AEROVEHICLE SYSTEM INCLUDING PLURALITY OF AUTOGYRO ASSEMBLIES
First Claim
1. An aerovehicle system, comprising:
- a towing vehicle;
a towed aerovehicle; and
a tow line releaseably connected between the towing vehicle and towed aerovehicle, the towed aerovehicle including;
a frame;
a plurality of autogyro assemblies connected to the frame; and
a controller to control operation of the plurality of autogyro assemblies for unmanned flight;
wherein, when the controller determines a stall in the towing vehicle, the controller automatically releases the tow line and controls the flight of the towed aerovehicle to a landing by substantially following a flight path determined by sensed signals.
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Abstract
An unmanned, towable aerovehicle is described and includes a container or frame to hold or support cargo, at least one and, in some examples, a plurality of autogyro assemblies connected to the container and to provide flight characteristics, and a controller to control operation the autogyro assembly for unmanned flight. The container or frame includes a connection to connect to a powered aircraft to provide forward motive force to power the autogyro assembly. In an example, the autogyro assembly includes a mast extending from the container, a rotatable hub on an end of the mast, and a plurality of blades connected to the hub for rotation to provide lift to the vehicle. In an example, an electrical motor rotates the blades prior to lift off to assist in take off. In an example, the electrical motor does not have enough power to sustain flight of the vehicle. The aerovehicle can further include plurality of autogyro assemblies to assist in flight. The aerovehicle can include surfaces that provide lift or control to assist in the flight profile of the aerovehicle.
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Citations
25 Claims
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1. An aerovehicle system, comprising:
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a towing vehicle; a towed aerovehicle; and a tow line releaseably connected between the towing vehicle and towed aerovehicle, the towed aerovehicle including; a frame; a plurality of autogyro assemblies connected to the frame; and a controller to control operation of the plurality of autogyro assemblies for unmanned flight; wherein, when the controller determines a stall in the towing vehicle, the controller automatically releases the tow line and controls the flight of the towed aerovehicle to a landing by substantially following a flight path determined by sensed signals. - 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)
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Specification