发明名称 |
Device for producing water on board of an airplane |
摘要 |
A device for producing water on board an aircraft includes at least one high temperature fuel cell entirely or partially integrated into a combustion chamber arrangement of a gas turbine aircraft engine. The combination of at least one fuel cell and a gas turbine engine is adapted to operate exclusively with hydrogen and atmospheric oxygen, and is embodied in an aircraft propulsion engine and/or an auxiliary power unit used for producing compressed air for a cabin and a power supply of the aircraft. The at least one high temperature fuel cell is fed with pure hydrogen on an anode side and with air on a cathode side. The combustion chambers of the turbine engine are fed with an air-hydrogen mixture, whereby at least the hydrogen supply can be regulated or completely shut off.
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申请公布号 |
US7767359(B2) |
申请公布日期 |
2010.08.03 |
申请号 |
US20050532545 |
申请日期 |
2005.04.22 |
申请人 |
AIRBUS DEUTSCHLAND GMBH |
发明人 |
HOFFJANN CLAUS;HEINRICH HANS-JUERGEN |
分类号 |
H01M8/04;B64D11/02;F02C6/04;H01M8/12 |
主分类号 |
H01M8/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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