发明名称 conjunto de anel de turbina.
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 substantially &pgr;-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 BRPI1013342(A8) 申请公布日期 2016.08.23
申请号 BR2010PI13342 申请日期 2010.03.01
申请人 SNECMA;SNECMA PROPULSION SOLIDE 发明人 ALAIN DOMINIQUE GENDRAUD;DAMIEN BONNEAU;FRANCK ROGER DENIS DENECE;GEORGES HABAROU;HUBERT ILLAND
分类号 F01D9/04;F01D11/08;F01D25/24 主分类号 F01D9/04
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