Centrifugal force amplification method and system for generating vehicle lift

1. A centrifugal force amplification vehicle lift system, comprising:

a first arrangement of two concentric and radially separated magnetic rings in a common plane and having a common center, said magnetic rings are positioned with said common plane substantially perpendicular to a force of gravity associated with a planetary body rotating at a rotational speed;

a first force generator coupled to said magnetic rings in said first arrangement for rotating said magnetic rings in said first arrangement in opposing directions in said common plane at speeds that are at least 20 times greater than the rotational speed of the planetary body, said first force generator including:

two concentric evacuated first tunnels, each of said evacuated first tunnels comprised of a superconducting material and encasing one of said magnetic rings,

wherein each of said magnetic rings is suspended within one of said evacuated first tunnels,

a first plurality of linear induction motors distributed about each of said evacuated first tunnels, and

a first controller coupled to said first plurality of linear induction motors for energizing said first plurality of linear induction motors, wherein said magnetic rings in said first arrangement are forced to rotate in said opposing directions;

a second arrangement of two concentric and radially separated compensating magnetic rings that are smaller in diameter than each of said magnetic rings in said first arrangement, said compensating magnetic rings lying in a plane coincident with said common plane of said magnetic rings in said first arrangement, said compensating magnetic rings having a common center, said compensating magnetic rings are positioned with said common center is offset from said common center of said magnetic rings in said first arrangement; and

a second force generator coupled to said compensating magnetic rings for rotating said compensating magnetic rings in said common plane thereof and in opposing directions at speeds that are at least 20 times greater than the rotational speed of the planetary body, said second force generator including:

two concentric evacuated second tunnels, each of said evacuated second tunnels comprised of a superconducting material and encasing one of said compensating magnetic rings wherein each of said compensating magnetic rings is suspended within one of said evacuated second tunnels associated therewith,

a second plurality of linear induction motors distributed about each of said evacuated second tunnels, and

a second controller coupled to said second plurality of linear induction motors to energize said second plurality of linear induction motors, wherein said compensating magnetic rings are forced to rotate in said opposing directions.

2. The centrifugal force amplification vehicle lift system of claim 1 ,

wherein said second force generator changes the speeds of said compensating magnetic rings in said second arrangement as said first force generator rotates said magnetic rings in said first arrangement.

3. The centrifugal force amplification vehicle lift system of claim 1 , wherein a location of said common center of said compensating magnetic rings in said second arrangement relative to said common center of said magnetic rings in said first arrangement is changed as said first force generator rotates said magnetic rings in said first arrangement and said second force generator rotates said compensating magnetic rings in said second arrangement.

4. The centrifugal force amplification vehicle lift system of claim 3 , wherein said second force generator changes the speeds of said compensating magnetic rings in said second arrangement as said first force generator rotates said magnetic rings in said first arrangement, and wherein a location of said common center of said compensating magnetic rings in said second arrangement relative to said common center of said magnetic rings in said first arrangement is changed as said first force generator rotates said magnetic rings in said first arrangement and said second force generator rotates said compensating magnetic rings in said second arrangement.

5. A canard aircraft, comprising:

a fuselage;

an engine mounted to the rear of the fuselage;

a main wing set mounted on the fuselage forward of the engine;

a canard wing set mounted at a front of the fuselage and in front of the main wing set; and

the centrifugal force amplification vehicle lift system of claim 1 is arranged at a location corresponding to a portion of the fuselage that intersects the main wing set.

6. The canard aircraft of claim 5 , wherein the canard aircraft has a canard shape.

7. The canard aircraft of claim 5 , wherein the concentric rings of the first arrangement each have a diameter of at least 22 feet.

8. A flying wing aircraft, comprising the centrifugal force amplification vehicle lift system of claim 1 arranged at a central portion.

9. The flying wing aircraft of claim 8 , wherein the flying wing aircraft has a canard shape.

10. The flying wing aircraft of claim 8 , wherein the concentric rings of the first arrangement each have a diameter of at least 22 feet.

11. The flying wing aircraft of claim 8 , the rings comprised of a composite of multi-walled carbon nanotubes and a magnetic material.

12. The centrifugal force amplification vehicle lift system of claim 1 , wherein the rotational speed of the planetary body is 1000 mph and corresponds to the Earth's equator.

13. The centrifugal force amplification vehicle lift system of claim 1 , wherein the rotational speed of the planetary body is 500 mph and corresponds to the Mars' equator.

14. The centrifugal force amplification vehicle lift system of claim 1 , wherein the rotational speed of the planetary body is 100 mph.