发明名称 Fuel cell-atmospheric-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 US7563527(B2) 申请公布日期 2009.07.21
申请号 US20050553692 申请日期 2005.10.18
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
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