TURBOJET ENGINE NACELLE THRUST REVERSER COMPRISING CASCADES SECURED TO THE MOBILE COWLS
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United States of America Patent
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app pub date -
Nov 24, 2015
filing date -
Jun 7, 2013
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Abandoned
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Abstract
A thrust reverser of a turbojet engine nacelle includes mobile cowls which retreat with respect to a front frame while causing via cylinders the tipping of the shutters initially folded inside these cowls, so as to substantially close an annular stream of cold air, and cascades disposed around the annular stream which receive the cold air flow in order to send it towards the front. In particular, the cascades are secured to the mobile cowls and slide.
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