항공기 냉각 시스템(4500) 은 증발기(4500, 5004), 응축기(4512, 4806), 어큐뮬레이터 및 펌프 시스템(4514)을 포함한다. 증발기(4500, 5004)는 액체(4516, 5032)를 사용하여 항공기(199, 400, 3127, 3855, 4502)에 있는 열 부하(4501, 4805, 5011) 세트를 냉각하도록 구성된다. 액체(4516, 5032)는 열 부하(4501, 4805, 5011) 세트를 냉각하는 것에 응답하여 증기(4519, 5031)를 형성한다. 응축기(4512, 4806)는 증발기(4500, 5004)로부터 증기(4519, 5031)를 받고 증기(4519, 5031)를 냉각시키고 증기(4519, 5031)를 냉각시킴에 따라 액체(4516, 5032)를 형성하도록 구성된다. 어큐뮬레이터(4513, 4808, 5008)는 응축기(4512, 4806)로부터 액체(4516, 5032)를 받아 액체(4516, 5032)를 저장하도록 구성된다. 펌프 시스템(4514)은 어큐뮬레이터(4513, 4808, 5008)에 저장된 액체(4516, 5032)를 증발기(4500, 5004)로 펌핑하도록 구성된다.
An aircraft cooling system (4500) comprises an evaporator (4500, 5004), condenser (4512, 4806), an accumulator, and a pump system (4514). The evaporator (4500, 5004) is configured to cool a set of heat loads (4501, 4805, 5011) in an aircraft (199, 400, 3127, 3855, 4502) using a liquid (4516, 5032). The liquid (4516, 5032) forms a vapor (4519, 5031) in response to cooling the set of heat loads (4501, 4805, 5011). The condenser (4512, 4806) is configured to receive the vapor (4519, 5031) from the evaporator (4500, 5004) and cool the vapor (4519, 5031) in which cooling the vapor (4519, 5031) forms the liquid (4516, 5032). The accumulator (4513, 4808, 5008)is configured to receive the liquid (4516, 5032) from the condenser (4512, 4806) and store the liquid (4516, 5032). The pump system (4514) is configured to pump the liquid (4516, 5032) stored in the accumulator (4513, 4808, 5008) to the evaporator (4500, 5004).
2 PUMPED TWO-PHASE COOLING OF AIRCRAFT ELECTRONICS
항공기 전자장치의 펌핑된 2상 냉각
2025-02-24
Patent
Electronic Resource
Korean
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY |