发明名称 Control of the blade tip clearance of the high-pressure turbine of a turbomachine
摘要 <p>The turbine stage has a rotor comprising a disk with mobile blades that rotate inside a sealing ring (22) held by a turbine casing (24). An annular thermal protection sheet mounted between the casing and the ring. The protection sheet is formed by a semi-annular curved plate (56) mounted end-to-end and attached by a fixation pin (70) on the casing. The pin comprises an end (80) exterior to the casing, where the end is set on a washer. The washer is threaded on the end of the pin and is applied on a radial external surface of the casing.</p>
申请公布号 EP2053200(A1) 申请公布日期 2009.04.29
申请号 EP20080166410 申请日期 2008.10.13
申请人 SNECMA 发明人 DAKOWSKI, MATHIEU;DORIN-COPPEE, CLAIRE, DORINE;GENDRAUD, ALAIN, DOMINIQUE;POMMIER, NICOLAS, AUGUSTE, MARCEL
分类号 F01D11/00;F01D11/08;F01D11/18;F01D11/24;F01D25/24 主分类号 F01D11/00
代理机构 代理人
主权项
地址