THRUST REVERSER COMPRISING FIXED CASCADES AND A SEALING MEMBRANE
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United States of America Patent
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Issued Date -
Mar 27, 2025
app pub date -
Jan 6, 2023
filing date -
Jan 6, 2023
priority date (Note) -
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Abstract
A thrust reverser for an aircraft propulsion assembly, including a fixed structure equipped with at least one cascade as well as a radially inner delimiting wall of a secondary vein, and a movable structure including at least one reverser cowling, the cascade being arranged, in the forward direct thrust position, in a housing of the reverser cowling, and, in the retracted thrust reversal position, the wall reveals a passage opening of the secondary vein towards the cascade, the thrust reverser also including at least one sealing membrane designed to deflect at least one portion of the secondary flow. A hook is provided for securing the membrane to a rear cascade support frame, and to the radially inner delimiting wall of the secondary vein.
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