发明名称 TURBINE RING ASSEMBLY
摘要 A turbine ring assembly includes a ring support structure and a plurality of ring sectors, each including a single piece of ceramic matrix composite material. Each ring sector includes a first portion forming an annular base with an inside face defining an inside face of the turbine ring and an outside face from which there extends two tab-forming portions including ends that are engaged in housings in the ring support structure. The ring sectors present a section that is substantiallyπ-shaped and the ends of the tabs are held without radial clearance by the ring support structure. The tabs can have a free length in meridian section that is not less than three times their mean width.
申请公布号 US2012027572(A1) 申请公布日期 2012.02.02
申请号 US201013255436 申请日期 2010.03.01
申请人 DENECE FRANCK ROGER DENIS;GENDRAUD ALAIN DOMINIQUE;HABAROU GEORGES;ILLAND HUBERT;BONNEAU DAMIEN;SNECMA PROPULSION SOLIDE, LE HAILLAN;SNECMA 发明人 DENECE FRANCK ROGER DENIS;GENDRAUD ALAIN DOMINIQUE;HABAROU GEORGES;ILLAND HUBERT;BONNEAU DAMIEN
分类号 F01D25/24 主分类号 F01D25/24
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