发明名称 Reduction of the blade tip clearance in a gas turbine
摘要 The turbine has a blade (10) mounted in rotation around an axis in a casing comprising a metallic ring (16) fixed around a turbine rotor. An internal cylindrical surface of the casing is covered with a layer (18) of abradable material. A peripheral shroud (26) is slidably mounted at apex of the blade and partially housed and guided in an annular groove (30) of the ring (16).
申请公布号 EP1469165(A1) 申请公布日期 2004.10.20
申请号 EP20040290819 申请日期 2004.03.26
申请人 SNECMA MOTEURS 发明人 NOTTIN, CLAUDE DANIEL
分类号 F01D5/20 主分类号 F01D5/20
代理机构 代理人
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