Variable-area thrust vectoring and reversing asymmetric aircraft

Details Variable-area thrust vectoring and reversing asymmetric aircraft Variable-area thrust vectoring and reversing asymmetric aircraft

1987-10-02

1989-03-21

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

23926541, 244 23D, 244110B, B64C 1502

Patent

active

048136077

ABSTRACT:
A variable-area, thrust vectoring, and thrust reversing aircraft propulsion nozzle includes mechanization which is uniquely simple, strong, and lightweight, as well as being able to endure the harsh, high-temperature environment of a jet engine exhaust flow. The nozzle employs a minimal number of actuators, and structure which is isolated from reversing thrust forces so that an overall objective of strength, simplicity, and lightweight is achieved by the invention.

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