| 摘要 |
PROBLEM TO BE SOLVED: To provide a two shaft gas turbine with improved reliability that improves output power and efficiency and is stably operated by establishing a balance between the driving force of a compressor and the output power of a high pressure turbine in the case wherein the two shaft gas turbine is applied to a system, in which the flow rate of fluid flowing into a combustor is increased compared with a simple cycle gas turbine. SOLUTION: A part of working fluid for driving the high pressure turbine 3H is allowed to flow not into the high pressure turbine 3H but into a low pressure turbine 3L. COPYRIGHT: (C)2010,JPO&INPIT |
