Invention Grant
US09243562B1 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.: US14620798Application Date: 2015-02-12
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Publication No.: US09243562B1Publication Date: 2016-01-26
- Inventor: Mickael Delapierre , Herve Gignoux , Gael Loro , Sylvie Wintenberger
- Applicant: SNECMA
- 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
- Main IPC: F02C7/047
- IPC: F02C7/047 ; F02C6/20 ; F02K3/06
Abstract:
A rotating inlet cowl for a turbine engine includes a rotation axis. The rotating inlet cowl includes a forward cone defining a forward end of the inlet cowl. The forward end is configured to be eccentric relative to the rotation axis of the inlet cowl. Furthermore, the forward cone is truncated by a truncation surface defining the forward end of the inlet cowl.
Public/Granted literature
- US20160003146A1 ROTATING INLET COWL FOR A TURBINE ENGINE, COMPRISING AN ECCENTRIC FORWARD END Public/Granted day:2016-01-07
Information query
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