IP Library Granted Patent US 9,604,726
Granted Patent B2
US 9,604,726 · App. 14/665,653 · Granted Mar 28, 2017

Parachute system mounted to payload

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Quick Facts
Patent No.
US 9,604,726
App. No.
14/665,653
Granted
Mar 28, 2017
Kind
B2
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.

Claims (56)

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.

Assignments (9)
CORRECTIVE ASSIGNMENT TO CORRECT THE THE REMOVAL OF THE INCORRECTLY RECORDED APPLICATION NUMBERS 14/149802 AND 15/419313 PREVIOUSLY RECORDED AT REEL: 44144 FRAME: 1. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Mar 4, 2024
From: GOOGLE INC.
To: GOOGLE LLC
Reel/Frame 068092/0502 →
MERGER Recorded Oct 20, 2022
From: AEROSTAR INTERNATIONAL, INC.
To: AEROSTAR INTERNATIONAL, LLC
Reel/Frame 061733/0285 →
CORRECTIVE ASSIGNMENT TO CORRECT THE STATE OF THE ASSIGNEE FROM MINNESOTA TO SOUTH DAKOTA AS PREVIOUSLY RECORDED AT REEL: 056282 FRAME: 0458. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Jun 6, 2022
From: LOON LLC
To: AEROSTAR INTERNATIONAL, INC.
Reel/Frame 061521/0291 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 18, 2021
From: LOON LLC
To: AEROSTAR INTERNATIONAL, INC.
Reel/Frame 056282/0458 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 8, 2020
From: X DEVELOPMENT LLC
To: LOON LLC
Reel/Frame 052345/0094 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 27, 2018
From: X DEVELOPMENT LLC
To: LOON LLC
Reel/Frame 048175/0720 →
CHANGE OF NAME Recorded Oct 6, 2017
From: GOOGLE INC.
To: GOOGLE LLC
Reel/Frame 044144/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 1, 2016
From: GOOGLE INC.
To: X DEVELOPMENT LLC
Reel/Frame 039900/0610 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 27, 2015
From: FOURIE, DANIEL
To: GOOGLE INC.
Reel/Frame 035279/0822 →