| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a fuel reformer system for a turbomachine system. <P>SOLUTION: The turbomachine system (2, 64, 158) includes a compressor portion (4, 74, 165) having a compressor inlet (6, 167) and a compressor outlet (7, 77, 168), a turbine portion (10, 80, 171) operatively connected to the compressor portion (4, 74, 165), a combustor (15, 86, 178) having a combustor inlet (17, 88, 181) fluidly connected to the compressor outlet (7, 77, 168) and a combustor outlet (18, 89, 182) fluidly connected to the turbine portion (10, 80, 171), and a reformer (32, 106, 204) having a reformer inlet (36, 109, 207) fluidly connected to the compressor outlet (7, 77, 168) and a reformer outlet (37, 110, 208) fluidly connected to the combustor inlet (17, 88, 181). The reformer (32, 106, 204) partially combusts air from the compressor portion (4, 74, 165) and a fuel to form a hydrogen-rich syngas. <P>COPYRIGHT: (C)2012,JPO&INPIT |
