IP Library Granted Patent US 11,142,350
Granted Patent B2
US 11,142,350 · App. 16/662,989 · Granted Oct 12, 2021

Compact scalable drag sail deployment assembly

Inventors: David Allen Spencer (West Lafayette, IN); Anthony George Cofer (Lafayette, IN)
Assignee: Purdue Research Foundation
B64G1/62B64G1/222
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Quick Facts
Patent No.
US 11,142,350
App. No.
16/662,989
Granted
Oct 12, 2021
Kind
B2
Abstract

A drag sail deployment assembly has an enclosure supporting four boom deployment assemblies and four retractable booms. Each boom deployment assembly includes a hub and motor. The hub is configured to hold a wound boom and to rotatably pay out the wound boom. The motor is disposed at least in part within an interior of the hub, and rotates the hub. Each boom is associated with a corresponding one of the four boom deployment assemblies. Each boom includes a plurality of spring elements disposed within a sleeve. Each boom is wound onto the hub of the corresponding boom deployment assembly in a first configuration wherein the spring elements are compressed toward each other. Each boom is configured to expand into a second configuration wherein central portions of the spring elements are spaced apart from each other when the boom is unwound from the hub of the corresponding boom deployment assembly.

Claims (26)

1. A drag sail deployment assembly, comprising:

an enclosure having first, second, third and fourth boom deployment assemblies, each boom deployment assembly having, a hub configured to hold a wound boom and to rotatably pay out the wound boom, the hub having a hollow interior;

a motor disposed at least in part within the hollow interior, the motor operably coupled to rotate the hub;

first, second, third and fourth retractable booms, each of the first, second, third and fourth retractable booms associated with a corresponding one of the first, second, third and fourth boom deployment assemblies, each boom comprising a plurality of spring elements disposed within a sleeve, each boom wound onto the hub of the corresponding boom deployment assembly in a first configuration wherein the spring elements are compressed toward each other, and each boom configured to expand into a second configuration wherein central portions of the spring elements are spaced apart from each other when the boom is unwound from the hub of the corresponding boom deployment assembly; and

wherein the first boom deployment assembly further comprises a hinged plate pivotally affixed to the hub, the hinged plate further secured to an end of the first retractable boom.

2. The drag sail deployment assembly of claim 1 , wherein the hinged plate is configured to cause the end of the first retractable boom to extend out in a predetermined direction with respect to the enclosure.

3. The drag sail deployment assembly of claim 2 , wherein at least one roller of the first boom deployment assembly stops the rotational movement of the hinged plate.

4. The drag sail deployment assembly of claim 1 , wherein the hinged plate has distal end having a first position and a second position, wherein in the first position the distal end engages a part of a hub surface around which the boom is wound, and wherein in the second position the distal end is spaced apart from the part of the hub surface around which the boom is wound.

5. The drag sail deployment assembly of claim 4 , wherein the hub includes a hollow tubular member having an opening, and wherein the hinged plate covers the opening in the first position.

6. The drag sail deployment assembly of claim 1 , wherein the first boom deployment assembly includes a boom guide in the form of a portion of a cylinder having a void through which the boom extends, the portion of the cylinder surrounding a majority of a circumference of the hub.

7. The drag sail deployment assembly of claim 6 , wherein the void extends less than one third of the circumferential distance of the portion of the cylinder.

8. The drag sail deployment assembly of claim 1 , further comprising a motor drive circuit configured including a controller and four drive circuits, each drive circuit operably coupled to provide drive signals to the motor of a corresponding boom deployment assembly.

9. The drag sail deployment assembly of claim 8 , further comprising a reduction gear set configured to provide at least 100 to 1 gear reduction.

10. The drag sail deployment assembly of claim 1 , further comprising a first arm rotatably attached to a frame, the first arm operably coupled to at least one roller, and wherein the arm is spring-based to rotate toward the hub, the at least one roller configured to engage the boom.

11. The drag sail deployment assembly of claim 10 , wherein the first arm is operably coupled to the at least one roller via a rocker hand.

12. A drag sail assembly, comprising:

an enclosure having first, second, third and fourth boom deployment assemblies, each boom deployment assembly having,

a hub configured to hold a wound boom and to rotatably pay out the wound boom, the hub having a hollow interior;

a motor disposed at least in part within the hollow interior, the motor operably coupled to rotate the hub;

first, second, third and fourth retractable booms, each of the first, second, third and fourth retractable booms associated with a corresponding one of the first, second, third and fourth boom deployment assemblies, each boom comprising a plurality of spring elements disposed within a sleeve, each boom wound onto the hub of the corresponding boom deployment assembly in a first configuration wherein the spring elements are compressed toward each other, and each boom configured to expand into a second configuration wherein central portions of the spring elements are spaced apart from each other when the boom is unwound from the hub of the corresponding boom deployment assembly; and

first, second, third and fourth sail segments coupled to respective pairs of the first, second, third and fourth retractable booms;

wherein the first boom deployment assembly further comprises a hinged plate rotatably affixed to the hub, the hinged plate further secured to an end of the first retractable boom.

13. The drag sail deployment assembly of claim 12 , wherein the hinged plate is configured to cause the end of the first retractable boom to extend out in a predetermined direction with respect to the enclosure.

14. The drag sail deployment assembly of claim 13 , wherein the first boom deployment assembly includes a boom guide in the form of a portion of a cylinder having a void through which the boom extends, the portion of the cylinder surrounding a majority of a circumference of the hub.

15. The drag sail deployment assembly of claim 12 , wherein the first boom deployment assembly includes a boom guide in the form of a portion of a cylinder having a void through which the boom extends, the portion of the cylinder surrounding a majority of a circumference of the hub.

16. The drag sail deployment assembly of claim 15 , wherein the void extends less than one third of the circumferential distance of the portion of the cylinder.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 29, 2021
From: COFER, ANTHONY GEORGE; SPENCER, DAVID ALLEN
To: PURDUE RESEARCH FOUNDATION
Reel/Frame 057643/0343 →
Continuity (2)
Provisional Application 62749786 · Oct 24, 2018
Related Publication 20200130872A1 · Apr 30, 2020