EXTRAPLANETARY HEAT EXCHANGER

Abstract

An extraplanetary habitat system includes a habitat located on a site including a layer of regolith material and one or more heat-generating systems located in the habitat. A heat exchanger is operably connected to the habitat. The heat exchanger is located beneath the layer of regolith material and is configured to conduct the heat from the habitat into the layer of regolith material. A method of cooling one or more heat generating components of an extraplanetary habitat includes directing a flow of fluid from the habitat to a heat exchanger located beneath a layer of regolith material, exchanging thermal energy between the flow of fluid and the regolith material, thereby cooling the volume of fluid, and directing the flow of fluid from the heat exchanger to the habitat, thus cooling the habitat.

Claims

1. An extraplanetary habitat system, comprising: a habitat disposed on a site comprising a layer of regolith material; one or more heat-generating systems disposed in the habitat; a heat exchanger operably connected to the one or more heat-generating systems, the heat exchanger disposed beneath the layer of regolith material and configured to conduct the heat from the habitat into the layer of regolith material.

2. The extraplanetary habitat system of claim 1, further comprising: an input pathway connecting the habitat to the heat exchanger, to direct a flow of fluid from the habitat to the heat exchanger; and an output pathway connecting the habitat to the heat exchanger, the flow of fluid cooled by the heat exchanger to the habitat.

3. The extraplanetary habitat system of claim 2, wherein the flow of fluid is one of air, water or refrigerant.

4. The extraplanetary habitat system of claim 2, further comprising one of a pump or a fan operably connected to one or more of the input pathway or the output pathway to urge the flow of fluid therethrough.

5. The extraplanetary habitat system of claim 2, wherein the heat exchanger includes a heat exchanger pathway through which the flow of fluid is directed to exchanger thermal energy with the regolith material.

6. The extraplanetary habitat system of claim 5, wherein the heat exchanger pathway is multi-pass.

7. The extraplanetary habitat system of claim 5, further comprising a plurality of fins extending from the heat exchanger pathway.

8. The extraplanetary habitat system of claim 1, wherein the heat exchanger is disposed at a depth of between 1 and 3 feet below a top surface of the regolith material.

9. The extraplanetary habitation system of claim 1, wherein the one or more heat generating systems includes an environmental control and life support system or a thermal control system.

10. A method of cooling one or more heat generating components of an extraplanetary habitat, comprising: directing a flow of fluid from the habitat to a heat exchanger located beneath a layer of regolith material; exchanging thermal energy between the flow of fluid and the regolith material, thereby cooling the volume of fluid; and directing the flow of fluid from the heat exchanger to the habitat, thus cooling the habitat.

11. The method of claim 10, comprising: flowing the flow of fluid from the habitat to the heat exchanger along an input pathway connecting the habitat to the heat exchanger; and flowing the flow of fluid from the heat exchanger to the habitat along an output pathway connecting the habitat to the heat exchanger.

12. The method of claim 11, wherein the flow of fluid is one of air, water or refrigerant.

13. The method of claim 11, further directing the fluid via one of a pump or a fan operably connected to one or more of the input pathway or the output pathway.

14. The method of claim 11, wherein the heat exchanger includes a heat exchanger pathway through which the flow of fluid is directed to exchanger thermal energy with the regolith material.

15. The method of claim 14, wherein the heat exchanger pathway is multipass.

16. The method of claim 14, further comprising a plurality of fins extending from the heat exchanger pathway.

17. The method of claim 10, wherein the heat exchanger is disposed at a depth of between 1 and 3 feet below a top surface of the regolith material.

18. The method of claim 10, wherein the one or more heat generating components includes an environmental control and life support system or a thermal control system.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0021] The following descriptions should not be considered limiting in any way. With reference to the accompanying drawings, like elements are numbered alike:

[0022] FIG. 1 is a schematic view of an embodiment of an extraplanetary habitat having a heat exchanger;

[0023] FIG. 2 is a plan view of an embodiment of a heat exchanger;

[0024] FIG. 3 is a plan view of another embodiment of a heat exchanger;

[0025] FIG. 4 is another plan view of an embodiment of a heat exchanger;

[0026] FIG. 5 is yet another plan view of an embodiment of a heat exchanger; and

[0027] FIG. 6 is a schematic view of yet another embodiment of a heat exchanger; and

[0028] FIG. 7 is a schematic view of another embodiment of an extraplanetary habitat having a heat exchanger.

DETAILED DESCRIPTION

[0029] A detailed description of one or more embodiments of the disclosed apparatus and method are presented herein by way of exemplification and not limitation with reference to the Figures.

[0030] Referring now to FIG. 1, illustrated is a schematic view of an extraplanetary habitat 10. The habitat 10 is located over a site 12 comprising a layer of regolith material 14. The site 12 is, for example, an extraterrestrial location, such as a moon, an asteroid or another planet. The habitat 10 includes one or more devices that generate heat and which are desired to be cooled. For example, the habitat 10 may include an environmental control and life support system (ECLSS) and/or a thermal control system or other components such as electronics or the like which generate heat through operation.

[0031] A heat exchanger 18 is connected to the habitat 10 to dissipate thermal energy from the habitat 10. The heat exchanger 18 is buried in the regolith material 14 and utilizes the thermal conductivity of the regolith material 14 to a working fluid circulated through the heat exchanger 18 in thermal energy dissipation. The regolith material 14 is especially useful in extraterrestrial environments such as the moon, as a gaseous atmosphere cannot be utilized there as a heat dissipator. The habitat 10 is connected to the heat exchanger 18 via an input pathway 20 and connected to the heat exchanger 18 at a heat exchanger inlet 22 and an output pathway 24 connected to the heat exchanger 18 at a heat exchanger outlet 26. The input pathway 20 and the output pathway 24 may be, for example, pipes, hoses or other conduits for conveying the working fluid between the heat exchanger 18 and the habitat 10.

[0032] In operation, relatively warm working fluid 28, for example, air, water, refrigerant, or other fluids is circulated from the habitat 10 to the heat exchanger 18 via the input pathway 20 and through the heat exchanger 18. At the heat exchanger, 18, thermal energy from the working fluid 28 is transferred to the regolith material 14 via conduction of the regolith material 14, thus cooling the working fluid 28. The cooled working fluid 28 is then returned to the habitat 10 via the output pathway 24. In some embodiments, a pump 44, or alternatively a fan, located, for example, along the input pathway 20 or the output pathway 24 is utilized to urge the working fluid 28 flow through the heat exchanger 18.

[0033] Referring now to FIG. 2, illustrated is an embodiment of a heat exchanger 18. In the embodiment illustrated, the heat exchanger 18 is a conduit 32 located in a trench 30 or hole formed in the regolith material 14, which, after installation of the heat exchanger 18, is refilled with regolith material 14. In the illustrated embodiment, the heat exchanger 18 is a single-pass heat exchanger 18. Alternatively, as illustrated in FIG. 3 the heat exchanger conduit 32 may have a multi-pass configuration. The heat exchanger conduit 32 is formed from a thermally conductive material such as copper or aluminum, which may need to be coated or alloyed to prevent galvanic corrosion, or plastic or composite materials. In another embodiment, shown in FIG. 4, the heat exchanger 18 has a spiral or coiled configuration. In some embodiments, the could configuration is formed by wrapping or winding of a flexible material, or in other embodiments by additive manufacturing or other suitable processes. Such materials may include, for example, a metal-impregnated polymer or the like.

[0034] As shown in FIGS. 5 and 6, in some embodiments, the heat exchanger 18 includes one or more fins 34 or other features extending from the heat exchanger conduit 32 to aid in conducting thermal energy from the working fluid 28 into the regolith material 14. In some embodiments, the fins 34 and the heat exchanger conduit 32 are formed from the same thermally conductive material as the conduit 32, while in other embodiments the fins 34 and the heat exchanger conduit 32 are formed from different materials.

[0035] The trench 30 is formed in the regolith material 14 at a depth 36 (shown in FIG. 1) to maximize thermal conductivity from the heat exchanger 18, while also minimizing the necessary depth for installation. In some embodiments (e.g. on the moon), the depth 36 is in the range of 1 to 3 feet.

[0036] Alternatively, in other embodiments, such as shown in FIG. 7 a trench 30 is not utilized. The heat exchanger 18 is placed on the surface of the site 12, and a mound 38 of regolith material 14 is formed around and over the heat exchanger 18. In some embodiments, the regolith material 14 around and atop the heat exchanger 18 has a thickness 40 in the range of 1 to 3 feet. The thickness 40 needed or utilized is temperature dependent, and other thicknesses may be utilized to achieve the desired thermal energy transfer. The shape of the mound 38 is not limited by the exemplary shape shown in FIG. 6.

[0037] Use of the regolith material 14 as a medium into which thermal energy generated by the ELCSS and/or other components of the habitat 10 is dissipated is effective and cost efficient, without requiring the use of more complex systems to reject the thermal energy.

[0038] The term “about” is intended to include the degree of error associated with measurement of the particular quantity based upon the equipment available at the time of filing the application.

[0039] The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the present disclosure. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, element components, and/or groups thereof.

[0040] While the present disclosure has been described with reference to an exemplary embodiment or embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the present disclosure. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the present disclosure without departing from the essential scope thereof. Therefore, it is intended that the present disclosure not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this present disclosure, but that the present disclosure will include all embodiments falling within the scope of the claims.