Jet pipe for supporting a thrust reverser for aircraft jet engin

Aeronautics and astronautics – Retarding and restraining devices – Friction brakes

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Details

23926527, 23926519, B64D 3304

Patent

active

053908791

ABSTRACT:
A jet exhaust pipe for aircraft jet engines comprising a fixed structure, a pair of movable shells surrounding the gas discharge end of the fixed structure, the shells being connected to the fixed structure on opposite sides thereof, a pair of thrust reverser doors pivotally connected to the fixed structure, and an actuator for moving the thrust reverser doors and the shells between a first, non-reversing position and a second, reversing position, wherein the shells form a portion of the gas flow surface of the jet exhaust pipe in the first position, and are out of the gas flow in the second position.

REFERENCES:
patent: 2975593 (1961-03-01), Bauger et al.
patent: 5054285 (1991-10-01), Geidel et al.
patent: 5176340 (1993-01-01), Lair

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