Invention Grant
- Patent Title: Aircraft turbojet engine comprising two thrust reverser modules
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Application No.: US17575686Application Date: 2022-01-14
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Publication No.: US11692511B2Publication Date: 2023-07-04
- Inventor: Jérôme Lescoup
- Applicant: Airbus Operations SAS
- Applicant Address: FR Toulouse
- Assignee: AIRBUS OPERATIONS SAS
- Current Assignee: AIRBUS OPERATIONS SAS
- Current Assignee Address: FR Toulouse
- Agency: Greer, Burns & Crain, Ltd.
- Priority: FR 00470 2021.01.19
- Main IPC: F02K1/80
- IPC: F02K1/80 ; F02K1/72 ; F02C7/28 ; F01D11/00 ; B64D29/08

Abstract:
A turbojet engine with two thrust reverser modules. Each module includes an outer casing, an inner casing and a securing system for securing the inner casing to the outer casing which comprises first and second hoods. A housing between the hoods has a securing wall, a seal with a sausage secured to the securing wall, and a crusher rigidly secured to the second hood and arranged so as to crush the sausage towards the securing wall when the second hood goes from the spaced-apart position to the close-together position. Therefore, the sausage moves in the longitudinal direction, thus limiting shearing of the seal and transverse movements owing to the manufacturing and assembly tolerances and the movements in flight.
Public/Granted literature
- US20220228540A1 AIRCRAFT TURBOJET ENGINE COMPRISING TWO THRUST REVERSER MODULES Public/Granted day:2022-07-21
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