GAS TURBINE ENGINE, PUSH INVESTION ASSEMBLY AND METHOD FOR OPERATING A PUSH INVERSION SYSTEM

摘要

The present invention relates to a thrust reversal assembly (44) for a gas turbine engine (10) and a method for its operation. the gas turbine engine comprises a central engine (14), a nacelle (12) involving, at least, a part of the center motor (14), defining a bypass duct (30) between the nacelle (12) and the center motor (14), wherein an outer door (48) movable between a stowed position (48) and a driven position (68) extends outside the nacelle (12) and a movable locking door (48, 50) between a stowed position and a driven position extends into an air flow duct (31) defined by the bypass duct (30) to deflect air outward.