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Analysis for Fatigue Failure Causes on a Large-scale Reciprocating Compressor Vibration by Torsional Vibration

机译:通过扭转振动对大型往复式压缩机振动进行疲劳失效的分析

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The crankshaft of a large-scale reciprocating compressor frequently cracks because of the fatigue failure and Ihc 1 st and 2nd crank bearings often are scuffed due to torsional vibration. Such problems are handled by connecting the 2nd and 3rd shaft with two plate flanges in the form of interference fit assembling. Using numerical simulation, models are built for the two crankshafts with modification. Modal analysis and dynamic response calculation of crankshaft system under different modification projects are performed. The results show that the frequency ratio r between sevenfold rotating speed of the initial crankshaft and the first order torsional vibration natural frequency is 1.016, which makes the initial crankshaft to resonate. With the enlarged rotating inertia-mass on modified crankshaft, the frequency ratio r increases to 1.064, and the resonance is eliminated. The rotating vibration displacement of the initial crankshaft at the 1st crank pin is far larger than that of the 6th, which is the primary cause of crank bearing scuffing. The inertia-mass of initial crankshaft results to additional stress with resonance, which is the primary cause of crank cracking for fatigue failure.
机译:由于疲劳故障,并且IHC 1和第二曲柄轴承通常由于扭转振动而经常磨损,因此大型往复式压缩机的曲轴经常裂缝。通过将2个和第三轴用两个板凸缘连接到干涉配合组装的形式来处理这些问题。使用数值模拟,模型是为两个具有修改的曲轴而构建的模型。执行不同修改项目下曲轴系统的模态分析和动态响应计算。结果表明,初始曲轴的七倍旋转速度与第一阶扭转振动自然频率之间的频率比r为1.016,使初始曲轴产生共振。随着改性曲轴上的扩大旋转惯性质量,频率比率R增加到1.064,消除了共振。在第一曲柄销处的初始曲轴的旋转振动位移远大于第六的旋转振动位移,这是曲柄轴承磨损的主要原因。初始曲轴的惯性质量导致额外的胁迫,这是疲劳破坏曲柄破裂的主要原因。

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