Invention Grant
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
- Patent Title: Rotating inlet cowl for a turbine engine, comprising an eccentric forward end
- Patent Title (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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Application No.: US13262386Application Date: 2010-03-31
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Publication No.: US08984855B2Publication Date: 2015-03-24
- Inventor: Mickael Delapierre , Herve Gignoux , Gael Loro , Sylvie Wintenberger
- Applicant: Mickael Delapierre , Herve Gignoux , Gael Loro , Sylvie Wintenberger
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0952056 20090331
- International Application: PCT/EP2010/054080 WO 20100331
- International Announcement: WO2010/112453 WO 20101007
- Main IPC: F02G3/00
- IPC: F02G3/00 ; F02K1/78 ; F02K99/00 ; F02K3/06 ; B64D15/16 ; B64D15/00 ; F03B15/22 ; F03D11/04 ; F04D29/60 ; F04D29/52 ; F02C7/047 ; F02C6/20
Abstract:
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.
Public/Granted literature
- US20120036827A1 ROTATING INLET COWL FOR A TURBINE ENGINE, COMPRISING AN ECCENTRIC FORWARD END Public/Granted day:2012-02-16
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