发明名称 Aircraft environment controller
摘要 An environment control unit for an airplane is configured so that air is drawn out of a cabin (2), oxygen and water molecules alone are separated from the drawn air by a selective permeable membrane (21), the permeated oxygen and water is supplied to the cabin (2) again. The remaining nitrogen is supplied to a fuel tank (41) in order to prevent explosion, it is possible to reduce the amount of air extracted from an engine (1) that is required to facilitate respiration for passengers and to prevent explosion.
申请公布号 US6527228(B2) 申请公布日期 2003.03.04
申请号 US20010926343 申请日期 2001.10.16
申请人 SHIMADZU CORPORATION 发明人 MITANI HISASHI
分类号 B64D13/02;B64D13/06;(IPC1-7):B64D13/06 主分类号 B64D13/02
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