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惯性力对挤压油膜阻尼器支承转子的响应的影响 被引量:2

Effects of Fluid Inertia Forces on Bistable andNonsynchronous Responses of SqueezeFilmDamperSupported Flexible Rotor
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摘要 分析了挤压油膜阻尼器的流体惯性力对柔性转子的非线性双稳态响应及非协调响应的影响。研究表明,惯性力的影响越大,挤压油膜阻尼器的刚度力越小,阻尼力越大,从而导致系统稳态响应的峰值转速降低,振幅减小。流体惯性力对系统在亚临界及超临界的双稳态响应及非协调响应具有明显的抑制作用。惯性力越大,产生双稳态响应或非协调响应的转速范围越小,非协调谐波分量越小,但有时惯性力太大也会引起新的非协调响应。 Previous studies of this important problem have been quite limited. We discussed that fluid inertia forces, long neglected in the design of aeroengine rotor supported on squeezefilmdamper bearings, exert appreciable influence and thus should not be neglected in engineering design. In order to compute the effects of fluid inertia forces, we started form the wellknown NavierStokes equation and derived Eqs.(5) and (6). They indicate that inertia forces are directly proportional to Reynolds number and that inertia forces are nonlinear functions of the displacement, velocity, and acceleration of the rotor axis at the bearings. The effects of fluid inertia forces on bistable responses were calculated and shown in Fig.1. Calculations were done mainly with Eq.(11).Figs.1a and 1b are for two different sets of parameters respectively. In Fig.1 ε-Ω curves for three different values of R es are shown; ε is the response, Ω is the ratio of rotor frequency to natural frequency and R es is Reynolds number divided by Ω . Fig.1 shows that inertia forces have obvious suppression effect on bistable response. The effects of fluid inertia forces on nonsynchronous responses were calculated and shown in Figs.2 through 4. Calculations were done by numerically integrating eqs.(1) through (4). Figs.2 through 4 are for three different sets of parameters. Figs.2 through 4 show that inertia forces in general have suppressing effect on nonsynchronous response. Occasionally, such as in Fig.2, excessive inertia forces do not have suppressing effect.
机构地区 西北工业大学
出处 《西北工业大学学报》 EI CAS CSCD 北大核心 1997年第2期294-299,共6页 Journal of Northwestern Polytechnical University
基金 霍英东青年教师基金 国家自然科学基金
关键词 挤压油膜阻尼器 惯性力 非协调响应 转子 阻尼器 squeeze film damper, fluid inertia force, bistable response, nonsynchronous response
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参考文献3

  • 1Zhang J,ASME Trans J Tribol,1993年,115卷,692页
  • 2孟光,J Gas Turbine and Power,1993年,115卷,341页
  • 3孟光,Rotating Mach Dyn,1987年,1卷,121页

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