Heat transfer system having a flexible deployable condenser tube

• US 5,117,901 A
• Filed: 02/01/1991
• Issued: 06/02/1992
• Est. Priority Date: 02/01/1991
• Status: Expired due to Term

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Martin Marietta Corporation
• Inventors: Cullimore, Brent A.
• Primary Examiner(s): DAVIS JR, ALBERT
• Application Number:
  US07/649,603
• Time in Patent Office: 487 Days
• Field of Search: 165/41, 165/86, 165/46, 165/104.26, 165/104.27, 244/163
• US Class Current: 165/86
• CPC Class Codes: B64G 1/50 for temperature control
• CPC Class Codes: B64G 1/503 Radiator panels
• CPC Class Codes: F28D 15/0208 using moving tubes
• CPC Class Codes: F28D 15/043 forming loops, e.g. capillary pumped loops

Abstract

A two-phase capillary pumped loop heat transfer system adapted primarily for use on space vehicles, includes a wickless condenser tube which receives gaseous phase working fluid from the evaporator capillaries, rejects heat from the working fluid to a heat sink (e.g. outer space) and thereby converts the gaseous phase working fluid to its liquid phase, and returns the liquid phase working fluid to the evaporator to complete the thermal cycle. A portion of the condenser tube is supported by a rigid radiator structure external to the spacecraft. At least a portion of the condenser tube is deformable to permit the radiator structure to be deployed from a first predetermined position to a second predetermined position with respect to the spacecraft. The deformable segment of the condenser tube can be formed into a helical coil used as a spring to assist deployment of the radiator panel.

Claims

1. A closed-loop heat transfer system adapted to transfer heat from a heat source within a housing to an external heat sink by means of a working fluid having a liquid phase and a gaseous phase, said heat transfer system comprising:

an evaporator within said housing having a plurality of capillaries adapted to accept heat from said heat source, each of said capillaries having a first end and a second end, said first ends receiving a flow of said working fluid, with heat from said heat source causing said working fluid flowing through said capillaries to convert to said gaseous phase which exits through said second ends;

a radiator structure external to said housing;

a hinge permitting said radiator structure to rotate about a predetermined axis with respect to said housing; and

an elongated wickless condenser tube adapted to reject heat from said working fluid to said heat sink and thereby convert said gaseous phase working fluid to its liquid phase, said condenser tube having;

(a) a first end sealed in fluid communication with said evaporator, adapted to receive said gaseous phase working fluid exiting from said second ends of said capillaries;

(b) a radiator segment external to said housing, secured to said radiator structure;

(c) a first helically coiled segment between said first end and said radiator segment;

(d) a second end adapted to return said liquid phase working fluid to said first ends of said capillaries; and

(e) a second helically coiled segment between said radiator segment and said second end;

said first and second coiled segments being wound about said axis to permit said radiator structure to be deployed from a first predetermined position to a second predetermined position with respect to said housing by deformation of said coiled segments.

2. The heat transfer system of claim 1 wherein at least one of said coiled segments is pre-stressed to act as a spring for deployment of said radiator structure from said first position to said second position.

3. The heat transfer system of claim 2 further comprising actuating means adapted to trigger deployment of said condenser tube from said first position to said second position.

4. The heat transfer system of claim 1 further comprising a pump adapted to boost the flow of said working fluid from said second end of said condenser tube to said first ends of said evaporator capillaries.

5. The heat transfer system of claim 1 further comprising a reservoir adapted to contain a quantity of said liquid phase working fluid returned by said second end of said condenser tube.

6. The heat transfer system of claim 1 further comprising a gas trap adapted to prevent working fluid vapor and noncondensible gases from entering said inlets of said evaporator capillaries.

7. The heat transfer system of claim 1 wherein said radiator structure comprises a plurality of substructures capable of relative motion with respect to one another as said radiator structure is deployed from said first predetermined position to said second predetermined position.