Apparatus, system, and method for flying an aircraft
First Claim
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1. An aircraft launch system, comprising:
- a riser coupleable to an aircraft, the aircraft comprising at least one first thrust generator configured to generate a first upward lift on the aircraft and the riser comprising;
an actuator; and
a tether coupled to the actuator; and
a sky crane coupled to the tether, wherein the sky crane is configured to generate a second upward lift on the sky crane to lift the sky crane above the aircraft and to provide a downward drag to resist downward motion of the sky crane when lifted above the aircraft, wherein the sky crane comprises one of a rigid wing, a parafoil, or a lighter-than-air flotation device;
wherein the actuator is operable to retract the tether and draw together the sky crane and the aircraft during a take-off while the at least one first thrust generator generates the first upward lift on the aircraft and while at least one of the second upward lift is generated or the downward drag is provided;
wherein the first upward lift is less than a total weight of the aircraft and the second upward lift is less than the total weight of the aircraft; and
wherein a sum of the first upward lift and at least one of the second upward lift or the downward drag is greater than a combined weight of the aircraft, the riser, and the sky crane.
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Abstract
An aircraft launch system includes a riser coupleable to an aircraft. The riser includes an actuator and a tether coupled to the actuator. The aircraft launch system further includes a sky crane coupled to the tether. The actuator is operable to retract the tether and draw together the sky crane and the aircraft.
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Citations
25 Claims
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1. An aircraft launch system, comprising:
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a riser coupleable to an aircraft, the aircraft comprising at least one first thrust generator configured to generate a first upward lift on the aircraft and the riser comprising; an actuator; and a tether coupled to the actuator; and a sky crane coupled to the tether, wherein the sky crane is configured to generate a second upward lift on the sky crane to lift the sky crane above the aircraft and to provide a downward drag to resist downward motion of the sky crane when lifted above the aircraft, wherein the sky crane comprises one of a rigid wing, a parafoil, or a lighter-than-air flotation device; wherein the actuator is operable to retract the tether and draw together the sky crane and the aircraft during a take-off while the at least one first thrust generator generates the first upward lift on the aircraft and while at least one of the second upward lift is generated or the downward drag is provided; wherein the first upward lift is less than a total weight of the aircraft and the second upward lift is less than the total weight of the aircraft; and wherein a sum of the first upward lift and at least one of the second upward lift or the downward drag is greater than a combined weight of the aircraft, the riser, and the sky crane. - View Dependent Claims (2, 3, 4, 5, 6, 7)
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8. An aircraft launch system, comprising:
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an aircraft comprising at least one first thrust generator configured to generate a first upward lift on the aircraft; a riser coupled to the aircraft, the riser comprising; an actuator; and a tether coupled to the actuator; and a sky crane coupled to the tether, wherein the sky crane is configured to generate a second upward lift on the sky crane to lift the sky crane above the aircraft and to provide a downward drag to resist downward motion of the sky crane when lifted above the aircraft, and wherein the sky crane comprises one of a rigid wing, a parafoil, or a lighter-than-air flotation device; wherein the actuator is operable to retract the tether and draw together the sky crane and the aircraft during a take-off while the at least one first thrust generator generates the first upward lift on the aircraft and while at least one of the second upward lift is generated or the downward drag is provided; wherein the first upward lift is less than a total weight of the aircraft and the second upward lift is less than the total weight of the aircraft; and wherein a sum of the first upward lift and at least one of the second upward lift or the downward drag is greater than a combined weight of the aircraft, the riser, and the sky crane. - View Dependent Claims (9, 10, 11, 12, 13, 14, 15, 16, 17)
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18. A method for flying an aircraft, comprising:
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tethering a sky crane to the aircraft via a tether, wherein the sky crane comprises one of a rigid wing, a parafoil, or a lighter-than-air flotation device; positioning the sky crane in the air vertically above the aircraft while the aircraft is on a ground surface; at least one of upwardly lifting the sky crane, with a first upward lift that is less than a total weight of the aircraft, or downwardly dragging the sky crane; upwardly lifting the aircraft with a combination of the first upward lift and a second upward lift generated by the aircraft, wherein the second upward lift is less than the total weight of the aircraft; and while or after upwardly lifting the aircraft and at least one of while or after upwardly lifting the sky crane or while downwardly dragging the sky crane, retracting the tether to draw the sky crane and aircraft together. - View Dependent Claims (19, 20, 21, 22, 23, 24, 25)
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Specification