首页> 外文会议>TRIB-vol.16; American Society of Mechanical Engineers(ASME) International Mechanical Engineering Congress and Exposition; 20051105-11; Orlando,FL(US) >NUMERICAL ANALYSIS OF THE LUBRICATION PERFORMANCES FOR ULTRA-THIN GAS FILM LUBRICATION OF MAGNETIC HEAD/DISK WITH A NEW FINITE DIFFERENCE METHOD
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NUMERICAL ANALYSIS OF THE LUBRICATION PERFORMANCES FOR ULTRA-THIN GAS FILM LUBRICATION OF MAGNETIC HEAD/DISK WITH A NEW FINITE DIFFERENCE METHOD

机译:磁头/盘超薄气膜润滑新的有限差分数值分析

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In the present paper, a new iterative algorithm of finite difference method to numerically solve the lubrication problems of magnetic head/disks under ultra thin gas film thickness is introduced. Pressure distributions are calculated when a slider deviates slowly or abruptly from the balance position due to perturbations. The results show that when the slider moves in the film thickness direction, the pressure always tends to force the slider back to the balance position. Steady flying simulations show that the pitch angle is the sensitive parameter to the load carrying capacity of the slider, which should be carefully controlled in design. Squeeze effect is apparent when abrupt movements or rotations happen, which can avoid, to some extent, fatal damages due to vibration or uncertain interferences.
机译:本文介绍了一种新的有限差分迭代算法,用于数值求解超薄气膜厚度下磁头/磁盘的润滑问题。当滑块由于扰动而缓慢或突然偏离平衡位置时,将计算压力分布。结果表明,当滑块在薄膜厚度方向上移动时,压力总是趋向于迫使滑块回到平衡位置。稳定的飞行模拟表明,俯仰角是滑块的承载能力的敏感参数,在设计中应谨慎控制。当突然移动或旋转时,挤压效应很明显,这可以在某种程度上避免由于振动或不确定的干扰而造成的致命伤害。

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