发明名称 AIR CONDITIONER FOR AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To reduce bleed air from an engine, enhance a fuel consumption, to provide a lightweight and compact system, and enhance reliability. SOLUTION: Bleed 1 is taken into a head exchanger 3, an evaporator 5 using a refrigerant of a VCS 51 is arranged in the downstream of the heat exchanger 3 of an ACS 50, air cooled therein is dehumidified under high pressure in a high pressure water separator 13, it is heated by a reheater 14, it is adiabatically expanded in a turbine 15, and moisture contained in it is removed perfectly in a low pressure water separator 17. The resulting dehumidified air is mixed with one portion of air of a cabin 20 in a mixing chamber 18 to supply fresh air of a comfortable temperature to the cabin 20.
申请公布号 JP2000318695(A) 申请公布日期 2000.11.21
申请号 JP19990129717 申请日期 1999.05.11
申请人 SHIMADZU CORP 发明人 URYU SHOJI
分类号 B64D13/08;B64D13/06;(IPC1-7):B64D13/08 主分类号 B64D13/08
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