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Re: jet powered coil



Original poster: "davep by way of Terry Fritz <twftesla-at-qwest-dot-net>" <davep-at-quik-dot-com>

> Here is how it would work:
 
> Gas turbo jet runs normally, the exhaust is used to spin

> another shaft with an Impeller at one end and the alternator

> at the other. Because it is not 

	Tricky to get the efficiency up.  It can be done.

> physically connected to the drive turbo I could slow it at

> will.

	THAT will cost efficiency, LOTS of efficiency,
	unless slowing is done with gears, or VERY carefully
	designed rotor.  And getting gears to live at
	50,000 RPM is tricky.  I believe that where
	Gas turbines are used for Shaft output (RR, Power
	Plants, choppers (??) they run them slower.  a LOT
	slower.

> This would make the HZ adjustable. I will have to create my

> own alternator to deal with the high rpm. I don't see the

> alternator spinning at more than 50,000 rpm

	Normal engineering practice limits such 3600 RPM and
	down.  Stresses in materials go up as square of speed.


> because it will not be attached to the main drive turbo.
> I was talking to Bert over on tesla-2 and he has a few novel ideas. 
> http://tesla-2-dot-org/pipermail/tesla-2/2002-September/date.html

> At this point I'm concerned with the voltage.

	Voltage can always be adjusted with a transformer.

> At the very least I would like to run a Jacobs ladder.

	3,000vac and up.

> I now know one could not run a conventional transformer on

> such high HZ.  One needs a ferrite core.
> Can the alternator be wound to produce high voltage directly?

	It CAN.  But.  It also needs to be INSULATED for the
	HV.  (I believe commercial, power station alternators
	are routinely wound for 5,000VAC and thereabouts.)

	best
	dwp

...the net of a million lies...
	Vernor Vinge
There are Many Web Sites which Say Many Things.
	-me