首页> 外文期刊>Journal of Tribology >Effect of Intermolecular Forces on the Static and Dynamic Performance of Air Bearing Sliders: Part I - Effect of Initial Excitations and Slider Form Factor on the Stability
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Effect of Intermolecular Forces on the Static and Dynamic Performance of Air Bearing Sliders: Part I - Effect of Initial Excitations and Slider Form Factor on the Stability

机译:分子间力对空气轴承滑块静态和动态性能的影响:第一部分-初始激励和滑块形状因数对稳定性的影响

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The mechanical spacing between the slider and the disk has to be reduced to less than 5 nm in order to achieve an areal density of 1 Tbit/in{sup}2. Certain physical phenomena, such as those that can be caused by intermolecular and surface forces, which do not have a significant effect at higher flying heights, become more important at such low head-media separations. These forces are attractive for head-media separation as low as 0.5 nm, which causes a reduction in the mechanical spacing as compared to what would be the case without them. Single degree of freedom models have been used in the past to model these forces, and these models have predicted unstable flying in the sub-5-nm flying height range. Changes in the pitch and the roll angles were not accounted for in such models. A 3-DOF air bearing dynamic simulator model is used in this study to investigate the effect of the intermolecular forces on the static and dynamic performance of the air bearing sliders. It is seen that the intermolecular forces increase the level of flying height modulations at low flying heights, which in turn results in dynamic instability of the system similar to what has also been observed in experiments. The effect of initial vertical, pitch, and roll excitations on the static and dynamic flying characteristics of the slider in the presence of the intermolecular forces has also been investigated. A stiffness matrix is defined to characterize the stability in the vertical, pitch, and roll directions. The fly height diagrams are used to examine the multiple equilibriums that exist for low flying heights. Finally, a study was carried out to compare the performance of pico and femto designs based on the hysteresis observed during the touchdown-takeoff simulations.
机译:滑块和磁盘之间的机械间距必须减小到小于5 nm,以实现1 Tbit / in {sup} 2的面密度。某些物理现象,例如可能由分子间和表面力引起的物理现象,在较高的飞行高度下没有显着影响,在如此低的打印头与介质之间的分离下,这些现象变得更为重要。这些力对于低至0.5 nm的磁头介质分离是有吸引力的,与没有它们的情况相比,这会导致机械间距的减小。过去已使用单自由度模型对这些力进行建模,并且这些模型已预测了在低于5 nm的飞行高度范围内的不稳定飞行。在此类模型中未考虑俯仰和侧倾角的变化。在此研究中使用了3-DOF空气轴承动态仿真器模型来研究分子间力对空气轴承滑块的静态和动态性能的影响。可以看出,分子间力在低飞行高度下增加了飞行高度调制的水平,这又导致系统的动态不稳定性,类似于在实验中也观察到的。还研究了在存在分子间力的情况下初始垂直,俯仰和侧倾激励对滑块静态和动态飞行特性的影响。定义刚度矩阵以表征垂直,俯仰和横滚方向的稳定性。飞行高度图用于检查低飞行高度存在的多重平衡。最后,进行了一项研究,根据在着陆起飞模拟过程中观察到的磁滞来比较微微和毫微微设计的性能。

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