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Prediction of periodic forced response of frictionally constrained turbine blades.

机译:摩擦约束涡轮叶片的周期性强制响应的预测。

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In turbine engine design, friction dampers are often employed to attenuate the turbine blade vibration and at the same time to increase aeroelastic stability of the turbine blades. The periodic forced response of turbine blades with shroud contacts and wedge dampers are investigated in this research. During the engine operation, the turbine blades may bend and twist to cause the friction contacts to experience friction constraint. The resulting constraint force can add friction damping as well as nonlinear spring force to the bladed disk system. When subjecting to periodic excitation, a 3D shroud contact model and a dual-interface friction model are employed to simulate the hysteresis loops of the constrained forces at the contact points of turbine bladed with shroud contacts or wedge dampers. The constrained forces can be considered as feedback forces that influence the response of the friction contacts. By using the Multi-Harmonic Balance Method along with Fast Fourier Transform, the constrained force can be approximated by a series of harmonic functions and this approach results in a set of nonlinear algebraic equations, which can be solved iteratively to yield the periodic response of blades having 3D nonlinear shroud constraint or wedge dampers.; It is shown that the resonant frequency shifts due to the additional spring constant introduced by the frictional constraint, and forced response is damped due to the additional friction damping introduced by frictional slip. In addition, the intermittent interface separation can cause multi-valued response that leads to jump phenomena. The predicted results are also compared with those of the direct time integration method so as to validate the proposed method, and the effect of super-harmonic components on the forced response and jump phenomenon is examined. It is shown that super-harmonic components may induce significant changes of the frictional characteristics such as the transitions between stick, slip and separation, and may affect the prediction of forced response and jump phenomena. It is demonstrated that the Multi-Harmonic Balance Method can predict accurately and efficiently for the periodic forced response by including the super-harmonic components in the analysis.
机译:在涡轮发动机设计中,通常使用摩擦阻尼器来减弱涡轮叶片的振动,同时增加涡轮叶片的气动弹性稳定性。在这项研究中,研究了带有护罩触点和楔形阻尼器的涡轮机叶片的周期性强迫响应。在发动机运行期间,涡轮机叶片可能会弯曲和扭曲,从而导致摩擦接触受到摩擦约束。所产生的约束力会增加摩擦阻尼以及带叶片的磁盘系统的非线性弹力。当受到周期性激励时,采用3D护罩接触模型和双界面摩擦模型来模拟在带有护罩触头或楔形阻尼器的涡轮机接触点处受约束力的磁滞回线。约束力可以被认为是影响摩擦接触的响应的反馈力。通过使用多谐波平衡方法和快速傅立叶变换,可以通过一系列谐波函数来近似估算受约束的力,并且这种方法可以生成一组非线性代数方程,可以迭代求解这些方程,从而得出叶片的周期性响应。具有3D非线性护罩约束或楔形阻尼器。结果表明,共振频率由于摩擦约束而引入的附加弹簧常数而发生偏移,而强制响应由于摩擦滑动所引入的附加摩擦阻尼而被阻尼。此外,间歇性的界面分离会导致多值响应,从而导致跳跃现象。将预测结果与直接时间积分法的预测结果进行比较,以验证该方法的有效性,并检验了超谐波分量对强迫响应和跳跃现象的影响。结果表明,超谐波分量可能引起摩擦特性的显着变化,例如粘滞,滑移和分离之间的过渡,并且可能影响对强迫响应和跳跃现象的预测。结果表明,通过在分析中包含超谐波分量,多重谐波平衡法可以准确,高效地预测周期性强迫响应。

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