GB1407871A - Directionally-solidified eutectic type alloys with aligned delta phase - Google Patents

Directionally-solidified eutectic type alloys with aligned delta phase

Info

Publication number
GB1407871A
GB1407871A GB312773A GB312773A GB1407871A GB 1407871 A GB1407871 A GB 1407871A GB 312773 A GB312773 A GB 312773A GB 312773 A GB312773 A GB 312773A GB 1407871 A GB1407871 A GB 1407871A
Authority
GB
United Kingdom
Prior art keywords
solidification
directionally
phase
aligned
delta phase
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
GB312773A
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 GB1407871A publication Critical patent/GB1407871A/en
Expired legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/058Alloys 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)
  • Joining Of Building Structures In Genera (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

1407871 Directionally solidified castings UNITED AIRCRAFT CORP 22 Jan 1973 [27 Jan 1972] 3127/73 Heading B3F A directionally solidified nickel-based alloy casting having an overall eutectic composition which is thermodynamically monovariant or multivariant consists of a lamellar phase dispersed in a matrix phase, the lamellae being in alignment with each other. The lamellar phase is Ni 3 Nb or Ni 3 Ta or Ni 3 (Nb.Ta) and the matrix phase is a nickel-based solid solution containing up to 35 wt. per cent Cr and/or up to 4 wt. per cent Al. The castings may be made by directional plane-front solidification at solidification rates of 2 to 10 cm./hr. Directional solidification with a cusped liquid/solid interface at higher solidification rates produces alloys with the aligned lamellar phase.
GB312773A 1972-01-27 1973-01-22 Directionally-solidified eutectic type alloys with aligned delta phase Expired GB1407871A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
GB1407871A true GB1407871A (en) 1975-10-01

Family

ID=22826632

Family Applications (1)

Application Number Title Priority Date Filing Date
GB312773A Expired GB1407871A (en) 1972-01-27 1973-01-22 Directionally-solidified eutectic type alloys with aligned delta phase

Country Status (11)

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

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2239537B1 (en) * 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
AU470203B2 (en) 1976-03-04
AU5101473A (en) 1974-07-11
FR2169385A1 (en) 1973-09-07
JPS4886725A (en) 1973-11-15
IT978447B (en) 1974-09-20
CA992357A (en) 1976-07-06
FR2169385B1 (en) 1979-02-23
CH563461A5 (en) 1975-06-30
NL7300928A (en) 1973-07-31
DE2303837A1 (en) 1973-08-02
BE794412A (en) 1973-05-16
US3793010A (en) 1974-02-19

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee