DE2303837A1 - Orientiert verfestigter legierungsguss - Google Patents

Orientiert verfestigter legierungsguss

Info

Publication number
DE2303837A1
DE2303837A1 DE2303837A DE2303837A DE2303837A1 DE 2303837 A1 DE2303837 A1 DE 2303837A1 DE 2303837 A DE2303837 A DE 2303837A DE 2303837 A DE2303837 A DE 2303837A DE 2303837 A1 DE2303837 A1 DE 2303837A1
Authority
DE
Germany
Prior art keywords
phase
aluminum
chromium
alloy
nickel
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.)
Pending
Application number
DE2303837A
Other languages
German (de)
English (en)
Inventor
Franklin David Lemkey
Earl Ryan Thompson
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.)
Raytheon Technologies 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 DE2303837A1 publication Critical patent/DE2303837A1/de
Pending 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
    • 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
    • C22C19/058—Alloys based on nickel or cobalt based on nickel with chromium without Mo and W

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)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Joining Of Building Structures In Genera (AREA)
DE2303837A 1972-01-27 1973-01-26 Orientiert verfestigter legierungsguss Pending DE2303837A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US22116572A 1972-01-27 1972-01-27

Publications (1)

Publication Number Publication Date
DE2303837A1 true DE2303837A1 (de) 1973-08-02

Family

ID=22826632

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2303837A Pending DE2303837A1 (de) 1972-01-27 1973-01-26 Orientiert verfestigter legierungsguss

Country Status (11)

Country Link
US (1) US3793010A (fr)
JP (1) JPS4886725A (fr)
AU (1) AU470203B2 (fr)
BE (1) BE794412A (fr)
CA (1) CA992357A (fr)
CH (1) CH563461A5 (fr)
DE (1) DE2303837A1 (fr)
FR (1) FR2169385B1 (fr)
GB (1) GB1407871A (fr)
IT (1) IT978447B (fr)
NL (1) NL7300928A (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2239537B1 (fr) * 1973-07-30 1976-11-12 Onera (Off Nat Aerospatiale)
US4055447A (en) * 1976-05-07 1977-10-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Directionally solidified eutectic γ-γ' nickel-base superalloys
US4288259A (en) * 1978-12-04 1981-09-08 United Technologies Corporation Tantalum modified gamma prime-alpha eutectic alloy
US4409451A (en) * 1981-08-31 1983-10-11 United Technologies Corporation Induction furnace having improved thermal profile
US4543235A (en) * 1982-09-22 1985-09-24 United Technologies Corporation Eutectic superalloy compositions and articles
GB2194960B (en) * 1986-03-17 1990-06-20 Stuart L Adelman Improved superalloy compositions and articles
US5649280A (en) * 1996-01-02 1997-07-15 General Electric Company Method for controlling grain size in Ni-base superalloys
US6969240B2 (en) * 2003-08-01 2005-11-29 Honeywell International Inc. Integral turbine composed of a cast single crystal blade ring diffusion bonded to a high strength disk
US8858874B2 (en) * 2007-11-23 2014-10-14 Rolls-Royce Plc Ternary nickel eutectic alloy
US11525172B1 (en) 2021-12-01 2022-12-13 L.E. Jones Company Nickel-niobium intermetallic alloy useful for valve seat inserts

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3554817A (en) * 1969-03-20 1971-01-12 United Aircraft Corp Cast nickel-columbium-aluminum alloy

Also Published As

Publication number Publication date
NL7300928A (fr) 1973-07-31
FR2169385B1 (fr) 1979-02-23
US3793010A (en) 1974-02-19
IT978447B (it) 1974-09-20
AU470203B2 (en) 1976-03-04
BE794412A (fr) 1973-05-16
JPS4886725A (fr) 1973-11-15
FR2169385A1 (fr) 1973-09-07
AU5101473A (en) 1974-07-11
CH563461A5 (fr) 1975-06-30
GB1407871A (en) 1975-10-01
CA992357A (en) 1976-07-06

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Legal Events

Date Code Title Description
OHA Expiration of time for request for examination