首页> 外国专利> MEASUREMENT METHOD FOR ROTOR BLADE DYNAMIC STRAIN FIELD BASED ON BLADE TIP TIMING AND SYSTEM THEREOF

MEASUREMENT METHOD FOR ROTOR BLADE DYNAMIC STRAIN FIELD BASED ON BLADE TIP TIMING AND SYSTEM THEREOF

机译:基于叶尖定时的转子叶片动态应变场测量方法及其系统

摘要

Disclosed are a measurement method for rotor blade (4) dynamic strain field based on blade tip timing and a system thereof. The method comprises the following steps: establishing a three-dimensional finite element model of the rotor blade (4) to be measured, and extracting modal parameters of the three-dimensional finite element model (S1); determining the number and circumferential installation positions of blade tip timing sensors (1) (S2); establishing a mapping relationship between blade single-point displacement and full-field dynamic strain (S3); obtaining blade tip single-point displacement of the rotor blade (4) based on the blade tip timing sensor (1) (S4); and obtaining the dynamic strain measurement of the rotor blade (4) at arbitrary position and in arbitrary direction according to the single-point displacement based on the mapping relationship (S5). The method only uses finite measure points of the blade tip to realize the reconstruction of the overall dynamic strain field of the rotor blade (4), and can achieve the measurement of the normal strain and the shear strain of all the nodes on the surface and in the interior of the rotor blade (4) under multi-modal vibration. The calculation process is simple, and online measurement can be easily carried out.
机译:公开了一种基于叶片尖端正时的转子叶片(4)动态应变场的测量方法及其系统。该方法包括以下步骤:建立待测量的转子叶片(4)的三维有限元模型,以及提取三维有限元模型的模态参数(S1);确定叶片尖端正时传感器(1)的数量和圆周安装位置(S2);建立叶片单点位移与全场动态应变之间的映射关系(S3);基于叶尖正时传感器(1)获得转子叶片(4)的叶尖单点位移(S4);根据映射关系,根据单点位移,求出动叶片(4)在任意位置,任意方向上的动应变(S5)。该方法仅利用叶片尖端的有限测量点即可实现对转子叶片(4)整体动态应变场的重构,并且可以实现对表面上所有节点的法向应变和剪切应变的测量。在多模态振动下转子叶片(4)的内部。计算过程简单,可以轻松进行在线测量。

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