Transformable and in-orbit manufacturable space debris collector

Patent metadata

Field	Value
Publication number	US-12415623-B2
Application number	US-202418588418-A
Country	US
Kind code	B2
Filing date	Feb 27, 2024
Priority date	Feb 28, 2023
Publication date	Sep 16, 2025
Grant date	Sep 16, 2025

Abstract

A material collection system includes a planar structure, at least one actuator, and a plurality of pull cables. The planar structure includes a plurality of interconnected geometric panels having a plurality of holes therethrough, and each interconnection between two geometric panels defines a foldable coupling. The plurality of pull cables pass through the holes such that a first end of each pull cable is coupled with at least one geometric panel and a second end of each pull cable is coupled with the at least one actuator. The planar structure is operable between a first stable geometric state and a second stable geometric state. An actuation to pull each of the plurality of pull cables transitions the planar structure between the first stable geometric state and the second stable geometric state.

First claim

We claim:

1. A material collection system operable in low gravity or zero gravity environments, comprising:
(a) a planar structure including a plurality of interconnected geometric panels, wherein each interconnection between two geometric panels defines a foldable coupling, wherein the planar structure defines a plurality of holes therethrough;
(b) at least one actuator; and
(c) a plurality of pull cables, wherein each pull cable of the plurality of pull cables passes through at least one hole of the plurality of holes, wherein a first end of each pull cable is coupled with at least one geometric panel and a second end of each pull cable is coupled with the at least one actuator;
wherein the planar structure is operable between a first stable geometric state and a second stable geometric state, wherein an actuation of the at least one actuator to pull each of the plurality of pull cables is operable to transition the planar structure between the first stable geometric state and the second stable geometric state.

2. The material collection system of claim 1 , wherein each geometric panel is formed of a first material and each foldable coupling is formed of a second material.

3. The material collection system of claim 2 , wherein the first material includes polylactic acid (PLA) and the second material includes thermoplastic polyurethane (TPU).

4. The material collection system of claim 2 , wherein the first material and the second material are joined together using one or more dovetail joints.

5. The material collection system of claim 1 , wherein the planar structure forms a conical Kresling pattern.

6. The material collection system of claim 1 , wherein the at least one actuator includes a plurality of servo motors.

7. The material collection system of claim 6 , wherein an amount of the plurality of servo motors equals an amount of the plurality of pull cables.

8. The material collection system of claim 1 , wherein each of the plurality of pull cables applies an equal amount of torque during the transition between the first stable geometric state and the second stable geometric state.

9. The material collection system of claim 1 , wherein each of the plurality of pull cables is configured to pull in a linear path during the transition between the first stable geometric state and the second stable geometric state.

10. A material collection system, comprising:
(a) a planar structure including a plurality of interconnected geometric panels shaped to fold into a conical Kresling pattern, wherein each interconnection between two geometric panels defines a foldable coupling, wherein the planar structure defines a plurality of holes therethrough;
(b) a plurality of pull cables, wherein each pull cable of the plurality of pull cables passes through at least one hole of the plurality of holes, wherein a first end of each pull cable is coupled with at least one geometric panel;
wherein the planar structure is operable between a first stable geometric state of the conical Kresling pattern and a second stable geometric state of the conical Kresling pattern, wherein an actuation to pull each of the plurality of pull cables is configured to transition the planar structure between the first stable geometric state of the conical Kresling pattern and the second stable geometric state of the conical Kresling pattern.

11. The material collection system of claim 10 , wherein each geometric panel is formed of a first material and each foldable coupling is formed of a second material.

12. The material collection system of claim 11 , wherein the first material includes polylactic acid (PLA) and the second material includes thermoplastic polyurethane (TPU).

13. The material collection system of claim 11 , wherein the first material and the second material are joined together using one or more dovetail joints.

14. The material collection system of claim 1 , wherein each of the plurality of pull cables is configured to pull in a linear path during the transition between the first stable geometric state and the second stable geometric state.

15. A method of configuring a debris collection system, wherein the debris collection system includes a planar structure having a plurality of interconnected geometric panels, at least one actuator, and a plurality of pull cables, the method comprising:
(a) forming the planar structure having opposing ends, each interconnection between two geometric panels defining a foldable coupling, and the plurality of interconnected geometric panels having a plurality of holes formed therethrough;
(b) coupling together the opposing ends of the planar structure;
(c) inserting a respective one of the plurality of pull cables through each of the plurality of holes formed through the planar structure; and
(d) attaching a first end of each respective pull cable to at least one geometric panel of the plurality of interconnected geometric panels and a second end of each respective pull cable to the at least one actuator.

16. The method of claim 15 , comprising:
prior to forming the planar structure, calculating a panel geometry for each of the plurality of interconnected geometric panels, and calculating a plurality of hole locations for each of the plurality of holes.

17. The method of claim 15 , comprising:
wherein forming the planar structure includes activating a dual-extrusion 3-dimensional printer.

18. The method of claim 15 , wherein each geometric panel is formed of a first material, wherein each interconnection between two respective geometric panels is formed of a second material, the method comprising:
wherein forming each interconnection of the planar structure includes forming a dovetail joint between the first material and the second material.

19. The method of claim 15 , comprising:
upon attaching a first end of each respective pull cable to at least one geometric panel of the plurality of interconnected geometric panels and a second end of each respective pull cable to the at least one actuator, selectively activating the at least one actuator to therefore translate the planar structure from a first stable state to a second stable state.

20. The method of claim 15 , wherein forming the planar structure includes forming the plurality of interconnected geometric panels such that they are foldable into a conical Kresling shape.

Assignees

• Purdue Research Foundation

Inventors

• Dai Ran
• Tanaka Yuto
• Anibha Aditya Arjun

Classifications

• B64G1/2224 Primary

  about multiple axes · CPC title

• B64G99/00

  Subject matter not provided for in other groups of this subclass · CPC title

• B64G4/00

  Tools specially adapted for use in space · CPC title

• B64G1/1081 Primary

  for debris removal · CPC title