Thermal control canister

• US 4,162,701 A
• Filed: 11/21/1977
• Issued: 07/31/1979
• Est. Priority Date: 11/21/1977
• Status: Expired due to Term

• Current Assignee: United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration
• Original Assignee: United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration
• Inventors: Ollendorf, Stanford
• Primary Examiner(s): Myhre, Charles J.
• Assistant Examiner(s): Miller, Carl S.
• Application Number:
  US05/853,677
• Time in Patent Office: 617 Days
• Field of Search: 165/32, 165/105, 244/1 R, 244/163
• US Class Current: 165/273
• CPC Class Codes: B64G 1/50 for temperature control
• CPC Class Codes: B64G 1/503 Radiator panels
• CPC Class Codes: B64G 1/506 Heat pipes
• CPC Class Codes: F28D 15/0275 Arrangements for coupling heat-pipes together or with other structures, e.g. with base blocks; Heat pipe cores
• CPC Class Codes: F28D 15/06 Control arrangements therefor
• CPC Class Codes: G05D 23/192 using a modification of the thermal impedance between a source and the load
• CPC Class Codes: G05D 23/24 the sensing element having a resistance varying with temperature, e.g. a thermistor

Abstract

A heat dissipating instrument package of a spacecraft, located in a canister having walls in heat transfer relationship with the package, is maintained at a substantially constant temperature. Fixed conductance heat pipes on the canister walls are connected to variable conductance heat pipes, mounted on a radiator structure separated from the canister walls by a thermal blanket. The effective radiating area of the radiator structure is controlled by the variable conductance heat pipes in response to a comparison of a sensed temperature of the instrument package or the canister wall with a seat point value. The comparison controls a heater in a gas reservoir containing a non-condensable gas of the variable conductance heat pipe. To enable the set point to be varied over a relatively wide range, such a 0°-30° C., a thermal radiation shield for the gas reservoir prevents radiant energy from the exterior environment and thermal energy reflected from the spacecraft from overheating the non-condensable gas. In one embodiment, variable conductance heat pipe headers are provided between the canister and radiators, with isothermalizer feeder pipes on the radiators and canister walls; in further embodiments, variable conductance heat pipe feeder pipes are coupled directly between the canister walls and one or more radiators.

Claims

1. Apparatus for maintaining a heat dissipating load at a substantially constant temperature, comprising:

a canister having a plurality of walls in close thermal heat transfer relationship for holding said load therein in heat exchange relationship with at least one of said walls;

a plurality of transfer heat pipes at each end of said canister and in heat exchange relationship with the exterior of each of said walls, said transfer heat pipes having longitudinal axes extending transverse to the longitudinal axis of said canister and having ends thereof in heat exchange relationship with adjacent ends of said transfer heat pipes on adjacent walls;

a plurality of isothermalizer heat pipes extending between said transfer heat pipes at each end of said canister and in heat exchange relationship with the exterior of said walls and said transfer heat pipes, said isothermalizer heat pipes having longitudinal axes extending parallel to the longitudinal axis of said canister;

a thermal insulator surrounding the exterior of said walls, said transfer heat pipes and said isothermalizer heat pipes;

a thermal radiator covering at least one portion of the exterior surface of said thermal insulator;

a plurality of heat pipes embedded within said thermal radiator having longitudinal axes extending parallel to the longitudinal axis of said canister; and

at least one feedback variable conductance heat pipe in heat exchange relationship with an end of said heat pipes and having a longitudinal axis transverse to the longitudinal axis of said canister, said feedback variable conductance heat pipe having one end extending inwardly through said thermal insulator and in heat exchange relationship with at least one of said transfer heat pipes at one of said ends of said canister, said variable conductance heat pipe including a reservoir having a noncondensible fluid therein that expands and contracts as a function of temperature for controlling the number of said heat pipes in heat exchange relationship with said feedback variable conductance heat pipe.

2. The apparatus of claim 1, wherein said walls of said canister are formed of a high thermal conductivity material.

3. The apparatus of claim 2 wherein said walls are aluminum.

4. The apparatus of claim 1 wherein said thermal insulator includes multiple layers of aluminized material.

5. The apparatus of claim 1 wherein said reservoir includes a radiation reflector to reflect radiation impinging on said reservoir, said radiation reflector causing said reservoir to have a variable set point temperature.

6. The apparatus of claim 5 wherein said set point temperature is variable over a range of 0 degrees celsius to 30 degrees celsius.

7. The apparatus of claim 6 wherein said reflector includes a pair of aluminum plates connected to said reservoir and in alignment with said radiation.

8. The apparatus of claim 6 wherein said reflector includes:

a reflective coating on the exterior surface of said reservoir for reflecting said radiation; and

an insulator surrounding a portion of said reservoir for reflecting said radiation.

9. The apparatus of claim 1 further including:

a heater within said reservoir for heating said noncondensible fluid;

a temperature sensor for sensing the temperature of said heat dissipating load;

controller means coupling said heater and said temperature sensor, said controller means being responsive to a temperature change by said temperature sensor for changing the current to said heater to selectively heat or cool said noncondensible fluid, said noncondensible fluid expanding or contracting in response to said changing current for effectively varying the number of said heat pipes in heat exchange relationship with said feedback variable conductive heat pipe.