kalamar
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Patent Issued for Anti-gravity Device
Claims made in the Patent about the technology:
1. A space vehicle propelled by the pressure of inflationary vacuum state is claimed comprising:
a hollow superconductive shield,
an inner shield, the inner shield disposed inside said hollow superconductive shield, said inner shield comprising an upper shell and a lower shell,
a support structure, the support structure disposed between said hollow superconductive shield and said inner shield concentrically to said hollow superconductive shield, said support structure comprised of an upper rotating element and a lower rotating element,
upper means for generating an electromagnetic field, the upper means for generating an electromagnetic field disposed between said hollow superconductive shield and said upper shell, affixed to said upper rotating element at an electromagnetic field-penetrable distance to said hollow superconductive shield,
lower means for generating an electromagnetic field, the lower means for generating an electromagnetic field disposed between said hollow superconductive shield and said lower shell, affixed to said lower rotating element at an electromagnetic field-penetrable distance to said hollow superconductive shield,
electric motors, the electric motors disposed inside said hollow superconductive shield along the central axis of said hollow superconductive shield,
a power source, the power source disposed inside said hollow superconductive shield, said power source electrically connected with said upper means for generating an electromagnetic field, said lower means for generating an electromagnetic field, and said electric motors,
life-support equipment, the life-support equipment disposed inside said inner shield,
a flux modulation controller, the flux modulation controller disposed inside said inner shield, said flux modulation controller in communication with said upper means for generating an electromagnetic field, said lower means for generating an electromagnetic field, said power source, and said electric motors, and
a crew, the crew disposed inside said inner shield accessibly to said life-support and said flux modulation controller.
2. The space vehicle of claim 1 wherein said hollow superconductive shield is composed of a high-temperature ceramic superconductor with a composite crystal structure, and is cooled to a temperature of about 40 degrees K.
3. The space vehicle of claim 1 wherein said inner shield is composed of insulating materials such as foamed ceramics.
4. The space vehicle of claim 1 wherein said power source is a nuclear generator.
5. The space vehicle of claim 1 wherein said flux modulation controller is a computer.
6. The space vehicle of claim 1 wherein said upper rotating element and said lower rotating element are pivoted, urged to rotate by said upper means for generating an electromagnetic field, said lower means for generating an electromagnetic field, and said electric motors.
7. The space vehicle of claim 1 wherein said hollow superconductive shield is pivoted and urged to rotate by said upper means for generating an electromagnetic field, said lower means for generating an electromagnetic field, and said electric motors.
8. A method for generating pressure anomaly of inflationary vacuum state is claimed comprising the following steps, some occurring simultaneously:
providing a space vehicle comprising a hollow superconductive shield, an inner shield, a support structure, upper means for generating an electromagnetic field, lower means for generating an electromagnetic field, electric motors, a power source, life-support equipment, a flux modulation controller, and a crew,
generating electrical energy in said power source,
converting said electrical energy into an electromagnetic field in said upper means for generating an electromagnetic field and said lower means for generating an electromagnetic field,
converting said electrical energy into mechanical energy in said electrical motors,
rotating said upper means for generating an electromagnetic field and said lower means for generating an electromagnetic field relative to said hollow superconductive shield,
converting said electromagnetic field into a gravitomagnetic field in said hollow superconductive shield,
propagating said gravitomagnetic field outward, orthogonal to the walls of said hollow superconductive shield, and
forming a pressure anomaly of inflationary vacuum state in the area of propagation of said gravitomagnetic field, the pressure anomaly of inflationary vacuum state comprised of an area of relatively lower vacuum pressure density in front of said space vehicle and an area of relatively higher vacuum pressure density behind said vehicle,
whereby said space vehicle is urged to move from said area of relatively higher vacuum pressure density toward said area of relatively lower vacuum pressure density.
9. The method of claim 8 wherein said pressure anomaly of inflationary vacuum state is a substantially droplet-shaped anomaly associated with lowered pressure of inflationary vacuum state provided by the propagation of a gravitomagnetic field radiating orthogonally away from the front of said hollow superconductive shield,
whereby providing for the gravitational imbalance where the lowered pressure of inflationary vacuum state is pulling said space vehicle forward.
10. The method of claim 8 wherein said pressure anomaly of inflationary vacuum state is a substantially droplet-shaped anomaly associated with elevated pressure of inflationary vacuum state provided by the propagation of a gravitomagnetic field radiating orthogonally away from the back of said hollow superconductive shield,
whereby providing for the gravitational imbalance where the elevated pressure of inflationary vacuum state is pushing said space vehicle forward.
11. The method of claim 8 wherein said pressure anomaly of inflationary vacuum state is comprised of a substantially droplet-shaped anomaly associated with lowered pressure of inflationary vacuum state and a substantially droplet-shaped anomaly associated with elevated pressure of inflationary vacuum state,
whereby providing for the gravitational imbalance where the lowered pressure of inflationary vacuum state is pulling, and the elevated pressure of inflationary vacuum state is pushing, said space vehicle forward.
12. The method of claim 8 wherein said pressure anomaly of inflationary vacuum state is a substantially egg-shaped anomaly associated with lowered pressure of inflationary vacuum state provided by the unequally-distributed gravitomagnetic field propagated in all directions orthogonally away from said hollow superconductive shield with an area of lowest vacuum pressure density disposed directly in front said space vehicle,
whereby providing for the gravitational imbalance such that the lowered pressure of inflationary vacuum state is pulling said space vehicle forward in modified spacetime.
13. The method of claim 8 wherein said pressure anomaly of inflationary vacuum state is a substantially egg-shaped anomaly associated with elevated pressure of inflationary vacuum state provided by the unequally-distributed gravitomagnetic field propagated in all directions orthogonally away from said hollow superconductive shield with an area of highest vacuum pressure density disposed directly behind said space vehicle, whereby providing for the gravitational imbalance such that the highest pressure of inflationary vacuum state is pushing said space vehicle forward in modified spacetime at a speed possibly approaching a local light-speed, the local light-speed which may be substantially higher than the light-speed in the ambient space.
http://www.physorg.com/news8042.html
Claims made in the Patent about the technology:
1. A space vehicle propelled by the pressure of inflationary vacuum state is claimed comprising:
a hollow superconductive shield,
an inner shield, the inner shield disposed inside said hollow superconductive shield, said inner shield comprising an upper shell and a lower shell,
a support structure, the support structure disposed between said hollow superconductive shield and said inner shield concentrically to said hollow superconductive shield, said support structure comprised of an upper rotating element and a lower rotating element,
upper means for generating an electromagnetic field, the upper means for generating an electromagnetic field disposed between said hollow superconductive shield and said upper shell, affixed to said upper rotating element at an electromagnetic field-penetrable distance to said hollow superconductive shield,
lower means for generating an electromagnetic field, the lower means for generating an electromagnetic field disposed between said hollow superconductive shield and said lower shell, affixed to said lower rotating element at an electromagnetic field-penetrable distance to said hollow superconductive shield,
electric motors, the electric motors disposed inside said hollow superconductive shield along the central axis of said hollow superconductive shield,
a power source, the power source disposed inside said hollow superconductive shield, said power source electrically connected with said upper means for generating an electromagnetic field, said lower means for generating an electromagnetic field, and said electric motors,
life-support equipment, the life-support equipment disposed inside said inner shield,
a flux modulation controller, the flux modulation controller disposed inside said inner shield, said flux modulation controller in communication with said upper means for generating an electromagnetic field, said lower means for generating an electromagnetic field, said power source, and said electric motors, and
a crew, the crew disposed inside said inner shield accessibly to said life-support and said flux modulation controller.
2. The space vehicle of claim 1 wherein said hollow superconductive shield is composed of a high-temperature ceramic superconductor with a composite crystal structure, and is cooled to a temperature of about 40 degrees K.
3. The space vehicle of claim 1 wherein said inner shield is composed of insulating materials such as foamed ceramics.
4. The space vehicle of claim 1 wherein said power source is a nuclear generator.
5. The space vehicle of claim 1 wherein said flux modulation controller is a computer.
6. The space vehicle of claim 1 wherein said upper rotating element and said lower rotating element are pivoted, urged to rotate by said upper means for generating an electromagnetic field, said lower means for generating an electromagnetic field, and said electric motors.
7. The space vehicle of claim 1 wherein said hollow superconductive shield is pivoted and urged to rotate by said upper means for generating an electromagnetic field, said lower means for generating an electromagnetic field, and said electric motors.
8. A method for generating pressure anomaly of inflationary vacuum state is claimed comprising the following steps, some occurring simultaneously:
providing a space vehicle comprising a hollow superconductive shield, an inner shield, a support structure, upper means for generating an electromagnetic field, lower means for generating an electromagnetic field, electric motors, a power source, life-support equipment, a flux modulation controller, and a crew,
generating electrical energy in said power source,
converting said electrical energy into an electromagnetic field in said upper means for generating an electromagnetic field and said lower means for generating an electromagnetic field,
converting said electrical energy into mechanical energy in said electrical motors,
rotating said upper means for generating an electromagnetic field and said lower means for generating an electromagnetic field relative to said hollow superconductive shield,
converting said electromagnetic field into a gravitomagnetic field in said hollow superconductive shield,
propagating said gravitomagnetic field outward, orthogonal to the walls of said hollow superconductive shield, and
forming a pressure anomaly of inflationary vacuum state in the area of propagation of said gravitomagnetic field, the pressure anomaly of inflationary vacuum state comprised of an area of relatively lower vacuum pressure density in front of said space vehicle and an area of relatively higher vacuum pressure density behind said vehicle,
whereby said space vehicle is urged to move from said area of relatively higher vacuum pressure density toward said area of relatively lower vacuum pressure density.
9. The method of claim 8 wherein said pressure anomaly of inflationary vacuum state is a substantially droplet-shaped anomaly associated with lowered pressure of inflationary vacuum state provided by the propagation of a gravitomagnetic field radiating orthogonally away from the front of said hollow superconductive shield,
whereby providing for the gravitational imbalance where the lowered pressure of inflationary vacuum state is pulling said space vehicle forward.
10. The method of claim 8 wherein said pressure anomaly of inflationary vacuum state is a substantially droplet-shaped anomaly associated with elevated pressure of inflationary vacuum state provided by the propagation of a gravitomagnetic field radiating orthogonally away from the back of said hollow superconductive shield,
whereby providing for the gravitational imbalance where the elevated pressure of inflationary vacuum state is pushing said space vehicle forward.
11. The method of claim 8 wherein said pressure anomaly of inflationary vacuum state is comprised of a substantially droplet-shaped anomaly associated with lowered pressure of inflationary vacuum state and a substantially droplet-shaped anomaly associated with elevated pressure of inflationary vacuum state,
whereby providing for the gravitational imbalance where the lowered pressure of inflationary vacuum state is pulling, and the elevated pressure of inflationary vacuum state is pushing, said space vehicle forward.
12. The method of claim 8 wherein said pressure anomaly of inflationary vacuum state is a substantially egg-shaped anomaly associated with lowered pressure of inflationary vacuum state provided by the unequally-distributed gravitomagnetic field propagated in all directions orthogonally away from said hollow superconductive shield with an area of lowest vacuum pressure density disposed directly in front said space vehicle,
whereby providing for the gravitational imbalance such that the lowered pressure of inflationary vacuum state is pulling said space vehicle forward in modified spacetime.
13. The method of claim 8 wherein said pressure anomaly of inflationary vacuum state is a substantially egg-shaped anomaly associated with elevated pressure of inflationary vacuum state provided by the unequally-distributed gravitomagnetic field propagated in all directions orthogonally away from said hollow superconductive shield with an area of highest vacuum pressure density disposed directly behind said space vehicle, whereby providing for the gravitational imbalance such that the highest pressure of inflationary vacuum state is pushing said space vehicle forward in modified spacetime at a speed possibly approaching a local light-speed, the local light-speed which may be substantially higher than the light-speed in the ambient space.
http://www.physorg.com/news8042.html