Invention Grant
- Patent Title: Door-type thrust reverser device for aircraft turbojet engine nacelle
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Application No.: US15286955Application Date: 2016-10-06
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Publication No.: US10605196B2Publication Date: 2020-03-31
- Inventor: Pierre Caruel , Thiery Le Docte
- Applicant: AIRCELLE
- Applicant Address: FR Gonfreville l'Orcher
- Assignee: AIRCELLE
- Current Assignee: AIRCELLE
- Current Assignee Address: FR Gonfreville l'Orcher
- Agency: Burris Law, PLLC
- Priority: FR1453106 20140408
- Main IPC: F02K1/60
- IPC: F02K1/60 ; F02K1/82 ; F02K1/70 ; F02K1/76

Abstract:
A door-type thrust reverser device for a turbojet engine nacelle is provided that includes a fixed structure, a mobile structure mobile with respect to said fixed structure, and at least one door mounted with the ability to pivot via pivots between a retracted position corresponding to the nacelle operating in direct-jet mode, and a deployed position corresponding to the nacelle operating in reverser-jet mode. The thrust reverser device includes a device for bleeding off some of a secondary or bypass airflow, which device is able to bleed off part of the secondary airflow from a duct through which the secondary airflow circulates and for conveying said bled-off airflow toward at least one pivot of the door, so as to cool areas on and/or around the door pivots.
Public/Granted literature
- US20170022934A1 DOOR-TYPE THRUST REVERSER DEVICE FOR AIRCRAFT TURBOJET ENGINE NACELLE Public/Granted day:2017-01-26
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