This is a new design for Gyroscopic Inductance circuit for DC current production using the gyroscope itself as the induction circuit for long term space flight. It will produce Direct current from a gyroscope functioning in a zero gravitational field as an inductance circuit. The two non-permeable gimbals=92 armatures rotate around a permanent inner magnet 180 degrees out of phase from one another giving 360 degrees of a full rotation that allow a 100% duty cycle when precession occurs. A north and south alignment on the spherical inner permanent magnet rotates around the central centrifugal spin axis witch doubles as a rotor flywheel. I have been working on the proto type for 15 years now utilizing nano carbon fiber as the coils in the inductor circuit; they are imbedded into the gyro=92s non- permeable gimbals in a zigzag pattern un-like the coils in an induction circuit. Magnetic couplers between the gyroscopes parts reduce further fatigue on the motor parts and reduce friction. There are strategically placed permeable alloys in the gimbal armatures when pulsed with DC current create magnetic field areas that interact with the rotor for start, stop and homing of the gimbals. if gravitational interference occurs in space flight a dc pulsed circuit 90 degrees adjacent from the rotor flywheel controlled with small pulses of current to control initial spin and braking on the central rotor while motor functions are restored as needed, This design has several viable applications for aro space industry. If solar panel deployment fails or damages to solar panels this is a solid backup for running the system operations of satellites and communication and instrumentation, imaging instrumentation devices for space flight.
RUSSELL JAMES HANCOCK Electronics Tech- Engineering Facilities and Planning Engineering Facilities and Planning
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