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 |
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代理人 |
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主权项 |
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地址 |
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