发明名称 |
ACCROISSEMENT THERMO-MECANIQUE DE LA RESISTANCE DES SUPERALLIAGES ( |
摘要 |
The superalloys are strengthened in a process involving both thermal and deformational treatments under controlled conditions. The method is particularly effective for the nickel-base superalloys of the gamma - gamma ' -type having a volume fraction of the gamma ' phase exceeding about 25 percent at room temperature, and for the superalloys precipitating the topologically close-packed phases such as the sigma phase. It relies on the establishment of a microstructure wherein the gamma ' phase is precipitated in a uniformly distributed array having an interparticle spacing not exceeding about 5 microns; warm working the alloy to effect an area reduction of at least 15 percent; and subjecting the alloy to a stabilization heat treatment. The strength increase is attributable to a particular thermally and mechanically stable array of microcrystalline imperfections thus established and, in those alloys precipitating the sigma phase, also by an altered sigma phase morphology. |
申请公布号 |
BE756653(A1) |
申请公布日期 |
1971.03.01 |
申请号 |
BED756653 |
申请日期 |
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申请人 |
UNITED AIRCRAFT CORP, 400 MAIN STREET, EAST HARTFORD, CONNECTITUT (E. U. A.) |
发明人 |
W. A. OWCZARSKI;J. M. OBLAK;W. A. OWCZARSKI;J. M. OBLAK. |
分类号 |
C22C19/05;C22F1/00;C22F1/10;(IPC1-7):21D/ |
主分类号 |
C22C19/05 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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