UNIT FOR SURFACE TREATMENT OF TOP LAYERS, ESPECIALLY OF METAL
    2.
    发明公开
    UNIT FOR SURFACE TREATMENT OF TOP LAYERS, ESPECIALLY OF METAL 有权
    UNIT表面处理上层,尤其是金属

    公开(公告)号:EP2519380A1

    公开(公告)日:2012-11-07

    申请号:EP10769085.1

    申请日:2010-09-21

    摘要: The subject of the invention is a unit for surface treatment of top layers, especially of metal, which is used for the treatment of top layers of working surfaces of machine parts, and especially for placement of coatings of micro- and nanometric solid greases in the unevenness of the surfaces of extrusion punches and on sliding guides of machine tools. Characterised in that the ram being a hammer (2) with a ball-shaped working area, connected with a piezoelectric actuator Q), which is driven by a high frequency voltage generator with a frequency changeable within the range of 10 Hz to 1000 Hz and a relative movement of the hammer (2) in relation to the treated material (3) along the acting line within the range of 0.05 to 5.0 mm.

    Method for peening the internal surface of a hollow part
    4.
    发明公开
    Method for peening the internal surface of a hollow part 审中-公开
    抛光的空心工件的内表面的方法

    公开(公告)号:EP1077109A3

    公开(公告)日:2003-10-15

    申请号:EP00115596.9

    申请日:2000-07-19

    IPC分类号: B24B39/06 B24B31/00 B24B39/00

    摘要: The rate of impact between the peening elements (14) and an internal surface (26) of a hollow part (12) is a function of the vibration frequency, and there is a cut-off frequency at which a hollow part (12) can vibrate and induce repeated impact between its internal surface (26) and the peening elements (14) because the rate of impact becomes erratic and loses its cyclical nature as the vibration frequency deviates from the cut-off frequency. The present invention provides a method for determining the cut-off frequency at which a hollow part can vibrate and maintain the repetitive nature of the impact between its internal surface and the peening elements. Such a method requires a peening element speed limit ratio, which is the ratio of the velocity of the hollow part compared to the velocity of the peening element above which the rate of impact begins to become erratic and lose its cyclical nature. The present invention utilizes the peening element speed limit ratio to determine the frequency at which to vibrate the hollow part when peening its internal surface so as to and maintain repeated impact between it and the peening elements.

    Hard disk burnishing head
    5.
    发明公开
    Hard disk burnishing head 有权
    PolierkopffürFestplatten

    公开(公告)号:EP1003157A3

    公开(公告)日:2001-08-29

    申请号:EP99309001.8

    申请日:1999-11-11

    IPC分类号: G11B5/84 G11B5/60 B24B39/06

    CPC分类号: G11B5/84 Y10T29/47

    摘要: The burnishing head for hard disk processing includes a solid body having generally rectangular surfaces, including an upper surface, a burnishing pad surface, a front surface, a rear surface and two side surfaces. A plurality of burnishing pads are disposed upon the burnishing pad surface. The pads are shaped such that each pad has a burnishing edge that is generally parallel to said front surface and therefore orthogonal to the direction of media travel. The burnishing pads are preferably configured such that two frontward leading pads are disposed proximate the front surface in a spaced apart relationship and one leading middle pad is disposed rearwardly of the two frontward leading pads and generally between the two frontward leading pads. Two rear pads are disposed generally rearwardly of the leading middle pad in a spaced apart relationship, and one rearward pad is disposed rearwardly of the two rear pads and generally between the two rear pads. In the preferred embodiment the pads are generally triangular in shape and the outer surface of the leading and rearward pads may be tapered. The method for manufacturing the burnishing head, includes the steps of making a series of parallel cuts in a surface of a solid body of material. The burnishing pads result from material that remains following the cuts.

    摘要翻译: 用于硬盘处理的抛光头包括具有大致矩形表面的固体,其包括上表面,抛光垫表面,前表面,后表面和两个侧表面。 多个抛光垫设置在抛光垫表面上。 焊盘成形为使得每个焊盘具有通常平行于所述前表面并因此正交于介质行进方向的抛光边缘。 抛光垫优选地被配置为使得两个前沿引导垫以间隔开的关系设置在前表面附近,并且一个前导中间焊盘设置在两个前向引导焊盘的后方,并且通常在两个前方引导焊盘之间。 两个后垫以间隔开的关系大致位于前中间垫的后方,并且一个后垫设置在两个后垫的后方并且通常位于两个后垫之间。 在优选实施例中,焊盘的形状通常为三角形,并且前焊盘和后焊盘的外表面可以是锥形的。 抛光头的制造方法包括在固体物质的表面上进行一系列平行切割的步骤。 抛光垫由切割后保留的材料产生。

    Micro-burnishing flex head structure
    6.
    发明公开
    Micro-burnishing flex head structure 失效
    微型扶手头结构

    公开(公告)号:EP0450226A3

    公开(公告)日:1991-12-18

    申请号:EP90310696.1

    申请日:1990-09-28

    IPC分类号: G11B5/84 B24B39/06

    CPC分类号: G11B5/84 B24B39/06 Y10T29/47

    摘要: An integrated, unitary micro-burnishing head structure for use with the surface of rigid magnetic recording media. In one type of embodiment, the proposed head structure includes a single elongate flexure body to one end of which is joined a media-contacting abrader head which may take any one of several different preferred shapes. In another embodiment, plural elongate flexure bodies are disposed in a comb-like array carrying abrader heads at one set of free ends, and joined adjacent their opposite ends through a common joinder structure.

    SCHLICHTFRÄSWERKZEUG, INSBESONDERE SCHAFTFRÄSER

    公开(公告)号:EP3356071A1

    公开(公告)日:2018-08-08

    申请号:EP16766958.9

    申请日:2016-09-16

    摘要: The invention relates to a finishing tool (1), in particular an end milling cutter, a) suitable and intended for removing material over the area of a workpiece surface and for smoothing the workpiece surface in a milling motion by rotation about a tool axis (A) in a predetermined direction of rotation (D) with simultaneous advancement in relation to the workpiece surface and comprising b) at least one chip-removing milling edge (30, 31 to 33), which b1) extends continuously and without interruptions axially in relation to the tool axis (A) over an axial length (L) on a circumferential surface (U) that is rotationally symmetrical, in particular cylindrical, around the tool axis and b2) during the milling motion removes workpiece chips from the workpiece surface over its entire axial length (L) with a radial depth of chip-removing penetration (T to Tmax), and c) at least one non-chip-removing pressing land (8), which c1) extends continuously and without interruptions axially in relation to the tool axis (A) over an axial length (L) on a circumferential surface that is rotationally symmetrical, in particular cylindrical, around the tool axis, c2) is arranged, as seen in the direction of rotation (D), following an associated milling edge (7) with an angular pitch (δ) and c3) during the milling motion presses into the workpiece surface machined by the associated milling edge over its entire length (L) with a radial depth of non-chip-removing penetration (T or R
    S - R
    D ) and smooths it, d) wherein the depth of chip-removing penetration (T to Tmax) is less than the axial length by a factor of at least 5 and the depth of non-chip-removing penetration (T or R
    S - R
    D ) is less than the axial length (L) by a factor of at least 10.

    Method and apparatus for increasing fatigue notch capability of airfoils
    9.
    发明公开
    Method and apparatus for increasing fatigue notch capability of airfoils 审中-公开
    的方法和装置的电阻增加至叶片的疲劳开裂

    公开(公告)号:EP1941968A2

    公开(公告)日:2008-07-09

    申请号:EP07123678.0

    申请日:2007-12-19

    IPC分类号: B23P9/02 B24B39/06 C21D7/08

    摘要: A method of reducing crack propagation in an airfoil (22) includes: providing an airfoil (22) having a root (36) spaced apart from a tip (34), spaced-apart leading and trailing edges (30, 32), a suction side (40) extending from the leading edge (30) to the trailing edge (32), and an opposed pressure side (38) extending from the leading edge (30) and the trailing edge (32), supporting the airfoil (22) against bending loads. The airfoil (22) is burnished using a burnishing element (42), so as to create at least one burnished section (68) of residual compressive stress. The at least one burnished section (68) is located adjacent the leading edge (30) and spaced from the leading edge (30) by an offset distance selected so as to avoid deformation of the leading edge (30).

    摘要翻译: 减少在一个翼型(22)裂纹扩展的方法,包括:在翼片(22)提供具有根(36)从前端(34)间隔开的,间隔开的前缘和后缘(30,32),抽吸 侧(40),从所述前缘(30)与后缘(32)延伸,并在与压力侧(38)从所述前缘(30)和后缘(32)延伸,支承所述翼型件(22) 对弯曲载荷。 该翼型件(22)是使用抛光元件(42),以便产生残余压缩应力中的至少一个抛光部分(68)抛光。 所述至少一个抛光部分(68)位于邻近前缘(30),并通过在偏移距离选择成避免所述前缘(30)的变形从所述前缘(30)隔开。