| 摘要 |
<p><P>PROBLEM TO BE SOLVED: To provide a gas turbine apparatus in which low caloric gas which is hardly used conventionally is stably burned, and combustible gas can be used at low costs with compact structure. <P>SOLUTION: The gas turbine apparatus 1 is provided with an air compressor 20 to compress the air, a burner 21 capable of burning the compressed air compressed by the air compressor 20, and a first fuel feeding system 24 to feed fuel into the burner 21. The gas turbine apparatus 1 is provided with a turbine 22 rotating by receiving gas from the burner 21, a regenerator 23 to heat-exchange between the compressed air fed into the burner 21 and the exhaust gas exhausted from the turbine 22, and a gas injector 25 to inject the low caloric gas LG into the exhaust gas exhausted from the turbine 22. <P>COPYRIGHT: (C)2006,JPO&NCIPI</p> |
