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).
PUMPED TWO-PHASE COOLING OF AIRCRAFT ELECTRONICS
GEPUMPTE ZWEIPHASENKÜHLUNG VON FLUGZEUGELEKTRONIK
REFROIDISSEMENT À DEUX PHASES POMPÉ DE L'ÉLECTRONIQUE D'UN AÉRONEF
19.02.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |