Invention Grant
- Patent Title: Suspension assembly for an aircraft turbojet engine
- Patent Title (中): 用于飞机涡轮喷气发动机的悬架组件
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Application No.: US13146211Application Date: 2010-01-21
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Publication No.: US08985508B2Publication Date: 2015-03-24
- Inventor: Pierre Caruel , Guy Bernard Vauchel
- Applicant: Pierre Caruel , Guy Bernard Vauchel
- Applicant Address: FR Gonfreville l'Orcher
- Assignee: Aircelle
- Current Assignee: Aircelle
- Current Assignee Address: FR Gonfreville l'Orcher
- Agency: Brinks Gilson & Lione
- Priority: FR0900470 20090204
- International Application: PCT/FR2010/050090 WO 20100121
- International Announcement: WO2010/089487 WO 20100812
- Main IPC: B64D27/18
- IPC: B64D27/18 ; B64D27/12 ; B64D27/26 ; B64D29/06
Abstract:
A suspension assembly for an aircraft turbojet engine includes a pylon and connecting rods for taking up the thrust of the turbojet engine which is connected to the pylon. In particular, the suspension assembly includes an insulator which is separate from the pylon and thermally insulates the connecting rods from the turbojet engine.
Public/Granted literature
- US20110284686A1 SUSPENSION ASSEMBLY FOR AN AIRCRAFT TURBOJET ENGINE Public/Granted day:2011-11-24
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