Thrust Vectoring Ignition Chamber Engine with Axial Fuel Intake System

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20210310357A1
SERIAL NO

17262758

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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This patent discloses thrust vectoring ignition chamber engine. Thrust vectoring ignition chamber used in this engine is an annular cylinder having nozzles mounted in a way such that during fuel suction phase they are sealed and during ignition of fuel they are unsealed so that hot jets of ignited fuel escaping through nozzles cause coupled rotatory motion on the ignition chamber. Engine uses specially designed dwell barrel cam mechanism for suction and compression of fuel. Flywheel mounted on extension of ignition chamber functions as output of the engine. Each half rotation of flywheel completes three phases namely fuel/air suction, compression and combustion. Thus this engine fires for every half revolution and therefore can give improved power boost.

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Patent Owner(s)

Patent OwnerAddress
GAUTAM RAVI SHANKARGAYA

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Gautam, Ravi Shankar Gaya, IN 10 1

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