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US Patent 7484356 Cascade reverser without blocker doors

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Patent
Patent
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Patent attributes

Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
0
Patent Number
74843560
Patent Inventor Names
Jean-Pierre Lair0
Date of Patent
February 3, 2009
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Patent Application Number
114918900
Date Filed
July 24, 2006
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Patent Citations Received
‌
US Patent 11781506 Splitter and guide vane arrangement for gas turbine engines
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US Patent 11661906 Propulsion system arrangement for turbofan gas turbine engine
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Patent Primary Examiner
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William H Rodríguez
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Patent abstract

A translating cowl composed of two sub-structures forms the thrust reverser for a turbofan engine. The two sub-structures form the rear part of a nacelle, are translatable, and have operative and inoperative modes of operation. The operative mode is used for direct or reverse thrust operation of the engine and the inoperative mode is used for access to the engine.

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