Title:
航空機内で水を生成するための装置
Document Type and Number:
Japanese Patent JP4484709
Kind Code:
B2
Abstract:
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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Inventors:
Hofyan Claus
Heinrich Hans Jürgen
Heinrich Hans Jürgen
Application Number:
JP2004547406A
Publication Date:
June 16, 2010
Filing Date:
October 21, 2003
Export Citation:
Assignee:
Airbus Operations Game Beher
International Classes:
F01K23/10; B64D11/00; B64D11/02; B64D27/02; B64D41/00; F02C3/20; F02C6/00; H01M8/06; H01M8/12
Domestic Patent References:
| JP2000311698A | ||||
| JP2001167781A | ||||
| JP4159423A | ||||
| JP200025696A | ||||
| JP7156892A | ||||
| JP667299U | ||||
| JP11200888A | ||||
| JP2000100461A |
Foreign References:
| GB2338750A |
Attorney, Agent or Firm:
Fujita Akira