发明名称 |
TURBO-BLOCK OF GAS-COMPRESSOR UNIT |
摘要 |
FIELD: machine building. ^ SUBSTANCE: invention is designed for implementation in gas-compressor units (GCU), gas-turbine electric stations and other power systems where there are used gas-turbine installations (GTI) as drive. The turbo-block of the gas-compressor unit consists of a gas-turbine installation and of an exhaust line including a spiral, diffuser and pipe. A system for heating room of unit installation is formed in the exhaust line. The system consists of radiators and of gas ducts communicating with radiators, collecting hot gas from the exhaust line of the gas-turbine installation and discharging it to atmosphere. Orifices of the intake gas ducts are arranged in the exhaust line and directed to a side of the spiral. ^ EFFECT: heating rooms of GCU with its own source of heat without expenditures for electric energy; avoiding additional equipment for heating. ^ 3 dwg |
申请公布号 |
RU2429359(C1) |
申请公布日期 |
2011.09.20 |
申请号 |
RU20100104612 |
申请日期 |
2010.02.09 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE "ISKRA" |
发明人 |
BOJARSHINOV VLADIMIR IVANOVICH;SALAMATOV VLADIMIR MIKHAJLOVICH;LAVROV SERGEJ ANATOL'EVICH;CHARNTSEV DMITRIJ ANATOL'EVICH;BARAKHTA GALINA DMITRIEVNA |
分类号 |
F02C6/18;F04D25/02 |
主分类号 |
F02C6/18 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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