Nacelle for an aircraft turbojet engine provided with a device for detecting deformation of its movable structure
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United States of America Patent
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Jul 19, 2022
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N/A
app pub date -
Dec 1, 2017
filing date -
Dec 7, 2016
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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.
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