Вплив шунтування високотемпературних тензорозісторів на точність виміру статичних деформацій елементів ГТД

Yuriy Husyev, Anatoliy Hol'tsov, Serhiy Kryhin
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Abstract

The development of gas turbine engines (GTE), for various purposes, is inextricably linked with an increase in their main characteristics. Simultaneously, the parameters of the working fluid increase, in particular, the temperature of the gas flow and the intensity of loads on structural elements with an increasing frequency of rotation of the rotors. The strength reliability of highly heated GTE elements is a factor that determines the life of the engine as a whole. The most common cases of damage to GTE elements are caused by static stresses, and mainly relate to the blade apparatus, compressor and gas turbine housings, combustion chambers and rotor elements operating in the temperature range of 200–750 °C. Errors in measuring static deformations of parts are usually associated with insufficient compensation for the temperature increment of resistance by the sensitive element (SE) of the strain gauge and with the occurrence of shunt currents between the SE and the body of the part through a binder insulator. The change in the electrical resistance of the strain gauge SE is perceived by the measuring system as an imaginary deformation. The measurement error due to shunting increases significantly with an increase in the temperature of the part under study, since this significantly reduces the specific electrical resistance of the binder insulator. A strain gauge sensor with two sensitive elements is considered in this work. The lower CE of the strain gauge sensor is located in the insulator-connector directly in the vicinity of the body of the part and perceives its main deformation. The upper Euro is located above the lower. The main axes of the elements are rotated relative to each other by 90 ° C and plays the role of temperature-compensating element and at the same time registers the transverse deformation of the part. An electrical model of the potential distribution in a strain gauge is presented. To determine the magnitude of shunt currents, Kirchhoff's rule was applied to a linear electric circuit, and finite-difference differential equations for the sum of currents in all nodes of the electric model were recorded. Finite-difference differential equations are transformed into a matrix one, the solution of which allows to obtain leakage currents in all nodes of the electric model of the strain gauge. The total leakage currents in the lower and upper SE strain gauge for different cases, as well as the relative errors of deformation measurement due to shunting, are obtained.
用于各种用途的燃气涡轮发动机(GTE)的发展与其主要特性的增加密不可分。同时,随着转子旋转频率的增加,工作流体的参数增加,特别是气流温度和结构元件的载荷强度增加。高温GTE元件的强度可靠性是决定发动机整体寿命的一个因素。GTE元件最常见的损坏是由静应力引起的,主要涉及在200-750℃温度范围内工作的叶片装置、压缩机和燃气轮机外壳、燃烧室和转子元件。测量零件静态变形的误差通常与应变片的敏感元件(SE)对电阻的温升补偿不足以及SE和零件本体之间通过粘结绝缘子发生分流电流有关。应变计SE电阻的变化被测量系统视为假想的变形。由于分流引起的测量误差随着所研究部件温度的升高而显著增加,因为这显著降低了粘结剂绝缘子的比电阻。本文研究了一种双灵敏元件应变计传感器。应变片传感器的下CE直接位于部件本体附近的绝缘子连接器中,感知其主要变形。上层欧元位于下层欧元之上。元件主轴相对旋转90°C,起到温度补偿元件的作用,同时记录零件的横向变形。提出了应变片中电位分布的电学模型。为了确定分流电流的大小,将Kirchhoff规则应用于线性电路,并记录电模型所有节点电流总和的有限差分微分方程。将有限差分微分方程转化为矩阵方程,求解得到应变片电模型各节点的漏电流。得到了下、上SE应变片在不同情况下的总泄漏电流,以及由于分流引起的变形测量的相对误差。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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