Invention Grant
- Patent Title: Thrust reverser for the nacelle of an aircraft turbofan engine
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Application No.: US18556312Application Date: 2022-04-27
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Publication No.: US12140107B2Publication Date: 2024-11-12
- Inventor: Sebastien Laurent Marie Pascal , Luigi Bisanti
- Applicant: SAFRAN NACELLES
- Applicant Address: FR Gonfreville-l'Orcher
- Assignee: SAFRAN NACELLES
- Current Assignee: SAFRAN NACELLES
- Current Assignee Address: FR Gonfreville-l'Orcher
- Agency: WOMBLE BOND DICKINSON (US) LLP
- Priority: FR2104530 20210430
- International Application: PCT/FR2022/050797 WO 20220427
- International Announcement: WO2022/229556 WO 20221103
- Main IPC: F02K1/72
- IPC: F02K1/72 ; F02K1/76 ; F02K1/80

Abstract:
A thrust reverser for an aircraft bypass turbojet engine nacelle, this thrust reverser having a generally annular shape around an axis and including in particular flaps for deflecting the secondary flow through gratings, each of these flaps having a rigid wall and sealing elements located on the outer face of this wall, these sealing elements extending along side edges of the flap so as to provide a seal along these edges in the first position.
Public/Granted literature
- US20240209813A1 THRUST REVERSER FOR THE NACELLE OF AN AIRCRAFT TURBOFAN ENGINE Public/Granted day:2024-06-27
Information query
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