发明授权
US07875135B2 High pressure turbine airfoil recovery device and method of heat treatment 有权
高压涡轮机翼回收装置及热处理方法

High pressure turbine airfoil recovery device and method of heat treatment
摘要:
Provided is a method for heat treating a precipitation-hardened article having a thick section and a thin section so that the thin section can be solution annealed while the metallurgical structure of the thick section is substantially unaffected by the solution-annealing process. The method restores the microstructure of the thin section uniformly by solution annealing the thin section to achieve a preselected microstructure but without affecting the microstructure of the thick section.
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