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
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Issued Date -
Jan 30, 2020
app pub date -
Dec 1, 2017
filing date -
Dec 1, 2017
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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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