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公开(公告)号：US06625866B2
公开(公告)日：2003-09-30
申请号：US09757680
申请日：2001-01-09
Applicant: Paul R. Stone , David E. Strand , Paul E. Nelson
Inventor： Paul R. Stone , David E. Strand , Paul E. Nelson
IPC: B23P1100
CPC classification number: B21J15/14 , B23P21/00 , B23P2700/01 , B64C3/18 , B64C3/26 , B64F5/10 , G05B19/4083 , G05B19/44 , G05B2219/36503 , G05B2219/49136 , Y10T29/49895 , Y10T29/49998 , Y10T29/5397 , Y10T29/53978 , Y10T409/303808 , Y10T409/306944 , Y10T409/307336 , Y10T428/12
Abstract: A method and apparatus for manufacturing large, semi-flexible metal components includes a fixture that holds the component blank in a desired position for manufacturing operations 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 part.
Abstract translation: 用于制造大型半柔性金属部件的方法和装置包括：通过使用原始数字部件定义记录的精密数控机床将部件坯料保持在期望位置以进行制造操作的夹具，利用细部件的关键特征之间的空间关系 或子组件，其由加工到部件和子组件中的协调特征表示，从而使部件和组件固有地决定部件的尺寸和轮廓。
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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.
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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。
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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
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。
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公开(公告)号：US06170157B2
公开(公告)日：2001-01-09
申请号：US09155236
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: B21D5388
CPC classification number: B64C3/185 , B23P21/00 , B23P2700/01 , B64C3/26 , B64F5/10 , G05B19/4083 , G05B19/44 , G05B2219/36503 , G05B2219/49136 , Y10T29/49622 , Y10T29/49764 , Y10T29/49954 , Y10T29/53983
Abstract: A method and apparatus for manufacturing wing spars includes a fixture that holds spar webs 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.
Abstract translation: 一种用于制造翼梁的方法和装置包括：通过使用原始数字部件定义记录的精确的数控机床保持用于钻孔和边缘修剪的翼梁的固定装置，利用加工的协调特征所表示的细节部件或子组件的关键特征之间的空间关系 进入部件和组件，从而使部件和组件固有地决定了机翼的尺寸和轮廓。
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Patent Agency Ranking
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。
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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。
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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。
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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。
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公开(公告)号：US6003812A
公开(公告)日：1999-12-21
申请号：US471664
申请日：1995-06-06
Applicant: Antonio C. Micale , David E. Strand
Inventor： Antonio C. Micale , David E. Strand
CPC classification number: B64C1/12 , B23P21/00 , B23Q35/02 , B25J9/1687 , B64C1/061 , B64C1/064 , B64F5/0009 , G05B19/41805 , B23P2700/01 , G05B2219/35012 , G05B2219/39468 , G05B2219/45064 , G05B2219/45197 , Y02P90/04 , Y02P90/08 , Y02P90/087 , Y02P90/16 , Y02P90/265 , Y10T29/49622 , Y10T29/49629 , Y10T29/49771 , Y10T29/4978 , Y10T29/49956 , Y10T29/49996 , Y10T29/49998 , Y10T408/03 , Y10T409/303752 , Y10T409/304144 , Y10T483/13 , Y10T483/138
Abstract: An airplane fuselage panel including a sheet having peripheral edges routed on routing surfaces, while the sheet is held immobile on a fixture, using a routing end effector carried by a precision computer controlled robot that is directed to the routing surfaces using a digital dataset taken directly from digital engineering part definition records. The sheet has coordination holes drilled while on the fixture using a drilling end effector carried by the precision computer controlled robot that is directed to drilling locations using the digital dataset taken directly from the digital engineering part definition records to accurately locate the hole locations relative to the peripheral edges. The airplane fuselage panel also includes parts, including stringers, stringer clips and shear ties, each having coordination holes drilled by computer controlled drills at locations that will match with corresponding coordination holes in the sheet, so that the parts will be accurately located in positions called for in the digital engineering part definition records when the coordination holes in the parts and the coordination holes in the sheet are aligned and the parts are riveted to the sheet in the accurately located positions.
Abstract translation: 一种飞机机身面板，其包括具有在路线表面上布置的外围边缘的片材，同时使用由精确计算机控制的机器人承载的路由末端执行器将片材固定在固定装置上，该机器人使用直接取得的数字数据集指向路线表面 从数字工程部分定义记录。 该片材在固定装置上使用由精密计算机控制的机器人承载的钻孔末端执行器钻出的协调孔，其使用直接从数字工程部件定义记录取得的数字数据集定向到钻孔位置，以精确地定位相对于 外围边缘。 飞机机身面板还包括部件，包括桁条，桁条夹和剪切连接件，每个部件具有通过计算机控制的钻头在与片材中相应的协调孔匹配的位置钻出的协调孔，使得部件将被准确地位于称为 用于在数字工程部件定义记录中，当部件中的协调孔和片材中的协调孔对准并且部件在准确定位的位置铆接到片材上时。
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