发明名称 |
FUEL CELL/CONSTANT PRESSURE TURBINE/HYBRID SYSTEM |
摘要 |
A fuel cell-atmospheric-pressure turbine hybrid system uses the thermal energy of a cell exhaust gas discharged from an atmospheric-pressure, high-temperature fuel cell effectively, does not need any additional emergency protective device, and enables the use of lightweight, easy-to-process structural and piping materials to reduces the cost. The fuel cell-atmospheric-pressure turbine hybrid system includes: a combustor 2 for burning an exhaust gas G1 discharged from an atmospheric-pressure, high-temperature fuel cell 1; a turbine 3 in which a combustion gas G2 discharged from the combustor 2 expands and the pressure of the combustion gas G2 drops to a negative pressure; a compressor 4 for compressing an exhaust gas G3 discharged from the turbine 3 to increase the pressure of the exhaust gas G3; and a heat exchanger 5 for transferring heat from the high-temperature exhaust gas G3 discharged from the turbine 3 to low-temperature air A to be supplied to the fuel cell 1. |
申请公布号 |
EP1643575(B1) |
申请公布日期 |
2009.03.11 |
申请号 |
EP20040746599 |
申请日期 |
2004.06.29 |
申请人 |
KAWASAKI JUKOGYO KABUSHIKI KAISHA |
发明人 |
TANAKA, KAZUO;HARADA, EIICHI,;SHOJI, TAKATOSHI;KITAJIMA, JUNICHI;YAMASHITA, SEIJI |
分类号 |
F01K23/10;H01M8/04;F02C6/00;F02C7/143;H01M8/00;H01M8/06;H01M16/00 |
主分类号 |
F01K23/10 |
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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