Patents by Inventor David E. Strand
David E. Strand has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 8695219Abstract: 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.Type: GrantFiled: March 31, 2009Date of Patent: April 15, 2014Assignee: The Boeing CompanyInventors: Clayton L. Munk, Paul E. Nelson, David E. Strand
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Publication number: 20090228134Abstract: 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.Type: ApplicationFiled: March 31, 2009Publication date: September 10, 2009Applicant: THE BOEING COMPANYInventors: Clayton L. Munk, Paul E. Nelson, David E. Strand
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Patent number: 7509740Abstract: 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.Type: GrantFiled: June 14, 2004Date of Patent: March 31, 2009Assignee: The Boeing CompanyInventors: Clayton L. Munk, Paul E. Nelson, David E. Strand
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Patent number: 6808143Abstract: 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.Type: GrantFiled: November 13, 2001Date of Patent: October 26, 2004Assignee: The Boeing CompanyInventors: Clayton L. Munk, Paul E. Nelson, David E. Strand
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Patent number: 6718614Abstract: 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.Type: GrantFiled: January 7, 2003Date of Patent: April 13, 2004Assignee: The Boeing CompanyInventors: Paul R. Stone, David E. Strand, Paul E. Nelson
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Patent number: 6625866Abstract: 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.Type: GrantFiled: January 9, 2001Date of Patent: September 30, 2003Assignee: The Boeing CompanyInventors: Paul R. Stone, David E. Strand, Paul E. Nelson
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Publication number: 20030094552Abstract: 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.Type: ApplicationFiled: January 7, 2003Publication date: May 22, 2003Applicant: The Boeing CompanyInventors: Paul R. Stone, David E. Strand, Paul E. Nelson
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Patent number: 6502808Abstract: 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.Type: GrantFiled: September 25, 2000Date of Patent: January 7, 2003Assignee: The Boeing CompanyInventors: Paul R. Stone, David E. Strand, Paul E. Nelson
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Publication number: 20020078545Abstract: 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.Type: ApplicationFiled: November 13, 2001Publication date: June 27, 2002Inventors: Clayton L. Munk, Paul E. Nelson, David E. Strand
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Patent number: 6314630Abstract: 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.Type: GrantFiled: September 21, 1998Date of Patent: November 13, 2001Assignee: The Boeing CompanyInventors: Clayton L. Munk, Paul E. Nelson, David E. Strand
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Publication number: 20010024603Abstract: 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.Type: ApplicationFiled: January 9, 2001Publication date: September 27, 2001Inventors: Paul R. Stone, David E. Strand, Paul E. Nelson
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Patent number: 6170157Abstract: 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.Type: GrantFiled: September 21, 1998Date of Patent: January 9, 2001Assignee: The Boeing CompanyInventors: Clayton L. Munk, Paul E. Nelson, David E. Strand
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Patent number: 6003812Abstract: 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.Type: GrantFiled: June 6, 1995Date of Patent: December 21, 1999Assignee: The Boeing CompanyInventors: Antonio C. Micale, David E. Strand
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Patent number: 5649888Abstract: A system for assembling parts on a sheet to form a panel includes a fixture for holding the sheet and presenting the sheet broadside to a robot. A rack within the reach of the robot holds a plurality of end effectors, each having an interconnect which can be gripped and centered by the robot when it picks up by the end effector. The end effectors include, 1) a drilling end effector having a drill for drilling holes in the sheet on centers determined by movement of the robot; 2) a routing end effector having a router for routing peripheral edge portions of the sheet along lines determined by movement of the router; 3) a probe end effector having a probe for sensing contact with surfaces on an index device mounted on the fixture at a known location to serve as a reference monument.Type: GrantFiled: June 6, 1995Date of Patent: July 22, 1997Assignee: The Boeing CompanyInventors: Antonio C. Micale, David E. Strand
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Patent number: 5615483Abstract: A method and apparatus for manufacturing panels and major airplane fuselage sections, including a reconfigurable fixture that holds panels for routing and drilling 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 holes drilled into the parts and subassemblies and making the parts and subassemblies intrinsically determinate of the dimensions and contour of the assembly.Type: GrantFiled: June 6, 1995Date of Patent: April 1, 1997Assignee: The Boeing CompanyInventors: Antonio C. Micale, David E. Strand
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Patent number: 5560102Abstract: A method and apparatus for manufacturing panels and major airplane fuselage sections, including a reconfigurable fixture that holds panels for routing and drilling 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 holes drilled into the parts and subassemblies and making the parts and subassemblies intrinsically determinate of the dimensions and contour of the assembly.Type: GrantFiled: October 13, 1992Date of Patent: October 1, 1996Assignee: The Boeing CompanyInventors: Antonio C. Micale, David E. Strand
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Patent number: 4380295Abstract: Drills (35), vertically oriented in a row/column array in a drill block (31), are moved in the column direction across a slot (49) located at a loading station (41). As the drills in each partially or fully occupied row reach the slot and drop, drill block movement halts. Thereafter a vertically oriented turn-over tube (51) is moved in the row direction beneath the slot (49). When an occupied drill position is reached, the drill drops into the turn-over tube, tube row movement temporarily halts, and the tube is rotated. The drill slides out of the turn-over tube (51) and down the channel (59) of a measuring station (43) until it hits a movable stop (61). After drill diameter is measured by a pneumatically positioned LVDT (87) and overall drill length is measured by a pneumatically positioned linear potentiometer (69)/proximity detector (PX3) combination, the stop (61) is withdrawn and the drill enters a clamp (95), which grips the adapter shank of the drill.Type: GrantFiled: April 6, 1981Date of Patent: April 19, 1983Assignee: The Boeing CompanyInventors: Mark S. Soderberg, Albert L. Hametner, Herman F. Leppink, David E. Strand