发明授权
US08984855B2 Rotating inlet cowl for a turbine engine, comprising an eccentric forward end
有权
用于涡轮发动机的旋转入口罩,包括偏心的前端
- 专利标题: Rotating inlet cowl for a turbine engine, comprising an eccentric forward end
- 专利标题(中): 用于涡轮发动机的旋转入口罩,包括偏心的前端
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申请号: US13262386申请日: 2010-03-31
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公开(公告)号: US08984855B2公开(公告)日: 2015-03-24
- 发明人: Mickael Delapierre , Herve Gignoux , Gael Loro , Sylvie Wintenberger
- 申请人: Mickael Delapierre , Herve Gignoux , Gael Loro , Sylvie Wintenberger
- 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: FR0952056 20090331
- 国际申请: PCT/EP2010/054080 WO 20100331
- 国际公布: WO2010/112453 WO 20101007
- 主分类号: F02G3/00
- IPC分类号: F02G3/00 ; F02K1/78 ; F02K99/00 ; F02K3/06 ; B64D15/16 ; B64D15/00 ; F03B15/22 ; F03D11/04 ; F04D29/60 ; F04D29/52 ; F02C7/047 ; F02C6/20
摘要:
A rotating inlet cowl for a turbine engine, having a rotation axis and for which the forward end is arranged to be eccentric relative to this rotation axis. Furthermore, a forward cone of the cowl is truncated by a truncation surface defining the forward end of the inlet cowl.
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