INTEGRATED THRUST REVERSER ACTUATION SYSTEM
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United States of America Patent
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Jul 11, 2014
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Jul 11, 2014
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Abstract
A turbofan engine assembly having a turbine engine and a nacelle that surrounds at least a portion of the turbine engine to define an annular bypass duct that defines a forward-to-aft bypass air flow path. The turbofan engine assembly further comprises a fixed portion and a movable portion which is movable in a direction along the bypass air flow path to an opened position that defines a thrust reversing outlet through which at least a portion of the bypass air flow may be directed. At least one actuator moves the movable portion to the opened position.
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