After many years, this can be answered with confidence. Basically, the utron is a mercury battery. So it generated electromagnetic charge that could be harnessed from the positive and negative tips of the utron. It was more like an electret, though.
Now the spinning disks were definitely made of electret material. That is the Townsend Brown principle. An electret is basically a battery that never dies. It doesn't necessarily have to make a large electrostatic field or charge field, sometimes they do that.. but it's basically a battery material (charged mass). So a current is passed over and through a spinning mass that is charged, then there's your Townsend Brown effect; it levitates.
So how do you make a mercury vapor electret?? Well... Copper can be used with Mercury! Mercury is the anode, and copper is the cathode! So here is a simple utron battery setup, putting mercury within copper plates inside an aluminum housed utron!
Furthermore, the mercury gets to spin around in a circle! (circular revolutions, which is known to produce an antigravity warping effect) .. By "warping effect" it alters time and space, but makes a torsion field!
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If people will remember when the Great Pyramid of Giza was breached, or maybe it was the long tunnel that led into the pyramids from a considerable distance away.. in any case, it was opened and the researchers died. It is believed that they died due to mercury vapor poisoning from mercury vapor escaping the chamber, and the researchers got a lung full.
In ancient Egypt, and in all other ancient structures throughout the world, pools of mercury were found sometimes. Mercury batteries from the vapor was used to power a lighting system within the ancient structures.
The utrons were a charge field that powered the system, and moved in co-counter rotation to the charged spinning mass creating the Townsend Brown effect -- levitation and an in combination with the central accumulator, a negative energy gravity cancellation effect.
Here is a patent link:
John St. CLAIR Patent Applications US2003230675 Rotor Inductance Propulsion System
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