TWO-DIMENSIONAL SUPERSONIC NOZZLE THRUST VECTORING USING STAGGERED RAMPS

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United States of America Patent

APP PUB NO 20190195169A1
SERIAL NO

16217370

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A system and method for vectoring the thrust of a supersonic, air-breathing engine. A thrust vectoring mechanism uses two asymmetrically staggered ramps; one placed at the throat, the other positioned at the exit lip of the nozzle of the engine to re-direct exhaust flow off-axis with the nozzle.

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Patent Owner(s)

Patent OwnerAddress
THE REGENTS OF THE UNIVERSITY OF CALIFORNIA1111 FRANKLIN STREET TWELFTH FLOOR OAKLAND CA 94607-5200

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Davis, Roger L Sacramento, US 5 121
Montes, Carlos F Sunnyvale, US 1 3

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