Balloon power sources with a buoyancy trade-off

Patent metadata

Field	Value
Publication number	US-9329600-B2
Application number	US-201514612945-A
Country	US
Kind code	B2
Filing date	Feb 3, 2015
Priority date	Aug 20, 2012
Publication date	May 3, 2016
Grant date	May 3, 2016

Abstract

Example embodiments may facilitate altitude control by a balloon in a balloon network. An example method involves: (a) causing a balloon to operate in a first mode, wherein the balloon comprises an envelope, a high-pressure storage chamber, and a solar power system, (b) while the balloon is operating in the first mode: (i) operating the solar power system to generate power for the balloon and (ii) using at least some of the power generated by the solar power system to move gas from the envelope to the high-pressure storage chamber such that the buoyancy of the balloon decreases; (c) causing the balloon to operate in a second mode; and while the balloon is operating in the second mode, moving gas from the high-pressure storage chamber to the envelope such that the buoyancy of the balloon increases.

First claim

What is claimed is:

1. An aerial vehicle comprising:
a solar power system configured to generate power for the aerial vehicle, wherein the aerial vehicle comprises an envelope and a high-pressure storage chamber;
a control system that is configured to cause the aerial vehicle to operate in at least a first mode and a second mode;
wherein, during operation in the first mode, the control system is configured to:
operate the solar power system to generate power;
decrease the buoyancy of the aerial vehicle by using at least some of the power generated by the solar power system to move gas from the envelope to the high-pressure storage chamber such that the buoyancy of the aerial vehicle decreases; and
increase the buoyancy of the aerial vehicle by: (a) operating a fuel cell of the aerial vehicle in reverse to produce gas, and (b) moving the gas produced by the fuel cell to the envelope;

wherein, during operation in the second mode, the control system is configured to:
decrease the buoyancy of the aerial vehicle by: (a) moving gas from the envelope to the fuel cell, and (b) operating the fuel cell so as to use the gas from the envelope to generate power; and
increase the buoyancy of the aerial vehicle by moving gas from the high-pressure storage chamber to the envelope.

2. The aerial vehicle of claim 1 , wherein the aerial vehicle is a balloon.

3. The aerial vehicle of claim 1 , wherein, during operation in the first mode, the control system is further configured to:
determine that the aerial vehicle should move in a given horizontal direction;
determine that wind at a lower altitude corresponds to the given horizontal direction; and
in response to determining that wind at the lower altitude corresponds to the given horizontal direction, use at least some of the power generated by the solar power system to move gas from the envelope to the high-pressure storage chamber such that the buoyancy of the aerial vehicle decreases.

4. The aerial vehicle of claim 1 , wherein, during operation in the first mode, the control system is further configured to:
determine that the aerial vehicle should move in a given horizontal direction;
determine that wind at a higher altitude corresponds to the given horizontal direction; and
in response to determining that wind at the higher altitude corresponds to the given horizontal direction, operate the fuel cell of the aerial vehicle in reverse and move the gas produced by the fuel cell to the envelope such that the buoyancy of the aerial vehicle increases.

5. The aerial vehicle of claim 1 , wherein, during operation in the second mode, the control system is further configured to:
determine that the aerial vehicle should move in a given horizontal direction;
determine that wind at a lower altitude corresponds to the given horizontal direction; and
in response to determining that wind at the lower altitude corresponds to the given horizontal direction, operate the fuel cell so as to use the gas from the envelope to generate power for the aerial vehicle, such that the buoyancy of the aerial vehicle decreases.

6. The aerial vehicle of claim 1 , wherein, during operation in the second mode, the control system is further configured to:
determine that the aerial vehicle should move in a given horizontal direction;
determine that wind at a higher altitude corresponds to the given horizontal direction; and
in response to determining that wind at the higher altitude corresponds to the given horizontal direction, move gas from the high-pressure storage chamber to the envelope such that the buoyancy of the aerial vehicle increases.

7. An aerial vehicle comprising:
a solar power system configured to generate power for the aerial vehicle, wherein the aerial vehicle comprises an envelope and a high-pressure storage chamber;
a control system that is configured to cause the aerial vehicle to operate in at least a first mode and a second mode;
wherein, during operation in the first mode, the control system is configured to:
operate the solar power system to generate power for the aerial vehicle;
use at least some of the power generated by the solar power system to move gas from the envelope to the high-pressure storage chamber such that the buoyancy of the aerial vehicle decreases;
determine that the aerial vehicle should move to a higher altitude and responsively: (a) operate a fuel cell of the aerial vehicle in reverse to produce gas, and (b) move the gas produced by the fuel cell to the envelope such that the buoyancy of the aerial vehicle increases; and

cause the aerial vehicle to operate in a second mode, wherein, during operation in the second mode, the control system is configured to determine that the aerial vehicle should move to a lower altitude and responsively: (a) move gas from the envelope to the fuel cell, and (b) operate the fuel cell so as to use the gas from the envelope to generate power for the aerial vehicle, such that the buoyancy of the aerial vehicle decreases.

8. The aerial vehicle of claim 7 , wherein the first mode is a daytime mode and the second mode is a nighttime mode.

9. The aerial vehicle of claim 8 , wherein the control system is further configured to:
detect a predetermined day-night transition condition; and
responsively cause the aerial vehicle to transition from operation in the daytime mode to operation in the nighttime mode.

10. The aerial vehicle of claim 7 , wherein, during operation in the second mode, the control system is further configured to move gas from the high-pressure storage chamber to the envelope such that the buoyancy of the aerial vehicle increases.

11. The aerial vehicle of claim 7 , wherein the aerial vehicle further comprises a battery, and wherein, during operation in the second mode, the control system is further configured to use power supplied by the battery.

12. The aerial vehicle of claim 7 , wherein, during operation in the first mode, the control system is further configured to:
determine that the aerial vehicle should move in a given horizontal direction;
determine that wind at a lower altitude corresponds to the given horizontal direction; and
in response to determining that wind at the lower altitude corresponds to the given horizontal direction, use at least some of the power generated by the solar power system to move gas from the envelope to the high-pressure storage chamber such that the buoyancy of the aerial vehicle decreases.

13. The aerial vehicle of claim 7 , wherein, during operation in the first mode, the control system is further configured to:
determine that the aerial vehicle should move in a given horizontal direction;
determine that wind at a higher altitude corresponds to the given horizontal direction; and
in response to determining that wind at the higher altitude corresponds to the given horizontal direction, operate the fuel cell of the aerial vehicle in reverse and move the gas produced by the fuel cell to the envelope such that the buoyancy of the aerial vehicle increases.

14. The aerial vehicle of claim 7 , wherein, during operation in the second mode, the control system is further configured to:
determine that the aerial vehicle should move in a given horizontal direction;
determine that wind at a lower altitude corresponds to the given horizontal direction; and
in response to determining that wind at the lower altitude corresponds to the given horizontal direction, operate the fuel cell so as to use the gas from the envelope to generate power for the aerial vehicle, such that the buoyancy of the aerial vehicle decreases.

15. The aerial vehicle of claim 7 ,

Assignees

• Google Inc

Inventors

• Devaul Richard Wayne
• Teller Eric
• Biffle Clifford L
• Weaver Joshua

Classifications

• G05D1/042 Primary

  specially adapted for aircraft · CPC title

• B64B1/40 Primary

  Balloons (B64B1/58 takes precedence; toy balloons A63H27/10) · CPC title

• B64B1/62

  Controlling gas pressure, heating, cooling, or discharging gas · CPC title

• C25B1/04

  by electrolysis of water · CPC title

• H02S20/30

  Supporting structures being movable or adjustable, e.g. for angle adjustment · CPC title