Aircraft engine interface fairing support

Details Aircraft engine interface fairing support Aircraft engine interface fairing support

1988-03-09

1990-01-09

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

With means controlling amount, shape or direction of...

23926533, 23926539, 60242, B64C 1506

Patent

active

048922544

ABSTRACT:
An actuator positioning convergent/divergent nozzle flaps is supported from a stiffner on a support structure. An interface fairing for separating possible hot gas flow from engine fumes is supported from the support structure at a location which avoids fairing deflecting as a function of stiffner deflection. Interference between the fairing and nozzle flap drive is thereby avoided.

REFERENCES:
patent: 2972226 (1961-02-01), Geary
patent: 2984068 (1961-05-01), Eatock
patent: 3712547 (1973-01-01), Smale et al.
patent: 3792815 (1974-02-01), Swavely et al.
patent: 4022948 (1977-05-01), Smith et al.
patent: 4456178 (1984-06-01), Jones et al.

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