Parachute system mounted to payload

Patent metadata

Field	Value
Publication number	US-9604726-B2
Application number	US-201514665653-A
Country	US
Kind code	B2
Filing date	Mar 23, 2015
Priority date	Mar 23, 2015
Publication date	Mar 28, 2017
Grant date	Mar 28, 2017

Abstract

A balloon system is provided including a balloon envelope, a payload secured to the balloon envelope, a first parachute positioned within a parachute container, the parachute container secured to the payload, a first bridle line having a first end secured to the balloon system and a second end secured to the parachute container, a controller positioned on the balloon system, wherein when the controller receives a signal to deploy the parachute container, the controller is operable to cause the parachute container to be released downwardly from the payload.

First claim

What is claimed is:

1. A balloon system comprising:
a balloon envelope;
a payload secured to the balloon envelope;
a first parachute positioned within a parachute container, the parachute container secured to the payload;
a first bridle line having a first end secured to the balloon system and a second end secured to the parachute container;
a controller positioned on the balloon system;
wherein when the controller receives a signal to deploy the parachute container, the controller is operable to cause the parachute container to be released downwardly from the payload; and
wherein the signal to deploy the parachute container is based on sensed change in pressure within the balloon envelope.

2. The balloon system of claim 1 , wherein the first bridle line has a length that is 5-20 times the distance between an apex of the balloon envelope and a bottom of the payload.

3. The balloon system of claim 2 , wherein the first bridle line has a length that is 8-10 times the distance between the apex of the balloon envelope and the bottom of the payload.

4. The balloon system of claim 1 , wherein the parachute container is secured to a bottom of the payload and dropped downwardly upon release.

5. The balloon system of claim 1 , wherein the parachute container is secured over a launch platform secured to the payload and directed to launch the parachute container downwardly at an angle of 0-90 degrees from vertical; and
wherein upon release of the parachute container, the parachute container is launched downwardly from the launch platform.

6. The balloon system of claim 5 , wherein the launch platform is directed to launch the parachute container downwardly at an angle of 0-45 degrees from vertical.

7. A balloon system comprising:
a balloon envelope;
a payload secured to the balloon envelope;
a first parachute positioned within a parachute container, the parachute container secured to the payload;
a first bridle line having a first end secured to the balloon system and a second end secured to the parachute container;
a controller positioned on the balloon system;
wherein when the controller receives a signal to deploy the parachute container, the controller is operable to cause the parachute container to be released downwardly from the payload; and
wherein the first parachute is a drogue parachute attached to a second main parachute with a second bridle line.

8. The balloon system of claim 7 , wherein the second main parachute is drawn out of the parachute container by the drogue parachute during the descent of the payload and balloon envelope.

9. The balloon system of claim 7 , wherein the drogue parachute is secured over a launch platform in the parachute container positioned over a compressed spring, and a static line secured to the first bridle line is adapted to release the drogue parachute at a predetermined distance beneath the payload.

10. A balloon system comprising:
a balloon envelope;
a payload secured to the balloon envelope;
a first parachute positioned within a parachute container, the parachute container secured to the payload;
a first bridle line having a first end secured to the balloon system and a second end secured to the parachute container;
a controller positioned on the balloon system;
wherein when the controller receives a signal to deploy the parachute container, the controller is operable to cause the parachute container to be released downwardly from the payload; and
wherein the signal to deploy the parachute container is based on a measured rate of descent or a measured change in the rate of descent of the payload.

11. A balloon system comprising:
a balloon envelope having a maximum diameter when inflated;
a payload secured to the balloon envelope;
a first parachute positioned within a parachute container, the parachute container secured to the payload;
a first bridle line having a first end secured to the balloon system and a second end secured to the parachute container;
a controller positioned on the balloon system;
wherein the bridle line has a length that is 5-20 times the distance between an apex of the balloon envelope and a bottom of the payload;
wherein when the controller receives a signal to deploy the parachute container, the controller is operable to cause the parachute container to be released downwardly from the payload at an angle of 0-90 degrees from vertical; and
wherein the first parachute is a drogue parachute attached to a second main parachute with a second bridle line.

12. The balloon system of claim 11 , wherein the parachute container is secured to a bottom of the payload, and drops downwardly upon release.

13. The balloon system of claim 11 , wherein the parachute container is secured over a launch platform secured to the payload and directed to launch the parachute container downwardly at an angle of 0-45 degrees from vertical; and
wherein upon release of the parachute container, the parachute container is launched downwardly from the launch platform at an angle of 0-45 degrees from vertical.

14. The balloon system of claim 11 , wherein the drogue parachute is secured over a launch platform in the parachute container positioned over a compressed spring, and a static line secured to the first bridle line is adapted to release the drogue parachute at a predetermined distance beneath the payload.

15. A method of deploying a parachute system on a balloon system comprising:
providing a balloon system including a balloon envelope, a payload secured to the balloon system, a first parachute positioned within a parachute container, the parachute container secured to the payload, a first bridle line having a first end secured to the balloon system and a second end secured to the parachute container, the first bridle line having a length that is 5-20 times the distance between an apex of the balloon envelope and a bottom of the payload;

receiving a signal to deploy the parachute container;
releasing the parachute container downwardly from the payload at an angle of 0-90 degrees from vertical; and
wherein the signal to deploy the parachute container is based on a measured rate of descent or a measured change in the rate of descent of the payload.

16. The method of claim 15 , wherein the first parachute is a drogue parachute attached to a second main parachute with a second bridle line.

17. The method of claim 15 , wherein the signal to deploy the parachute container is also based on sensed change in pressure within the balloon envelope.

18. A method of deploying a parachute system on a balloon system comprising:
providing a balloon system including a balloon envelope, a payload secured to the balloon system, a first parachute positioned within a parachute container, the parachute container secured over a launch platform secured to the payload and directed to launch the parachute container downwardly at an angle of 0-45 degrees from vertical, a first bridle line having a first end secured to the balloon system and a second end secured to the parachute container, the first bridle line having a length that is 5-20 times the distance between an apex of the balloon envelope and a bottom of the payload;
receiving a signal to deploy the parachute container based on sensed change in pressure within the balloon envelope; and
launching the parachute container downwardly from the launch platform at an angle of 0-45 degrees from vertical.

Assignees

• Google Inc
• X Dev Llc

Inventors

• Fourie Daniel

Classifications

• B64B1/40 Primary

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

• B64D17/80

  in association with aircraft, e.g. for braking thereof · CPC title

• B64D17/62 Primary

  Deployment · CPC title

• B64D17/64

  by extractor parachute · CPC title

• B64D1/12

  Releasing · CPC title