IP Library Granted Patent US 11,897,593
Granted Patent B2
US 11,897,593 · App. 16/888,999 · Granted Feb 13, 2024

Telescoping support structure

Inventor: John Cromie (Menlo Park, CA)
Assignee: Aerostar International, LLC
B64B1/40B66D5/02H04W84/06
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Quick Facts
Patent No.
US 11,897,593
App. No.
16/888,999
Granted
Feb 13, 2024
Kind
B2
Abstract

The technology relates to a telescoping support structure which can be suspended between two objects. The telescoping support structure uses projections between adjacent tubular sections in order to prevent the adjacent tubular sections from falling away from one another. Although the telescoping support structure may be utilized in various different environments and circumstances, it may be of particular usefulness in the field of high-altitude ballooning. For instance, when used in a balloon system, the telescoping support structure may be suspended between two objects such as an upper payload structure and a lower payload structure. As another example, the telescoping support structure may be suspended between a balloon envelope and a payload which, in some examples, may include an upper and a lower payload structure.

Claims (49)

1. A method of deploying a balloon system with a telescoping support structure, the method comprising:

while the telescoping support structure is in a collapsed configuration:

attaching a first terminal section of the telescoping support structure to a first portion of the balloon system,

attaching a second terminal section of the telescoping support structure to a second portion of the balloon system,

inflating a balloon envelope of the balloon system, and launching the balloon system into the air; and

extending the telescoping support structure when the balloon system reaches a first desired altitude; and

wherein the first portion of the balloon system is the balloon envelope and the second portion of the balloon system is a payload.

2. The method of claim 1 , wherein, as a result of extending the telescoping support structure when the balloon system reaches a first desired altitude, the payload moves away from the balloon envelope.

3. The method of claim 1 , wherein the first terminal section is nested at least partially within the second terminal section when the telescoping support structure is in a collapsed configuration.

4. The method of claim 1 , wherein the telescoping support structure includes one or more intermediate sections, the one or more intermediate sections being arranged between the first terminal section and the second terminal section when the telescoping support structure is extended.

5. A method of deploying a balloon system with a telescoping support structure, the method comprising:

while the telescoping support structure is in a collapsed configuration:

attaching a first terminal section of the telescoping support structure to a first portion of the balloon system,

attaching a second terminal section of the telescoping support structure to a second portion of the balloon system,

inflating a balloon envelope of the balloon system, and launching the balloon system into the air;

extending the telescoping support structure when the balloon system reaches a first desired altitude; and

wherein the balloon system comprises an upper payload and a lower payload, the first portion of the balloon system is the upper payload, and the second portion of the balloon system is the lower payload.

6. The method of claim 5 , wherein, as a result of extending the telescoping support structure when the balloon system reaches a first desired altitude, the lower payload moves away from the upper payload.

7. A method of deploying a balloon system with a telescoping support structure, the method comprising:

while the telescoping support structure is in a collapsed configuration:

attaching a first terminal section of the telescoping support structure to a first portion of the balloon system,

attaching a second terminal section of the telescoping support structure to a second portion of the balloon system,

inflating a balloon envelope of the balloon system, and launching the balloon system into the air;

extending the telescoping support structure when the balloon system reaches a first desired altitude;

wherein extending the telescoping support structure when the balloon system reaches a first desired altitude comprises extending a cable connected to the first terminal section and the second terminal section; and

wherein extending the cable connected to the first terminal section and the second terminal section comprises rotating a spool on which the cable is wrapped.

8. The method of claim 7 , wherein the spool includes a wire configured to restrain at least some of the cable on the spool when the telescoping support structure is in a collapsed configuration; and extending the cable connected to the first terminal section and the second terminal section comprises severing the wire.

9. The method of claim 7 , further comprising controlling a rate at which the telescoping support structure is extended using a damper mechanism.

10. The method of claim 9 , wherein the damper mechanism comprises a passive damper which produces torque in response to rotation of the spool.

11. The method of claim 9 , wherein the damper mechanism comprises an active damper which includes a motor.

12. The method of claim 11 , wherein extending the telescoping support structure when the balloon system reaches a first desired altitude results in a partial extension of the telescoping support structure.

13. The method of claim 12 , further comprising extending the telescoping support structure so that it is fully extended when the balloon system reaches a second desired altitude.

14. A method of deploying a balloon system with a telescoping support structure, the method comprising:

while the telescoping support structure is in a collapsed configuration:

attaching a first terminal section of the telescoping support structure to a first portion of the balloon system,

attaching a second terminal section of the telescoping support structure to a second portion of the balloon system,

inflating a balloon envelope of the balloon system, and launching the balloon system into the air;

extending the telescoping support structure when the balloon system reaches a first desired altitude; and

further comprising sending a signal to the balloon system, and wherein the step of extending the telescoping support structure when the balloon system reaches a first desired altitude is done in response to the balloon system receiving the signal.

15. The method of claim 14 wherein, as a result of extending the telescoping support structure when the balloon system reaches a first desired altitude, a payload carried by the balloon system moves away from the balloon envelope.

16. The method of claim 14 further comprising controlling a rate at which the telescoping support structure is extended using a damper mechanism.

17. A method of deploying a balloon system with a telescoping support structure, the method comprising:

while the telescoping support structure is in a collapsed configuration:

attaching a first terminal section of the telescoping support structure to a first portion of the balloon system,

attaching a second terminal section of the telescoping support structure to a second portion of the balloon system,

inflating a balloon envelope of the balloon system, and launching the balloon system into the air;

extending the telescoping support structure when the balloon system reaches a first desired altitude; and

further comprising monitoring an altitude of balloon system with an altitude sensor, and wherein the step of extending the telescoping support structure when the balloon system reaches a first desired altitude is done in response to the altitude sensor indicating that the balloon system is at a desired altitude.

18. The method of claim 17 wherein, as a result of extending the telescoping support structure when the balloon system reaches a first desired altitude, a payload carried by the balloon system moves away from the balloon envelope.

Assignments (5)
MERGER Recorded Oct 19, 2022
From: AEROSTAR INTERNATIONAL, INC.
To: AEROSTAR INTERNATIONAL, LLC
Reel/Frame 061727/0886 →
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 Jun 3, 2020
From: CROMIE, JOHN
To: X DEVELOPMENT LLC
Reel/Frame 052824/0619 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 3, 2020
From: X DEVELOPMENT LLC
To: LOON LLC
Reel/Frame 052827/0889 →
Continuity (2)
Continuation 15843116 · Dec 15, 2017
Related Publication 20200331580A1 · Oct 22, 2020