Aerial platform powered via an optical transmission element

Patent metadata

Field	Value
Publication number	US-9800091-B2
Application number	US-201214124993-A
Country	US
Kind code	B2
Filing date	Jun 9, 2012
Priority date	Jun 9, 2011
Publication date	Oct 24, 2017
Grant date	Oct 24, 2017

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.

First claim

What is claimed is:

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

Assignees

• Nugent Jr Thomas J
• Bashford David
• Kare Jordin T
• Lasermotive Inc

Inventors

• Nugent Jr Thomas J
• Bashford David
• Kare Jordin T

Classifications

• H02J2105/32

  for aircrafts · CPC title

• H02J7/70

  characterised by the mechanical construction · CPC title

• B64U10/30

  Lighter-than-air aircraft, e.g. aerostatic aircraft · CPC title

• B64U2201/202

  using tethers for connecting to ground station · CPC title

• H04B10/807

  Optical power feeding, i.e. transmitting power using an optical signal · CPC title