发明名称 CLOSED BRAYTON CYCLE GAS TURBINE DEVICE
摘要 PROBLEM TO BE SOLVED: To shorten time up to self-sustaining of a system and to miniaturize a starting motor by providing a passage communicating from an air reserving tank of operating gas made into high pressure to a gas turbine entrance and a passage communicating with a heater entrance and disposing a device for controlling supply of operating gas on each passage. SOLUTION: Entrance gas supply lines 5, 4 for supplying operating gas 15 from an air reserving tank 11 to a gas turbine 6 and a heater 8, respectively, are provided between the air reserving tank 11 and an entrance of the gas turbine 6 and between the air reserving tank 11 and an entrance of the heater 8, respectively. In each line 5, 4, entrance opening and closing valves 14, 13 are interposed. When a system is started, a gas compressor 7 is driven by a starting motor 12, operating gas 15a is compressed, and an output is generated in also the gas turbine 6 by supplying high pressure operating gas from the air reserving tank 11 to the gas turbine 6 via the gas supply line 5 at almost the same time as this compression. At the same time, the heater 8 is operated and operating gas 15b of high pressure can be early supplied to the gas turbine 6.
申请公布号 JP2000154733(A) 申请公布日期 2000.06.06
申请号 JP19980329823 申请日期 1998.11.19
申请人 MITSUBISHI HEAVY IND LTD 发明人 OSAKO TAKESHI;MATSUMURA TOSHIYUKI;EGUCHI SEIJI
分类号 F02C1/10;(IPC1-7):F02C1/10 主分类号 F02C1/10
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