IPC분류정보
국가/구분 |
United States(US) Patent
등록
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국제특허분류(IPC7판) |
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출원번호 |
US-0778675
(2013-02-27)
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등록번호 |
US-9863725
(2018-01-09)
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발명자
/ 주소 |
- Dudis, Douglas S.
- Schmidt, Joel E.
- Miller, Douglas J.
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출원인 / 주소 |
- The United States of America as represented by the Secretary of the Air Force
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대리인 / 주소 |
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인용정보 |
피인용 횟수 :
0 인용 특허 :
23 |
초록
▼
Ammonium carbamate-based methods and systems for management of thermal loads, particularly low-quality, high-flux thermal loads. The increase in temperature in heat sensitive devices is mitigated by the endothermic decomposition of ammonium carbamate into carbon dioxide and ammonia gases. This proce
Ammonium carbamate-based methods and systems for management of thermal loads, particularly low-quality, high-flux thermal loads. The increase in temperature in heat sensitive devices is mitigated by the endothermic decomposition of ammonium carbamate into carbon dioxide and ammonia gases. This process has an energy density an order of magnitude greater than conventional thermal management materials and is particularly useful for temperatures between 20° C. and 100° C. Systems incorporating ammonium carbamate may be controlled by regulating the fluid flow, overhead pressure, temperature, or combinations thereof.
대표청구항
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1. An ammonium carbamate-based thermal management system comprising: a flow controller comprising a control unit, a coolant fluid for absorbing heat from a thermal load, a coolant fluid circulation pump, a flow valve, and at least one temperature sensor, wherein the coolant fluid circulation pump is
1. An ammonium carbamate-based thermal management system comprising: a flow controller comprising a control unit, a coolant fluid for absorbing heat from a thermal load, a coolant fluid circulation pump, a flow valve, and at least one temperature sensor, wherein the coolant fluid circulation pump is fluidly coupled to the thermal load, and wherein the flow controller is configured to regulate a flow of the coolant fluid from the thermal load;a primary heat exchanger coupled to the flow controller, wherein the primary heat exchanger comprises ammonium carbamate and a non-aqueous heat transfer fluid that is non-reactive with the ammonium carbamate, wherein the primary heat exchanger is configured to transfer heat from the coolant fluid to the heat transfer fluid and the ammonium carbamate, and wherein the ammonium carbamate endothermically decomposes into ammonia gas and carbon dioxide gas upon the transfer of heat from the coolant fluid;a vacuum source coupled to the primary heat exchanger, wherein the vacuum source is configured to provide the primary heat exchanger with a pressure lower than atmospheric pressure; anda pressure controller coupled to the primary heat exchanger and to the vacuum source, wherein the pressure controller is configured to maintain pressures lower than atmospheric pressure in the primary heat exchanger to remove the ammonia gas and the carbon dioxide gas from the primary heat exchanger, thereby regulating an overhead pressure within the ammonium carbamate-based thermal management system. 2. The ammonium carbamate-based thermal management system of claim 1 wherein the vacuum source comprises a vacuum pump and a valve. 3. The ammonium carbamate-based thermal management system of claim 1 further comprising at least one heating element between the primary heat exchanger and the vacuum source, wherein the heating element is configured to prevent the ammonia gas and the carbon dioxide gas from combining to reform ammonium carbamate prior to removal from the ammonium carbamate-based thermal management system. 4. The ammonium carbamate-based thermal management system of claim 1 further comprising a storage chamber. 5. The ammonium carbamate-based thermal management system of claim 4 wherein the storage chamber further comprises a reservoir liquid in which at least one of the ammonia gas and the carbon dioxide gas are soluble. 6. The ammonium carbamate-based thermal management system of claim 1 further comprising a redirection component, wherein the redirection component is configured to direct the ammonia gas or the carbon dioxide gas from the vacuum source to at least one secondary application. 7. The ammonium carbamate-based thermal management system of claim 1 further comprising a secondary heat exchanger coupled to the vacuum source, wherein the secondary heat exchanger is configured to exothermically combine the ammonia gas and the carbon dioxide gas to form regenerated ammonium carbamate, and wherein the regenerated ammonium carbamate is transferred back into the primary heat exchanger. 8. The ammonium carbamate-based thermal management system of claim 1 wherein the primary heat exchanger further comprises a circulation mechanism. 9. The ammonium carbamate-based thermal management system of claim 1, wherein the heat transfer fluid comprises a non-solvent heat transfer fluid, whereby the ammonium carbamate forms a suspension in the non-solvent heat transfer fluid. 10. The ammonium carbamate-based thermal management system of claim 1, wherein the heat transfer fluid comprises a heat transfer solvent, whereby the ammonium carbamate forms a solution in the heat transfer solvent. 11. The ammonium carbamate-based thermal management system of claim 1, wherein the primary heat exchanger comprises a plurality of coils configured such that the coolant fluid flows through the plurality of coils, and wherein an exterior surface of the plurality of coils is in contact with the heat transfer fluid. 12. The ammonium carbamate-based thermal management system of claim 1, wherein the primary heat exchanger comprises a plurality of thermally conductive structures configured such that heat from the coolant fluid is transferred to the thermally conductive structures, and wherein an exterior surface of the thermally conductive structures is in contact with the heat transfer fluid. 13. The ammonium carbamate-based thermal management system of claim 1, wherein the thermal load is selected from the group consisting of an electronic component, an avionic system, an antenna, a laser, a battery, and a fuel cell. 14. An ammonium carbamate-based thermal management system comprising: a thermal load selected from the group consisting of an electronic component, an avionic system, an antenna, a laser, a battery, and a fuel cell;an ammonium carbamate-based heat exchanger comprising ammonium carbamate and a non-aqueous heat transfer fluid, wherein heat absorbed into the heat transfer fluid causes an endothermic decomposition of ammonium carbamate into ammonia gas and carbon dioxide gas;a circulation loop comprising a coolant fluid and a coolant fluid circulation pump, wherein the circulation loop is fluidly coupled to the thermal load and the ammonium carbamate-based heat exchanger, and wherein the coolant fluid absorbs heat away from the thermal load and transfers heat to the ammonium carbamate-based heat exchanger; anda control system comprisinga pressure controller coupled to the ammonium carbamate-based heat exchanger, wherein the pressure controller regulates pressure within the ammonium carbamate-based heat exchanger at a level less than atmospheric pressure, and facilitates transfer of the ammonia gas and carbon dioxide gas formed by the endothermic decomposition of ammonium carbamate out of the ammonium carbamate-based heat exchanger;a flow valve in the circulation loop to regulate a flow of the coolant fluid; andat least one temperature sensor for sensing a temperature of the coolant fluid, wherein the control system is configured to control a rate of the endothermic decomposition of ammonium carbamate by controlling operation of the pressure controller, the flow valve, and/or the coolant fluid circulation pump.
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