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
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
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