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LOSS REDUCTION DEVICE FOR USE IN PARTIAL ADMISSION TURBINE AND PARTIAL ADMISSION TURBINE

机译:用于部分进气涡轮和部分进气涡轮的减损装置

摘要

This loss reduction device for use in a partial admission turbine of at least one embodiment is for use in a partial admission turbine that includes a governing-stage nozzle that is configured to have an admission section and a non-admission section for a working fluid in the circumferential direction, The loss reduction device is provided with an annular disk section, disposed on the opposite side of the governing-stage nozzle so that a gap exists with respect to a rotor disk to an outer circumferential surface of which is attached a governing-stage rotor blade on which the working fluid admitted from the governing-stage nozzle acts. The annular disk section: has an opening section formed at a position corresponding to the admission section of the governing-stage nozzle; and is configured so that the inner circumferential edge thereof is located further radially inward than the outer circumferential surface of the rotor disk.
机译:用于至少一个实施例的部分进气涡轮中的该减少损失的装置用于部分进气涡轮中,该部分进气涡轮包括调节级喷嘴,该调节级喷嘴构造成具有用于工作流体的进气部分和非进气部分。损耗减小装置设有环形盘部,该环形盘部设置在调节级喷嘴的相对侧上,从而相对于转子盘存在间隙,在该转子盘的外周表面上安装有调节器。从调节级喷嘴吸入的工作流体作用在该级转子叶片上。环形盘部分:在与调节级喷嘴的进入部分相对应的位置处形成有开口部分;且构造成使得其内周边缘位于比转子盘的外周表面更径向向内的位置。

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