ENGINE WITH A THRUST REVERSER LOCKOUT MECHANISM

A turbofan engine having a thrust reverser having at least one movable control surface, movable to and from a reversing position where at least a portion of the bypass air flow is at least partially reversed, a thrust reverser actuation system having multiple actuators and a lockout mechanism movabl...

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Bibliographische Detailangaben
Hauptverfasser: OZANICH, Brent Michael, WILLETT, Kenneth R, SPIRY, Jonathan LaReine, LARKIN, Jeffrey Michael, BECK, Daniel Peter, CONWAY, George Arnold
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:A turbofan engine having a thrust reverser having at least one movable control surface, movable to and from a reversing position where at least a portion of the bypass air flow is at least partially reversed, a thrust reverser actuation system having multiple actuators and a lockout mechanism movable between an inhibit condition, wherein movement of the multiple actuators is prevented, and a permit condition, wherein movement of the multiple actuators is permitted.