发明名称 GAS TURBINE ENGINE AIRFOILS
摘要 A composite article includes a compressively stressed plating which provides increased static strength and fatigue life. In particular, a fan exit guide vane (1), made of a graphite fiber reinforced composite material and including a conductive plating (7), achieves a 380% increase in static load capability over an unplated composite vane and a low cycle fatigue life of over 1 million cycles through the application of a compressively stressed nickel plating (8) which produces a residual compressive stress state of between -5,000 and -15,000 psi.
申请公布号 GB2194553(B) 申请公布日期 1991.03.06
申请号 GB19870018302 申请日期 1987.08.03
申请人 * UNITED TECHNOLOGIES CORPORATION 发明人 JEFFREY SCOTT * LESHANE;KOSTAS * ROUTSIS;CHARLES RAY * WATSON
分类号 C25D7/00;B32B15/01;C23C28/02;C23C30/00;F01D5/28;F03B3/12 主分类号 C25D7/00
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