GB1036148A - Improvements in or relating to alloys - Google Patents

Improvements in or relating to alloys

Info

Publication number
GB1036148A
GB1036148A GB3468163A GB3468163A GB1036148A GB 1036148 A GB1036148 A GB 1036148A GB 3468163 A GB3468163 A GB 3468163A GB 3468163 A GB3468163 A GB 3468163A GB 1036148 A GB1036148 A GB 1036148A
Authority
GB
United Kingdom
Prior art keywords
alloys
relating
remainder
twice
nickel alloy
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
GB3468163A
Inventor
Adam Dunlop
Henry Cave Child
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.)
Birmingham Small Arms Co Ltd
Original Assignee
Birmingham Small Arms 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 Birmingham Small Arms Co Ltd filed Critical Birmingham Small Arms Co Ltd
Priority to GB3468163A priority Critical patent/GB1036148A/en
Priority to SE10540/64A priority patent/SE318728B/xx
Priority to CH1149064A priority patent/CH440721A/en
Publication of GB1036148A publication Critical patent/GB1036148A/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
    • 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

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Catalysts (AREA)
  • Conductive Materials (AREA)

Abstract

A nickel alloy has the following percentage composition: .C.0.05-0.5 .Cr.3-10 .Co.0-20 .Al.2-8 .W.2-20 and/or .Mo.1-10 .Nb.>3-7 and/or .Ta.2-14 .B.0.001-0.1 .Zr.0-0.3 Ni (at least 40) the remainder Ta and twice Nb should be between 2 and 14.
GB3468163A 1963-09-03 1963-09-03 Improvements in or relating to alloys Expired GB1036148A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB3468163A GB1036148A (en) 1963-09-03 1963-09-03 Improvements in or relating to alloys
SE10540/64A SE318728B (en) 1963-09-03 1964-09-02
CH1149064A CH440721A (en) 1963-09-03 1964-09-03 Nickel alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3468163A GB1036148A (en) 1963-09-03 1963-09-03 Improvements in or relating to alloys

Publications (1)

Publication Number Publication Date
GB1036148A true GB1036148A (en) 1966-07-13

Family

ID=10368655

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3468163A Expired GB1036148A (en) 1963-09-03 1963-09-03 Improvements in or relating to alloys

Country Status (3)

Country Link
CH (1) CH440721A (en)
GB (1) GB1036148A (en)
SE (1) SE318728B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2230747A1 (en) * 1973-05-25 1974-12-20 Terekhov Kuzma Heat resistant nickel alloy - contg. lanthanum for jet engine components
CN112760525A (en) * 2019-11-01 2021-05-07 利宝地工程有限公司 High gamma prime nickel-based superalloy, use thereof and method of manufacturing a turbine engine component

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2230747A1 (en) * 1973-05-25 1974-12-20 Terekhov Kuzma Heat resistant nickel alloy - contg. lanthanum for jet engine components
CN112760525A (en) * 2019-11-01 2021-05-07 利宝地工程有限公司 High gamma prime nickel-based superalloy, use thereof and method of manufacturing a turbine engine component

Also Published As

Publication number Publication date
SE318728B (en) 1969-12-15
CH440721A (en) 1967-07-31

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