Invention Grant
- Patent Title: Thrust reverser for a turbojet engine nacelle comprising an end-of-travel stop on the primary guide rail
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Application No.: US15076907Application Date: 2016-03-22
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Publication No.: US09835113B2Publication Date: 2017-12-05
- Inventor: Alexis Loncle
- Applicant: AIRCELLE
- Applicant Address: FR Gontreville l'Orcher
- Assignee: AIRCELLE
- Current Assignee: AIRCELLE
- Current Assignee Address: FR Gontreville l'Orcher
- Agency: Burris Law, PLLC
- Priority: FR1359104 20130923
- Main IPC: F02K1/78
- IPC: F02K1/78 ; F02K1/76 ; F02K1/72 ; B64D29/06 ; E05B63/18 ; F02K1/80

Abstract:
The present disclosure relates to a thrust reverser for a turbojet engine nacelle, including cowls that move backwards to open the thrust reverser. Each cowl includes a primary axial guide rail that receives most of the loads of the cowl, and secondary rails guiding an outer portion of each cowl. The thrust reverser includes a rear end stop for each cowl is arranged on the primary axial guide rails.
Public/Granted literature
- US20160281640A1 THRUST REVERSER FOR A TURBOJET ENGINE NACELLE COMPRISING AN END-OF-TRAVEL STOP ON THE PRIMARY GUIDE RAIL Public/Granted day:2016-09-29
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