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12 条记录 (耗时 0.016 秒)

    Determinant wing assembly
    1.
    发明授权
    Determinant wing assembly 有权
    决定性翼组件

    公开(公告)号：US08695219B2

    公开(公告)日：2014-04-15

    申请号：US12416024

    申请日：2009-03-31

    申请人： Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    发明人： Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    IPC分类号： B21D53/88 ,  B64C1/00

    CPC分类号： B64F5/10 ,  Y10T29/49622 ,  Y10T29/49778 ,  Y10T29/4978 ,  Y10T29/49895 ,  Y10T29/49998 ,  Y10T29/53983

    摘要： A method and apparatus for manufacturing wings includes a fixture that holds wing panels for drilling and edge trimming by accurate numerically controlled machine tools using original numerical part definition records, utilizing spatial relationships between key features of detail parts or subassemblies as represented by coordination features machined into the parts and subassemblies, thereby making the parts and subassemblies intrinsically determinant of the dimensions and contour of the wing. Spars are attached to the wing panel using the coordination holes to locate the spars accurately on the panel in accordance with the original engineering design, and in-spar ribs are attached to rib posts on the spar using accurately drilled coordination holes in the ends of the rib and in the rib post. The wing contour is determined by the configuration of the spars and ribs rather than by any conventional hard tooling which determines the wing contour in conventional processes.

    摘要翻译： 用于制造机翼的方法和装置包括一个固定装置，其通过使用原始数字部分定义记录的精确的数控机床来保持用于钻孔和边缘修剪的翼板，利用细节部件或子组件的关键特征之间的空间关系，由协调特征加工成 部件和组件，从而使部件和组件固有地决定了机翼的尺寸和轮廓。 翼片使用协调孔连接到翼板上，以根据原始工程设计将翼梁准确地定位在面板上，并且翼梁用肋板上的肋柱连接，使用准确钻孔的协调孔 肋骨和肋骨柱。 机翼轮廓由翼梁和肋骨的结构决定，而不是通过任何常规的硬工具来确定传统工艺中的机翼轮廓。

    Autonomous carrier for continuously moving wing assembly line
    5.
    发明授权
    Autonomous carrier for continuously moving wing assembly line 有权
    用于连续移动机翼装配线的自主承运人

    公开(公告)号：US08539658B2

    公开(公告)日：2013-09-24

    申请号：US12550666

    申请日：2009-08-31

    申请人： Clayton L. Munk

    发明人： Clayton L. Munk

    IPC分类号： B23Q3/00

    CPC分类号： B25B11/02 ,  B23P2700/01 ,  B64F5/10 ,  Y10T29/53961 ,  Y10T29/53978

    摘要： A method and apparatus for moving a structure. The structure is supported on a carrier. The carrier comprises a platform having a first side and a second side, a movement system associated with the first side and configured to move the platform on a surface, a support system associated with the second side of the platform and configured to support the structure on the platform, and a leveling system configured to substantially maintain the structure in a desired orientation during movement of the platform on the surface. The carrier is moved with the structure over the surface. At least one of the movement system and the support system is adjusted to substantially maintain the structure in the desired orientation.

    摘要翻译： 一种用于移动结构的方法和装置。 运营商支持该结构。 载体包括具有第一侧和第二侧的平台，与第一侧相关联并且被配置为在平台上移动平台的移动系统，与平台的第二侧相关联并被配置为将结构支撑在 所述平台以及调平系统被配置为在所述平台在所述表面上移动期间将所述结构基本上保持在期望的取向。 载体以表面的结构移动。 移动系统和支撑系统中的至少一个被调节以基本上将结构保持在期望的方位。

    Autonomous Carrier for Continuously Moving Wing Assembly Line
    7.
    发明申请
    Autonomous Carrier for Continuously Moving Wing Assembly Line 有权
    用于连续移动翼组装线的自主承载

    公开(公告)号：US20110054694A1

    公开(公告)日：2011-03-03

    申请号：US12550666

    申请日：2009-08-31

    申请人： Clayton L. Munk

    发明人： Clayton L. Munk

    IPC分类号： G05D3/12 ,  G05B13/02

    CPC分类号： B25B11/02 ,  B23P2700/01 ,  B64F5/10 ,  Y10T29/53961 ,  Y10T29/53978

    摘要： A method and apparatus for moving a structure. The structure is supported on a carrier. The carrier comprises a platform having a first side and a second side, a movement system associated with the first side and configured to move the platform on a surface, a support system associated with the second side of the platform and configured to support the structure on the platform, and a leveling system configured to substantially maintain the structure in a desired orientation during movement of the platform on the surface. The carrier is moved with the structure over the surface. At least one of the movement system and the support system is adjusted to substantially maintain the structure in the desired orientation.

    摘要翻译： 一种用于移动结构的方法和装置。 运营商支持该结构。 载体包括具有第一侧和第二侧的平台，与第一侧相关联并且被配置为在平台上移动平台的移动系统，与平台的第二侧相关联并被配置为将结构支撑在 所述平台以及调平系统被配置为在所述平台在所述表面上移动期间将所述结构基本上保持在期望的取向。 载体以表面的结构移动。 移动系统和支撑系统中的至少一个被调节以基本上将结构保持在期望的方位。

    Method of manufacturing a wing
    8.
    发明授权
    Method of manufacturing a wing 有权
    制造翼的方法

    公开(公告)号：US07509740B2

    公开(公告)日：2009-03-31

    申请号：US10867398

    申请日：2004-06-14

    申请人： Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    发明人： Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    IPC分类号： B21D53/92

    CPC分类号： B64F5/10 ,  Y10T29/49622 ,  Y10T29/49778 ,  Y10T29/4978 ,  Y10T29/49895 ,  Y10T29/49998 ,  Y10T29/53983

    摘要： A method and apparatus for manufacturing wings includes a fixture that holds wing panels for drilling and edge trimming by accurate numerically controlled machine tools using original numerical part definition records, utilizing spatial relationships between key features of detail parts or subassemblies as represented by coordination features machined into the parts and subassemblies, thereby making the parts and subassemblies intrinsically determinant of the dimensions and contour of the wing. Spars are attached to the wing panel using the coordination holes to locate the spars accurately on the panel in accordance with the original engineering design, and in-spar ribs are attached to rib posts on the spar using accurately drilled coordination holes in the ends of the rib and in the rib post. The wing contour is determined by the configuration of the spars and ribs rather than by any conventional hard tooling which determines the wing contour in conventional processes.

    摘要翻译： 用于制造机翼的方法和装置包括一个固定装置，其通过使用原始数字部分定义记录的精确的数控机床来保持用于钻孔和边缘修剪的翼板，利用细节部件或子组件的关键特征之间的空间关系，由协调特征加工成 部件和组件，从而使部件和组件固有地决定了机翼的尺寸和轮廓。 翼片使用协调孔连接到翼板上，以根据原始工程设计将翼梁准确地定位在面板上，并且翼梁用肋板上的肋柱连接，使用准确钻孔的协调孔 肋骨和肋骨柱。 机翼轮廓由翼梁和肋骨的结构决定，而不是通过任何常规的硬工具来确定传统工艺中的机翼轮廓。

    Determinant wing assembly
    9.
    发明授权
    Determinant wing assembly 有权
    决定性翼组件

    公开(公告)号：US06314630B1

    公开(公告)日：2001-11-13

    申请号：US09155251

    申请日：1998-09-21

    申请人： Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    发明人： Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    IPC分类号： B23Q1700

    CPC分类号： G05B19/44 ,  B23P21/00 ,  B23P2700/01 ,  B25B5/122 ,  B25B5/163 ,  B25B11/005 ,  B25B11/007 ,  B64C3/18 ,  B64C3/26 ,  B64F5/10 ,  G05B19/401 ,  G05B19/4083 ,  G05B2219/36503 ,  G05B2219/49136 ,  Y02P90/265 ,  Y10T29/49764 ,  Y10T29/49885 ,  Y10T29/49895 ,  Y10T29/49904

    摘要： A method and apparatus for manufacturing wings includes a fixture that holds wing panels for drilling and edge trimming by accurate numerically controlled machine tools using original numerical part definition records, utilizing spatial relationships between key features of detail parts or subassemblies as represented by coordination features machined into the parts and subassemblies, thereby making the parts and subassemblies intrinsically determinant of the dimensions and contour of the wing. Spars are attached to the wing panel using the coordination holes to locate the spars accurately on the panel in accordance with the original engineering design, and in-spar ribs are attached to rib posts on the spar using accurately drilled coordination holes in the ends of the rib and in the rib post. The wing contour is determined by the configuration of the spars and ribs rather than by any conventional hard tooling which determines the wing contour in conventional processes.

    摘要翻译： 用于制造机翼的方法和装置包括一个固定装置，其通过使用原始数字部分定义记录的精确的数控机床来保持用于钻孔和边缘修剪的翼板，利用细节部件或子组件的关键特征之间的空间关系，由协调特征加工成 部件和组件，从而使部件和组件固有地决定了机翼的尺寸和轮廓。 翼片使用协调孔连接到翼板上，以根据原始工程设计将翼梁准确地定位在面板上，并且翼梁用肋板上的肋柱连接，使用准确钻孔的协调孔 肋骨和肋骨柱。 机翼轮廓由翼梁和肋骨的结构决定，而不是通过任何常规的硬工具来确定传统工艺中的机翼轮廓。