GB1318267A - Superalloys incorporating precipitated topologically close-packed phases - Google Patents

Superalloys incorporating precipitated topologically close-packed phases

Info

Publication number
GB1318267A
GB1318267A GB4232670A GB4232670A GB1318267A GB 1318267 A GB1318267 A GB 1318267A GB 4232670 A GB4232670 A GB 4232670A GB 4232670 A GB4232670 A GB 4232670A GB 1318267 A GB1318267 A GB 1318267A
Authority
GB
United Kingdom
Prior art keywords
superalloys
phase
topologically close
packed
ageing
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
Application number
GB4232670A
Other languages
English (en)
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.)
RTX Corp
Original Assignee
United Aircraft 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 Aircraft Corp filed Critical United Aircraft Corp
Publication of GB1318267A publication Critical patent/GB1318267A/en
Expired 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
    • C22C19/00—Alloys based on nickel or cobalt

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
  • Inorganic Compounds Of Heavy Metals (AREA)
  • Manufacture And Refinement Of Metals (AREA)
GB4232670A 1969-09-26 1970-09-03 Superalloys incorporating precipitated topologically close-packed phases Expired GB1318267A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US86149669A 1969-09-26 1969-09-26

Publications (1)

Publication Number Publication Date
GB1318267A true GB1318267A (en) 1973-05-23

Family

ID=25335973

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4232670A Expired GB1318267A (en) 1969-09-26 1970-09-03 Superalloys incorporating precipitated topologically close-packed phases

Country Status (9)

Country Link
US (1) US3620855A (enrdf_load_stackoverflow)
JP (1) JPS5117491B1 (enrdf_load_stackoverflow)
BE (1) BE756652A (enrdf_load_stackoverflow)
CA (1) CA930204A (enrdf_load_stackoverflow)
CH (1) CH557881A (enrdf_load_stackoverflow)
DE (1) DE2043053A1 (enrdf_load_stackoverflow)
FR (1) FR2062624A5 (enrdf_load_stackoverflow)
GB (1) GB1318267A (enrdf_load_stackoverflow)
NL (1) NL7014191A (enrdf_load_stackoverflow)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3445768A1 (de) * 1983-12-27 1985-07-04 United Technologies Corp., Hartford, Conn. Verfahren zum schmieden von superlegierungen
DE3445767A1 (de) * 1983-12-27 1985-07-04 United Technologies Corp., Hartford, Conn. Verfahren zum Schmieden von Superlegierungen auf Nickelbasis sowie ein Gegenstand aus einer Superlegierung auf Nickelbasis mit verbesserter Schmiedbarkeit
FR2593830A1 (fr) * 1986-02-06 1987-08-07 Snecma Superalliage a matrice a base de nickel notamment elabore en metallurgie des poudres et disque de turbomachine constitue en cet alliage
US7208116B2 (en) 2000-09-29 2007-04-24 Rolls-Royce Plc Nickel base superalloy

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3816920A (en) * 1972-11-30 1974-06-18 Gillette Co Novel cutting edges and processes for making them
US3973952A (en) * 1973-06-11 1976-08-10 The International Nickel Company, Inc. Heat resistant alloy casting
US4769087A (en) * 1986-06-02 1988-09-06 United Technologies Corporation Nickel base superalloy articles and method for making
US4908069A (en) * 1987-10-19 1990-03-13 Sps Technologies, Inc. Alloys containing gamma prime phase and process for forming same
US5169463A (en) * 1987-10-19 1992-12-08 Sps Technologies, Inc. Alloys containing gamma prime phase and particles and process for forming same
FR2712307B1 (fr) * 1993-11-10 1996-09-27 United Technologies Corp Articles en super-alliage à haute résistance mécanique et à la fissuration et leur procédé de fabrication.
EP1959024A4 (en) * 2005-12-05 2009-12-23 Japan Science & Tech Agency CO-BASED ALLOY AND PROCESS FOR PRODUCING THE SAME
CN109921014B (zh) * 2017-12-13 2021-10-01 荆门市格林美新材料有限公司 具有亚晶结构的镍基锂离子电池正极材料及其制备方法
CN114990408B (zh) * 2022-04-26 2023-02-10 沈阳航空航天大学 综合力学性能优异的NiCoCrFeAlTi中熵合金及其制备方法

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3147155A (en) * 1961-08-02 1964-09-01 Int Nickel Co Hot-working process

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3445768A1 (de) * 1983-12-27 1985-07-04 United Technologies Corp., Hartford, Conn. Verfahren zum schmieden von superlegierungen
DE3445767A1 (de) * 1983-12-27 1985-07-04 United Technologies Corp., Hartford, Conn. Verfahren zum Schmieden von Superlegierungen auf Nickelbasis sowie ein Gegenstand aus einer Superlegierung auf Nickelbasis mit verbesserter Schmiedbarkeit
GB2152076A (en) * 1983-12-27 1985-07-31 United Technologies Corp Improved forgeability in nickel base superalloys
FR2593830A1 (fr) * 1986-02-06 1987-08-07 Snecma Superalliage a matrice a base de nickel notamment elabore en metallurgie des poudres et disque de turbomachine constitue en cet alliage
EP0237378A1 (fr) * 1986-02-06 1987-09-16 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Superalliage à matrice à base de nickel notamment élaboré en métallurgie des poudres et disque de turbomachine constitué en cet alliage
US7208116B2 (en) 2000-09-29 2007-04-24 Rolls-Royce Plc Nickel base superalloy

Also Published As

Publication number Publication date
FR2062624A5 (enrdf_load_stackoverflow) 1971-06-25
NL7014191A (enrdf_load_stackoverflow) 1971-03-30
CA930204A (en) 1973-07-17
CH557881A (de) 1975-01-15
JPS5117491B1 (enrdf_load_stackoverflow) 1976-06-02
DE2043053A1 (de) 1971-04-22
US3620855A (en) 1971-11-16
BE756652A (fr) 1971-03-01

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees