Undercut For Bushing Retention For SLS Details
    1.
    发明申请
    Undercut For Bushing Retention For SLS Details 审中-公开
    底切保留SLS详细信息

    公开(公告)号:US20050280189A1

    公开(公告)日:2005-12-22

    申请号:US10710144

    申请日:2004-06-22

    IPC分类号: B29C35/08 B29C41/02 B29C67/00

    摘要: In accordance with one aspect of the present invention, a system for manufacturing a tool within a laser sintering system includes a chamber enclosing a sinter material. The laser sintering system grows or sinters sections of the tool and tool contoured details from the sinter material in response to signals from a controller, wherein controller generates the signals as a function of a predetermined tool design. The contoured details include attachment holes, which are strengthened by bushings.

    摘要翻译: 根据本发明的一个方面,用于在激光烧结系统内制造工具的系统包括包围烧结材料的腔室。 激光烧结系统响应于来自控制器的信号,从烧结材料生长或烧结工具的部分和工具轮廓细节,其中控制器根据预定的工具设计生成信号。 轮廓细节包括通过衬套加强的附接孔。

    Formation of a pattern of holes in a structure
    2.
    发明授权
    Formation of a pattern of holes in a structure 有权
    在结构中形成孔洞图案

    公开(公告)号:US08454280B2

    公开(公告)日:2013-06-04

    申请号:US11676254

    申请日:2007-02-16

    IPC分类号: B23B35/00 B23B47/28

    摘要: A drill template includes a vacuum housing with a skirt having a CAD-formed contact surface formed to an exact fit with a mold line surface of a structure. The drill template includes at least one drill guide bushing extending through the vacuum housing from a top surface to an interior surface of the vacuum housing; a vacuum port integral to the vacuum housing; and at least one index hole for positioning and aligning the vacuum housing on the structure. Index holes extend from the top surface through to the CAD-formed contact surface of the vacuum housing. A CAD-formed edge of part locator is formed according to a CAD solid model of the aircraft fuselage and fits to a precise location of the structure for precisely positioning the template on the structure. A vacuum port provides vacuum to the interior of the vacuum housing for removing drilling debris and dust.

    摘要翻译: 钻模模板包括具有裙部的真空壳体,其具有形成为与结构的模具线表面精确配合的CAD形成的接触表面。 钻模板包括从真空壳体的顶表面延伸穿过真空壳体至内表面的至少一个钻导引套管; 与真空壳体成一体的真空口; 以及用于在结构上定位和对准真空壳体的至少一个分度孔。 索引孔从顶表面延伸到真空壳体的CAD形成的接触表面。 部件定位器的CAD形成边缘根据飞机机身的CAD实体模型形成,并适合于结构的精确位置,以将模板精确地定位在结构上。 真空口为真空外壳的内部提供真空,用于清除钻屑和灰尘。

    SLS For Tooling Applications
    3.
    发明申请
    SLS For Tooling Applications 审中-公开
    SLS用于模具应用

    公开(公告)号:US20050287031A1

    公开(公告)日:2005-12-29

    申请号:US10710163

    申请日:2004-06-23

    IPC分类号: B22F3/105 B29C67/00

    CPC分类号: B29C64/153

    摘要: A system for sintering a tool within a laser sintering system includes a chamber enclosing a sinter material. The laser sintering system grows or sinters the tool from the sinter material in response to signals from a controller. The controller generates these signals as a function of a predetermined tool design. A heat sink is positioned within the chamber to cool features of the tool, thereby limiting warping of these features during sintering of the tool.

    摘要翻译: 用于在激光烧结系统内烧结工具的系统包括封闭烧结材料的腔室。 激光烧结系统响应于来自控制器的信号,从烧结材料生长或烧结工具。 控制器根据预定的工具设计生成这些信号。 散热器定位在室内以冷却工具的特征,从而在工具烧结期间限制这些特征的翘曲。

    Integral Nut Slot System In SLS Details
    4.
    发明申请
    Integral Nut Slot System In SLS Details 审中-公开
    SLS详细信息中的积分螺母槽系统

    公开(公告)号:US20050285314A1

    公开(公告)日:2005-12-29

    申请号:US10710231

    申请日:2004-06-28

    IPC分类号: B29C35/08 B29C67/00

    CPC分类号: B29C64/153

    摘要: A system for manufacturing a tool within a laser sintering system includes a chamber enclosing a sinter material. The laser sintering system grows or sinters a section of the tool from the sinter material in response to signals from a controller. The controller generates the signals as a function of a predetermined tool design. The predetermined tool design includes defining a slot in the section of the tool, wherein the slot receives a weld-nut after sintering is complete for strengthening a portion of the section of the tool.

    摘要翻译: 一种用于在激光烧结系统内制造工具的系统包括包围烧结材料的腔室。 激光烧结系统响应于来自控制器的信号,从烧结材料生长或烧结工具的一部分。 控制器根据预定的工具设计生成信号。 预定的工具设计包括在工具的部分中限定狭槽,其中在完成烧结之后,狭槽接收焊接螺母,以加强工具的该部分的一部分。

    Drill template with integral vacuum attach
    5.
    发明申请
    Drill template with integral vacuum attach 有权
    具有整体真空附件的钻模板

    公开(公告)号:US20050084344A1

    公开(公告)日:2005-04-21

    申请号:US10690367

    申请日:2003-10-20

    摘要: A drill template includes a vacuum housing with a skirt having a CAD-formed contact surface formed to an exact fit with a mold line surface of a structure. The drill template includes at least one drill guide bushing extending through the vacuum housing from a top surface to an interior surface of the vacuum housing; a vacuum port integral to the vacuum housing; and at least one index hole for positioning and aligning the vacuum housing on the structure. Index holes extend from the top surface through to the CAD-formed contact surface of the vacuum housing. A CAD-formed edge of part locator is formed according to a CAD solid model of the aircraft fuselage and fits to a precise location of the structure for precisely positioning the template on the structure. A vacuum port provides vacuum to the interior of the vacuum housing for removing drilling debris and dust.

    摘要翻译: 钻模模板包括具有裙部的真空壳体,其具有形成为与结构的模具线表面精确配合的CAD形成的接触表面。 钻模板包括从真空壳体的顶表面延伸穿过真空壳体至内表面的至少一个钻导引套管; 与真空壳体成一体的真空口; 以及用于在结构上定位和对准真空壳体的至少一个分度孔。 索引孔从顶表面延伸到真空壳体的CAD形成的接触表面。 部件定位器的CAD形成边缘根据飞机机身的CAD实体模型形成,并适合于结构的精确位置,以将模板精确地定位在结构上。 真空口为真空外壳的内部提供真空,用于清除钻屑和灰尘。

    FORMATION OF A PATTERN OF HOLES IN A STRUCTURE
    6.
    发明申请
    FORMATION OF A PATTERN OF HOLES IN A STRUCTURE 有权
    形成一个结构中的洞穴图案

    公开(公告)号:US20070140800A1

    公开(公告)日:2007-06-21

    申请号:US11676254

    申请日:2007-02-16

    IPC分类号: B23B35/00

    摘要: A drill template includes a vacuum housing with a skirt having a CAD-formed contact surface formed to an exact fit with a mold line surface of a structure. The drill template includes at least one drill guide bushing extending through the vacuum housing from a top surface to an interior surface of the vacuum housing; a vacuum port integral to the vacuum housing; and at least one index hole for positioning and aligning the vacuum housing on the structure. Index holes extend from the top surface through to the CAD-formed contact surface of the vacuum housing. A CAD-formed edge of part locator is formed according to a CAD solid model of the aircraft fuselage and fits to a precise location of the structure for precisely positioning the template on the structure. A vacuum port provides vacuum to the interior of the vacuum housing for removing drilling debris and dust.

    摘要翻译: 钻模模板包括具有裙部的真空壳体,其具有形成为与结构的模具线表面精确配合的CAD形成的接触表面。 钻模板包括从真空壳体的顶表面延伸穿过真空壳体至内表面的至少一个钻导引套管; 与真空壳体成一体的真空口; 以及用于在结构上定位和对准真空壳体的至少一个分度孔。 索引孔从顶表面延伸到真空壳体的CAD形成的接触表面。 部件定位器的CAD形成边缘根据飞机机身的CAD实体模型形成,并适合于结构的精确位置,以将模板精确地定位在结构上。 真空口为真空外壳的内部提供真空,用于清除钻屑和灰尘。

    Drill template with integral vacuum attach
    7.
    发明授权
    Drill template with integral vacuum attach 有权
    具有整体真空附件的钻模板

    公开(公告)号:US07195429B2

    公开(公告)日:2007-03-27

    申请号:US10690367

    申请日:2003-10-20

    IPC分类号: B23B47/28

    摘要: A drill template includes a vacuum housing with a skirt having a CAD-formed contact surface formed to an exact fit with a mold line surface of a structure. The drill template includes at least one drill guide bushing extending through the vacuum housing from a top surface to an interior surface of the vacuum housing; a vacuum port integral to the vacuum housing; and at least one index hole for positioning and aligning the vacuum housing on the structure. Index holes extend from the top surface through to the CAD-formed contact surface of the vacuum housing. A CAD-formed edge of part locator is formed according to a CAD solid model of the aircraft fuselage and fits to a precise location of the structure for precisely positioning the template on the structure. A vacuum port provides vacuum to the interior of the vacuum housing for removing drilling debris and dust.

    摘要翻译: 钻模模板包括具有裙部的真空壳体,其具有形成为与结构的模具线表面精确配合的CAD形成的接触表面。 钻模板包括从真空壳体的顶表面延伸穿过真空壳体至内表面的至少一个钻导引套管; 与真空壳体成一体的真空口; 以及用于在结构上定位和对准真空壳体的至少一个分度孔。 索引孔从顶表面延伸到真空壳体的CAD形成的接触表面。 部件定位器的CAD形成边缘根据飞机机身的CAD实体模型形成,并适合于结构的精确位置,以将模板精确地定位在结构上。 真空口为真空外壳的内部提供真空,用于清除钻屑和灰尘。