GB733489A - Improvements relating to nickel-chromium-cobalt alloys - Google Patents

Improvements relating to nickel-chromium-cobalt alloys

Info

Publication number
GB733489A
GB733489A GB1733252A GB1733252A GB733489A GB 733489 A GB733489 A GB 733489A GB 1733252 A GB1733252 A GB 1733252A GB 1733252 A GB1733252 A GB 1733252A GB 733489 A GB733489 A GB 733489A
Authority
GB
United Kingdom
Prior art keywords
per cent
hours
alloys
chromium
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.)
Expired
Application number
GB1733252A
Inventor
Walter Betteridge
Arthur William Franklin
Ronald Alfred Smith
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.)
Mond Nickel Co Ltd
Original Assignee
Mond Nickel Co Ltd
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 Mond Nickel Co Ltd filed Critical Mond Nickel Co Ltd
Priority to GB1733252A priority Critical patent/GB733489A/en
Publication of GB733489A publication Critical patent/GB733489A/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)
  • Heat Treatment Of Steel (AREA)

Abstract

Articles resistant to corrosion and creep and made of alloys of the following composition: Cr 4.0-12.0, Co 10.0-55.0, Ti 0.5-8.0, Al 0.3-8.0, B 0.001-0.1, Zr 0.01-0.2, Mo 0-15.0, C 0-0.5 per cent, Ni, with impurities and residual deoxidants, the balance. The proportions of Ti, Al, Mo and C are so selected that the alloy when tested under a stress of 9 tons/square inch at 870 DEG C. has a life to fracture of 100 hours or more after subjection to a heat treatment comprising heating at 1200 DEG C. for 3 hours, cooling rapidly to 850 DEG C., maintaining this temperature for 24 hours and ageing at 700 DEG C. for 16 hours. The alloy may also contain one or more of the following elements Fe up to 10 per cent, W up to 5.0 per cent, Mn up to 10. per cent, Si up to 1.5 per cent and Nb or Ta or both up to 1.0 per cent in total. The alloys may be solution heated at a temperature not less than 1150 DEG C., given an intermediate heating at 750-1000 DEG C. and finally agehardened, e.g. at 700 DEG C. Specification 632,712 is referred to.
GB1733252A 1952-07-09 1952-07-09 Improvements relating to nickel-chromium-cobalt alloys Expired GB733489A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1733252A GB733489A (en) 1952-07-09 1952-07-09 Improvements relating to nickel-chromium-cobalt alloys

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1733252A GB733489A (en) 1952-07-09 1952-07-09 Improvements relating to nickel-chromium-cobalt alloys

Publications (1)

Publication Number Publication Date
GB733489A true GB733489A (en) 1955-07-13

Family

ID=10093316

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1733252A Expired GB733489A (en) 1952-07-09 1952-07-09 Improvements relating to nickel-chromium-cobalt alloys

Country Status (1)

Country Link
GB (1) GB733489A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3110587A (en) * 1959-06-23 1963-11-12 Int Nickel Co Nickel-chromium base alloy
DE1184964B (en) * 1957-09-16 1965-01-07 Mond Nickel Co Ltd Use of a nickel alloy for precision castings, mainly turbine blades
US3166412A (en) * 1962-08-31 1965-01-19 Int Nickel Co Cast nickel-base alloy for gas turbine rotors
US3166411A (en) * 1958-10-21 1965-01-19 Int Nickel Co Nickel-chromium alloys
DE1217627B (en) * 1959-06-23 1966-05-26 Int Nickel Ltd Use of a kneaded and aged nickel-chromium-cobalt alloy
DE1231907B (en) * 1961-01-30 1967-01-05 Int Nickel Ltd Use of a kneaded and aged nickel-chromium-cobalt alloy for objects with high impact strength
DE1235597B (en) * 1956-10-29 1967-03-02 Int Nickel Ltd Use of a nickel-chromium-cobalt alloy as a material for castings with high creep strength at 980µ
DE1239103B (en) * 1958-10-21 1967-04-20 Int Nickel Ltd Use of a nickel-chromium-cobalt-molybdenum alloy for creep-resistant and corrosion-resistant objects
FR2593830A1 (en) * 1986-02-06 1987-08-07 Snecma NICKEL-BASED MATRIX SUPERALLIAGE, ESPECIALLY IN POWDER METALLURGY, AND TURBOMACHINE DISK COMPRISING THE SAME
EP1842934A1 (en) * 2004-12-02 2007-10-10 National Institute for Materials Science Heat-resistant superalloy

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1235597B (en) * 1956-10-29 1967-03-02 Int Nickel Ltd Use of a nickel-chromium-cobalt alloy as a material for castings with high creep strength at 980µ
DE1184964B (en) * 1957-09-16 1965-01-07 Mond Nickel Co Ltd Use of a nickel alloy for precision castings, mainly turbine blades
US3166411A (en) * 1958-10-21 1965-01-19 Int Nickel Co Nickel-chromium alloys
DE1239103B (en) * 1958-10-21 1967-04-20 Int Nickel Ltd Use of a nickel-chromium-cobalt-molybdenum alloy for creep-resistant and corrosion-resistant objects
US3110587A (en) * 1959-06-23 1963-11-12 Int Nickel Co Nickel-chromium base alloy
DE1217627B (en) * 1959-06-23 1966-05-26 Int Nickel Ltd Use of a kneaded and aged nickel-chromium-cobalt alloy
DE1231907B (en) * 1961-01-30 1967-01-05 Int Nickel Ltd Use of a kneaded and aged nickel-chromium-cobalt alloy for objects with high impact strength
US3166412A (en) * 1962-08-31 1965-01-19 Int Nickel Co Cast nickel-base alloy for gas turbine rotors
FR2593830A1 (en) * 1986-02-06 1987-08-07 Snecma NICKEL-BASED MATRIX SUPERALLIAGE, ESPECIALLY IN POWDER METALLURGY, AND TURBOMACHINE DISK COMPRISING THE SAME
EP0237378A1 (en) * 1986-02-06 1987-09-16 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Superalloy having a nickel base matrix, manufactured by powder-metallurgical processing, and gas turbine discs made from this alloy
EP1842934A1 (en) * 2004-12-02 2007-10-10 National Institute for Materials Science Heat-resistant superalloy
EP1842934A4 (en) * 2004-12-02 2008-03-05 Nat Inst For Materials Science SUPERALLIAGE RESISTANT TO HEAT

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