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.
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.
HAMANO NOBUHIKO
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Shintaro Hotta
Ryoji Kosugi
Tomohiro Mori
Tetsuya Hirosawa
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