发明名称 Hoop stress relief mechanism for gas turbine engines
摘要 A hoop stress relief mechanism is disclosed for use on a rotary body to relieve stress caused by both thermal and centrifugal forces. The mechanism may consist of a J-shaped slot cut from the outer rim of the rotary body a distance inwardly toward the axis of rotation, the slot having a curve in its inward end that curves back towards the outer rim. The J-shaped slot may extend through the rotary body to join its two faces. The J-shaped slot may be fabricated by an electric discharge wire machine. The electric discharge wire machine may make multiple passes in order to smooth the bottom surface of the curved slot portion.
申请公布号 US7097422(B2) 申请公布日期 2006.08.29
申请号 US20040771689 申请日期 2004.02.03
申请人 HONEYWELL INTERNATIONAL, INC. 发明人 RICE DEREK A.;WALDMAN DAVID R.;HOW REDGE;SERAG MAHER A.;RIPPEY PAUL D.;SILCOX CHARLES P.;CHESTER HENRY L.;THIYAGARAJAN RAMASAMI (RAJAN);LIU HSIN-YI;HRUSKA PAUL E.;JACKSON RICHARD E.;INNES DAVID A.;BAILEY GORDON B.
分类号 F01D25/26 主分类号 F01D25/26
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