Two-phase thermal control system with a spherical wicked reservoir

• US 4,957,157 A
• Filed: 04/13/1989
• Issued: 09/18/1990
• Est. Priority Date: 04/13/1989
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: General Electric Company
• Inventors: Dowdy, Mack W., Benko, Doanld J.
• Primary Examiner(s): DAVIS JR, ALBERT
• Application Number:
  US07/337,774
• Time in Patent Office: 523 Days
• Field of Search: 165/104.27, 165/41, 244/163
• US Class Current: 165/104.27
• 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 15/043 forming loops, e.g. capillary pumped loops
• CPC Class Codes: F28F 2200/005 Testing heat pipes

Abstract

A closed-loop two-phase thermal control loop includes an evaporator which receives subcooled coolant liquid from a condenser and heat from a source, and vaporizes the coolant to form coolant vapor. A condenser which is coupled to a thermal radiator accepts the coolant vapor and radiates thermally to space, thereby condensing the coolant vapor to liquid and subcooling the liquid. As the temperature of the environment surrounding the condenser radiator changes, the mass of vapor within the system tends to change, thereby causing undesirable pressure changes. A spherical wicked coolant reservoir is coupled to the liquid side of the closed thermal control loop. The reservoir is exposed foro thermal radiation and electrically heated, so that the temperature is thereby controlled in order to control vapor pressure within the reservoir. By controlling the reservoir vapor pressure, small pressure differentials are generated, which cause coolant liquid to be accepted or expelled while maintaining the closed loop pressure. The reservoir includes a wick for maintaining liquid coolant adjacent heat transfer areas, and also includes a standpipe supporting shaped vanes. The coolant adheres to the vanes and to the wick under zero-gravity conditions in a manner which allows at least partial simulation in an Earth gravity.

Claims

1. A capillary-pumped thermal control system for pumping fluid coolant around a closed loop, said system being usable in microgravity and also being capable of being tested in a gravity environment, comprising:

an evaporator for absorbing heat and using the absorbed heat to vaporize said coolant to produce coolant vapor near a preselected pressure,

at least one condenser coupled to said evaporator for receiving said coolant vapor, said condenser including a heat rejecting radiator for absorbing heat from said coolant vapor and for transferring said heat to the surroundings by thermal radiation to cause said coolant vapor to revert to liquid form, whereby when said condenser is exposed to a relatively warm environment, the ratio of the volume of liquid coolant to coolant vapor in said condenser is relatively small, and when said condenser is exposed to a relatively cold environment, said ratio is larger, which tends to change the amount of liquid in said closed loop and thereby change said preselected pressure;

a liquid path for coupling said liquid coolant to said evaporator;

a closed spherical reservoir coupled by a pipe to said liquid path of said closed loop, said spherical reservoir including a wall defining a first hemisphere which in a Earth gravity environment is the upper hemisphere and also defining a second hemisphere opposite said first hemisphere, at least a portion of the exterior of said wall of said upper hemisphere being thermally exposed to allow thermal radiation and at least a portion of said wall of said upper hemisphere being coupled to controllable heaters, the interior surface of said wall being in thermal contact with a thin wick at least in the vicinity of those regions of said wall which are exposed for thermal radiation and in those regions to which said heaters are coupled, said pipe opening into said wall of said reservoir at the center of said lower hemisphere, and communicating with a standpipe, which standpipe extends from said wall at said pipe opening in a radial inward direction about to the center of said spherical reservoir to thereby define a principal axis of said reservoir, said spherical reservoir further including a plurality of fins extending along and supported by said standpipe, said fins being made from a material which is wetted by said coolant, each of said fins extending away from said axis defined by said standpipe.

2. A system according to claim 1 wherein said coolant is ammonia.

3. A system according to claim 1 wherein said fins are essentially planar.

4. A system according to claim 3 wherein each of said fins defines a curved free edge which is not in contact with any solid structure.

5. A system according to claim 1 wherein at least a portion of each of said fins lies in that portion of the spherical volume of said reservoir which lies within said lower hemisphere.

6. A system according to claim 1 wherein said standpipe comprises:

a pipe-like support structure defining a bore and a plurality of fenestrations; and

a hollow, cylindrical wick defining an inner bore and having an outer diameter substantially equal to the inner diameter of said bore of said pipe-like support structure, said hollow, cylindrical wick extending through said bore of at least that portion of said pipe-like support structure defining said plurality of fenestrations.

7. A system according to claim 6 further comprising:

a wicked plug completely filling one of the bore of said pipe and said bore of said pipe-like support structure near the region in which said standpipe communicates with said pipe.

8. A system according to claim 7 wherein one end of said hollow, cylindrical wick is in contact with said wicked plug.

9. A system according to claim 6 further comprising a flat, elongated, wick defining first and second elongated sides and first and second ends, said flat, elongated, wick extending through said inner bore defined within said hollow, cylindrical wick, with said elongated sides in contact with the interior of said hollow, cylindrical wick.

10. A system according to claim 9 further comprising:

a wicked plug completely filling the bore of one of said pipe and said pipe-like support structure near the region in which said standpipe communicates with said pipe; and

wherein

said first end of said flat, elongated, rectangular wick has said first end in contact with said wicked plug.

11. A system according to claim 1 further comprising at least one elongated feed wick located in part adjacent to said wall in said lower hemisphere and also extending at least to said thin wick for allowing the flow of coolant in said liquid state between said lower hemisphere to said thin wick.

12. A system according to claim 1 wherein said evaporator is a wicked evaporator incorporating pumping capacity without the need for a moving pump.

13. A system according to claim 1 wherein said fins are planar, and are equally spaced about said standpipe and each supported along one edge by said standpipe, and wherein said fins extend radially away from said standpipe.

14. A system according to claim 1 wherein said wall of said spherical reservoir is mechanically and thermally coupled to a panel which extends orthogonal to said principal axis of said spherical reservoir at a location spaced away from said first hemisphere.

15. A system according to claim 6 further comprising at least one elongated feed channel defined between first and second elongated wicks, said feed channel defining first and second elongated flat sides and first and second ends, said feed channel extending about said interior of said spherical reservoir with said first elongated flat side of said elongated feed channel substantially in contact with said thin wick in those regions of said interior over which said thin wick extends and substantially in contact with said wall of said spherical reservoir in those regions of said interior over which said thin wick does not extend.

16. A system according to claim 15 wherein said first and second ends of said elongated feed channel are located contiguous with the juncture of said standpipe and said wall of said spherical reservoir.

17. A closed spherical reservoir adapted to be coupled by a pipe to a liquid coolant path of a thermal control loop, said spherical reservoir including a wall defining a first hemisphere which in a Earth gravity environment is the upper hemisphere and also defining a second hemisphere opposite said first hemisphere, at least a portion of the exterior of said wall of said upper hemisphere being thermally exposed to allow thermal radiation and at least a portion of said wall of said upper hemisphere being coupled to controllable heaters, the interior surface of said wall being in thermal contact with a thin wick at least in the vicinity of those regions of said wall which are exposed for thermal radiation and in those regions to which said heaters are coupled, said pipe opening into said wall of said reservoir at the center of said lower hemisphere, and communicating with a standpipe, which standpipe extends from said wall at said pipe opening in a radial inward direction about to the center of said spherical reservoir to thereby define a principal axis of said reservoir, said spherical reservoir further including a plurality of fins extending along and supported by said standpipe, said fins being made from a material which is wetted by said coolant, each of said fins extending away from said axis defined by said standpipe.