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
530 South Norris Street
Tucson, Arizona 85719
(520) 225-4625 fax (520) 225-4965
Cellular (520) 400-2578
