Turbo jet-engine thrust reverser with scoop doors linked to a di

Power plants – Reaction motor – Interrelated reaction motors

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F02K 302

Patent

active

061518867

ABSTRACT:
A turbojet-engine thrust-reverser comprising pivoting hollow doors (3) which in the forward-thrust mode are integrated into the external cowling of the turbojet-engine and which in the thrust-reversal mode constitute scoop-type flow-deflecting baffles. A displaceable external cowling panel (20) covers both the fore frame (8) of the stationary structure and the cross-section of the flow exhaust of the door (3) when in the forward-thrust mode. The external cowling panel (20) is pivotable on a panel pivot (24) situated downstream of the pivot (9) of the door (3) and its upstream edge moves radially outward to simultaneously clear a space above the fore frame (8) and the exhaust cross-section for the deflected flow.

REFERENCES:
patent: 3475913 (1969-11-01), Mortlock et al.
patent: 5983625 (1999-11-01), Gonidec et al.
patent: 6000216 (1999-12-01), Vauchel
patent: 6082096 (2000-04-01), Vauchel

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