Invention Grant
US08876018B2 Arrangement of thrust reverser flap link rods on the internal fixed structure of a turbojet engine nacelle
有权
涡轮喷气发动机舱的内部固定结构上的推力反向挡板连杆的布置
- Patent Title: Arrangement of thrust reverser flap link rods on the internal fixed structure of a turbojet engine nacelle
- Patent Title (中): 涡轮喷气发动机舱的内部固定结构上的推力反向挡板连杆的布置
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Application No.: US13656948Application Date: 2012-10-22
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Publication No.: US08876018B2Publication Date: 2014-11-04
- Inventor: Guy Bernard Vauchel , Peter Segat
- Applicant: Aircelle
- Applicant Address: FR Gonfreville l'Orcher
- Assignee: Aircelle
- Current Assignee: Aircelle
- Current Assignee Address: FR Gonfreville l'Orcher
- Agency: Brinks Gilson & Lione
- Priority: FR1052972 20100420
- Main IPC: B63H11/00
- IPC: B63H11/00 ; B64D33/04 ; F02K1/00 ; F02K3/02 ; F02K1/62 ; F16C7/02 ; F02K1/72 ; B64D29/06 ; F02K1/76
Abstract:
An arrangement is provided that includes a thrust reverser flap link rod on an internal fixed structure of a turbojet engine nacelle. The link rod is connected to the internal fixed structure by an elastic means that is a spring.
Public/Granted literature
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