Marine vessel-towable aerovehicle system with automated tow line release

• US 8,646,719 B2
• Filed: 08/22/2011
• Issued: 02/11/2014
• Est. Priority Date: 08/23/2010
• Status: Active Grant

• Current Assignee: Air Support Technologies LLC
• Original Assignee: Heliplane LLC
• Inventors: Morris, John William, Jarnot, Charles A.
• Primary Examiner(s): Dinh, Tien
• Assistant Examiner(s): Fabula, Michael A
• Application Number:
  US13/215,034
• Publication Number:
  US 20120091259A1
• Time in Patent Office: 904 Days
• Field of Search: 244/33, 244/30, 244/31, 244/114.R, 244/115, 244/116, 244/153.R, 244/154, 244/155.R, 244/155.A, 244/6, 244/8, 244/17.11, 244/17.19, 244/17.23
• US Class Current: 244/1.TD
• CPC Class Codes: B64C 19/00 Aircraft control not otherwise provided for
• CPC Class Codes: B64C 27/02 Gyroplanes
• CPC Class Codes: B64D 3/00 Aircraft adaptations to facilitate towing or being towed B64D39/00 takes precedence
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 30/291 Detachable rotors or rotor supports
• CPC Class Codes: B64U 80/82 Airborne vehicles

Abstract

An unmanned, towable air vehicle is described and includes electronic sensors to increase the detection range relative to the horizon detection limitations of a surface craft, an autogyro assembly to provide lift, and a controller to control operation the autogyro assembly for unmanned flight. A forward motive force powers the autogyro assembly to provide lift. 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. The electrical motor does not have enough power to sustain flight of the vehicle in an example.

Claims

1. A marine-aerovehicle system, comprising:

a marine vessel capable of towing;

a towed aerovehicle; and

a tow line releasably connected between the towing vessel and towed aerovehicle, the towed aerovehicle including;

a flight body;

an autogyro assembly connected to the flight body; and

a controller to control operation of the autogyro assembly for unmanned flight;

wherein when the controller determines a stop in the towing vessel, the controller automatically releases the tow line and controls the towed aerovehicle flight to a landing by substantially following a flight path determined by sensed signals and a programmed destination.

2. The marine-aerovehicle system of claim 1, wherein the autogyro assembly comprises a mast extending from the body, a rotatable hub on an end of the mast, and a plurality of blades connected to the hub.

3. The marine-aerovehicle system of claim 2, wherein the autogyro assembly comprises a motor to rotate the blades prior to lift off to assist in take off, and wherein the motor does not have enough power to power the aerovehicle through takeoff absent a further motive force.

4. The marine-aerovehicle system of claim 1, wherein the controller senses forward motion to control the autogyro assembly.

5. The marine-aerovehicle system of claim 1, wherein the controller receives a signal from the towing vessel and controls the autogyro assembly using the received signal.

6. The marine-aerovehicle system of claim 2, wherein the controller controls the rotational speed of the hub.

7. The marine-aerovehicle system of claim 2, wherein the autogyro assembly comprises actuators to control one or more angles of the plurality of airfoil blades, and wherein the controller controls the actuators.

8. The marine-aerovehicle system of claim 1, wherein the flight body comprises a container to hold cargo, a rear stabilizer, and an undercarriage to support the container when on the ground.

9. The marine-aerovehicle system of claim 8, wherein the undercarriage includes a trolley that contacts the ground to provide mobility and is removable from the container.

10. The marine-aerovehicle system of claim 2, wherein the controller issues control signals to position the blades for different stages of flight.

11. The marine-aerovehicle system of claim 10, wherein the controller issues a takeoff control signal to set the blades for takeoff, wherein an angle of incidence of the blades is greater at takeoff than during flight.

12. The marine-aerovehicle system of claim 11, wherein the controller issues a prerotation control signal to set the blades for pre-takeoff, wherein the angle of incidence of the airfoil blades is greater at takeoff and flight than at prerotation.

13. The marine-aerovehicle system of claim 12, wherein the controller issues a landing control signal to set the blades for landing, wherein the angle of incidence of the blades is greatest at landing.

14. The marine-aerovehicle system of claim 13, wherein the controller sets the landing angle of incidence to 45 degrees or greater and sets the flight angle of incidence to less 30 degrees.

15. The marine-aerovehicle system of claim 1, further comprising a propulsion system and wherein the controller controls operation of the propulsion system.

16. The marine-aerovehicle system of claim 15, wherein the propulsion system has sufficient thrust to assist in a cargo-laden flight and an essentially cargo-free flight but does not have enough thrust to fly a flight body full of cargo.

17. The marine-aerovehicle system of claim 1, wherein the tow line includes a mechanical component to transfer trust from the towing vessel to the flight body and an electrical component that transfer electrical signals from the towing vessel to the controller.

18. The marine-aerovehicle system of claim 1, wherein the controller receives signals from other controllers of nearby aerovehicles.

19. The marine-aerovehicle system of claim 18, wherein the controller acts as a master controller and issues control signals to nearby aerovehicles.

20. The marine-aerovehicle system of claim 18, wherein the plurality of the nearby aerovehicles are towed by the towing vessel.

21. The marine-aerovehicle system of claim 1, wherein the flight body includes sensors that produce signals, and wherein controller receives the signals and applies instructions to the signals to output control signals.

22. The marine-aerovehicle system of claim 21, wherein the sensors include weight sensors on flight body to determine at least one of the weight and center of gravity of the flight body and cargo, and wherein the controller issues a control signal to adjust the position of the autogyro assembly on the flight body.

23. The marine-aerovehicle system of claim 22, wherein the controller issues signals to control actuators that adjust a longitudinal position of the autogyro assembly, a lateral position of the autogyro assembly, or both.

24. The marine-aerovehicle system of claim 1, wherein the controller receives a forward air speed indicator to control the speed of the flight body and keep the speed below a never-exceed velocity.

25. The marine-aerovehicle system of claim 1, wherein the controller receives a rotation speed signal from the autogyro assembly and issues a brake signal if the rotational speed exceeds a safe rotational speed.

26. The marine-aerovehicle system of claim 16, wherein the propulsion system includes an on-board motor, a drive shaft connected to the motor and extending outside the flight body, and a propeller connected to the drive shaft.