GB769822A - Improvements in nickel-base alloys - Google Patents

Improvements in nickel-base alloys

Info

Publication number
GB769822A
GB769822A GB15072/55A GB1507255A GB769822A GB 769822 A GB769822 A GB 769822A GB 15072/55 A GB15072/55 A GB 15072/55A GB 1507255 A GB1507255 A GB 1507255A GB 769822 A GB769822 A GB 769822A
Authority
GB
United Kingdom
Prior art keywords
per cent
nickel
base alloys
balance
gas turbine
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
GB15072/55A
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
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 Motors Liquidation Co filed Critical Motors Liquidation Co
Publication of GB769822A publication Critical patent/GB769822A/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
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/056Alloys 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%

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)

Abstract

A high-temperature creep resistant alloy particularly for gas turbine blades has a composition within the following range .C.0 - 0.25.per cent .Mn.0 - 1.0.per cent .Si.0 - 1.0.per cent .Cr.13.0 - 17.0.per cent .Mo.4.0 - 6.0.per cent .Ti.1.5 - 3.0.per cent .Al.1.0 - 4.0.per cent .B.0.01 - 0.15.per cent .Fe.0.1 - less than 8.0.per cent .Ni.-.the balance
GB15072/55A 1954-06-28 1955-05-25 Improvements in nickel-base alloys Expired GB769822A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US769822XA 1954-06-28 1954-06-28

Publications (1)

Publication Number Publication Date
GB769822A true GB769822A (en) 1957-03-13

Family

ID=22135412

Family Applications (1)

Application Number Title Priority Date Filing Date
GB15072/55A Expired GB769822A (en) 1954-06-28 1955-05-25 Improvements in nickel-base alloys

Country Status (1)

Country Link
GB (1) GB769822A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2975051A (en) * 1959-09-29 1961-03-14 Gen Electric Nickel base alloy
US3067030A (en) * 1958-08-13 1962-12-04 Dunn Eugene Ludwick Nickel base alloy

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3067030A (en) * 1958-08-13 1962-12-04 Dunn Eugene Ludwick Nickel base alloy
US2975051A (en) * 1959-09-29 1961-03-14 Gen Electric Nickel base alloy

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