Invention Grant
- Patent Title: Thrust reverser with flaps controlled by a mechanism equipped with aeronautical bellcranks
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Application No.: US17770900Application Date: 2020-10-20
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Publication No.: US11885281B2Publication Date: 2024-01-30
- Inventor: Josse Plaquin , Cedric François Pierre Renault
- Applicant: SAFRAN NACELLES
- Applicant Address: FR Gonfreville-l'Orcher
- Assignee: SAFRAN NACELLES
- Current Assignee: SAFRAN NACELLES
- Current Assignee Address: FR Gonfreville-l'Orcher
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR 11975 2019.10.25
- International Application: PCT/FR2020/051885 2020.10.20
- International Announcement: WO2021/079054A 2021.04.29
- Date entered country: 2022-04-21
- Main IPC: F02K1/72
- IPC: F02K1/72 ; F02K1/76

Abstract:
An aeronautical thrust reverser including a sliding cowl, shutter flaps and deflection cascades. The reverser includes, for each flap, a return member hinged to the sliding cowl, to a driving connecting rod itself hinged to a front frame of the reverser, and to a return connecting rod itself hinged to the flap, the latter being moreover hinged by its rear end to the sliding cowl. The return member, the driving connecting rod and the return connecting rod form an actuation system capable of opening the secondary flow duct in a direct thrust configuration.
Public/Granted literature
- US20220397078A1 THRUST REVERSER WITH FLAPS CONTROLLED BY A MECHANISM EQUIPPED WITH AERONAUTICAL BELLCRANKS Public/Granted day:2022-12-15
Information query
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