Hybrid unmanned vehicle for high altitude operations
First Claim
1. An aerial vehicle comprising:
- an aerodynamic envelope enclosing a volume of lifting gas;
suspension lines engaging the aerodynamic envelope;
a rotor suspended from the aerodynamic envelope by the suspension lines; and
a gondola including a positional translator for translating the gondola with respect to the aerodynamic envelope, the positional translator engaging the rotor, wherein the gondola is suspended below the envelope by the rotor, and the gondola is able to rotate and translate with respect to the aerodynamic envelope.
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0 Petitions
Accused Products
Abstract
A hybrid aerial vehicle is optimized, for example, and not by way of limitation, to operate above 100,000 feet in altitude and provide persistent and maneuverable flight while carrying a wide array of communications and sensing payloads. The hybrid vehicle may use the high altitude winds to gain altitude by pitching up with the center of gravity (CG) control and using its propulsion drive to thrust into the wind to create aerodynamic lift to rise above the neutral buoyancy altitude. The hybrid vehicle will pitch down with the CG control so as to use gravity and propulsion to accelerate. Yaw control directs the flight towards any compass direction by rotating the gondola. This maneuvering capability permits the vehicle to station operate persistently, even in high winds. The lighter-than-air inflatable saucer shape is optimized for maintaining an aerodynamic cross-section to the prevailing wind from any direction in the vehicle horizontal plane. A gondola below the saucer contains a motor, batteries, solar collector, sensors, and yaw and CG control mechanisms.
68 Citations
38 Claims
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1. An aerial vehicle comprising:
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an aerodynamic envelope enclosing a volume of lifting gas; suspension lines engaging the aerodynamic envelope; a rotor suspended from the aerodynamic envelope by the suspension lines; and a gondola including a positional translator for translating the gondola with respect to the aerodynamic envelope, the positional translator engaging the rotor, wherein the gondola is suspended below the envelope by the rotor, and the gondola is able to rotate and translate with respect to the aerodynamic envelope. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27)
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28. A method of deploying remote sensors above a selected altitude, the method comprising:
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providing an aerial vehicle comprising; an aerodynamic envelope enclosing one or more volumes of lighter than air gas; suspension lines engaging the aerodynamic envelope; and a gondola, the gondola being suspended from the aerodynamic envelope by the suspension lines, and the gondola including a propulsion system for horizontal control; controlling the rotational orientation of the gondola with respect to the aerodynamic envelope; and controlling a pitch of the aerial vehicle by controlling a position of a center of mass of the gondola to shift the weight of the gondola relative to the aerodynamic envelope. - View Dependent Claims (29, 30, 31, 32)
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33. A method comprising:
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providing an aerial vehicle, the aerial vehicle comprising; an aerodynamic envelope enclosing a volume of lifting gas; suspension lines engaging the aerodynamic envelope; a rotor suspended from the aerodynamic envelope by the suspension lines; a gondola including a positional translator for translating the gondola with respect to the aerodynamic envelope, the positional translator engaging the rotor, wherein the gondola is suspended from the aerodynamic envelope by the rotor, and the gondola is able to rotate and translate with respect to the aerodynamic envelope; and a propulsion system disposed on the gondola, wherein the propulsion system is aligned with an axis of the gondola to produce thrust along the axis; controlling the rotational orientation of the gondola with respect to the aerodynamic envelope to align the axis of the gondola with a prevailing wind; generating thrust from the propulsion system to propel the aerial vehicle into the prevailing wind; and controlling a position of the center of mass of the gondola along the axis of the gondola with respect to the aerodynamic envelope to increase a pitch of the aerial vehicle to cause the aerial vehicle to climb beyond an altitude at which the aerial vehicle is neutrally buoyant. - View Dependent Claims (34, 35, 36, 37)
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38. An aerial vehicle comprising:
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an aerodynamic envelope enclosing a volume of lifting gas; a lower stage including; suspension lines engaging the aerodynamic envelope; a rotor suspended from the aerodynamic envelope by the suspension lines; and a gondola suspended from the aerodynamic envelope and including a positional translator for translating the gondola with respect to the aerodynamic envelope, wherein the rotor enables the gondola to rotate with respect to the aerodynamic envelope and the positional translator enables the gondola to translate with respect to the aerodynamic envelope.
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Specification