TETHERED AERIAL SYSTEM FOR DATA GATHERING

• US 20130233964A1
• Filed: 03/07/2012
• Published: 09/12/2013
• Est. Priority Date: 03/07/2012
• Status: Abandoned Application

• Current Assignee: Aurora Flight Sciences Corporation (The Boeing Co.)
• Original Assignee: Aurora Flight Sciences Corporation (The Boeing Co.)
• Inventors: Woodworth, Adam, Peverill, James
• Application Number:
  US13/413,696
• Publication Number:
  US 20130233964A1
• Time in Patent Office: Days
• US Class Current: 244/2
• CPC Class Codes: B64C 25/58 Arrangements or adaptations of shock-absorbers or springs shimmy-dampers B64C25/50
• CPC Class Codes: B64C 27/006 Safety devices
• CPC Class Codes: B64C 27/20 Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
• CPC Class Codes: B64C 37/02 Flying units formed by separate aircraft towing B64D3/00; aircraft transported by aircraft B64D5/00; air-refuelling B64D39/00
• CPC Class Codes: B64C 39/022 Tethered aircraft
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64C 9/00 Adjustable control surfaces or members, e.g. rudders trimming stabilising surfaces B64C5/10
• CPC Class Codes: B64D 17/80 in association with aircraft, e.g. for braking thereof
• CPC Class Codes: B64F 3/02 with means for supplying electricity to aircraft during flight
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 10/14 with four distinct rotor axes, e.g. quadcopters
• CPC Class Codes: B64U 10/60 Tethered aircraft
• CPC Class Codes: B64U 2201/102 adapted for flying in formations
• CPC Class Codes: B64U 2201/202 using tethers for connecting to ground station
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 30/26 Ducted or shrouded rotors
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 70/93 for use on a land or nautical vehicle
• CPC Class Codes: G05D 1/0866 specially adapted to captive aircraft
• CPC Class Codes: G05D 1/104 involving a plurality of aircrafts, e.g. formation flying traffic control systems for aircraft G08G5/00
• CPC Class Codes: H02G 11/00 : Arrangements of electric cables or lines between relatively-movable parts

Abstract

A tethered unmanned aerial vehicle (“UAV”) may be outfitted with a sensor payload for data gathering. The tethered UAV may be tethered to a ground station for constricting the flight space of the UAV while also providing the option for power delivery and/or bidirectional communications. The tethered UAV'"'"'s flight path may be extended by introducing one or more secondary UAVs that cooperate to extend the horizontal flight path of a primary UAV. The ground station, which may be coupled with the tethered aerial vehicle, may comprise a listening switch configured to determine a condition of the tether such that the supply of power to the tether may be terminated when tether damage or a tether severance is detected.

Claims

1. An aerial vehicle system for gathering data, the aerial vehicle system comprising:

a ground station;

a first aerial vehicle, wherein the first aerial vehicle comprises a sensor payload;

a second aerial vehicle;

a first tether portion operatively coupled between the ground station and the second aerial vehicle; and

a second tether portion operatively coupled between the second aerial vehicle and the first aerial vehicle;

wherein the first tether portion is configured to deliver power from the ground station to the second aerial vehicle and the second tether portion is configured to deliver power to the first aerial vehicle.

2. The aerial vehicle system of claim 1, wherein the ground station comprises a device for adjusting the tension or length of the first tether portion.

3. The aerial vehicle system of claim 1, wherein the first or second aerial vehicle comprises a device for adjusting the tension or length of the first or second tether portion.

4. The aerial vehicle system of claim 1, wherein the ground station is coupled with a mobile platform.

5. The aerial vehicle system of claim 1, wherein the ground station is coupled with a stationary platform.

6. The aerial vehicle system of claim 1, wherein the ground station is configured to deliver power from a power source to the first aerial vehicle or the second aerial vehicle.

7. The aerial vehicle system of claim 1, wherein the ground station comprises a listening switch configured to determine a condition of the first or second tether portions.

8. The aerial vehicle system of claim 7, wherein the listening switch causes the supply of power to the first or second tether portions to be terminated when tether damage or a tether severance is detected.

9. The aerial vehicle system of claim 1, wherein the first tether portion and the second tether portion are further configured to communicate data.

10. A safety system for use with a tethered aerial vehicle, the safety system comprising:

a ground station, wherein the ground station is configured to deliver power from a power source;

a tether for coupling the aerial vehicle with the ground station, wherein the tether is configured to transmit power from the ground station to the aerial vehicle;

a device positioned between the ground station and the aerial vehicle for adjusting the tension or length of the tether; and

a listening switch, the listening switch being coupled with the ground station and positioned between the power source and the tether;

wherein supply of power from the power source to the tether is terminated when the listening switch detects tether damage or tether severance.

11. The safety system of claim 10, wherein the ground station is coupled with a mobile platform.

12. The safety system of claim 10, wherein the ground station is coupled with a stationary platform.

13. The safety system of claim 10, wherein the tether is further configured to communicate data.

14. A safety method for use with a tethered aerial vehicle, the safety method comprising the steps of:

transmitting an electrical signal from a ground station to an aerial vehicle through a tether and back to the ground station via the same tether;

listening for the electrical signal to be received back at the ground station;

wherein the electrical signal received at the ground station is utilized as a received signal value;

wherein the received signal value to set to zero or null when the electrical signal is not received at the ground station;

comparing the received signal value to the transmitted electrical signal to determine a signal loss value;

triggering the ground station to stop transmitting power through the tether when the received signal value is zero or null;

instructing each aerial vehicle coupled to the tether to return to the ground station when the signal loss value has exceeded a predetermined signal loss threshold value; and

authorizing each aerial vehicle coupled to the tether to continue its current flight plan when the signal loss value has not exceeded the predetermined signal loss threshold value.

15. The safety method of claim 14, wherein each aerial vehicle coupled to the tether enters safe-fall mode when the ground station stops transmitting power through the tether.

16. An unmanned tethered aerial vehicle for increasing safety during descent, the unmanned tethered aerial vehicle comprising:

a tether, wherein the tether is configured to couple with a ground station that is configured to supply power to the aerial vehicle;

one or more propellers;

a descent stabilization device for controlling the altitude of the aerial vehicle during descent; and

a force-impact attenuator for reducing peak force during ground impact when power through the tether is no longer available.

17. The unmanned tethered aerial vehicle of claim 16, wherein the tether is further configured to communicate data.

18. The unmanned tethered aerial vehicle of claim 16, wherein the force-impact attenuator is positioned on a leading porting of the aerial vehicle during descent such that the force attenuator is a first portion of the aerial vehicle to strike the ground first and attenuate the force of impact.

19. The unmanned tethered aerial vehicle of claim 16, wherein the descent stabilization device comprises at least one of:

(i) a parachute;

(ii) stabilizing fins;

or (iii) reaction wheel.

20. The unmanned tethered aerial vehicle of claim 16, further comprising flight control surfaces configured to steer the unmanned tethered aerial vehicle during descent.

21. The unmanned tethered aerial vehicle of claim 20, wherein the flight control surfaces are actuated by power generated by the propulsion system auto-rotating during descent.