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Theoretical and experimental research on turbo-generator shaft alignment using strain gauge method

机译:基于应变片法的涡轮发电机轴对中理论与实验研究

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摘要

Shaft alignment is a key factor for the safe and reliable operation of a turbine unit. This paper presents an approach to estimate the turbo-generator shaft alignment using strain gauge technique with two measuring sections nearby each coupling. The change of shaft bending moment is linearly proportional to the change of bearing elevation and reaction force. So the bearing load distribution can be identified from the strain values and bending moments which are measured using strain gauge. The transfer matrix method is used to calculate the detailed shaft alignment data including deflection, slopes, bearing reaction forces, influence coefficients, sag/gap values. Experiments were carried out on a test rig with 3 rotors, 2 couplings and 6 bearings. It was shown that the strain gauge identification results agree well with the results using the jack-up method. The maximum relative error of each bearing loads is almost 8.7. The sag/gap values using the strain gauge method are close to those using the laser alignment method. The maximum relative error is less than 7.5. Results also show that the strain gauge method is sensitive to possible disturbances in the bearing elevation. In the end, strain gauge alignment technique with two measuring sections nearby each coupling was applied on the shaft alignment estimation of a 600MW turbine unit successfully. The bearing loads and shaft deflection were obtained accurately.
机译:轴对中是涡轮机组安全可靠运行的关键因素。本文提出了一种使用应变片技术估计涡轮发电机轴对中的方法,每个联轴器附近有两个测量部分。轴弯矩的变化与轴承高度和反作用力的变化成线性正比。因此,轴承载荷分布可以从应变值和弯矩中识别出来,这些应变值和弯矩是使用应变片测量的。传递矩阵法用于计算详细的轴对中数据,包括挠度、斜率、轴承反作用力、影响系数、落差/间隙值。实验是在具有 3 个转子、2 个联轴器和 6 个轴承的试验台上进行的。结果表明,应变片的识别结果与自升法的结果吻合较好。每个轴承载荷的最大相对误差几乎为8.7%。使用应变片方法的流降/间隙值与使用激光对准方法的压差/间隙值接近。最大相对误差小于7.5%。结果还表明,应变片法对轴承标角可能产生的扰动很敏感。最后,将应变片对准技术(每个联轴器附近有两个测量段)成功地应用于一台600MW涡轮机组的轴对中估计。轴承载荷和轴挠度得到准确。

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