A thrust reverser system for a gas turbine engine includes a duct including a cowling movable between an open position and a closed position in a direction transverse to a centerline of the gas turbine engine. The thrust reverser is supported within the cowling and movable between an axial closed position, an axial intermediate position and an axial open position. A controller is actuateable to command movement of the thrust reverser from the axial closed position to the axial intermediate position such that the cowling is free to move to the open position.
Thrust reverser maintenance actuation system
2015-12-22
Patent
Elektronische Ressource
Englisch
Boeing 777 thrust reverser actuation system
Online Contents | 1998
|Electric Thrust Reverser Actuation Systems
SAE Technical Papers | 2002
|Boeing 777 thrust reverser actuation system
Emerald Group Publishing | 1998
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