发明名称 OPERATION OF A GAS TURBINE PLANT HAVING A COMPRESSOR AND A TURBINE
摘要 A method for operating a gas turbine plant having a compressor and a turbine, where a limit value of a guide blade adjustment for the compressor of the gas turbine is identified depending on at least one drive shaft speed of the gas turbine plant. For the at least one drive shaft speed, a maximum allowable turbine entry temperature corresponding to the limit value of the guide vane adjustment for the compressor or a maximum allowable temperature for the turbine of the gas turbine, which is dependent on the turbine entry temperature, is identified. The gas turbine is operated in consideration of the identified maximum allowable turbine entry temperature or the identified maximum allowable temperature.
申请公布号 US2016348592(A1) 申请公布日期 2016.12.01
申请号 US201515116607 申请日期 2015.02.05
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 Dierkes Rebecca;Engler Thorsten;Gorynski Markus;Sternemann Ansgar
分类号 F02C9/20;F02C7/042;F02C3/04 主分类号 F02C9/20
代理机构 代理人
主权项 1. A method for operating a gas turbine plant having a compressor and a turbine, the method comprising: in dependence on at least one drive shaft speed of the gas turbine plant, identifying a limit value of a guide blade adjustment for the compressor of the gas turbine and for the at least one drive shaft speed identifying a maximum allowable turbine entry temperature corresponding to the limit value of the guide blade adjustment for the compressor or a maximum allowable temperature dependent on the turbine entry temperature for the turbine of the gas turbine, and operating the gas turbine taking into account the identified maximum allowable turbine entry temperature or the identified maximum allowable temperature.
地址 München DE