首页> 外文期刊>Microsystem technologies >Static and dynamic flying characteristics of a slider on bit-patterned media (dynamic responses based on frequency domain analysis)
【24h】

Static and dynamic flying characteristics of a slider on bit-patterned media (dynamic responses based on frequency domain analysis)

机译:位图媒体上滑块的静态和动态飞行特性(基于频域分析的动态响应)

获取原文
获取原文并翻译 | 示例
           

摘要

Recording media with grooves, such as discrete track media (DTM) and bit-patterned media (BPM), are considered to be promising media for achieving ultrahigh recording densities. It is thus important to analyze the static and dynamic characteristics of flying head sliders on DTM and BPM using the molecular gas film lubrication equation and the van der Waals (vdW) equation. In this study, we consider BPM with rectangular bits. We express the disk recess as a Fourier series and determine the quasi-static and time-dependent components. We also develop a perturbation method for small groove depths for calculating static slider attitudes and dynamic responses in the frequency domain. The numerical results predict that the grooves will significantly reduce the quasi-static flying height h_0. They also predict that for a small groove depth h_(groove), flying height decrease Δh_0 almost agree with the value of uniform disk recess obtained by a Fourier series expansion, which also agrees with empirical results. Dynamic slider characteristics obtained by the frequency domain analysis is useful for sliders suffering from excitations of several tens of kHz such as sliders flying at transition between data zone and servo zone, although the dynamic spacing fluctuation by realistic BPM media is negligible.
机译:具有凹槽的记录介质,例如离散轨道介质(DTM)和位模式介质(BPM),被认为是实现超高记录密度的有前途的介质。因此,重要的是使用分子气膜润滑方程式和van der Waals(vdW)方程式分析DTM和BPM上的飞头滑块的静态和动态特性。在这项研究中,我们考虑具有矩形位的BPM。我们将磁盘凹槽表示为傅立叶级数,并确定准静态和随时间变化的分量。我们还开发了一种针对小凹槽深度的摄动方法,用于计算频域中的静态滑块姿态和动态响应。数值结果表明,凹槽将显着降低准静态飞行高度h_0。他们还预测,对于较小的凹槽深度h_(groove),浮动高度降低Δh_0几乎与通过傅立叶级数展开获得的均匀磁盘凹入值相符,这也与经验结果相符。通过频域分析获得的动态滑块特性对于遭受数十kHz激励的滑块很有用,例如,在数据区和伺服区之间的过渡处飞行的滑块,尽管实际BPM介质的动态间距波动可以忽略不计。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号