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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers, Part J. Journal of engineering tribology >Dynamic modeling of an eccentric face seal including coupled rotordynamics, face contact, and inertial maneuver loads
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Dynamic modeling of an eccentric face seal including coupled rotordynamics, face contact, and inertial maneuver loads

机译:偏心面密封的动态建模,包括耦合旋转动力学,面部接触和惯性机动负荷

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摘要

Mechanical face seals are constitutive components of turbomachines, which in turn can be constitutive to other systems (e.g. aircraft). Furthermore, the rotating element of a face seal is inextricably coupled to the turbomachine via a flexible mount, and the stationary seal element is coupled to the rotating seal element via the fluid film existing between the seal faces. Consequentially, understanding interactions between the seal and turbomachine is important for quantifying seal performance and improving its design. With few exceptions, previous works study the face seal dynamics independent from the rotordynamics. In addition, most prior investigations consider only angular and axial seal dynamics and neglect eccentric (i.e. lateral) deflections of the seal element(s). For the first time, this work develops a comprehensive and novel model of a mechanical face seal in the inertial reference frame including coupled rotordynamics and inertial maneuver loads of the overall system. The model is developed for a general seal geometry where both seal elements, stationary and rotating, are flexibly mounted and allowed to undergo angular, axial, and eccentric deflections. In addition, the seal model presented here accounts for transient operation, fluid shear forces, seal face contact, friction, and thermoelastic deformation. Finally, various faults due to manufacturing imperfections, component flaws, and/or installation errors can be accounted for by incorporating static angular misalignment of both seal elements, dynamic angular misalignment of the rotating seal element, eccentric rotating imbalance, and axial offset of the rotating seal element center of mass. Throughout this work, the equations of motion developed are valid for both steady-state and transient operation. This comprehensive model significantly advances the state of the art in mechanical face seal dynamic modeling and represents a pivotal step towards analyzing seal performance regarding a broad diversity of realistic problems.
机译:机械面密封件是涡轮机构的本构型组分,涡轮机组又可以是其他系统(例如飞机)的构成型。此外,面部密封的旋转元件通过柔性安装件不可指伸地连接到涡轮机,并且静止密封元件通过在密封面之间的流体膜联接到旋转密封元件。因此,了解密封和涡轮机之间的相互作用对于量化密封性能并改善其设计非常重要。凭借少数例外,以前的作品研究了独立于圈动力学的面部密封动态。此外,大多数现有研究仅考虑只有角度和轴向密封动态和忽略密封元件的偏心(即横向)偏转。这项工作首次开发了惯性参考帧中的机械面密封件的全面和新型模型,包括耦合的圈子动力学和整个系统的惯性操纵负载。该模型是为通用密封几何设计的,其中密封元件,静止和旋转,可灵活地安装并允许经过角度,轴向和偏心偏转。此外,这里呈现的密封模型占瞬态操作,流体剪切力,密封面接触,摩擦和热弹性变形。最后,通过制造缺陷,部件缺陷和/或安装错误引起的各种故障可以通过结合密封元件的静态角度未对准,旋转密封元件的动态角度未对准,偏心旋转不平衡和旋转的轴向偏移密封元件质量中心。在此工作中,开发的运动方程对于稳态和瞬态操作都有效。这种综合模型在机械面密封动态建模中显着推进了现有技术,并且代表了分析关于逼真问题的广泛多样性的密封性能的枢转步骤。

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