发明名称 SLIGHTLY PRESSURIZED FUEL GAS TURBINE
摘要 PURPOSE:To eliminate the need of especially disposing a gas compressor so as to reduce the expenditure for installing an apparatus by owing compression of slightly pressurized fuel gas to the shaft power of a gas turbine and using its revolution and drive power. CONSTITUTION:A gas supply chamber 7 having an air intake port is disposed at the air supply side of a compressor 2 and a slightly pressurized fuel gas pipe 12 is connected thereto via a flow control valve 11. Air is thereby carried from the intake port 6 to the gas supply chamber 7 by the compressor 2 which is driven by a gas turbine 1 and is compressed along with the slightly pressurized fuel gas which is fed from nozzles formed in ejecttion pipes 9 and 10 in the form of mixture gas, which is squeezed to be sent into a combustion chamber 3 and ignited to be burnt therein. The need of independently installing a special gas compressor is therefore eliminated so that the expenditure for installing an apparatus may be reduced extremely.
申请公布号 JPS59122729(A) 申请公布日期 1984.07.16
申请号 JP19820233009 申请日期 1982.12.28
申请人 TOKYO DENRYOKU KK;CHIYODA KAKO KENSETSU KK 发明人 TAKEDA HARUO;KOBAYASHI KENJI
分类号 F02C3/22;(IPC1-7):02C3/22 主分类号 F02C3/22
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