phases precipitees topologiquement d'assemblage serre
US3677830A (en) * 1970-02-26 1972-07-18 United Aircraft Corp Processing of the precipitation hardening nickel-base superalloys
US3676225A (en) * 1970-06-25 1972-07-11 United Aircraft Corp Thermomechanical processing of intermediate service temperature nickel-base superalloys
US3753790A (en) * 1972-08-02 1973-08-21 Gen Electric Heat treatment to dissolve low melting phases in superalloys
US3975219A (en) * 1975-09-02 1976-08-17 United Technologies Corporation Thermomechanical treatment for nickel base superalloys
US4328045A (en) * 1978-12-26 1982-05-04 United Technologies Corporation Heat treated single crystal articles and process

Also Published As

Publication number Publication date
DK162942C (da) 1992-05-25
JPS6362584B2 (fr) 1988-12-02
IL73865A (en) 1987-09-16
GB2151951B (en) 1987-03-25
IT8424262A1 (it) 1986-06-27
DE3445768C2 (fr) 1992-04-23
JPS60170548A (ja) 1985-09-04
SE462103B (sv) 1990-05-07
CH665145A5 (de) 1988-04-29
GB2151951A (en) 1985-07-31
FR2557147B1 (fr) 1987-07-17
DK609584A (da) 1985-06-28
FR2557147A1 (fr) 1985-06-28
US4579602A (en) 1986-04-01
SE8406445D0 (sv) 1984-12-18
DK609584D0 (da) 1984-12-19
CA1229004A (fr) 1987-11-10
DE3445768A1 (de) 1985-07-04
NL8403732A (nl) 1985-07-16
NO165930B (no) 1991-01-21
IT1181942B (it) 1987-09-30
SE8406445L (sv) 1985-06-28
IT8424262A0 (it) 1984-12-27
NO845117L (no) 1985-06-28
DK162942B (da) 1991-12-30
GB8431277D0 (en) 1985-01-23
NO165930C (no) 1991-05-02
IL73865A0 (en) 1985-03-31

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Legal Events

Date Code Title Description
RE Patent lapsed

Owner name: UNITED TECHNOLOGIES CORP.

Effective date: 19921231