发明授权
US09194241B2 CMC turbine nozzle adapted to support a metallic turbine internal casing by a radial contact
有权
CMC涡轮喷嘴适于通过径向接触来支撑金属涡轮内部壳体
- 专利标题: CMC turbine nozzle adapted to support a metallic turbine internal casing by a radial contact
- 专利标题(中): CMC涡轮喷嘴适于通过径向接触来支撑金属涡轮内部壳体
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申请号: US13435910申请日: 2012-03-30
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公开(公告)号: US09194241B2公开(公告)日: 2015-11-24
- 发明人: Antoine Jean-Philippe Beaujard , Gilles Alain Charier , Jean Pierre Mareix , Didier Fabre
- 申请人: Antoine Jean-Philippe Beaujard , Gilles Alain Charier , Jean Pierre Mareix , Didier Fabre
- 申请人地址: FR Paris
- 专利权人: SNECMA
- 当前专利权人: SNECMA
- 当前专利权人地址: FR Paris
- 代理机构: Oblon, McClelland, Maier & Neustadt, L.L.P.
- 优先权: FR1152635 20110330
- 主分类号: F01D1/02
- IPC分类号: F01D1/02 ; F01D5/28 ; F01D9/06 ; F01D25/24
摘要:
A composite material turbine nozzle blade including an airfoil adapted to have a cooling fluid flow through it and extending between a shroud and a root is provided. The shroud is shaped to be attached to one or more turbine casings of a turbomachine and the root is shaped to provide a junction with a turbine internal casing. The root is produced with a loosened texture and includes an external upstream side loosened texture lug and an external downstream side loosened texture lug. The ends of the two external side lugs extend radially relative to the rotation axis of the turbomachine to form a device for supporting and centering the internal casing.
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