Gyromotor

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United States of America Patent

APP PUB NO 20120024633A1
SERIAL NO

13135932

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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Gyromotor is a type of action and reaction motor which generates thrust without plume ejection. Whereas rockets react equal and opposite to ejected mass momentum, Gyromotor cycles gyroscopes, each mounted on the end of a moment arm, in a back and forth rowing motion to drive a spacecraft, without external mass ejection analogous to rowing a boat. Gyroscope inertial properties are configured to provide maximum resistance torque during the drive stroke and reconfigured to provide minimum torque resistance during the return stroke. The gyroscopes are turned by a moment arm so the torque resistance provides a useful linear pseudo force component to drive the spacecraft, with said linear force greater during the drive stroke than the return stroke, analogous to an oar in water during the drive stroke and in air during the return stroke. The space craft moves in reaction to the net linear pseudo forces and momentum is conserved. The pseudo forces are caused by the change of direction of each gyroscope spin axis during its moment arm rotation, similar to centripetal and coriolis effect, pseudo forces.

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Patent Owner(s)

Patent OwnerAddress
VRANISH JOHN MNot Provided

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Vranish, John M Crofton, US 49 1360

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