Re: electromagnets in the practice

On Sep 4, 4:16=A0am, rtk <rtarunku...@[EMAIL PROTECTED]
> wrote:
> First of all I am astonished by the experiment that is done by you. I
> have one small doubt in that. Since you used an "I" section I think
> that the path that is followed by the flux wont be the same as that of
> a flux due to the bar magnet. I think if you repeat the experiment
> with a core having a shape of bar the result would be good.

you might be intresed in this new technology ,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