Saucer shaped gyroscopically stabilized vertical take-off and landing aircraft
First Claim
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1. A vertical take-off and landing aircraft, comprising:
- an outer saucer-shaped hull configured to rotate around a central axis of the aircraft thereby creating a gyroscopic effect for the aircraft;
a plurality of air foil propellers positioned on a top surface of the outer saucer-shaped hull and configured to be in a closed position or an open position;
an inner stationary hull having a central axis substantially aligned with a central axis of the outer saucer-shaped hull and configured to be positioned within an annular opening of the outer saucer-shaped hull;
a plurality of motors located between the outer saucer-shaped hull and the inner stationary hull and configured to rotate the outer saucer-shaped hull relative to the inner stationary hull; and
a plurality of pistons positioned within the inner stationary hull and configured to travel substantially perpendicular to a top surface of the inner stationary hull so as to draw air into the aircraft; and
a sinusoidal ring configured so that a height of a top surface of the ring varies in a sine-wave fashion around its perimeter, wherein the sinusoidal ring is in mechanical communication with the outer saucer-shaped hull such that rotation of the outer saucer-shaped hull results in rotation of the sinusoidal ring, and wherein the plurality of pistons are in mechanical communication with the top surface of the sinusoidal ring such that motion of each piston varies as the sinusoidal ring rotates.
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Abstract
An aircraft that is housed within a gyroscope providing for improved flight stability that includes an inner hull which remains stationary within a rotating outer hull. A rotating sine-wave ring is used to activate and move a plurality of pistons which will intake air from above the upper surface of the inner hull configuration and create a negative pressure on the aircraft. The craft contains compression chambers which receive the air and which feed the various impeller thrusters which are rotational within three-fourths of a hemisphere.
24 Citations
20 Claims
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1. A vertical take-off and landing aircraft, comprising:
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an outer saucer-shaped hull configured to rotate around a central axis of the aircraft thereby creating a gyroscopic effect for the aircraft; a plurality of air foil propellers positioned on a top surface of the outer saucer-shaped hull and configured to be in a closed position or an open position; an inner stationary hull having a central axis substantially aligned with a central axis of the outer saucer-shaped hull and configured to be positioned within an annular opening of the outer saucer-shaped hull; a plurality of motors located between the outer saucer-shaped hull and the inner stationary hull and configured to rotate the outer saucer-shaped hull relative to the inner stationary hull; and a plurality of pistons positioned within the inner stationary hull and configured to travel substantially perpendicular to a top surface of the inner stationary hull so as to draw air into the aircraft; and a sinusoidal ring configured so that a height of a top surface of the ring varies in a sine-wave fashion around its perimeter, wherein the sinusoidal ring is in mechanical communication with the outer saucer-shaped hull such that rotation of the outer saucer-shaped hull results in rotation of the sinusoidal ring, and wherein the plurality of pistons are in mechanical communication with the top surface of the sinusoidal ring such that motion of each piston varies as the sinusoidal ring rotates. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20)
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Specification