发明名称 |
METHOD OF OPERATION OF GAS TURBINE |
摘要 |
FIELD: gas turbines. SUBSTANCE: gas turbine has air compressor 4, combustion chamber 3 and turbine 5 which drives air compressor 4. Gas turbine may work on combustible mixture calculated stoichiometrically. Air compressor 4 feeds air in amount sufficient for combustion and cooling of combustible gas to permissible turbine inlet temperature due to mixing it with water steam delivered from external steam cycle. provision is also made for operation of gas turbine at intermediate heating taking place between high-pressure turbine 9 and low-pressure turbine 10; waste gas of high-pressure turbine 9 is heated due to heat transfer from gas of combustion chamber before high pressure turbine 9 which is cooled down. EFFECT: enhanced efficiency. 1 dwg |
申请公布号 |
RU95105594(A) |
申请公布日期 |
1996.11.20 |
申请号 |
RU19950105594 |
申请日期 |
1995.01.16 |
申请人 |
GAZ-EHLEKTRITSITETS-UND VASSERVERKE KEL'N AG |
发明人 |
VOL'FGANG VINKLER;KURT ZAURER |
分类号 |
F02C3/30;F01K21/04;F02C6/00;F02C7/16 |
主分类号 |
F02C3/30 |
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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