Patents by Inventor Joseph A Marshall, IV
Joseph A Marshall, IV 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: 10478999Abstract: Cells of a composite cell array are cured by placing tool blocks in the cells and inserting thermally conductive elements in each of the tool blocks. The thermally conductive elements are convectively heated by a flow of hot air. The heated conductive elements conduct heat to the tooling blocks, which then conduct heat to the cells to cure the composite and adhesive.Type: GrantFiled: January 25, 2016Date of Patent: November 19, 2019Assignee: The Boeing CompanyInventors: Joseph Lawrence Hafenrichter, Joseph A. Marshall, IV
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Patent number: 10118712Abstract: The disclosure provides in one embodiment an electrical conductor pathway system for diverting an electric charge. The electrical conductor pathway system includes a substrate having a first surface to be printed on and having one or more grounding points. The electrical conductor pathway system further includes a direct write conductive material pattern printed directly onto the first surface via a direct write printing process. The direct write conductive material pattern forms one or more electrical pathways interconnected with the one or more grounding points. The one or more electrical pathways interconnected with the one or more grounding points divert the electric charge from the first surface to the one or more grounding points.Type: GrantFiled: March 31, 2016Date of Patent: November 6, 2018Assignee: The Boeing CompanyInventors: Victoria L. Garcia, Mark J. Gardner, Otis F. Layton, Jeffrey Lynn Duce, Joseph A. Marshall, IV
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Patent number: 9736888Abstract: Described herein is a composite panel that includes a first layer made from an electrically non-conductive material. The composite panel also includes a resistance heater printed onto the first layer. Further, the composite panel includes a second layer adjacent the resistance heater, the resistance heater being positioned between the first layer and the second layer. The second layer is made from an electrically non-conductive material.Type: GrantFiled: March 12, 2015Date of Patent: August 15, 2017Assignee: The Boeing CompanyInventors: Jeffrey L. Duce, Joseph A. Marshall, IV, Ashley House, Jason Turner
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Patent number: 9515393Abstract: Systems and methods according to the present disclosure for assembling conformal arrays utilize an outer tool for insertion into an open cell of a conformal array, an inner tool for insertion into the outer tool, and an adhesive source for delivering adhesive to the edges of the open cell via the inner tool and the outer tool. An assembled conformal array includes adhesive extending along the edges of the open cell.Type: GrantFiled: October 27, 2014Date of Patent: December 6, 2016Assignee: The Boeing CompanyInventors: Joseph A. Marshall, IV, Joseph Lawrence Hafenrichter, Manny Salazar Urcia, Jr., Paul Chih-Yung Chang
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Publication number: 20160270152Abstract: Described herein is a composite panel that includes a first layer made from an electrically non-conductive material. The composite panel also includes a resistance heater printed onto the first layer. Further, the composite panel includes a second layer adjacent the resistance heater, the resistance heater being positioned between the first layer and the second layer. The second layer is made from an electrically non-conductive material.Type: ApplicationFiled: March 12, 2015Publication date: September 15, 2016Inventors: Jeffrey L. Duce, Joseph A. Marshall, IV, Ashley House, Jason Turner
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Publication number: 20160214735Abstract: The disclosure provides in one embodiment an electrical conductor pathway system for diverting an electric charge. The electrical conductor pathway system includes a substrate having a first surface to be printed on and having one or more grounding points. The electrical conductor pathway system further includes a direct write conductive material pattern printed directly onto the first surface via a direct write printing process. The direct write conductive material pattern forms one or more electrical pathways interconnected with the one or more grounding points. The one or more electrical pathways interconnected with the one or more grounding points divert the electric charge from the first surface to the one or more grounding points.Type: ApplicationFiled: March 31, 2016Publication date: July 28, 2016Inventors: Victoria L. Garcia, Mark J. Gardner, Otis F. Layton, Jeffrey Lynn Duce, Joseph A. Marshall, IV
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Publication number: 20160136849Abstract: Cells of a composite cell array are cured by placing tool blocks in the cells and inserting thermally conductive elements in each of the tool blocks. The thermally conductive elements are convectively heated by a flow of hot air. The heated conductive elements conduct heat to the tooling blocks, which then conduct heat to the cells to cure the composite and adhesive.Type: ApplicationFiled: January 25, 2016Publication date: May 19, 2016Inventors: Joseph Lawrence Hafenrichter, Joseph A. Marshall, IV
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Patent number: 9318812Abstract: In one embodiment a method to form a load bearing antenna aperture comprises forming a honeycomb core structure having a plurality of wall sections, the wall sections including electromagnetic radiating elements, and wherein lower surfaces of the wall sections defines a first surface and upper surfaces of the wall sections define a second surface, positioning a back skin to the first surface of the honeycomb core structure with an adhesive layer which comprises a layer of adhesive film and a paste adhesive disposed on the layer of adhesive film. Other embodiments are disclosed.Type: GrantFiled: April 19, 2013Date of Patent: April 19, 2016Assignee: THE BOEING COMPANYInventors: Douglas A. McCarville, Joseph A. Marshall, IV, Manny S. Urcia, Otis F. Layton
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Patent number: 9270016Abstract: A method and apparatus comprising a resin layer, a number of conductive elements, and a number of layers of reinforcement material. The number of conductive elements is on the resin layer. The number of conductive elements has a configuration that forms an antenna system. The number of layers of reinforcement material forms a reinforcement for a composite structure, and at least a portion of the resin layer forms a matrix for the composite structure.Type: GrantFiled: July 15, 2011Date of Patent: February 23, 2016Assignee: THE BOEING COMPANYInventors: Matthew A. Stoneback, Joseph A. Marshall, IV, Daniel Joseph Sego, Otis Franklin Layton, Kevin O'Brien Gaw
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Patent number: 9242440Abstract: Cells of a composite cell array are cured by placing tool blocks in the cells and inserting thermally conductive elements in each of the tool blocks. The thermally conductive elements are convectively heated by a flow of hot air. The heated conductive elements conduct heat to the tooling blocks, which then conduct heat to the cells to cure the composite and adhesive.Type: GrantFiled: May 16, 2013Date of Patent: January 26, 2016Assignee: THE BOEING COMPANYInventors: Joseph Lawrence Hafenrichter, Joseph A. Marshall, IV
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Patent number: 9190727Abstract: A structural wideband aperture assembly and methods are presented. A non-conductive structural backsheet comprises electrical vias. A structural egg-crate core comprises a grid of core strips coupled to the non-conductive structural backsheet and is configured substantially perpendicular to the non-conductive structural backsheet around open boxes. A non-structural grid of antenna feed cards is configured substantially perpendicular to the non-conductive structural backsheet and crosses the core strips. A non-structural grid of antenna feed cards comprises intersections configured within the open boxes, and electronic feed-lines aligned with the electrical vias. Antenna array unit cells comprising antenna cards coupled to the non-structural grid of antenna feed cards and configured to fit within the open boxes.Type: GrantFiled: October 1, 2013Date of Patent: November 17, 2015Assignee: The Boeing CompanyInventors: Manny S. Urcia, Charles W. Manry, Jr., Joseph A. Marshall, IV, Tai A. Lam, Otis F. Layton
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Patent number: 9127597Abstract: Concepts and technologies are disclosed herein for a sensor system for detecting, characterizing, monitoring, and analyzing data. According to some embodiments disclosed herein, a monitoring system is configured to obtain data from a sensor system. The sensor system includes two or more sensors and can indicate an operating state detected at a monitored structure by the sensors. The monitoring system also obtains operational data including a threshold value for the sensors and an expected value for the sensors. The monitoring system is configured to adjust the thresholds based, at least partially, upon the operational data to obtain an adjusted threshold value, and to compare the data value to the adjusted threshold. The monitoring system can determine if the monitored structure is operating in an alarm condition.Type: GrantFiled: September 23, 2011Date of Patent: September 8, 2015Assignee: The Boeing CompanyInventors: Kathryn A. Masiello, Robert Steven Wright, Jeffrey Lynn Duce, Bradley J. Mitchell, Joseph A. Marshall, IV
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Patent number: 9059517Abstract: Systems and methods according to the present disclosure for assembling conformal arrays utilize an outer tool for insertion into an open cell of a conformal array, an inner tool for insertion into the outer tool, and an adhesive source for delivering adhesive to the edges of the open cell via the inner tool and the outer tool. An assembled conformal array includes adhesive extending along the edges of the open cell.Type: GrantFiled: September 4, 2012Date of Patent: June 16, 2015Assignee: The Boeing CompanyInventors: Joseph A. Marshall, IV, Joseph Lawrence Hafenrichter, Manny Salazar Urcia, Jr., Paul Chih-Yung Chang
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Publication number: 20150041058Abstract: Systems and methods according to the present disclosure for assembling conformal arrays utilize an outer tool for insertion into an open cell of a conformal array, an inner tool for insertion into the outer tool, and an adhesive source for delivering adhesive to the edges of the open cell via the inner tool and the outer tool. An assembled conformal array includes adhesive extending along the edges of the open cell.Type: ApplicationFiled: October 27, 2014Publication date: February 12, 2015Applicant: The Boeing CompanyInventors: Joseph A. Marshall, IV, Joseph Lawrence Hafenrichter, Manny Salazar Urcia, JR., Paul Chih-Yung Chang
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Patent number: 8912975Abstract: A method and apparatus for reworking an antenna aperture. A plurality of antenna cells comprise walls and antenna elements on the walls. Replacement antenna cells are placed adjacent to the plurality of antenna cells. The replacement antenna cells comprise a replacement wall and a replacement antenna element on the replacement wall. A conductive splice is attached to the replacement antenna element and to a one of the antenna elements on a one of the walls.Type: GrantFiled: September 20, 2012Date of Patent: December 16, 2014Assignee: The Boeing CompanyInventors: Joseph L. Hafenrichter, Joseph A. Marshall, IV, Jeffrey Lynn Duce, Manny Salazar Urcia, Jr., Otis Franklin Layton, David L. Banks
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Publication number: 20140338812Abstract: Cells of a composite cell array are cured by placing tool blocks in the cells and inserting thermally conductive elements in each of the tool blocks. The thermally conductive elements are convectively heated by a flow of hot air. The heated conductive elements conduct heat to the tooling blocks, which then conduct heat to the cells to cure the composite and adhesive.Type: ApplicationFiled: May 16, 2013Publication date: November 20, 2014Inventors: Joseph Lawrence Hafenrichter, Joseph A. Marshall, IV
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Publication number: 20140060733Abstract: Systems and methods according to the present disclosure for assembling conformal arrays utilize an outer tool for insertion into an open cell of a conformal array, an inner tool for insertion into the outer tool, and an adhesive source for delivering adhesive to the edges of the open cell via the inner tool and the outer tool. An assembled conformal array includes adhesive extending along the edges of the open cell.Type: ApplicationFiled: September 4, 2012Publication date: March 6, 2014Applicant: The Boeing CompanyInventors: Joseph A. Marshall, IV, Joseph Lawrence Hafenrichter, Manny Salazar Urcia, JR., Paul Chih-Yung Chang
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Publication number: 20130229321Abstract: In one embodiment a method to form a load bearing antenna aperture comprises forming a honeycomb core structure having a plurality of wall sections, the wall sections including electromagnetic radiating elements, and wherein lower surfaces of the wall sections defines a first surface and upper surfaces of the wall sections define a second surface, positioning a back skin to the first surface of the honeycomb core structure with an adhesive layer which comprises a layer of adhesive film and a paste adhesive disposed on the layer of adhesive film. Other embodiments are disclosed.Type: ApplicationFiled: April 19, 2013Publication date: September 5, 2013Applicant: The Boeing CompanyInventors: Douglas A. McCarville, Joseph A. Marshall, IV, Manny S. Urcia, Otis F. Layton
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Publication number: 20130079955Abstract: Concepts and technologies are disclosed herein for a sensor system for detecting, characterizing, monitoring, and analyzing data. According to some embodiments disclosed herein, a monitoring system is configured to obtain data from a sensor system. The sensor system includes two or more sensors and can indicate an operating state detected at a monitored structure by the sensors. The monitoring system also obtains operational data including a threshold value for the sensors and an expected value for the sensors. The monitoring system is configured to adjust the thresholds based, at least partially, upon the operational data to obtain an adjusted threshold value, and to compare the data value to the adjusted threshold. The monitoring system can determine if the monitored structure is operating in an alarm condition.Type: ApplicationFiled: September 23, 2011Publication date: March 28, 2013Applicant: THE BOEING COMPANYInventors: Kathryn A. Masiello, Robert Steven Wright, Jeffrey Lynn Duce, Bradley J. Mitchell, Joseph A. Marshall, IV
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Publication number: 20130016019Abstract: A method and apparatus comprising a resin layer, a number of conductive elements, and a number of layers of reinforcement material. The number of conductive elements is on the resin layer. The number of conductive elements has a configuration that forms an antenna system. The number of layers of reinforcement material forms a reinforcement for a composite structure, and at least a portion of the resin layer forms a matrix for the composite structure.Type: ApplicationFiled: July 15, 2011Publication date: January 17, 2013Applicant: THE BOEING COMPANYInventors: Matthew A. Stoneback, Joseph A. Marshall, IV, Daniel Joseph Sego, Otis Franklin Layton, Kevin O'Brien Gaw