Engine and thrust reverser actuation system
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United States of America Patent
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Mar 6, 2018
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N/A
app pub date -
Mar 10, 2016
filing date -
Nov 16, 2012
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Abstract
A thrust reverser actuation system for a jet engine having a turbine engine surrounded by a nacelle to define an annular air flow path between the turbine engine and the nacelle, with a thrust reverser having a movable element to reverse the direction of at least a portion of the air flow along the air flow path, where the thrust reverser actuation system includes a hydraulic actuator configured to be operably coupled to the movable element, and a remote actuator that controls the inhibit function of the hydraulic system.
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