Adjustable fairing for thrust reversers

Aeronautics and astronautics – Retarding and restraining devices – Friction brakes

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Details

23926533, B64C 1500

Patent

active

057303924

ABSTRACT:
A fairing for aerodynamically covering the actuation mechanism of a variable area exhaust nozzle, comprising an upper and a lower longitudinally extending half-fairing member and having a generally arcuate cross-section, each of the half-fairing members having an upstream and a downstream end, and two longitudinal edges, the half-fairing members being pivotally connected to each other at a pivot point near the upstream edges and a connection along one of the longitudinal edges of each of said half-fairing members for interengaging the other of the half-fairing members and allowing the half-fairing members to rotate about the pivot point for changing the aerodynamic surface area of the fairing upon variation of the area of the exhaust nozzle.

REFERENCES:
patent: 2989845 (1961-06-01), Howald
patent: 3833187 (1974-09-01), Kahler et al.
patent: 4049220 (1977-09-01), Rodgers
patent: 4349155 (1982-09-01), Donguy
patent: 4410152 (1983-10-01), Kennedy et al.
patent: 5181676 (1993-01-01), Lair
patent: 5221048 (1993-06-01), Lair
patent: 5343696 (1994-09-01), Rohra et al.

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