Fuselage tail jet engine thrust reverser and method

Aeronautics and astronautics – Retarding and restraining devices – Friction brakes

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Details

244 125, 244 23D, 244100R, 244 50, 181222, 23926529, B64D 3304

Patent

active

RE0315915

ABSTRACT:
Production of a downwardly and forwardly directed reverse thrust discharged from a reverse-thrust duct is controlled during landing by a door in the rearward-discharge duct having its rearward portion pivotally mounted for swinging of its forward portion between a position lodged in a recess in the side of the rearward-discharge duct and a position in which the forward edge of the door is spaced from the recess and the door is inclined to deflect jet exhaust from the rearward-discharge duct into the reverse-thrust duct branching from the rearward-discharge duct. The discharge end of the reverse-thrust duct can be closed by a second door and actuating [means] mechanism interconnecting the two doors can move them simultaneously through proportionate degrees of movement.

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