Tool for certifying a head-gimbal assembly

    公开(公告)号:US20070157458A1

    公开(公告)日:2007-07-12

    申请号:US11717481

    申请日:2007-03-13

    IPC分类号: G11B5/127 H04R31/00

    摘要: A device and method for testing a slider of a head-gimbal assembly during disc drive manufacturing. The device includes a test disc, an actuator arm and a control module. The test disc has a first circumferential area for detecting contact between the slider and the test disc and a second circumferential area for burnishing sliders that contact the first circumferential area as the test disc rotates at or above the predetermined velocity. The head-gimbal assembly is affixed to a support, or flexure, on the actuator arm such that the slider is operable to move between an inner diameter and an outer diameter of the test disc. The control module controls rotation of the test disc and movement of the actuator arm, and thus the slider, relative to the test disc. The control module monitors the slider-disc interface for contact therebetween. If contact is detected, the slider is either burnished or the head-gimbal assembly is discarded altogether.

    Disc stabilization system
    2.
    发明申请
    Disc stabilization system 失效
    光盘稳定系统

    公开(公告)号:US20050041331A1

    公开(公告)日:2005-02-24

    申请号:US10647190

    申请日:2003-08-21

    IPC分类号: G11B5/60 G11B33/08 G11B33/14

    摘要: A disc stabilization system comprises a spinning disc with a disc surface deflectable by shock. The disc surface is in contact with a gas layer adjacent the disc surface. When the suspension system is subjected to a mechanical shock, the disc can deflect. The amplitude and duration of the deflection due to mechanical shock is limited by a wing feature. The wing feature includes an aerodynamic surface that interacts with the gas layer to generate an aerodynamic force on the disc surface. A strut supports the wing feature over the disc surface in a position such that the aerodynamic force increases as the disc surface deflects toward the aerodynamic surface.

    摘要翻译: 盘稳定系统包括具有通过冲击可偏转的盘表面的旋转盘。 盘表面与邻近盘表面的气体层接触。 当悬架系统受到机械冲击时,盘可以偏转。 机械冲击引起的偏转的幅度和持续时间受到机翼特征的限制。 机翼特征包括与气体层相互作用以在盘表面上产生空气动力的空气动力学表面。 支柱支撑在盘表面上的翼部特征,使得当盘表面朝向空气动力学表面偏转时,空气动力增加。