Energy-efficient launch system for aerial vehicles

Patent metadata

Field	Value
Publication number	US-10556709-B1
Application number	US-201715451218-A
Country	US
Kind code	B1
Filing date	Mar 6, 2017
Priority date	Mar 6, 2017
Publication date	Feb 11, 2020
Grant date	Feb 11, 2020

Abstract

An energy-efficient launch system that utilizes the principles of whip dynamics to launch payloads at high speeds is described. The launch system may include a marine vehicle having an onboard power source. A tapered, superconducting cable may be retractably connected to the marine vehicle via a winch and electrically connected to the power source. One or more aerial vehicles may be coupled to and receive power via the cable. To launch a payload at the end of the cable, the marine vehicle, winch, and/or aerial vehicles may be operated in coordination to create, propagate, and accelerate a whip waveform along the cable toward the payload.

First claim

What is claimed is:

1. A launch apparatus, comprising:
a marine vehicle comprising a power source;
a superconducting cable coupled at a first end to the marine vehicle via a winch, wherein a diameter of the superconducting cable tapers from the first end toward a second end distal from the first end;
a plurality of aerial vehicles spaced along and coupled to the superconducting cable, each of the plurality of aerial vehicles receiving power from the power source via the superconducting cable;
a payload carried by a final aerial vehicle of the plurality of aerial vehicles, the final aerial vehicle coupled to the second end of the superconducting cable; and
a controller in communication with the marine vehicle, the winch, and the plurality of aerial vehicles, the controller configured to at least:
instruct the marine vehicle to travel at a determined velocity and provide power to the plurality of aerial vehicles via the superconducting cable;
instruct the winch to wind the superconducting cable to cause a waveform to propagate along the superconducting cable from the first end to the second end;
instruct the plurality of aerial vehicles to cause the waveform to propagate along the superconducting cable toward the second end; and
instruct the final aerial vehicle to release the payload as the waveform reaches the second end, thereby launching the payload.

2. The launch apparatus of claim 1 , wherein each of the plurality of aerial vehicles includes a propulsion mechanism including at least one of a propeller and a propeller motor, a fan, a jet, a turbojet, a turbofan, an electric jet, or a jet engine.

3. The launch apparatus of claim 1 , wherein the waveform comprises a shape including at least one of a half wave, a full wave, or a loop, the waveform propagating along the superconducting cable at an initial speed at the first end and at a final speed at the second end, the final speed being greater than the initial speed.

4. The launch apparatus of claim 3 , wherein a combination of the tapering diameter of the superconducting cable, the winding of the superconducting cable by the winch, and at least one of the shape or the initial speed of the waveform propagating along the superconducting cable causes the payload to be released at the final speed.

5. The launch apparatus of claim 1 , wherein instructing the final aerial vehicle to release the payload comprises releasing, from the superconducting cable, the final aerial vehicle together with the payload.

6. An apparatus, comprising:
a vehicle comprising a power source;
a cable movably coupled at a first end to the vehicle;
at least one aerial vehicle coupled to a second end of the cable distal from the first end, the at least one aerial vehicle receiving power from the power source via the cable, and the at least one aerial vehicle carrying a payload; and
a controller in communication with the vehicle and the at least one aerial vehicle, the controller configured to at least:
instruct the vehicle to travel at a determined velocity and provide power to the at least one aerial vehicle via the cable;
cause a waveform to propagate along the cable from the first end to the second end; and
instruct the at least one aerial vehicle to release the payload as the waveform reaches the second end, thereby launching the payload.

7. The apparatus of claim 6 , wherein the vehicle is at least one of a marine vehicle, an aerial vehicle, or a land-based vehicle.

8. The apparatus of claim 6 , wherein the cable comprises a superconducting cable having a diameter that tapers from the first end to the second end.

9. The apparatus of claim 8 , wherein the cable is movably coupled at the first end to the vehicle via a winch; and
wherein causing the waveform to propagate along the cable from the first end to the second end comprises instructing the winch to retract the cable to cause the waveform to propagate along the cable.

10. The apparatus of claim 9 , wherein the at least one aerial vehicle comprises a plurality of aerial vehicles spaced along and coupled to the cable between the first end and the second end.

11. The apparatus of claim 10 , wherein at least some of the plurality of aerial vehicles comprise propulsion mechanisms including at least one of propellers and propeller motors, fans, jets, turbojets, turbofans, electric jets, or jet engines that receive power from the power source via the cable.

12. The apparatus of claim 10 , wherein at least some of the plurality of aerial vehicles comprise a fixed wing.

13. The apparatus of claim 10 , wherein causing the waveform to propagate along the cable from the first end to the second end comprises instructing at least some of the plurality of aerial vehicles to introduce the waveform that propagates along the cable toward the second end, the waveform having an initial shape and an initial speed.

14. The apparatus of claim 13 , wherein at least one of the tapering diameter of the cable, the retracting of the cable by the winch, or at least one of the initial shape or the initial speed of the waveform propagating along the cable causes the payload to be released at a final speed greater than the initial speed.

15. A method, comprising:
instructing a vehicle to travel at a determined velocity, the vehicle comprising a power source and a cable retractably coupled to the vehicle at a first end, a plurality of aerial vehicles being spaced along and coupled to the cable;
causing a retraction mechanism to retract the cable to cause a waveform to propagate along the cable from the first end to a second end distal from the first end; and
instructing a release of a payload from the second end of the cable as the waveform reaches the second end.

16. The method of claim 15 , wherein the payload is one of a final aerial vehicle of the plurality of aerial vehicles at the second end, or carried by the final aerial vehicle at the second end.

17. The method of claim 15 , further comprising:
instructing at least some of the plurality of aerial vehicles to decouple from the cable as the waveform propagates along the cable toward the second end.

18. The method of claim 15 , further comprising instructing at least some of the plurality of aerial vehicles to cause the waveform to propagate along the cable toward the second end, the at least some of the plurality of aerial vehicles receiving power from the power source via the cable; and
wherein the waveform having an initial shape and an initial speed.

19. The method of claim 18 , wherein at least one of a tapering diameter of the cable, the retracting of the cable by the retraction mechanism, or at least one of the initial shape or the initial speed of the waveform propagating along the cable causes the payload to be released at a final speed greater than the initial speed.

20. The method of claim 15 , further comprising:
upon release of the payload from the final aerial vehicle, at least one of:
instructing the vehicle to stop;
at least one of stopping the retracting of the cable or extending the cable by the retraction mechanism; or
instructing at least some of the plurality of aerial vehicles to slow or stop a movement of the cable.

Assignees

• Amazon Tech Inc

Inventors

• Kimchi Gur
• Legrand Iii Louis Leroi

Classifications

• B64F1/08 Primary

  using winches · CPC title

• B64D27/10

  of gas-turbine type  (jet aircraft B64D27/16) · CPC title

• B64D1/12

  Releasing · CPC title

• B64D27/16

  of jet type · CPC title

• B64U50/12

  using turbine engines, e.g. turbojets or turbofans · CPC title