发明名称 |
TURBINE POUR UNE TURBOMACHINE, TELLE QU'UN TURBOREACTEUR OU UN TURBOPROPULSEUR D'AVION |
摘要 |
<p>The turbine has a distributor (1) whose radial blades (5) are connected by its ends radially external to an annular platform (3). The platform comprises cylindrical edges engaged on rails (11, 15) of a casing (2) at upstream and downstream so as to ensure fixation of the distributor on the casing. Upstream and downstream edges (9, 13) of the distributor are supported against the casing via composite ceramic matrix runners (23), where the runners are made of thermically insulator material. The runners comprise cores surrounded by a sheath and formed by folding of a metal foil.</p> |
申请公布号 |
FR2961850(B1) |
申请公布日期 |
2013.05.10 |
申请号 |
FR20100055164 |
申请日期 |
2010.06.28 |
申请人 |
SNECMA |
发明人 |
GENDRAUD ALAIN, DOMINIQUE;MORVAN ALEXANDRA;PRESTEL SEBASTIEN, JEAN, LAURENT;RENAUD JULIEN |
分类号 |
F01D25/08 |
主分类号 |
F01D25/08 |
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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