Invention Grant
- Patent Title: Thrust reverser system having limited aerodynamic disturbance
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Application No.: US16007006Application Date: 2018-06-13
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Publication No.: US10669970B2Publication Date: 2020-06-02
- Inventor: Olivier Pautis , Lionel Czapla
- Applicant: Airbus Operations S.A.S.
- Applicant Address: FR
- Assignee: Airbus Operations S.A.S.
- Current Assignee: Airbus Operations S.A.S.
- Current Assignee Address: FR
- Agency: Lerner, David, Littenberg, Krumholz & Mentlik, LLP
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@ec87015
- Main IPC: F02K1/70
- IPC: F02K1/70 ; F02K1/76 ; F02K1/72

Abstract:
A thrust reverser system includes two thrust reversal cascades, of which the first cascade is entrained by an actuator, and which are configured to adopt a retracted position in which they are housed in a space located outside the duct. The action of the actuator brings about: rearward displacement of the first cascade in the direction of a nacelle opening; and during part of the rearward displacement of the second cascade, simultaneous pivoting of this second cascade under the action of a control lever, the interaction of which with a fixed guide rail forces the front end of the lever to move radially inwards while the lever is entrained rearwards by the second cascade.
Public/Granted literature
- US20180372024A1 Thrust Reverser System Having Limited Aerodynamic Disturbance Public/Granted day:2018-12-27
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