首页> 外国专利> METHOD FOR CALCULATING UNSTEADY FORCE ACTING ON ROTOR BLADE OR STATOR BLADE, TURBINE DESIGN TECHNIQUE AND TURBINE MANUFACTURING METHOD

METHOD FOR CALCULATING UNSTEADY FORCE ACTING ON ROTOR BLADE OR STATOR BLADE, TURBINE DESIGN TECHNIQUE AND TURBINE MANUFACTURING METHOD

机译:转子叶片或定子叶片非定常作用力的计算方法,汽轮机设计技术和汽轮机制造方法

摘要

A turbine design method that can easily construct a turbine stage structure in which an unsteady force acting on a rotor blade can be reduced and degradation in performance and increase in rotor shaft length can be prevented is provided. For example, unsteady forces and exciting forces by the potential field interaction acting on the rotor blade are respectively obtained by the viscous flow solution (21) and the inviscid flow solution (22) with respect to a plurality of distances between stator and rotor blades, exciting forces by the wake interaction acting on the rotor blade are obtained from a difference between a viscous flow solution result and an inviscid flow solution result, the exciting forces by the potential field interaction and the wake interaction are mathematically expressed (23) as functions of the distance between stator and rotor blades, the unsteady force acting on the rotor blade when the distance between stator and rotor blades is an arbitrary value is calculated (24) based on the mathematically-expressed exciting forces by the potential field interaction and the wake interaction, and the distance between stator and rotor blades is determined (30) based on a calculation result.
机译:提供一种涡轮设计方法,其可以容易地构造涡轮级结构,在该涡轮级结构中,可以减小作用在转子叶片上的不稳定力,并且可以防止性能下降和转子轴长度的增加。例如,关于定子叶片和转子叶片之间的多个距离,通过粘性流动解(21)和粘性流动解(22)分别求出作用在转子叶片上的由于势场相互作用而产生的不稳定力和激振力,由粘性流解结果与非粘性流解结果之间的差获得由作用在转子叶片上的尾流相互作用产生的激振力,将势场相互作用和尾流相互作用引起的激振力用数学公式表示为(23)定子和转子叶片之间的距离,当定子和转子叶片之间的距离为任意值时作用在转子叶片上的非定常力是根据数学表达的励磁力通过势场相互作用和尾流相互作用计算的(24) ,并且基于计算结果确定定子叶片与转子叶片之间的距离(30)。

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