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Design approach of the turbine, the determination method of the unsteady forces acting on the turbine preparation and rotor blade or the like

机译:涡轮的设计方法,作用在涡轮预备件上的非定常力的确定方法以及转子叶片等

摘要

PROBLEM TO BE SOLVED: To provide a turbine design method capable of easily constructing a turbine stage structure which reduces non-stationary force acting on a moving blade or static blade and can prevent deterioration of performance or increase of rotor shaft length.;SOLUTION: Non-stationary force and exciting force due to potential interference respectively acting on a moving blade are determined with respect to arbitrary distance between static and moving blades, for example, by a viscous analysis (21) and a non-viscous analysis (22), the exciting force due to wake interference acting on the moving blade is determined from a difference between a viscous analysis result and a non-viscous analysis result, phases of the exciting forces due to potential interference and wake interference are respectively subjected to mathematization (23a) as functions of the distances between static and moving blades, a difference between the phases of the exciting force due to potential interference and the exciting force due to wake interference, subjected to mathematization is caused so as not to be approximated to the same phase, thereby, the distance between static and moving blades which does not make the non-stationary force operating on the moving blade excessive is calculated (24a) and the distance between static and moving blades is decided (30) based on the calculated result.;COPYRIGHT: (C)2014,JPO&INPIT
机译:解决的问题:提供一种涡轮设计方法,该方法能够容易地构建涡轮级结构,从而减少作用在动叶片或静叶片上的非平稳力,并可以防止性能下降或转子轴长度增加。关于静叶片和动叶片之间的任意距离,例如通过粘性分析(21)和非粘性分析(22)来确定分别作用在动叶片上的,由于潜在的干扰引起的静止力和激振力。根据粘性分析结果与非粘性分析结果之间的差来确定由作用在活动叶片上的尾流干扰引起的激振力,将由潜在干扰和尾流干扰引起的激振力的相位分别进行数学化(23a),即静叶片和动叶片之间的距离的函数,由于潜在干扰而引起的激振力相位之间的差异并且,由于唤醒干扰而引起的激振力经过数学处理而变得不近似于同一相位,因此,静叶片与动叶片之间的距离不会使作用在动叶片上的非平稳力过大。计算(24a),并根据计算结果确定(30)静态和活动叶片之间的距离。;版权所有:(C)2014,JPO&INPIT

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