发明名称 Segmented composite inner shrouds
摘要 A shroud for supporting the vanes in the hot sections of a gas turbine engine is comprised of composite segments retained in a metal ring. The metal ring has a positive coefficient of expansion, while the segments have a zero (or much smaller) coefficient. When the ring is heated and grows, it carries the segments with it, so that there is an apparent corresponding growth of the segments.
申请公布号 US5062767(A) 申请公布日期 1991.11.05
申请号 US19900516493 申请日期 1990.04.27
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE 发明人 WORLEY, KEVIN L.;MAYERS, JOHN L.;BURCHETTE, HERBERT L.
分类号 F01D9/04;F01D11/18 主分类号 F01D9/04
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