Aerial platform powered via an optical transmission element

• US 9,800,091 B2
• Filed: 06/09/2012
• Issued: 10/24/2017
• Est. Priority Date: 06/09/2011
• Status: Active Grant

• Current Assignee: LaserMotive Inc.
• Original Assignee: LaserMotive Inc.
• Inventors: Nugent, Jr., Thomas J., Bashford, David, Kare, Jordin T.
• Primary Examiner(s): Dinh, Tien
• Assistant Examiner(s): Fabula, Michael A
• Application Number:
  US14/124,993
• Publication Number:
  US 20150041598A1
• Time in Patent Office: 1,963 Days
• Field of Search: None
• CPC Class Codes: B64B 1/50 Captive balloons
• CPC Class Codes: B64F 3/00 Ground installations specially adapted for captive aircraft
• 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 10/16 with five or more distinct rotor axes, e.g. octocopters
• CPC Class Codes: B64U 10/17 Helicopters flying platforms B64U10/13
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• CPC Class Codes: B64U 10/30 Lighter-than-air aircraft, e.g. aerostatic aircraft
• CPC Class Codes: B64U 10/60 Tethered aircraft
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 2201/202 using tethers for connecting to ground station
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 50/31 generated by photovoltaics
• CPC Class Codes: B64U 50/34 In-flight charging photovoltaics B64U50/31
• CPC Class Codes: B64U 80/70 in containers B64U80/60 takes precedence
• CPC Class Codes: G03B 15/006 Apparatus mounted on flying objects
• CPC Class Codes: G05D 1/0055 with safety arrangements
• CPC Class Codes: G05D 1/0866 specially adapted to captive aircraft
• CPC Class Codes: H02J 2310/44 for aircrafts
• CPC Class Codes: H02J 50/30 using light, e.g. lasers
• CPC Class Codes: H02J 50/402 : the two or more transmitting or the two or more receiving devices being integrated in the same unit, e.g. power mats with several coils or antennas with several sub-antennas
• CPC Class Codes: H02J 7/0042 : characterised by the mechanical construction
• CPC Class Codes: H04B 10/807 : Optical power feeding, i.e. transmitting power using an optical signal

Abstract

An aerial platform receives power in the form of light, for example laser light, transmitted via an optical fiber from a remote optical power source. The platform comprises a receiver which converts at least a portion of the light to a different form of power, for example electric power. The platform also comprises a propulsion element which consumes the different form of power to generate propulsive thrust. Supplying power to the aerial platform from a remote source enables the platform to remain aloft longer than a battery or fuel tank carried by the platform would allow. Transmitting the power in the form of light is preferable in many cases to transmitting electric power, because electrical conductors are generally heavier than optical fibers, and are hazardous in the presence of lightning or a high-voltage power line.

Claims

1. A system, comprising:

an optical transmission element having a first end and a second end;

an optical power source coupled to the first end of the optical transmission element and operable to transmit optical power towards the second end of the optical transmission element;

an aerial platform;

an energy storage device integrated with the aerial platform;

a data transfer mechanism to pass information between the optical power source and the aerial platform;

an optical power receiver of the aerial platform physically coupled to the second end of the optical transmission element and operable to receive at least some of the optical power produced by the optical power source, the optical power receiver further operable to convert at least a portion of the received optical power into captured electric power;

a propulsion element of the aerial platform operable to use at least a portion of the captured electric power to propel the aerial platform; and

at least one controller programmed to vary how much optical power is output from the optical power source based on an indication from the aerial platform, wherein the indication from the aerial platform is generated by at least one sensor circuit of the aerial platform and communicated via the data transfer mechanism, wherein the indication from the aerial platform is based on a temperature of the optical power receiver or a state of charge of the energy storage device.

2. The system of claim 1 wherein the at least one sensor circuit is a temperature sensor or a charge state sensor.

3. The system of claim 1 wherein the optical transmission element comprises at least one of the following:

a single-mode optical fiber,

a multimode step-index optical fiber,

a multimode gradient-index optical fiber,

a photonic crystal fiber, and

a plastic optical fiber.

4. The system of claim 1 wherein the aerial platform is selected from a group, comprising:

a fixed-wing unmanned aerial vehicle,

a vertical-takeoff-and-landing unmanned aerial vehicle, and

an aerostat.

5. The system of claim 1 wherein the optical power receiver comprises at least one of the following:

a photovoltaic cell,

a thermophotovoltaic cell,

a thermoelectric device, and

a heat engine.

6. The system of claim 1, wherein the energy storage device integrated with the aerial platform is operable to store captured electric power and operable to supply captured electric power to the propulsion element.

7. The system of claim 6 wherein the energy storage device comprises at least one of the following:

a primary battery,

a secondary battery,

a capacitor,

a supercapacitor, and

a flywheel.

8. The system of claim 1 wherein the optical power source comprises at least one of the following:

an incoherent array of diode lasers,

an at least partially coherent array of diode lasers,

a solid-state laser,

a diode-pumped fiber laser,

a disk laser, and

a diode pumped alkali vapor laser.

9. The system of claim 1 further comprising:

a tether coupled to the aerial platform, the tether operable to constrain motion of the aerial platform relative to the optical power source.

10. The system of claim 9, wherein the tether comprises at least a portion of the optical power transmission element.

11. The system of claim 9, wherein the tether comprises at least one of the following:

a strength member,

a sheath,

an optical communications fiber,

an optical fiber for illumination,

an electrical signal conductor,

an electrical power conductor, and

a static-dissipating conductive element.

12. The system of claim 9 further comprising:

a tether deployment mechanism operable to controllably deploy and retract the tether.

13. The system of claim 1 further comprising:

a base unit, and

a tether coupled to the base unit and to the aerial platform, the tether operable to constrain motion of the aerial platform relative to the base unit.

14. The system of claim 1, further comprising a controller programmed to maintain the aerial platform in stable flight, wherein to maintain the aerial platform in stable flight, the controller is programmed to automatically control at least one of the following:

altitude of the aerial platform during flight,

position, relative to the optical power source, of the aerial platform during flight,

pitch angle of the aerial platform during flight,

roll angle of the aerial platform during flight,

yaw angle of the aerial platform during flight,

velocity of the aerial platform during flight,

flight path of the aerial platform during flight,

tension on a tether coupled to the aerial platform during flight.

15. The system of claim 1, further comprising a safety system operable to detect an unsafe condition.

16. The system of claim 15, wherein the safety system comprises a laser-light detection apparatus operable to detect the unsafe condition, wherein the laser-light detection apparatus, in response to detecting the unsafe condition, is operable to direct a suspension of optical power emission from the optical power source.

17. A method to operate an aerial platform, the method comprising:

transmitting, via an optical transmission element, optical power from an optical power source to an optical power receiver attached to an aerial platform;

generating by at least one sensor circuit associated with the aerial platform an indication based on a temperature of the optical power receiver or a state of charge of an energy storage element associated with the aerial platform;

communicating the indication generated by the at least one sensor circuit from the aerial platform to the optical power source via a data transfer mechanism;

operating at least one controller programmed to vary how much optical power is output from the optical power source based on the indication from the aerial platform;

converting at least a portion of the optical power received by the optical power receiver into captured energy and storing the captured energy in the energy storage element, the captured energy having a form of power usable by a propulsion element to propel the aerial platform;

supplying captured energy to the propulsion element; and

propelling the aerial platform with captured energy consumed by the propulsion element.

18. The method of claim 17, wherein propelling the aerial platform comprises:

producing vertical thrust,

producing horizontal thrust, and

producing attitude control torque about an axis of the platform.

19. The method of claim 17, wherein the captured energy includes electrical power.

20. The method of claim 17, comprises:

storing at least a portion of the captured energy in the energy storage element integrated with the aerial platform; and

supplying electrical power from the energy storage element to propel the aerial platform.

21. The method of claim 20, further comprising at least one of the following:

limiting how much captured energy is stored in the energy storage element to an amount of stored energy insufficient for the propulsion element to propel the aerial platform beyond a specified flight envelope during a time when the optical power receiver does not receive optical power, and

limiting how much captured energy can be supplied by the energy storage element, such that a provided amount of captured energy supplied from the energy storage element is insufficient for the propulsion element to propel the aerial platform beyond a specified flight envelope during the time when the optical power receiver does not receive optical power.

22. The method of claim 17, wherein generating the indication from the aerial platform by the at least one sensor circuit includes generating a temperature value from a temperature sensor based on a temperature of the optical power receiver or generating a charge value from a charge state sensor based on a state of charge of the energy storage element.

23. The method of claim 17, further comprising automatically controlling, via the at least one controller, at least one of the following:

altitude of the aerial platform during flight,

position, relative to the optical power source, of the aerial platform during flight,

pitch angle of the aerial platform during flight,

roll angle of the aerial platform during flight,

yaw angle of the aerial platform during flight,

velocity of the aerial platform during flight,

flight path of the aerial platform during flight, and

tension on a tether coupled to the aerial platform during flight.

24. The method of claim 17, further comprising:

detecting an unsafe condition via safety system logic integrated with the aerial platform; and

in response to detecting the unsafe condition, operating the at least one controller to automatically direct performance of at least one of the following;

landing the aerial platform,

communicating a command to the optical power source via the data transfer mechanism to direct a suspension of optical power emission from the optical power source,

detaching, via an emergency disconnect mechanism, an end of a tether from a point of attachment, the tether having a first end coupled to the optical power source and a second end coupled to the aerial platform,

severing, via the emergency disconnect mechanism, the tether, and

generating a user notification and communicating the user notification from the aerial platform to the optical power source via the data transfer mechanism, for output via a user interface associated with the optical power source.

25. A device to power an aerial platform, comprising:

a laser-based optical power source coupleable to a first end of an optical transmission element, the laser-based optical power source arranged to transmit optical energy towards a second end of the optical transmission element coupleable to the aerial platform, wherein an optical power receiver of the aerial platform is arranged to receive at least some of the optical energy produced by the laser-based optical power source and further arranged to convert at least a portion of the received optical energy into captured electric power for storage in an energy storage element associated with the aerial platform;

at least one detection device arranged to receive aerial platform information from the aerial platform via a data transfer mechanism coupled between the optical power source and the aerial platform, wherein the aerial platform information is generated by at least one sensor circuit associated with the aerial platform, wherein the at least one sensor is arranged to pass sensor information to an aerial-platform-based controller, and wherein the aerial-platform-based controller is arranged to pass the sensor information to the at least one detection device via the data transfer mechanism;

a safety system coupled to the at least one detection device, the safety system arranged to generate a determination that integrity of the optical transmission element is compromised based on the aerial platform information, wherein the safety system is arranged to direct the aerial platform to land based on a determined unsafe condition; and

an optical-power-source-based controller programmed to variably direct how much optical energy is output from the optical power source based on the aerial platform information communicated via the data transfer mechanism.

26. The device of claim 25, further comprising:

a base unit;

a tether coupleable to the aerial platform, the tether operable to constrain motion of the aerial platform relative to the base unit;

a tether deployment mechanism operable to controllably deploy and retract the tether; and

an emergency disconnect mechanism coupled to the safety system and arranged to release the aerial platform based on a determined unsafe condition.

27. The device of claim 26, wherein the optical-power-source-based controller is programmed to controllably deploy the tether via the tether deployment mechanism to a determined length based on length data from at least one first sensor circuit and wherein the optical-power-source-based controller is programmed to control tension of a deployed tether based on tension data from at least one second sensor circuit.

28. The device of claim 25, wherein the determined unsafe condition includes at least one of:

an unsafe wind speed condition determined using information generated by at least one wind speed sensor circuit;

an unsafe wind gust condition determined using information generated by the at least one wind speed sensor circuit;

an unsafe altitude condition determined using information generated by at least one altimeter sensor circuit;

an unsafe velocity condition determined using information generated by at least one accelerometer circuit;

an unsafe orientation condition determined using information generated by at least one orientation circuit;

an unsafe energy level condition determined using information generated by at least one charge state sensor circuit;

a hardware fault determined via safety system logic integrated with the aerial platform;

a break in the tether determined via the safety system logic integrated with the aerial platform;

a software fault determined via the safety system logic integrated with the aerial platform; and

an unsafe temperature condition determined using information generated by at least one temperature sensor circuit.

29. The device of claim 25 wherein the aerial platform information is representative of a temperature of the optical power receiver.