Disk engine with circumferential swirl radial combustor

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 12018613
SERIAL NO

17846633

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Abstract

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A disk engine and system configured to provide high power at a reduced axial length is disclosed herein. The disk engine includes a radial compressor, a compressor discharge manifold positioned circumferentially about compressor, a combustion chamber positioned within the discharge manifold and a radial turbine positioned radially inward of the combustion chamber.

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Patent Owner(s)

Patent OwnerAddress
GOVERNMENT OF THE UNITED STATES AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE2240 B STREET BUILDING 11 AREA B WRIGHT-PATTERSON AFB OH 45433-7109

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bohan, Brian Dayton, US 2 0
Polanka, Marc Huber Heights, US 4 0
Staton, Bennett Beavercreek, US 2 0

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