Invention Grant
- Patent Title: Connecting a propulsion system to a structural element of an aircraft
- Patent Title (中): 将推进系统连接到飞机的结构元件
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Application No.: US12349697Application Date: 2009-01-07
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Publication No.: US08827203B2Publication Date: 2014-09-09
- Inventor: Wouter Balk
- Applicant: Wouter Balk
- Applicant Address: FR Paris
- Assignee: Snecma
- Current Assignee: Snecma
- Current Assignee Address: FR Paris
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0800336 20080123
- Main IPC: B64D27/00
- IPC: B64D27/00

Abstract:
An aircraft propulsion system (110) comprising a bypass turbojet engine surrounded by a nacelle defining a flow passage for the secondary stream flows, and connection means for connecting the engine to a wing (132) of an aircraft and comprising a pylon (134) substantially parallel to the longitudinal axis (135) of the engine together with suspension means suspending the engine from the pylon, the pylon being angularly offset from a vertical plane (150) containing the longitudinal axis of the engine and from the top of the nacelle, and being situated outside the flow path for the secondary stream.
Public/Granted literature
- US20090184198A1 CONNECTING A PROPULSION SYSTEM TO A STRUCTURAL ELEMENT OF AN AIRCRAFT Public/Granted day:2009-07-23
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