Flexible heat transport design for development applications

• US 5,787,969 A
• Filed: 12/22/1995
• Issued: 08/04/1998
• Est. Priority Date: 12/22/1995
• Status: Expired due to Term

• Current Assignee: Hughes Electronics Corporation (Rtx Corporation)
• Original Assignee: Hughes Electronics Corporation (Rtx Corporation)
• Inventors: Drolen, Bruce L., Ito, Calvin H., Esposto, David B., Fleischman, George L.
• Primary Examiner(s): Ford, John K.
• Application Number:
  US08/577,435
• Time in Patent Office: 956 Days
• Field of Search: 165/41, 165/86, 165/77, 165/104.26, 165/104.27, 244/163, 244/158 R, 244/173, 137/340
• US Class Current: 165/41
• CPC Class Codes: B64G 1/50 for temperature control
• CPC Class Codes: B64G 1/641 Interstage or payload connectors docking systems B64G1/646
• CPC Class Codes: B64G 1/645 Separators
• CPC Class Codes: E05D 1/02 made of one piece
• CPC Class Codes: F28D 15/0266 with separate evaporating and condensing chambers connected by at least one conduit; Loop-type heat pipes; with multiple or common evaporating or condensing chambers F28D15/043 takes precedence

Abstract

A closed-loop heat pipe transport design for a deployment application having a flexible section which connects to a payload structure and a deployable structure. The flexible section is a coil which is offset from the axis of rotation of the deployable structure. Upon rotation of the deployable structure around a predetermined axis, the flexible coil decompresses and sweeps in an arcuate fashion with a portion of said flexible coil aligning with the axis. When the deployable structure has completed its rotation and is fully deployed, the flexible coil will rest in substantially the same plane as it did before sweeping.

Claims

1. A payload structure for a deployment application, comprising:

a deployable structure external to said payload structure;

a hinge permitting said deployable structure to rotate about a predetermined axis with respect to said payload structure; and

at least one flex coil having concentric coils, connected on one end to said payload structure and on the other end to said deployable structure, said at least one flex coil being both offset from said hinge axis and between said payload structure and said deployable structure, and said concentric coils being non-concentric after said deployable structure is deployed.

2. The payload structure for a deployment application of claim 1, wherein a portion of said at least one flex coil aligns with said axis after said deployable structure rotates.

3. The payload structure for a deployment application of claim 1, wherein said at least one flex coil completes an arcuate sweep in a plane substantially the same as a plane on which said at least one flex coil rested before said deployable structure rotated.

4. The payload structure for a deployment application of claim 1, wherein said at least one flex coil is made of a flexible material.

5. The payload structure for a deployment application of claim 1, wherein said at least one flex coil is made of a flexible metal.

6. The payload structure for a deployment application of claim 1, wherein said deployable structure is a radiator.

7. A method of deploying a deployable structure from a payload structure, comprising the steps of:

connecting said deployable structure by a hinge having a fixed axis to said payload structure;

attaching at least one flex coil having concentric coils to said deployable structure and to said payload structure, said flex coil being offset from said fixed axis;

securing said deployable structure to said payload structure with a lock;

unsecuring said lock after launching said deployable structure;

rotating said deployable structure around said fixed axis; and

sweeping said flex coil in an arcuate fashion, such that said flex coil sweeps in a plane which is substantially the same as a plane said flex coil rested on before said rotation of said deployable structure, and said concentric coils being non-concentric after said deployable structure is deployed.

8. The method of deploying a deployable structure from a payload structure of claim 8 wherein a portion of said at least one flex coil aligns with said fixed axis after said deployable structure rotates.

9. The method of deploying a deployable structure from a payload structure of claim 8 wherein said deployable structure is a radiator.