GB817710A - Improvements in ferrous alloys - Google Patents

Improvements in ferrous alloys

Info

Publication number
GB817710A
GB817710A GB1060457A GB1060457A GB817710A GB 817710 A GB817710 A GB 817710A GB 1060457 A GB1060457 A GB 1060457A GB 1060457 A GB1060457 A GB 1060457A GB 817710 A GB817710 A GB 817710A
Authority
GB
United Kingdom
Prior art keywords
range
impurities
alloy
ferrous alloys
examples
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
GB1060457A
Inventor
Percy Herbert Frith
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.)
Bristol Aero Engines Ltd
Original Assignee
Bristol Aero Engines Ltd
Filing date
Publication date
Application filed by Bristol Aero Engines Ltd filed Critical Bristol Aero Engines Ltd
Publication of GB817710A publication Critical patent/GB817710A/en
Expired legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/58Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese

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

An alloy suitable for forming, by casting, components of gas turbine and other engines which are not subjected to temperatures above 500 DEG C. in use, has a composition in the following range in per cent by weight: C up to 0.12, Si 1.5-2.5, Cr 10.0-13.5, Mn 1.5-4.5, Ni 1.5-4.5, Fe and impurities the balance. The total of the contents of Mn and Ni being between 4.5 and 7.0. The alloy may be heat treated at a temperature in the range 600-650 DEG C. for not less than one hour and then cooled in air. Examples of alloys within the range are given, the examples containing specified proportions of S, P and N as impurities.
GB1060457A 1957-04-01 Improvements in ferrous alloys Expired GB817710A (en)

Publications (1)

Publication Number Publication Date
GB817710A true GB817710A (en) 1959-08-06

Family

ID=1700844

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1060457A Expired GB817710A (en) 1957-04-01 Improvements in ferrous alloys

Country Status (1)

Country Link
GB (1) GB817710A (en)

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