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Blade synchronous vibration measurements of a new upgraded heavy duty gas turbine MGT-70(3) by using tip-timing method

机译:刀片同步振动测量新的升级重型燃气涡轮机MGT-70(3)使用尖端定时方法

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The work described in this paper is part of a comprehensive prototype test conducted on a heavy duty power generation gas turbine recently upgraded by MAPNA Turbine Engineering and Manufacturing Company (TUGA). A Blade tip-Timing system is proposed to determine the synchronous vibration characteristics of the rotor blades and to validate the design calculations. The last three stages of turbine section are equipped with tip-timing sensors. Six probes are positioned along the circumferential direction for each stage. The locations of sensors are accurately chosen based on the values of the natural frequencies and the number of necessary modes needed to be captured. The vibration parameters of the blades are obtained by post-processing and analyzing of the acquired data. The resonance frequencies are plotted against rotating speed during transient acceleration of the machine and the damping and amplitude of vibration in resonance condition are also determined. The obtained results meet the designer expectations and confirm a safe operation from vibrational point of view. (C) 2020 Elsevier Ltd. All rights reserved.
机译:本文描述的工作是在最近由Mapna涡轮机工程和制造公司(Tuga)升级的重型发电燃气轮机进行的全面原型测试的一部分。提出刀片尖端定时系统以确定转子叶片的同步振动特性并验证设计计算。涡轮部分的最后三个阶段配备了尖端定时传感器。六个探针沿着每个阶段的圆周方向定位。基于自然频率的值和捕获所需模式的数量来精确选择传感器的位置。叶片的振动参数通过后处理和分析获取的数据而获得。在机器的瞬态加速期间绘制谐振频率反向旋转速度,并且还确定谐振条件中的阻尼和振动的振动。所获得的结果符合设计人员期望,并从振动的角度确认安全运行。 (c)2020 elestvier有限公司保留所有权利。

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