Patents by Inventor Nick S. Evans
Nick S. Evans 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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Publication number: 20200339274Abstract: A method for aligning a removable sensor on a vehicle includes connecting the removable sensor to a sensor mounting device. The method further includes connecting a connector of an alignment apparatus to either (i) the removable sensor such that a spatial reference component of the alignment apparatus has a known position and orientation relative to a current position and orientation of the removable sensor or (ii) a fixed connection location on the vehicle such that the spatial reference component indicates a desired position and orientation of the removable sensor. In addition the method includes adjusting the current position and orientation of the removable sensor by reference to the alignment apparatus to cause the current position and orientation of the removable sensor to match the desired position and orientation of the removable sensor.Type: ApplicationFiled: April 24, 2019Publication date: October 29, 2020Inventors: Kevin S. Callahan, Nick S. Evans, Eric R. Muir
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Patent number: 10818091Abstract: A visualization system using mixed reality provides an “extended view” to the pilot or other crew of an aircraft. The extended view enables the user to visualize obstructed objects projected onto the real world scene viewed by the pilot using an optical the see-through display (OSTD) thus providing the user with greater situational awareness. A LIDAR point cloud model of the environment around the aircraft is generated from two or more laser scanning devices providing a 360 degree panoramic view. The combined point cloud model is aligned with the pilot's real world view based on the pilot's “pose” and projected onto the OSTD as an overlay so that the pilot sees the combined point cloud model in relation to the real world as seen by the pilot. One aspect of the invention is that the raw sensor data from the LIDAR devices is displayed on the actual real-world scene as a point cloud without any further image processing to enhance the user's perception.Type: GrantFiled: January 2, 2019Date of Patent: October 27, 2020Assignee: THE BOEING COMPANYInventors: Nick S. Evans, Mathew T. DeAngelis
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Publication number: 20200233404Abstract: A method of operating an automated machine is provided for inserting wires into grommet cavity locations of an electrical connector to compensate for manufacturing tolerances associated with the electrical connector. The method comprises inserting wires into grommet cavity locations of the electrical connector based upon a plug map having offset values to compensate for manufacturing tolerances associated with the electrical connector. The method may further comprise selecting from a plurality of pre-generated plug maps having offset values the closest matching pre-generated plug map for the electrical connector based upon offset values associated with each of the plurality of pre-generated plugs maps. The selected pre-generated plug map having offset values corresponds to the plug map used to insert wires into grommet cavity locations of the electrical connector.Type: ApplicationFiled: April 6, 2020Publication date: July 23, 2020Applicant: The Boeing CompanyInventors: Eerik J. Helmick, Bradley J. Mitchell, Nick S. Evans
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Publication number: 20200211287Abstract: A visualization system using mixed reality provides an “extended view” to the pilot or other crew of an aircraft. The extended view enables the user to visualize obstructed objects projected onto the real world scene viewed by the pilot using an optical the see-through display (OSTD) thus providing the user with greater situational awareness. A LIDAR point cloud model of the environment around the aircraft is generated from two or more laser scanning devices providing a 360 degree panoramic view. The combined point cloud model is aligned with the pilot's real world view based on the pilot's “pose” and projected onto the OSTD as an overlay so that the pilot sees the combined point cloud model in relation to the real world as seen by the pilot. One aspect of the invention is that the raw sensor data from the LIDAR devices is displayed on the actual real-world scene as a point cloud without any further image processing to enhance the user's perception.Type: ApplicationFiled: January 2, 2019Publication date: July 2, 2020Inventors: Nick S. Evans, Mathew T. DeAngelis
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Publication number: 20200161824Abstract: An automated system for processing an end of a cable. The system includes: a cable delivery system; a cable processing module; a pallet supported by the cable delivery system; a drive wheel rotatably coupled to the pallet; a motor operatively coupled for driving rotation of the drive wheel; and an idler wheel rotatably coupled to the pallet and forming a nip with the drive wheel. The cable processing module includes cable processing equipment configured to perform an operation on an end of a cable and a computer system. The computer system is configured to: (a) cause the drive wheel to rotate in a cable pushing direction to cause a specified length of cable to be inserted into the cable processing equipment; (b) activate the cable processing equipment to perform an operation on the inserted end of the cable; and (c) cause the drive wheel to rotate in a cable pulling direction to cause the specified length of cable to be removed from the cable processing equipment.Type: ApplicationFiled: November 19, 2018Publication date: May 21, 2020Applicant: The Boeing CompanyInventors: Grace L. Duncan, Bradley J. Mitchell, Damien O. Martin, Dinh X. Tran, Eerik J. Helmick, Aphea Ann Thornton, Nick S. Evans, David S. Wright, Lars E. Blacken, Keith M. Cutler
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Publication number: 20200161843Abstract: A shield trim is performed by tearing bunched shield strands circumferentially along a circular edge. The apparatus includes a pair of aligned metal plates that have been drilled through multiple times such that holes of varying diameters pass may be passed through both plates. A cable gripper on the entry side of the device clamps the cable in place. A shield gripper on the rear side of the device closes over the exposed shielding of the cable, and the two plates are pushed together. The shield gripper travels with the rear plate, pushing the shield over the wires and causing the shield to bunch between the two plates. With the two plates pushed together, both grippers open and the cable is pulled free from the device. This pull forces a stress concentration on the shield strands as they are pulled and subsequently torn across the sharp edge of the hole, producing a uniformly trimmed shield.Type: ApplicationFiled: November 19, 2018Publication date: May 21, 2020Applicant: The Boeing CompanyInventors: Grace L. Duncan, Bradley J. Mitchell, Nick S. Evans, Damien O. Martin
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Patent number: 10649442Abstract: A method 500 of operating an automated machine 100 is provided for inserting wires into grommet cavity locations 110 of an electrical connector 112 to compensate for manufacturing tolerances associated with the electrical connector. The method comprises inserting wires into grommet cavity locations of the electrical connector based upon a plug map 300 having offset values to compensate for manufacturing tolerances associated with the electrical connector. The method may further comprise selecting from a plurality of pre-generated plug maps having offset values the closest matching pre-generated plug map for the electrical connector based upon offset values associated with each of the plurality of pre-generated plugs maps. The selected pre-generated plug map having offset values corresponds to the plug map used to insert wires into grommet cavity locations of the electrical connector.Type: GrantFiled: April 25, 2016Date of Patent: May 12, 2020Assignee: The Boeing CompanyInventors: Eerik J. Helmick, Bradley J. Mitchell, Nick S. Evans
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Patent number: 10587101Abstract: A cable processing apparatus including a frame; a cable guide coupled to the frame; a first cable clamp adjacent the cable guide; a second cable clamp adjacent the cable guide where the first cable clamp is disposed between the cable guide and the second cable clamp; and a controller configured to move the second cable clamp to a clamped position such that a cable extending through the cable guide is clamped by the second cable clamp, move the second cable clamp, relative to the cable guide, in a direction extending along the cable such that a first portion of the insulation is removed from the cable at the first score to expose shielding of the cable, and move the second cable clamp, relative to the first cable clamp, in the direction extending along the cable to cut the shielding to expose one or more conductor of the cable.Type: GrantFiled: March 29, 2017Date of Patent: March 10, 2020Assignee: The Boeing CompanyInventors: Damien O. Martin, Nick S. Evans, Bradley J. Mitchell, Eerik J. Helmick
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Publication number: 20200048028Abstract: A method of reducing entanglement of wires includes receiving, at a tray, one or more first wires of a first wire group from a wire feed system of a wire processing machine. In addition, the method includes receiving, at the tray, one or more second wires of a second wire group from the wire feed system after receiving the first wire group at the tray. The method further includes physically separating, using a separator device associated with the tray, at least a portion of the first wire group from the second wire group. The method also includes moving the second wire group relative to the first wire group, reducing movement of at least a portion of the first wire group relative to a tray surface during movement of the second wire group relative to the first wire group.Type: ApplicationFiled: October 16, 2019Publication date: February 13, 2020Inventors: Eerik J. Helmick, Bradley J. Mitchell, Nick S. Evans, Damien O. Martin, Aphea Ann Thornton
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Publication number: 20200048027Abstract: A method of reducing entanglement of wires includes receiving from a wire feed system of a wire processing machine a first wire on a tray surface providing a wire-to-surface coefficient of friction between the tray surface and the first wire. In addition, the method includes receiving from the wire feed system a second wire at least partially on top of the first wire, the wire-to-surface coefficient of friction being higher than a wire-to-wire coefficient of friction between the first wire and the second wire. The method also includes moving the second wire relative to the first wire, and reducing movement of at least a portion of the first wire relative to the tray surface during movement of the second wire relative to the first wire due to the wire-to-surface coefficient of friction being higher than the wire-to-wire coefficient of friction.Type: ApplicationFiled: October 16, 2019Publication date: February 13, 2020Inventors: Bradley J. Mitchell, Nick S. Evans, Damien O. Martin, Aphea Ann Thornton, Eerik J. Helmick
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Publication number: 20200027362Abstract: Example implementations relate to autonomous airport runway navigation. An example system includes a first sensor and a second sensor coupled to an aircraft at a first location and a second location, respectively, and a computing system configured to receive sensor data from one or both of the first sensor and the second sensor to detect airport markings positioned proximate a runway. The computing system is further configured to identify a centerline of the runway based on the airport markings and receive sensor data from both of the first sensor and the second sensor to determine a lateral displacement that represents a distance between a reference point of the aircraft and the centerline of the runway. The computing system is further configured to control instructions that indicate adjustments for aligning the reference point of the aircraft with the centerline of the runway during subsequent navigation of the aircraft.Type: ApplicationFiled: July 19, 2018Publication date: January 23, 2020Inventors: Stephen Dame, Dragos D. Margineantu, Nick S. Evans, Tyler C. Staudinger, Brian K. Rupnik, Matthew A. Moser, Kevin S. Callahan, Brain T. Whitehead
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Patent number: 10501284Abstract: A wire processing system includes a tray having at least one tray surface configured to sequentially receive a first wire and a second wire from a wire feed system of a wire processing machine. The tray surface has a surface feature configured to provide a wire-to-surface coefficient of friction between the tray surface and the first wire higher than a wire-to-wire coefficient of friction between the first wire and the second wire laying on top of the first wire. The wire-to-surface coefficient of friction reduces movement of at least a portion of the first wire relative to the tray surface during movement of the second wire relative to the first wire.Type: GrantFiled: June 22, 2016Date of Patent: December 10, 2019Assignee: The Boeing CompanyInventors: Eerik J. Helmick, Bradley J. Mitchell, Nick S. Evans, Damien O. Martin, Aphea Ann Thornton
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Patent number: 10501283Abstract: A wire processing system includes a tray having at least one tray surface configured to sequentially receive a first wire and a second wire from a wire feed system of a wire processing machine. The tray surface has a surface feature configured to provide a wire-to-surface coefficient of friction between the tray surface and the first wire higher than a wire-to-wire coefficient of friction between the first wire and the second wire laying on top of the first wire. The wire-to-surface coefficient of friction reduces movement of at least a portion of the first wire relative to the tray surface during movement of the second wire relative to the first wire.Type: GrantFiled: June 22, 2016Date of Patent: December 10, 2019Assignee: The Boeing CompanyInventors: Bradley J. Mitchell, Nick S. Evans, Damien O. Martin, Aphea Ann Thornton, Eerik J. Helmick
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Patent number: 10350878Abstract: A system for additively manufacturing a composite part comprises a delivery guide, movable relative to a surface. The delivery guide is configured to deposit at least a segment of a continuous flexible line along a print path. The continuous flexible line comprises a non-resin component and a thermosetting-resin component. The thermosetting-resin component comprises a first part and a second part. The non-resin component comprises a first element and a second element. The system further comprises a first resin-part applicator, configured to apply the first part to the first element, and a second resin-part applicator, configured to apply the second part to the second element. The system also comprises a feed mechanism, configured to pull the first element through the first resin-part applicator, to pull the second element through the second resin-part applicator, and to push the continuous flexible line out of the delivery guide.Type: GrantFiled: March 7, 2016Date of Patent: July 16, 2019Assignee: The Boeing CompanyInventors: Nick S. Evans, Faraòn Torres, Ryan G. Ziegler, Samuel F. Harrison, Ciro J. Grijalva, III, Hayden S. Osborn
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Patent number: 10352345Abstract: An adhesive-bonded attachment device includes a mounting base including a mounting surface, a structural adhesive disposed on the mounting surface, and a pressure-sensitive adhesive disposed on the mounting surface bordering the structural adhesive, wherein the structural adhesive and the pressure-sensitive adhesive define a bonding surface configured to be bonded to a contact surface of a structure, and an attachment feature disposed on said mounting base.Type: GrantFiled: December 5, 2016Date of Patent: July 16, 2019Assignee: The Boeing CompanyInventors: Nick S. Evans, Lenny E. Lay
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Patent number: 10343355Abstract: A system for additively manufacturing a composite part (102) comprises a delivery guide, movable relative to a surface. The delivery guide is configured to deposit at least a segment of a continuous flexible line along a print path. The continuous flexible line comprises a non-resin component and a thermosetting resin component that comprises a first part and a second part of a thermosetting resin. The print path is stationary relative to the surface. The delivery guide comprises a first inlet configured to receive the non-resin component, and a second inlet configured to receive at least the first part of the thermosetting resin. The delivery guide is further configured to apply the first part and the second part of the thermosetting resin to the non-resin component. The system 100 further comprises a feed mechanism, configured to push the continuous flexible line out of the delivery guide.Type: GrantFiled: January 14, 2016Date of Patent: July 9, 2019Assignee: The Boeing CompanyInventors: Nick S. Evans, Faraón Torres, Ryan G. Ziegler, Samuel F. Harrison, Ciro J. Grijalva, III, Hayden S. Osborn
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Patent number: 10343330Abstract: A system for additively manufacturing a composite part is disclosed. The system comprises a delivery guide, movable relative to a surface. The delivery guide is configured to deposit at least a segment of a continuous flexible line along a print path. The print path is stationary relative to the surface. The continuous flexible line comprises a non-resin component and a thermosetting-epoxy-resin component that is partially cured. The system also comprises a feed mechanism, configured to push the continuous flexible line through the delivery guide. The system further comprises a cooling system, configured to maintain the thermosetting-epoxy-resin component of the continuous flexible line below a threshold temperature prior to depositing the segment of the continuous flexible along the print path via the delivery guide.Type: GrantFiled: November 3, 2015Date of Patent: July 9, 2019Assignee: The Boeing CompanyInventors: Nick S. Evans, Faraón Torres, Ryan G. Ziegler, Samuel F. Harrison, Ciro J. Grijalva, III, Hayden S. Osborn
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Publication number: 20190151995Abstract: A wire guide and a laser wire-processing device that includes a wire guide are provided. The laser wire-processing device includes a housing and an aperture in a side of the housing, wherein the aperture defines a longitudinal axis that is substantially perpendicular to the aperture. The laser wire-processing device also includes a backstop arranged in the housing and aligned with the longitudinal axis, the backstop defining a wire-contact surface in a facing relationship with the aperture. The laser wire-processing device also includes a wire guide arranged in the housing to manipulate a wire inserted through the aperture into a desired position relative to the longitudinal axis between the aperture and the backstop. The laser wire-processing device also includes a laser operable to direct a laser beam toward an insulation layer of the wire. The wire guide could be a tube arranged in the device or a backstop guide.Type: ApplicationFiled: January 3, 2019Publication date: May 23, 2019Inventors: Nick S. Evans, Bradley J. Mitchell, Mark Blumenkrantz
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Patent number: 10279580Abstract: A method of additively manufacturing a composite part comprises depositing a segment of a continuous flexible line along a print path. The continuous flexible line comprises a non-resin component and further comprises a photopolymer-resin component that is uncured. The method further comprises delivering a predetermined or actively determined amount of curing energy at least to a portion of the segment of the continuous flexible line at a controlled rate while advancing the continuous flexible line toward the print path and after the segment of the continuous flexible line is deposited along the print path to at least partially cure at least the portion of the segment of the continuous flexible line.Type: GrantFiled: August 31, 2015Date of Patent: May 7, 2019Assignee: The Boeing CompanyInventors: Nick S. Evans, Faraón Torres, Ryan G. Ziegler, Samuel F. Harrison, Ciro J. Grijalva, III, Hayden S. Osborn
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Publication number: 20190091929Abstract: An extruder for depositing a material includes an extruder body including an extruder drive system and defining a body axis, and an extruder nozzle. The extruder nozzle includes a nozzle tip defining an exit orifice, a reconfigurable arm defining a material path in fluid communication with the exit orifice, the reconfigurable arm including a proximal end coupled to the extruder body and coaxial with the body axis, and a distal end coupled to the nozzle tip, and a plurality of actuators operatively associated with the reconfigurable arm and configured to move the reconfigurable arm between an initial configuration, in which the distal end of the reconfigurable arm is coaxial with the body axis, to a displaced configuration. In the displaced configuration, the distal end of the reconfigurable arm is at least one of positioned offset from the body axis and oriented at an angle relative to the body axis.Type: ApplicationFiled: September 27, 2017Publication date: March 28, 2019Applicant: The Boeing CompanyInventors: Samuel Harrison, Nick S. Evans, Faraon Torres, Michael P. Kozar, Mark S. Wilenski