METHOD AND DEVICE FOR SUPPLYING WATER INTO INTERIOR OF AIRCRAFT

PURPOSE: To achieve the reduction of the portable water amount, the miniaturization of a water supplying system, and the reduction of the weight as well as to always secure water required for an airplane, by introducing exhaust gas of a jet engine to a water recovery facility and sequentially coolin...

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Bibliographische Detailangaben
Hauptverfasser: ROBERUTO POTSUPU, TOOMASU RITSUTERU, TOOMASU SHIERAA, BUERUNAA TSUIMUMAAMAN, YURUGEN DORAATO, FUERIKUSU NICHIYUKE, RUDORUFU PURERUSU
Format: Patent
Sprache:eng
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Zusammenfassung:PURPOSE: To achieve the reduction of the portable water amount, the miniaturization of a water supplying system, and the reduction of the weight as well as to always secure water required for an airplane, by introducing exhaust gas of a jet engine to a water recovery facility and sequentially cooling, separating, collecting and processing exhaust gas. CONSTITUTION: The exhaust gas flow 12 generated when kerosene is burnt in a jet engine is at least partially supplied to a water recovery facility 4. In the water recovery facility 4, the exhaust gas flow 12 is guided by an exhaust gas guide device 7, cooled by a cooling device 13 and condensed. Next, the condensed water is separated by a water separator 14, and the recovered water is collected as the rotary flow using the weight and centrifugal force. On the other hand, the residual exhaust gas flow 19 is guided from the water recovery facility 4 and mixed with bypass air flowing in the jet engine. The collected water is supplied to a water storage tank 23 through a water processing device 18 by a pump device 17.