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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Identification of Rotordynamic Force Coefficients of a Metal Mesh Foil Bearing Using Impact Load Excitations
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Identification of Rotordynamic Force Coefficients of a Metal Mesh Foil Bearing Using Impact Load Excitations

机译:基于冲击载荷激励的金属网箔轴承转子动力系数识别

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摘要

Metal mesh foil bearings (MMFBs) are inexpensive compliant gas bearing type that aim to enable high speed, high temperature operation of small turbomachinery. A MMFB with an inner diameter of 28.00 mm and length of 28.05 mm is constructed with low cost and common materials. The bearing incorporates a copper mesh ring, 20% in compactness, and offering large material damping beneath a 0.127 mm thick preformed top foil. Prior experimentations (published papers) provide the bearing structure force coefficients and the break away torque for bearing lift off. Presently, the MMFB replaces a compressor in a small turbocharger driven test rig. Impact load tests aid to identify the direct and cross-coupled rotor dynamic force coefficients, of the floating MMFB while operating at a speed of 50 krpm. Tests conducted with and without shaft rotation show the MMFB direct stiffness is less than its structural (static) stiffness, ~25% lower at an excitation frequency of 200 Hz. The thin air film acting in series with the metal mesh support and separating the rotating shaft and the bearing inner surface while airborne reduces the bearing stiffness. The equivalent viscous damping is nearly identical with and without shaft rotation. The identified loss factor, best representing the hysteretic type damping from the metal mesh, is high at ~0.50 in the frequency range 0-200 Hz. This magnitude reveals large mechanical energy dissipation ability from the MMFB. The measurements also show appreciable cross directional motions from the unidirectional impact loads, thus generating appreciable cross-coupled force coefficients. Rotor speed coast down measurements reveal pronounced subsynchronous whirl motion amplitudes locked at distinct frequencies. The MMFB stiffness hardening nonlinearity produces the rich frequency forced response. The synchronous as well as subsynchronous motions peak while the shaft traverses its critical speeds. The measurements establish reliable operation of the test MMFB while airborne.
机译:金属网箔轴承(MMFBs)是价格便宜的气体轴承类型,旨在使小型涡轮机械能够高速,高温运行。内径为28.00毫米,长度为28.05毫米的MMFB用低成本和普通材料制成。该轴承带有一个铜网环,密实度为20%,并在0.127毫米厚的预制顶箔下方提供大的材料阻尼。先前的实验(已发表的论文)提供了轴承结构力系数和轴承抬起的分离扭矩。目前,MMFB在小型涡轮增压器驱动的试验台上取代了压缩机。冲击载荷测试有助于确定以50 krpm的速度运行时浮动MMFB的直接和交叉耦合的转子动态力系数。在有轴旋转和无轴旋转的情况下进行的测试均表明,MMFB的直接刚度小于其结构(静态)刚度,在200 Hz的激励频率下降低了约25%。空气薄膜与金属丝网支撑件串联作用,并在空气传播时将旋转轴和轴承内表面分开,从而降低了轴承刚度。无论有无轴旋转,等效的粘性阻尼几乎相同。在0-200 Hz的频率范围内,所确定的损耗因子最能代表金属网的滞后型阻尼,该损耗因子很高,约为0.50。此大小表明MMFB具有很大的机械耗能能力。测量结果还显示了来自单向冲击载荷的可观的横向运动,从而生成了可观的横向耦合力系数。转子惯性滑行测量显示锁定在不同频率的明显次同步旋转运动幅度。 MMFB刚度硬化非线性会产生丰富的频率强制响应。同步运动和次同步运动在轴经过其临界速度时达到峰值。这些测量值可以确定机载测试MMFB在空中的可靠运行。

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