DE60008116D1 - Superlegierung mit optimiertem Hochtemperaturwirkungsgrad in Hochdruckturbinenscheiben - Google Patents

Superlegierung mit optimiertem Hochtemperaturwirkungsgrad in Hochdruckturbinenscheiben

Info

Publication number
DE60008116D1
DE60008116D1 DE60008116T DE60008116T DE60008116D1 DE 60008116 D1 DE60008116 D1 DE 60008116D1 DE 60008116 T DE60008116 T DE 60008116T DE 60008116 T DE60008116 T DE 60008116T DE 60008116 D1 DE60008116 D1 DE 60008116D1
Authority
DE
Germany
Prior art keywords
superalloy
pressure turbine
temperature efficiency
turbine disks
optimized
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE60008116T
Other languages
English (en)
Other versions
DE60008116T2 (de
Inventor
David Paul Mourer
Eric Scott Huron
Kenneth Rees Bain
Enrique Edgar Montero
Paul Leray Reynolds
John Joseph Schirra
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE60008116D1 publication Critical patent/DE60008116D1/de
Publication of DE60008116T2 publication Critical patent/DE60008116T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/04—Making non-ferrous alloys by powder metallurgy
    • C22C1/0433—Nickel- or cobalt-based alloys
    • C22C1/0441—Alloys based on intermetallic compounds of the type rare earth - Co, Ni
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/03—Alloys based on nickel or cobalt based on nickel
    • C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/056—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/03—Alloys based on nickel or cobalt based on nickel
    • C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/057—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being less 10%
    • 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
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24—After-treatment of workpieces or articles
    • B22F2003/248—Thermal after-treatment
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
    • B22F2998/10—Processes characterised by the sequence of their steps

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Powder Metallurgy (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE2000608116 2000-09-29 2000-09-29 Superlegierung mit optimiertem Hochtemperatur-Leistungsvermögen in Hochdruck-Turbinenscheiben Expired - Lifetime DE60008116T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP20000308571 EP1201777B1 (de) 2000-09-29 2000-09-29 Superlegierung mit optimiertem Hochtemperaturwirkungsgrad in Hochdruckturbinenscheiben

Publications (2)

Publication Number Publication Date
DE60008116D1 true DE60008116D1 (de) 2004-03-11
DE60008116T2 DE60008116T2 (de) 2004-09-16

Family

ID=8173294

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2000608116 Expired - Lifetime DE60008116T2 (de) 2000-09-29 2000-09-29 Superlegierung mit optimiertem Hochtemperatur-Leistungsvermögen in Hochdruck-Turbinenscheiben

Country Status (2)

Country Link
EP (1) EP1201777B1 (de)
DE (1) DE60008116T2 (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6974508B1 (en) 2002-10-29 2005-12-13 The United States Of America As Represented By The United States National Aeronautics And Space Administration Nickel base superalloy turbine disk
US7138020B2 (en) * 2003-10-15 2006-11-21 General Electric Company Method for reducing heat treatment residual stresses in super-solvus solutioned nickel-base superalloy articles
US20100008790A1 (en) 2005-03-30 2010-01-14 United Technologies Corporation Superalloy compositions, articles, and methods of manufacture
US7708846B2 (en) 2005-11-28 2010-05-04 United Technologies Corporation Superalloy stabilization
US20070141374A1 (en) * 2005-12-19 2007-06-21 General Electric Company Environmentally resistant disk
US7553384B2 (en) * 2006-01-25 2009-06-30 General Electric Company Local heat treatment for improved fatigue resistance in turbine components
US9783873B2 (en) 2012-02-14 2017-10-10 United Technologies Corporation Superalloy compositions, articles, and methods of manufacture
US9752215B2 (en) 2012-02-14 2017-09-05 United Technologies Corporation Superalloy compositions, articles, and methods of manufacture
CN103341586B (zh) * 2013-06-07 2015-07-22 中国石油天然气集团公司 一种实现gh4738镍基高温合金涡轮盘成形方法
GB201400352D0 (en) 2014-01-09 2014-02-26 Rolls Royce Plc A nickel based alloy composition
EP3042973B1 (de) 2015-01-07 2017-08-16 Rolls-Royce plc Nickellegierung
GB2539957B (en) 2015-07-03 2017-12-27 Rolls Royce Plc A nickel-base superalloy
US20170291265A1 (en) 2016-04-11 2017-10-12 United Technologies Corporation Braze material for hybrid structures
US10718041B2 (en) 2017-06-26 2020-07-21 Raytheon Technologies Corporation Solid-state welding of coarse grain powder metallurgy nickel-based superalloys
US20190063256A1 (en) * 2017-08-31 2019-02-28 United Technologies Corporation High yield strength nickel alloy with augmented precipitation hardening
GB202015106D0 (en) * 2020-08-20 2020-11-11 Rolls Royce Plc Alloy
CN112981186B (zh) * 2021-04-22 2021-08-24 北京钢研高纳科技股份有限公司 低层错能的高温合金、结构件及其应用
CN114672696B (zh) * 2022-03-21 2023-03-14 钢铁研究总院有限公司 一种Ni-Co基高温合金及其制备方法和应用

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2593830B1 (fr) * 1986-02-06 1988-04-08 Snecma Superalliage a matrice a base de nickel notamment elabore en metallurgie des poudres et disque de turbomachine constitue en cet alliage
US4769087A (en) * 1986-06-02 1988-09-06 United Technologies Corporation Nickel base superalloy articles and method for making
US5143563A (en) * 1989-10-04 1992-09-01 General Electric Company Creep, stress rupture and hold-time fatigue crack resistant alloys

Also Published As

Publication number Publication date
EP1201777A1 (de) 2002-05-02
DE60008116T2 (de) 2004-09-16
EP1201777B1 (de) 2004-02-04

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: ROEGER UND KOLLEGEN, 73728 ESSLINGEN