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Method of cooling a turbine stage, and a gas turbine having a cooled the turbine stages

机译:冷却涡轮级的方法以及具有冷却的涡轮级的燃气轮机

摘要

The turbine (1) has a cooling medium feed device for feeding cooling medium i.e. air, into the interior of a guide vane (11) of a turbine stage (8) for cooling the guide vane. A rear edge (16) of the guide vane at a pressure side (18) is provided with a cooling medium outlet opening (25) for discharging the cooling medium out of the guide vane into a main flow. The feed device has a mass flow control device (20) i.e. throttle valve, for increasing the mass flow through the outlet opening during a partial-load operation of the turbine compared to that during a full load operation. An independent claim is also included for a method for cooling a turbine stage of a gas turbine.
机译:涡轮机(1)具有用于将冷却介质即空气供给到涡轮级(8)的导向叶片(11)的内部的冷却介质供给装置,以冷却导向叶片。导向叶片在压力侧(18)的后边缘(16)设置有冷却介质出口(25),用于将冷却介质从导向叶片排出到主流中。进料装置具有质量流量控制装置(20),即节流阀,用于与在涡轮机的部分负荷运行期间相比在全负荷运行期间增加通过出口的质量流量。还包括用于冷却燃气涡轮机的涡轮机级的方法的独立权利要求。

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