Device for increasing and deflecting thrust of jet-propulsion en

Power plants – Reaction motor – With thrust direction modifying means

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23926535, F02K 100, F02K 138

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active

045878048

ABSTRACT:
A vertical/short takeoff and landing (V/STOL) aircraft in which the exhaust gas from a jet-propulsion engine is discharged through an exhaust gas passage, secondary air induction passages are formed on the outer sides of the nozzle for communicatively connecting the outside atmosphere to the upstream end of the exhaust gas passage, to induct outside air as secondary air into the exhaust gas passage to be mixed with the exhaust gas. Inlet flap gates are respectively provided at the inlet ends of the secondary air induction passages. A deflector device is provided at the outlet part of the exhaust gas passage and includes guide vanes movable to a central zone in a deflected flow path.

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patent: 4392615 (1983-07-01), Madden

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