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Gyroscopic Inductance

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’ 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’s 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
 
N

Nemo

Jan 1, 1970
0
....
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

OK I am willing to believe this, what puzzles me is
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,

(minor point) what is gravitational interference?
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.

Until it runs down. Producing current will drain rotational energy out
of the system. Or are you claiming it is some form of perpetual energy
generator?

Personally if I were designing a satellite I would be wary of putting
something spinning at high revs in my delicate assembly. If anything
went wrong and it broke free it could wreak havoc. I assume satellites
have gyros for navigational / orientation purposes, but with heavy
armour around them... (don't really know enough about this). Similarly
an aircraft won't want something equivalent to a small bomb inside it.
Imagine the safety certification issues. I do know that gyro storage of
energy is generally best for big pulses of power, it's not too efficient
for a high energy density torage device. That's what batteries or, if
cost is no object, fuel cells are for.
 
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