GB730801A - Nickel-chromium base alloy - Google Patents

Nickel-chromium base alloy

Info

Publication number
GB730801A
GB730801A GB2684752A GB2684752A GB730801A GB 730801 A GB730801 A GB 730801A GB 2684752 A GB2684752 A GB 2684752A GB 2684752 A GB2684752 A GB 2684752A GB 730801 A GB730801 A GB 730801A
Authority
GB
United Kingdom
Prior art keywords
per cent
nickel
base alloy
alloy
chromium base
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
GB2684752A
Inventor
Harold Ernest Gresham
Marcus Alan Wheeler
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB2684752A priority Critical patent/GB730801A/en
Publication of GB730801A publication Critical patent/GB730801A/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
    • C22C19/053—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 30% but less than 40%

Abstract

A nickel-base alloy, particularly for cast or wrought parts of internal combustion turbines, has the following composition: .Cr.15.0-30.0.per cent .Mo.7.5-12.0.per cent .Ti.1.0- 3.0.per cent .Al.0.1- 2.0.per cent .C.0 - 0.3.per cent .Fe.0 - 2.0.per cent .Mn.0 - 1.5.per cent .Si.0 - 1.5.per cent Ni, and any impurities, the balance The alloy may also contain up to 10 per cent of Co. The alloy may be given a heat treatment, e.g. solution treatment at 1120 DEG C. for 6 hours, followed by ageing at 750 DEG C. for 16 hours. Specifications 583,162 and 583,212 are referred to.
GB2684752A 1952-10-25 1952-10-25 Nickel-chromium base alloy Expired GB730801A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2684752A GB730801A (en) 1952-10-25 1952-10-25 Nickel-chromium base alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2684752A GB730801A (en) 1952-10-25 1952-10-25 Nickel-chromium base alloy

Publications (1)

Publication Number Publication Date
GB730801A true GB730801A (en) 1955-06-01

Family

ID=10250194

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2684752A Expired GB730801A (en) 1952-10-25 1952-10-25 Nickel-chromium base alloy

Country Status (1)

Country Link
GB (1) GB730801A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0091308A2 (en) * 1982-04-05 1983-10-12 Teledyne Industries, Inc. Corrosion resistant nickel base alloy

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0091308A2 (en) * 1982-04-05 1983-10-12 Teledyne Industries, Inc. Corrosion resistant nickel base alloy
GB2117793A (en) * 1982-04-05 1983-10-19 Teledyne Ind Corrosion resistant nickel base alloy
EP0091308A3 (en) * 1982-04-05 1984-09-05 Teledyne Industries, Inc. Corrosion resistant nickel base alloy

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