INTEGRATED THRUST REVERSER ACTUATION SYSTEM

摘要

A turbofan engine assembly (10) having a turbine engine (16) and a nacelle (20) that surrounds at least a portion of the turbine engine (16) to define an annular bypass duct (22) that defines a forward-to-aft bypass air flow path. The turbofan engine assembly (10) further comprises a fixed portion (33) and a movable portion (27) which is movable in a direction along the bypass air flow path to an opened position that defines a thrust reversing outlet (28) through which at least a portion of the bypass air flow may be directed. At least one actuator (38) moves the movable portion (27) to the opened position.