IP Library Granted Patent US 9,174,738
Granted Patent B1
US 9,174,738 · App. 13/862,434 · Granted Nov 3, 2015

Drag disk, small

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Quick Facts
Patent No.
US 9,174,738
App. No.
13/862,434
Granted
Nov 3, 2015
Kind
B1
Abstract

A payload drag structure having a drag disk comprised of a lightweight, flexible material, a tubular section positioned around a periphery of the drag disk, a flexible member positioned within the tubular section, a cross member having a plurality of aims attached about the periphery of the drag disk, wherein one or more arms of the cross member are adapted for attachment to a payload harness, wherein the payload harness is adapted for attachment to arms of the cross member, and wherein a payload may be secured within the payload harness.

Claims (51)

1. A payload drag structure comprising:

a drag disk comprised of a flexible material;

a tubular section positioned around a periphery of the drag disk;

a flexible member positioned within the tubular section;

a payload harness positioned beneath the drag disk;

a cross member having a plurality of arms attached about the periphery of the drag disk and extending inwardly in a single plane, wherein one or more of the arms of the cross member are adapted for attachment to the payload harness;

wherein the payload harness is adapted for attachment to arms of the cross member and is capable of securing a payload.

2. The payload drag structure of claim 1 , wherein the cross member has four arms connected to a centrally positioned member of the drag disk.

3. The payload drag structure of claim 2 , wherein the four arms of the cross member are attached at equidistant points about the periphery of the drag disk.

4. The payload drag structure of claim 1 , wherein the arms of the cross member are attached to a ring that is located at or near a center of the drag disk.

5. The payload drag structure of claim 1 , wherein the arms of the cross member are comprised of a flexible webbing material.

6. The payload drag structure of claim 1 , wherein the arms of the cross member are sewn into the drag disk.

7. The payload drag structure of claim 1 , wherein one or more arms of the cross member have an end with a loop to provide an attachment point on the drag disk.

8. The payload drag structure of claim 1 , wherein a plurality of holes are positioned in the drag disk.

9. The payload drag structure of claim 8 , wherein the plurality of holes are circular holes having a diameter of three inches.

10. The payload drag structure of claim 8 , wherein there are eight circular holes in the drag disk.

11. The payload drag structure of claim 1 , wherein the drag disk is comprised of ripstop nylon.

12. The payload drag structure of claim 5 , wherein the arms of the cross member are comprised of nylon webbing material.

13. The payload drag structure of claim 8 , wherein at least one of the plurality of holes is located near the center of the drag disk to allow for wiring to extend through the drag disk.

14. The payload drag structure of claim 1 , wherein the flexible member is comprised of carbon fiber or fiberglass.

15. The payload drag structure of claim 14 , wherein the flexible member has a height of about 1 inch and a width from about ⅛ inch to about ¼ inch.

16. The payload drag structure of claim 1 , wherein the tubular section extends continuously around the periphery of the drag disk.

17. The payload drag structure of claim 1 , wherein an upper portion of the payload harness has four downwardly extending members beneath the drag disk.

18. The payload drag structure of claim 1 , wherein an upper portion of the payload harness is attached to the arms of the cross member.

19. The payload drag structure of claim 1 , wherein an upper portion of the payload harness is comprised of nylon webbing.

20. The payload drag structure of claim 1 , wherein the drag disk has a diameter of about 32 inches to about 64 inches.

21. The payload drag structure of claim 1 , wherein an upper portion of the payload harness is attached directly to the one or more arms of the cross member.

22. The payload drag structure of claim 1 , wherein a lower portion of the payload harness is attached to an upper portion of the payload harness, and the payload is secured between the upper portion of the payload harness and the lower portion of the payload harness.

23. The payload drag structure of claim 19 , wherein the upper portion of the payload harness is integrally formed with the arms of the cross member.

24. The payload drag structure of claim 1 , wherein an upper portion of the payload harness is attached to a lower portion of the payload harness using cam buckles.

25. The payload drag structure of claim 1 , wherein a lower portion of the payload harness is comprised of a plurality of members that are each attached to a ring or square member positioned beneath the drag disk.

26. A balloon, comprising:

a balloon envelope;

a payload drag structure positioned beneath the balloon envelope, the payload drag structure comprising:

a drag disk comprised of a lightweight, flexible material;

a tubular section positioned around a periphery of the drag disk;

a flexible member positioned within the tubular section;

a cross member having a plurality of arms attached about the periphery of the drag disk and extending inwardly in a single plane;

a payload harness extending below the drag disk;

wherein the payload harness is adapted to secure a payload;

a control system configured to initiate a process to cause the balloon envelope to no longer provide lift to the payload; and

wherein the payload drag structure serves to slow the descent of the payload to the earth.

27. The balloon of claim 26 , wherein the balloon envelope is attached to the drag disk or the payload.

28. The balloon of claim 26 , wherein the plurality of arms of the cross member are sewn into the drag disk.

29. The balloon of claim 26 , wherein a plurality of holes are positioned in the drag disk.

30. The balloon of claim 26 , wherein the drag disk is made of ripstop nylon and at least some of the plurality of arms are comprised of a flexible webbing material.

31. The balloon of claim 26 , wherein the flexible member is comprised of carbon fiber or fiberglass.

32. The balloon of claim 31 , wherein the flexible member has a height of about 1 inch and a width from about ⅛ inch to about ¼ inch.

33. The balloon of claim 26 , wherein the tubular section extends continuously around the periphery of the drag disk.

34. The balloon of claim 26 , wherein the payload harness is comprised of an upper portion that is attached to a lower portion.

35. The balloon of claim 26 , wherein the payload harness is comprised of a flexible webbing material.

Assignments (7)
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 →
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 May 29, 2013
From: ROACH, KEVIN; DEVAUL, RICHARD WAYNE; CLARIN, PHILLIP
To: GOOGLE INC.
Reel/Frame 030502/0382 →