NACELLE FOR AN AIRCRAFT TURBOJET ENGINE PROVIDED WITH A DEVICE FOR DETECTING DEFORMATION OF ITS MOVABLE STRUCTURE

    公开(公告)号:US20200031485A1

    公开(公告)日:2020-01-30

    申请号:US16467718

    申请日:2017-12-01

    Abstract: A nacelle for an aircraft turbojet engine includes a thrust-reversing device with a fixed structure and a movable structure translatably movable along an axis substantially parallel with a longitudinal axis of the nacelle between a retracted position in which it provides aerodynamic continuity with the fixed structure of the nacelle during operation of the nacelle with forward thrust and a deployed position in which it opens a passage intended for the circulation of a diverted secondary air flow during operation of the nacelle with reverse thrust. The nacelle includes at least one position sensor configured and arranged in the nacelle for detecting a deformation of the movable structure exceeding a permitted predetermined deformation threshold.

    THRUST REVERSER FOR NACELLE OF AIRCRAFT TURBOFAN

    公开(公告)号:US20170328305A1

    公开(公告)日:2017-11-16

    申请号:US15371281

    申请日:2016-12-07

    CPC classification number: F02K1/72 F02K1/1261 F02K1/763 Y02T50/671

    Abstract: A thrust reverser for a nacelle of an aircraft turbojet engine includes at least one movable thrust reverser cowl, a means for locking the cowl, a variable section outlet nozzle, and at least one actuator including an actuator rod. The thrust reverser is provided with a resilient coupler comprising a body which is rigidly connected to the thrust reverser cowl and a resilient return and abutment device that engages with the actuating rod of the actuator such as to resiliently return the nozzle to a neutral position. The return device is calibrated such that, when the cowl is unlocked, the return device opposes the relative movement of the actuating rod relative to the cowl, such as to enable the movement of the cowl and the nozzle, and when the cover is locked, the actuator drives the actuating rod against the return device to enable the movement of the nozzle.

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