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