发明名称 AIRCRAFT FUEL TANK ULLAGE GAS MANAGEMENT SYSTEM
摘要 An aircraft fuel tank ullage gas management system is disclosed. The system includes an electrochemical cell 30 having a membrane electrode assembly 10 that includes a cathode 14 and anode 16 separated by an electrolyte separator 12. A cathode fluid flow path is in fluid communication with the cathode, and receives the flow of cabin air from the cabin air fluid flow path and discharges nitrogen-enriched air. An anode fluid flow path is in fluid communication with the anode, and discharges oxygen or oxygen-enriched air. The electrochemical cell also includes water in fluid communication with the anode. The system includes an electrical power source 20 and electrical connections to the anode and cathode for providing an electric potential difference between the anode and cathode. An ullage flow path receives nitrogen-enriched air from the cathode fluid flow path and delivers it to the fuel tank 62. An optional flow path delivers humidified oxygen-enriched air back to the cabin.
申请公布号 EP3023518(A1) 申请公布日期 2016.05.25
申请号 EP20150196007 申请日期 2015.11.24
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 DARLING, ROBERT MASON;PERRY, MICHAEL L.
分类号 C25B15/08;C25B1/04;C25B9/10 主分类号 C25B15/08
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