The embodiment of the invention provides an aircraft environment control system, an aircraft power system and an aircraft. The aircraft environment control system, the aircraft power system and the aircraft comprise a first air compressor, an intercooler, a second air compressor, a primary radiating device, a heat regenerator, a first condenser, a water separator, a first turbine, a second turbine, a third turbine, a second condenser and a third condenser, the first air compressor, the intercooler, the second air compressor, the primary radiating device, the hot side of the heat regenerator, the hot side of the first condenser, the water separator, the cold side of the heat regenerator, the first turbine, the cold side of the first condenser, the second turbine and the aircraft cockpit are sequentially communicated to form a fresh air branch. The primary scattering device, the third turbine, the second condenser, the third condenser and the intercooler are sequentially communicated to form a Rankine cycle branch; an output shaft of the third turbine is connected with the second gas compressor so as to drive the second gas compressor to operate. Through the processing scheme disclosed by the invention, the energy efficiency of the system can be improved.
本公开实施例中提供了一种飞机环控系统、飞机动力系统以及飞机。飞机环控系统、飞机动力系统以及飞机包括包括第一压气机、间冷器、第二压气机、初散装置、回热器、第一冷凝器、水分离器、第一涡轮、第二涡轮、第三涡轮、第二冷凝器和第三冷凝器,其中,第一压气机、间冷器、第二压气机、初散装置、回热器的热边、第一冷凝器的热边、水分离器、回热器的冷边、第一涡轮、第一冷凝器的冷边、第二涡轮以及飞机座舱依次连通形成新风支路;间冷器、初散装置、第三涡轮、第二冷凝器、第三冷凝器以及间冷器依次连通形成朗肯循环支路;其中,第三涡轮的输出轴与第二压气机连接以驱动第二压气机运行。通过本公开的处理方案,能够提高系统的能源效率。
Aircraft environment control system, aircraft power system and aircraft
一种飞机环控系统、飞机动力系统以及飞机
21.11.2023
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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