发明名称 AIRCRAFT AIR CONDITIONER
摘要 PROBLEM TO BE SOLVED: To effectively save fuel consumption of a system without inviting size-enlargement and decrease in reliability. SOLUTION: An air conditioning part 4 for supplying a pressure cabin 2 with conditioned air by controlling temperature and pressure of extracted air X from an engine 1 comprises a heat exchanger 4 for pre-cooling the extracted air X by ram air L and a vapor cycle system 5 for further cooling the extracted air X passing through the heat exchanger 4. Thereby the extracted air X is able to be extracted from a lower pressure stage of the engine 1 and a quantity of the extracted air is able to be reduced by half, and as in the case of providing an air cycle system and a vapor cycle system in parallel, the volume and the number of parts is effectively prevented from being doubled.
申请公布号 JP2000065432(A) 申请公布日期 2000.03.03
申请号 JP19980234413 申请日期 1998.08.20
申请人 SHIMADZU CORP 发明人 SHIGESADA YORIKAZU;MITANI HISASHI
分类号 F25B9/00;B64D13/06;F25B25/00;(IPC1-7):F25B9/00 主分类号 F25B9/00
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