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METHOD FOR CALCULATING ROTOR ASSEMBLY AXIS ECCENTRICITY BASED ON RADIAL RUN-OUT MEASUREMENT

机译:基于径向跳动测量的转子总轴偏心度计算方法

摘要

A method for calculating rotor assembly axis eccentricity based on a radial run-out measurement, comprising the calculation of a matrix representation of data of each point and a relative run-out value, the establishment of an equivalent spring model, and, the calculation of a contact force of each point in ideal conditions, and of the direction and magnitude of eccentricity; the calculation of a relative run-out value of each point and a process in which an assembly interference of each point is calculated correspondingly on the basis of run-out data of two stop opening fitting surfaces; the establishment of the equivalent spring model is based on a flexible distension hypothesis, forces and displacement relations of each phase in a contact process are analyzed, and an uneven contact force of each point is produced with an uneven interference; and the determination of the magnitude of eccentricity is essentially, based on the equivalent spring model, a calculation on the basis of an equilibrium formula to ultimately determine the magnitude of eccentricity. The present method implements a prediction of axis eccentricity prior to assembly on the basis of measured run-out data in actual production, increases the concentricity of rotors when assembled, and carries important actual guiding significance for an axis prediction and assembly phase adjustment and optimization in an aviation engine rotor assembly process.
机译:一种基于径向跳动测量值的转子组件轴线偏心率的计算方法,该方法包括计算每个点的数据和相对跳动值的矩阵表示,建立等效弹簧模型以及计算在理想条件下每个点的接触力,以及偏心的方向和大小;计算每个点的相对跳动值,以及基于两个止挡开口配合面的跳动数据相应地计算每个点的装配干涉的过程;基于弹性胀大假设建立等效弹簧模型,分析了接触过程中各相的力和位移关系,产生了各点受力不均,干涉不均的现象。偏心量的确定基本上是基于等效弹簧模型,是基于平衡公式的计算,最终确定了偏心量。本方法在实际生产中根据测得的跳动数据实现了装配前轴偏心的预测,增加了装配时转子的同心度,对轴的预测,装配相位的调整和优化具有重要的实际指导意义。航空发动机转子的组装过程。

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