Invention Grant
- Patent Title: Propulsion system with integrated pylon
- Patent Title (中): 集成塔式推进系统
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Application No.: US11857735Application Date: 2007-09-19
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Publication No.: US07938359B2Publication Date: 2011-05-10
- Inventor: Thibaud Jean-Baptiste Guibert , Guillaume Lefort , Marc Patrick Tesniere
- Applicant: Thibaud Jean-Baptiste Guibert , Guillaume Lefort , Marc Patrick Tesniere
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0608216 20060920
- Main IPC: B64D27/00
- IPC: B64D27/00 ; B64D27/26 ; B64D29/06
Abstract:
A propulsion system for an airplane having an integrated pylon includes a bypass turbojet and a nacelle. The nacelle has a downstream cylindrical part which is rigid and is attached at its upstream end to an intermediate case of the engine. This downstream cylindrical part also includes a longitudinal beam for attaching rods to secure the engine to the airplane.
Public/Granted literature
- US20080067287A1 PROPULSION SYSTEM WITH INTEGRATED PYLON Public/Granted day:2008-03-20
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