Patents by Inventor Mark Davis Haynes
Mark Davis Haynes 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: 20230280280Abstract: A handheld device for making 3D topography measurements of surface discontinuities in high performance structures, such as aerostructures (e.g., aluminum fuselages). Lights illuminate the discontinuity from multiple angles, and a camera captures images of the discontinuity. A thickness sensor generates thickness data regarding a thickness of the base material and the top protective coating. A position sensor generates position data regarding a location of the discontinuity on the structure. A processor generates geometry data regarding a geometry of the discontinuity based on the images, performs an analysis of the geometry, thickness, and position data, and communicates a result of the analysis on a display. A conforming membrane and/or a gel and an opaque lubricant may be applied over and conform to the discontinuity in order to make more uniform a reflectivity difference and a color difference between the discontinuity and an adjacent portion of the structure.Type: ApplicationFiled: May 10, 2023Publication date: September 7, 2023Inventor: Mark Davis Haynes
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Publication number: 20230252648Abstract: A system for inspecting features of an airframe, the system including a feature inspection device configured to measure an aspect of a first feature and a tracking subsystem configured to determine a position of the feature inspection device when the feature inspection device measures the aspect of the first feature. The system is configured to determine a position of the first feature on the airframe via the feature inspection device and the tracking subsystem, the determination of the position of the first feature being independent from the measurement of the aspect of the first feature.Type: ApplicationFiled: April 18, 2023Publication date: August 10, 2023Applicant: Spirit AeroSystems, Inc.Inventors: Mark Davis Haynes, Glen Paul Cork, Bharath Achyutha Rao, John Thomas Baumfalk-Lee, Matthew W. McKenna, Bruce E. Gabel, Scott Bishop, Gregorio Balandran
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Patent number: 11680910Abstract: A handheld device for making 3D topography measurements of surface discontinuities in high performance structures, such as aerostructures (e.g., aluminum fuselages). Lights illuminate the discontinuity from multiple angles, and a camera captures images of the discontinuity. A thickness sensor generates thickness data regarding a thickness of the base material and the top protective coating. A position sensor generates position data regarding a location of the discontinuity on the structure. A processor generates geometry data regarding a geometry of the discontinuity based on the images, performs an analysis of the geometry, thickness, and position data, and communicates a result of the analysis on a display. A conforming membrane and/or a gel and an opaque lubricant may be applied over and conform to the discontinuity in order to make more uniform a reflectivity difference and a color difference between the discontinuity and an adjacent portion of the structure.Type: GrantFiled: July 30, 2020Date of Patent: June 20, 2023Assignee: Spirit AeroSystems, Inc.Inventor: Mark Davis Haynes
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Patent number: 11631184Abstract: A system for inspecting features of an airframe, the system including a feature inspection device configured to measure an aspect of a first feature and a tracking subsystem configured to determine a position of the feature inspection device when the feature inspection device measures the aspect of the first feature. The system is configured to determine a position of the first feature on the airframe via the feature inspection device and the tracking subsystem, the determination of the position of the first feature being independent from the measurement of the aspect of the first feature.Type: GrantFiled: September 18, 2020Date of Patent: April 18, 2023Assignee: SPIRIT AEROSYSTEMS, INC.Inventors: Mark Davis Haynes, Glen Paul Cork, Bharath Achyutha Rao, John Thomas Baumfalk-Lee, Matthew W. McKenna, Bruce E. Gabel, Scott Bishop, Gregorio Balandran
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Publication number: 20220092793Abstract: A system for inspecting features of an airframe, the system including a feature inspection device configured to measure an aspect of a first feature and a tracking subsystem configured to determine a position of the feature inspection device when the feature inspection device measures the aspect of the first feature. The system is configured to determine a position of the first feature on the airframe via the feature inspection device and the tracking subsystem, the determination of the position of the first feature being independent from the measurement of the aspect of the first feature.Type: ApplicationFiled: September 18, 2020Publication date: March 24, 2022Applicant: SPIRIT AEROSYSTEMS, INC.Inventors: Mark Davis Haynes, Glen Paul Cork, Bharath Achyutha Rao, John Thomas Baumfalk-Lee, Matthew W. McKenna, Bruce E. Gabel, Scott Bishop, Gregorio Balandran
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Publication number: 20220092766Abstract: A system for inspecting features of an airframe, the system including a feature inspection device configured to measure an aspect of a first feature and a tracking subsystem configured to determine a position of the feature inspection device when the feature inspection device measures the aspect of the first feature. The system is configured to determine a position of the first feature on the airframe via the feature inspection device and the tracking subsystem, the determination of the position of the first feature being independent from the measurement of the aspect of the first feature.Type: ApplicationFiled: September 3, 2021Publication date: March 24, 2022Applicant: Spirit AeroSystems, Inc.Inventors: Mark Davis Haynes, Glen Paul Cork, Bharath Achyutha Rao, John Thomas Baumfalk-Lee, Matthew W. McKenna, Bruce E. Gabel, Scott Bishop, Gregorio Balandran
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Patent number: 10837916Abstract: A handheld device for making 3D topography measurements of surface discontinuities in high performance structures, such as aerostructures (e.g., aluminum fuselages). Lights illuminate the discontinuity from multiple angles, and a camera captures images of the discontinuity. A thickness sensor generates thickness data regarding a thickness of the base material and the top protective coating. A position sensor generates position data regarding a location of the discontinuity on the structure. A processor generates geometry data regarding a geometry of the discontinuity based on the images, performs an analysis of the geometry, thickness, and position data, and communicates a result of the analysis on a display. A conforming membrane and/or a gel and an opaque lubricant may be applied over and conform to the discontinuity in order to make more uniform a reflectivity difference and a color difference between the discontinuity and an adjacent portion of the structure.Type: GrantFiled: October 17, 2017Date of Patent: November 17, 2020Assignee: Spirit AeroSystems, Inc.Inventor: Mark Davis Haynes
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Publication number: 20200355619Abstract: A handheld device for making 3D topography measurements of surface discontinuities in high performance structures, such as aerostructures (e.g., aluminum fuselages). Lights illuminate the discontinuity from multiple angles, and a camera captures images of the discontinuity. A thickness sensor generates thickness data regarding a thickness of the base material and the top protective coating. A position sensor generates position data regarding a location of the discontinuity on the structure. A processor generates geometry data regarding a geometry of the discontinuity based on the images, performs an analysis of the geometry, thickness, and position data, and communicates a result of the analysis on a display. A conforming membrane and/or a gel and an opaque lubricant may be applied over and conform to the discontinuity in order to make more uniform a reflectivity difference and a color difference between the discontinuity and an adjacent portion of the structure.Type: ApplicationFiled: July 30, 2020Publication date: November 12, 2020Applicant: SPIRIT AEROSYSTEMS, INC.Inventor: Mark Davis Haynes
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Patent number: 10591420Abstract: An in-line laser profilometry inspection system broadly comprises a first laser, a first sensor, a second laser, a second sensor, a camera, a calibration standard, and an interface. The lasers transmit first and second light signals to a stringer charge or other part. The sensors detect the light signals reflecting off first and second edge walls of the part. The camera obtains a top-down image of the part. The calibration standard provides structure for calibrating the inspection system via the lasers and sensors. The interface allows a user to oversee part inspection. Data generated from the reflected light signals corresponding to a part profile may be analyzed based on at least first and second derivatives of the part profile such that the part is inspected during a cutting procedure.Type: GrantFiled: April 30, 2019Date of Patent: March 17, 2020Assignee: Spirit AeroSystems, Inc.Inventors: Mark Davis Haynes, Glen Paul Cork
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Publication number: 20180259461Abstract: A handheld device for making 3D topography measurements of surface discontinuities in high performance structures, such as aerostructures (e.g., aluminum fuselages). Lights illuminate the discontinuity from multiple angles, and a camera captures images of the discontinuity. A thickness sensor generates thickness data regarding a thickness of the base material and the top protective coating. A position sensor generates position data regarding a location of the discontinuity on the structure. A processor generates geometry data regarding a geometry of the discontinuity based on the images, performs an analysis of the geometry, thickness, and position data, and communicates a result of the analysis on a display. A conforming membrane and/or a gel and an opaque lubricant may be applied over and conform to the discontinuity in order to make more uniform a reflectivity difference and a color difference between the discontinuity and an adjacent portion of the structure.Type: ApplicationFiled: October 17, 2017Publication date: September 13, 2018Applicant: SPIRIT AEROSYSTEMS, INC.Inventor: Mark Davis Haynes