首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >ON THE FORCE COEFFICIENTS OF A FLOODED, OPEN ENDS SHORT LENGTH SQUEEZE FILM DAMPER: FROM THEORY TO PRACTICE (AND BACK)
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ON THE FORCE COEFFICIENTS OF A FLOODED, OPEN ENDS SHORT LENGTH SQUEEZE FILM DAMPER: FROM THEORY TO PRACTICE (AND BACK)

机译:关于充斥的,开口的短长度挤压膜阻尼器的力系数:从理论到实践(反过来)

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Gas turbine aircraft engine manufacturers push for simple squeeze film damper (SFD) designs, short in length, yet able to provide enough damping to ameliorate rotor vibrations. SFDs employ orifices to feed lubricant directly into the film land or into a deep groove. The holes, acting as pressure sources (or sinks), both disrupt the film land continuity and reduce the generation of squeeze film dynamic pressure. Overly simple predictive formulations disregard the feedholes and deliver damping (C) and inertia (M) force coefficients not in agreement with experimental findings. Presently, to bridge the gap between simple theory and practice, the paper presents measurements of the dynamic forced response of an idealized SFD that disposes of the feedholes altogether. The short-length SFD, whose diameter D=125 mm, has one end submerged (flooded) within a lubricant bath and the other end exposed to ambient. ISO VG 2 lubricant flows by gravity through the film land of length L=25.4 mm and clearance c=0.122 mm. From dynamic load tests over excitation frequency range 10-250 Hz, experimental damping coefficients (Cxx, Crr) from the flooded damper agree well with predictions from the classical open ends model with a full film for small amplitude whirl motions (r/c ≪ 1), centered and off-centered. Air ingestion inevitably occurs for large amplitude motions (r/c > 0.4) thus exacerbating the difference between predictions and tests results. For reference, identical tests were conducted with a practical SFD supplied with lubricant (P_(in)=0.4 bar) via three orifice feedholes, 120° apart at the film land mid plane. A comparison of test results shows as expected, that for small amplitude (r/c ~ 0.05) orbits, the flooded damper generates on average 30% more damping than the practical configuration as the latter's feedholes distort the generation of pressure. For large amplitude motions (r/c > 0.4), however, the flooded damper provides slightly lesser damping and inertia coefficients than the SFD with feedholes whose pressurized lubricant delivery alleviates air ingestion in the film land. The often invoked open ends SFD classical model is not accurate for the practical engineered design of an apparently simple mechanical element.
机译:燃气涡轮飞机发动机制造商推动了简单的压缩膜阻尼器(SFD)设计,该设计的长度较短,但能够提供足够的阻尼以减轻转子的振动。 SFD使用孔将润滑剂直接供入薄膜区或深槽中。用作压力源(或凹陷)的孔既破坏了膜的连续性,又减少了挤压膜动压力的产生。过于简单的预测公式忽略了进料孔,并提供了与实验结果不一致的阻尼(C)和惯性(M)力系数。目前,为弥合简单理论与实践之间的鸿沟,本文提出了一种理想的SFD的动态强迫响应的测量方法,该SFD完全布置了馈电孔。直径为D = 125毫米的短长度SFD,其一端浸没(淹没)在润滑剂浴中,而另一端则暴露于环境中。 ISO VG 2润滑剂在重力作用下流过长度L = 25.4 mm和间隙c = 0.122 mm的薄膜区域。通过在10-250 Hz激励频率范围内进行动态负载测试,淹没式阻尼器的实验阻尼系数(Cxx,Crr)与经典的开放式模型的预测非常吻合,该模型对于小振幅涡动运动具有完整的薄膜(r / c≪ 1 ),居中和偏离中心。大振幅运动(r / c> 0.4)不可避免地会发生空气摄入,从而加剧了预测和测试结果之间的差异。作为参考,使用一个实际的SFD进行了相同的测试,该润滑剂通过三个孔口进料孔(在膜地中间平面相隔120°)供应了润滑剂(P_(in)= 0.4 bar)。对测试结果的比较表明,如预期的那样,对于小振幅(r / c〜0.05)轨道,淹没式阻尼器产生的阻尼平均比实际配置高出30%,因为后者的进料孔会扭曲压力的产生。但是,对于大振幅运动(r / c> 0.4),溢流阻尼器的阻尼和惯性系数比带进料孔的SFD略小,后者的加压润滑剂输送可减轻薄膜区域的空气摄入。对于表面上简单的机械元件的实际工程设计,经常调用的开放式SFD经典模型并不准确。

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