具有负粘性阻尼和位移相关干摩擦阻尼的类梁结构的稳定性和强迫响应

W. Whiteman, A. Ferri
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引用次数: 0

摘要

研究了受位移相关库仑摩擦力阻尼的类梁结构的弯曲振动。由于干摩擦阻尼元件的几何特性,摩擦力随梁的横向位移线性增长。最近的研究表明,与位移相关的干摩擦力系统的阻尼类似于线性结构阻尼。利用这一事实,可以使每个周期的能量损失像振动位移振幅的平方一样增长,而不是像具有恒定法向力的摩擦阻尼系统那样与振幅线性增长。此外,干摩擦非常适合恶劣的环境,如高温和高转速与燃气轮机相关。这些观察结果表明,在涡轮和风扇叶片应用中,与位移相关的干摩擦可能是抑制颤振的有效手段。不稳定气动力在本研究中表示为负粘性阻尼。这种简单的气动模型常用于捕捉气动弹性系统颤振的基本特征。进行了单模态和多模态分析。结果表明,在一定条件下,位移相关干摩擦阻尼器的能量损失足以克服破坏稳定的负粘性阻尼。这一结果进一步表明,可以设计涡轮叶片系统中摩擦界面的几何形状和位置,从而增强阻尼并更好地控制颤振。
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Stability and Forced Response of Beam-Like Structures Having Negative Viscous Damping and Displacement-Dependent Dry Friction Damping
The flexural vibration of a beam-like structure damped with a displacement-dependent Coulomb friction force is examined. Due to the geometry of the dry friction damping element, the friction force grows linearly with the beam’s transverse displacement. Recent studies have shown that the damping of systems with displacement-dependent dry friction forces resembles linear structural damping. Taking advantage of this fact, the energy loss per cycle can be made to grow like the square of the vibratory displacement amplitude rather than linearly with amplitude as in the case of frictionally damped systems with constant normal forces. Furthermore, dry friction is well suited to hostile environments such as the high temperatures and high rotation speeds associated with gas turbines. These observations suggest that displacement-dependent dry friction may be an effective means of flutter suppression in turbine and fan blade applications. Destabilizing aerodynamic forces are represented in this study as negative viscous damping. This simple aerodynamic model is often used to capture the basic features of flutter in aeroelastic systems. Both single and multiple-mode analyses are conducted. Results show that energy losses from the displacement-dependent dry friction damper are large enough to overcome the destabilizing negative viscous damping under certain conditions. This result further suggests that it may be possible to design the geometry and location of frictional interfaces in turbine blade systems so that damping may be enhanced and flutter better controlled.
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Experimental Evaluation of a Semi-Active Friction Damper The Effects of Tangential Contact Stiffness on a Harmonically Forced Friction Oscillator Estimating Coulomb and Viscous Friction From Free-Vibration Decrements Stochastic Description of Dry Friction in Metal-to-Metal Contact Under Harmonic Excitation Spatial Impact of a Flexible Link Using a Nonlinear Contact Force
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