Unmanned fluid-propelled aerial vehicle

Patent metadata

Field	Value
Publication number	US-9751597-B1
Application number	US-201514700958-A
Country	US
Kind code	B1
Filing date	Apr 30, 2015
Priority date	Jul 15, 2014
Publication date	Sep 5, 2017
Grant date	Sep 5, 2017

Abstract

A water-propelled or water-powered unmanned aerial vehicle including a base configured to carry a payload, and at least one nozzle attached thereto. The at least one nozzle is configured to selectively receive pressurized fluid from a source located remotely from the vehicle. The vehicle includes a control system configured to alter or otherwise selectively dictate the flow of fluid through the at least one nozzle and/or the orientation of the at least one nozzle with respect to the base in response to a received control signal for providing controlled unmanned vehicle flight.

First claim

What is claimed is:

1. A water-propelled unmanned aerial vehicle comprising:
a base configured to carry a payload enclosed therein;
at least one nozzle attached to the base, the nozzle configured to selectively receive and expel pressurized water from a source located remotely from the vehicle;
a control system configured to alter at least one of the flow of water through the at least one nozzle; and the orientation of the at least one nozzle with respect to the base, in response to a received control signal, to provide controlled flight of the vehicle;
an actuator responsive to a control signal generated by the control system for altering the orientation of the at least one nozzle with respect to the base; and
an electrical generator configured to be driven by the water and operatively connected to the control system for supplying electrical power thereto.

2. The aerial vehicle of claim 1 , wherein the actuator comprises a linear actuator having a first end attached to the base and a second end, movable with respect to the first end, and attached to the at least one nozzle.

3. The aerial vehicle of claim 1 , further comprising at least one of a global positioning sensor (GPS), an accelerometer, a gyroscope and an altimeter, in communication with the control system, to provide controlled flight of the vehicle.

4. A water-propelled unmanned aerial vehicle comprising:
a base defining a payload bay configured to carry a payload enclosed therein;
a plurality of nozzles attached to the base, the nozzles configured to selectively receive and expel pressurized water from a source located remotely from the vehicle;
a control system configured to alter at least one of the flow of water through the at least one nozzle; and the orientation of at least one of the plurality of nozzles with respect to the base, in response to a received control signal, to provide controlled flight of the vehicle;
an actuator responsive to a control signal generated by the control system for altering the orientation of at least one of the plurality of nozzles with respect to the base; and
an electrical generator operatively connected to the control system for supplying electrical power thereto.

5. An unmanned payload lifting system comprising:
a water-propelled aerial vehicle including a nozzle configured to receive and expel pressurized water to provide vertical thrust to said vehicle;
a marine surface vehicle including a pump;
a fluid conduit operatively attached to the marine surface vehicle and the aerial vehicle and configured to convey pressurized water from the pump to the nozzle;
a control system arranged on the aerial vehicle and configured to alter at least one of the flow of water through the nozzle; and the orientation of the nozzle, with respect to the aerial vehicle to control aerial movement of said aerial vehicle;
an actuator responsive to a control signal generated by the control system for altering the orientation of the nozzle with respect to the aerial vehicle;

an electrical conduit operatively connected between the marine surface vehicle and the aerial vehicle; and
an electrical generator arranged on the marine surface vehicle and operatively connected to the control system via the electrical conduit for supplying electrical power thereto.

6. The system of claim 5 , wherein the control system includes:
an aerial vehicle controller associated with the aerial vehicle; and
a surface vehicle controller associated with the surface vehicle and in communication with the aerial vehicle controller.

7. The system of claim 6 , wherein the surface vehicle controller is in wireless communication with the aerial vehicle controller.

8. The system of claim 7 , wherein the surface vehicle controller is responsive to control signals received from the aerial vehicle for controlling the position of the surface vehicle and the water flow rate from the surface vehicle.

9. The system of claim 6 , wherein the surface vehicle further comprises a winch for storing the fluid conduit, wherein the winch is responsive to control signals received from at least one of the aerial vehicle controller and the surface vehicle controller for selectively altering the length of the conduit during flight of the aerial vehicle.

10. The system of claim 5 , wherein the surface vehicle further comprises at least one of a pump monitoring sensor, an accelerometer, a GPS and a conduit reel position sensor.

11. The system of claim 5 , wherein the surface vehicle further comprises an inlet control valve for controlling the volume of water drawn in by the fluid pump from a water source.

12. The system of claim 5 , wherein the surface vehicle further comprises a memory device, the memory device storing instructions including a predetermined vehicle flight plan for providing autonomous flight of the aerial vehicle.

13. The system of claim 5 , wherein the surface vehicle further comprises a communications system configured to provide communication between at least one of the aerial vehicle and a remote command station.

14. The system of claim 5 , wherein the surface vehicle further comprises a steering system and a propulsion system for providing heading and velocity control of the surface vehicle.

15. The aerial vehicle of claim 4 , wherein the control system comprises a memory device, the memory device storing instructions including a predetermined vehicle flight plan for providing autonomous vehicle flight.

16. The aerial vehicle of claim 4 , wherein the plurality of nozzles comprise:
a first plurality of nozzles arranged radially about, and rotatably attached to, the base; and
a horizontal thrust nozzle fixedly attached to the base and oriented so as to expel pressurized water in a direction generally horizontally with respect to the base.

17. The aerial vehicle of claim 4 , further comprising a plurality of arms, each arm being fixedly attached to a respective nozzle of the first plurality of nozzles,
wherein the actuator comprises a plurality of linear actuators, each linear actuator comprising a first end fixedly attached to the base, and a second end moveable with respect to the first end in response to a control signal received from the control system, and
wherein the second moveable end of each of the plurality of linear actuators is in contact engagement with a respective one of the plurality of arms.

18. The aerial vehicle of claim 4 , further comprising:
a manifold controller operatively connected to the control system; and
a plurality of valves associated with the plurality of nozzles, the plurality of valves in communication with the pressurized water and configured to alter the flow of water through each of the nozzles in response to a control signal received from the manifold controller.

Assignees

• Lockheed Corp

Inventors

• Low Nathan E
• Demas Peter J

Classifications

• B64U2201/202

  using tethers for connecting to ground station · CPC title

• B64U80/84

  Waterborne vehicles · CPC title

• B64C2201/121

  Operations & Transport · mapped topic

• B63B35/00 Primary

  Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for · CPC title

• B64C39/022

  Tethered aircraft · CPC title