中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

42 records (took 0.02 seconds)

    Vacuum cup with precision hard stop
    2.
    发明授权
    Vacuum cup with precision hard stop 有权

    公开(公告)号：US06502808B1

    公开(公告)日：2003-01-07

    申请号：US09669322

    申请日：2000-09-25

    Applicant: Paul R. Stone ,  David E. Strand ,  Paul E. Nelson

    Inventor： Paul R. Stone ,  David E. Strand ,  Paul E. Nelson

    IPC: B23B3130

    CPC classification number: B25B11/005 ,  B23B31/307 ,  Y10T29/49998

    Abstract: A method and apparatus for holding a part on a fixture in a precisely known predetermined position includes pressing a surface of the part against a vacuum head and sealing an annular elastomeric sealing ring against the part surface. A valve button of a valve is engaged by the part surface to open the valve and establish communication between a vacuum source. The part is pulled by the vacuum against a hard stop in the vacuum head having a fixed precisely known relationship to said vacuum head reference surface. The hard-stop can be mounted in the base of the vacuum head for pivoting about at least one axis to self-align the hard-stop face with the part face.

    Vacuum cup with precision hard stop
    3.
    发明授权
    Vacuum cup with precision hard stop 有权
    真空杯精密硬盘

    公开(公告)号：US06718614B2

    公开(公告)日：2004-04-13

    申请号：US10338568

    申请日：2003-01-07

    Applicant: Paul R. Stone ,  David E. Strand ,  Paul E. Nelson

    Inventor： Paul R. Stone ,  David E. Strand ,  Paul E. Nelson

    IPC: B23Q700

    CPC classification number: B25B11/005 ,  B23B31/307 ,  Y10T29/49998

    Abstract: A method and apparatus for holding a part on a fixture in a precisely known predetermined position includes pressing a surface of the part against a vacuum head and sealing an annular elastomeric sealing ring against the part surface. A valve button of a valve is engaged by the part surface to open the valve and establish communication between a vacuum source. The part is pulled by the vacuum against a hard stop in the vacuum head having a fixed precisely known relationship to said vacuum head reference surface. The hard-stop can be mounted in the base of the vacuum head for pivoting about at least one axis to self-align the hard-stop face with the part face.

    Abstract translation: 用于将精确保持在精确已知的预定位置的夹具上的零件夹持的方法和装置包括将零件的表面压在真空头上并将环形弹性体密封环密封在零件表面上。 阀的阀按钮通过部件表面接合以打开阀门并建立真空源之间的连通。 该部件通过真空被吸附在具有与所述真空头参考表面固定的精确已知关系的真空头中的硬止动件上。 硬止动件可以安装在真空头的基座中，用于围绕至少一个轴线枢转以使硬止动面与部件面自对准。

    Determinant Wing Assembly
    4.
    发明申请
    Determinant Wing Assembly 有权
    决定性翼组件

    公开(公告)号：US20090228134A1

    公开(公告)日：2009-09-10

    申请号：US12416024

    申请日：2009-03-31

    Applicant: Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    Inventor： Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    IPC: G06F19/00

    CPC classification number: B64F5/10 ,  Y10T29/49622 ,  Y10T29/49778 ,  Y10T29/4978 ,  Y10T29/49895 ,  Y10T29/49998 ,  Y10T29/53983

    Abstract: 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.

    Abstract translation: 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
    5.
    发明授权
    Determinant wing assembly 有权
    决定性翼组件

    公开(公告)号：US06808143B2

    公开(公告)日：2004-10-26

    申请号：US10001536

    申请日：2001-11-13

    Applicant: Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    Inventor： Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    IPC: B64C326

    CPC classification number: 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

    Abstract: 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.

    Abstract translation: 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
    7.
    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

    Applicant: Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    Inventor： Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    IPC: B21D53/88 ,  B64C1/00

    CPC classification number: B64F5/10 ,  Y10T29/49622 ,  Y10T29/49778 ,  Y10T29/4978 ,  Y10T29/49895 ,  Y10T29/49998 ,  Y10T29/53983

    Abstract: 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.

    Abstract translation: 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。

    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

    Applicant: Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    Inventor： Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    IPC: B21D53/92

    CPC classification number: B64F5/10 ,  Y10T29/49622 ,  Y10T29/49778 ,  Y10T29/4978 ,  Y10T29/49895 ,  Y10T29/49998 ,  Y10T29/53983

    Abstract: 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.

    Abstract translation: 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

    Applicant: Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    Inventor： Clayton L. Munk ,  Paul E. Nelson ,  David E. Strand

    IPC: B23Q1700

    CPC classification number: 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

    Abstract: 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.

    Abstract translation: 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。

    Aircraft control surface actuation system with helical actuation path
    10.
    发明授权
    Aircraft control surface actuation system with helical actuation path 有权
    具有螺旋驱动路径的飞机控制面驱动系统

    公开(公告)号：US08590834B1

    公开(公告)日：2013-11-26

    申请号：US13295187

    申请日：2011-11-14

    Applicant: Paul E. Nelson

    Inventor： Paul E. Nelson

    IPC: B64C3/50

    CPC classification number: B64C13/28

    Abstract: An aircraft control surface actuation system including a wing member and an aircraft control surface hingedly connected to the wing member along a pivot axis, wherein the aircraft control surface is configured to axially move along the pivot axis when the aircraft control surface pivots relative to the wing member about the pivot axis.

    Abstract translation: 飞行器控制表面致动系统，包括翼构件和飞行器控制表面，所述翼构件和飞行器控制表面沿着枢转轴线铰接地连接到翼构件，其中飞行器控制表面构造成当飞行器控制表面相对于翼片枢转时沿着枢转轴线轴向移动 关于枢轴的成员。

Patent Agency Ranking