Invention Grant
- Patent Title: Thrust reverser for an aircraft bypass turbojet engine nacelle
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Application No.: US17999106Application Date: 2021-05-17
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Publication No.: US12049853B2Publication Date: 2024-07-30
- Inventor: Xavier Cazuc , Jean-Philippe Joret , Vincent Jean-François Peyron , Sébastien Laurent Marie Pascal
- Applicant: SAFRAN NACELLES
- Applicant Address: FR Gonfreville-l'Orcher
- Assignee: SAFRAN NACELLES
- Current Assignee: SAFRAN NACELLES
- Current Assignee Address: FR Gonfreville-l'Orcher
- Agency: CHRISTENSEN O'CONNOR JOHNSON KINDNESS PLLC
- Priority: FR 05254 2020.05.20
- International Application: PCT/FR2021/050846 2021.05.17
- International Announcement: WO2021/234254A 2021.11.25
- Date entered country: 2022-11-17
- Main IPC: F02K1/72
- IPC: F02K1/72 ; F02K3/06

Abstract:
A thrust reverser for an aircraft bypass turbojet engine nacelle has a generally annular shape around an axis and includes an annular frame for securing deflection grids. The frame has a first frusto-conical wall widening in the downstream direction and including an upstream peripheral edge configured to be attached to a casing of the turbojet engine. A downstream peripheral edge of the wall extends in the continuation of the wall and secures the upstream ends of the grids. A second annular wall extends radially outwards from an outer frusto-conical face of the first wall. The first and second walls are integrally formed and the second wall has axial openings through which actuators pass.
Public/Granted literature
- US20230184195A1 THRUST REVERSER FOR AN AIRCRAFT BYPASS TURBOJET ENGINE NACELLE Public/Granted day:2023-06-15
Information query
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