Patents by Inventor Paul H. Shelley, JR.

Paul H. Shelley, JR. 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).

  • Patent number: 11215566
    Abstract: A system and method for internally inspecting a tubular composite part so as to identify and measure adhesive flow therewithin are provided, along with an endpoint adapter assembly of a near infrared (NIR) spectrometer. The system includes an end point adapter that fits within and maintains a consistent cross-sectional position within the tubular composite part. The system also includes a plurality of optical fibers extending radially outward from the end point adapter. The end point adapter moves longitudinally through the tubular composite part and receives light with the plurality of optical fibers following interaction of the light with the tubular composite part. The system further includes a NIR imaging spectrometer configured to disperse the light being collected by the plurality of optical fibers across an NIR spectrum and a NIR camera configured to generate images of the tubular composite part based on dispersed light.
    Type: Grant
    Filed: July 14, 2016
    Date of Patent: January 4, 2022
    Assignee: The Boeing Company
    Inventors: Paul H. Shelley, Jr., Christopher Wayne Fay
  • Patent number: 9903809
    Abstract: A system for measuring thermal degradation of composites includes a cylindrical body; a bottom cover having a lower central aperture; an upper concave mirror facing the bottom cover with an upper central orifice concentric with a central axis of the body; a lower concave mirror facing the upper concave mirror with a lower central orifice concentric with the central axis; a source of actinic radiation between the upper concave mirror and the lower concave mirror on the central axis to direct actinic radiation through the lower central orifice and lower central aperture; and a camera with an image sensor positioned concentrically relative to the upper central orifice; wherein the bottom cover is adjustable relative to the cylindrical body to provide a focusing function for the image sensor by varying the distance from the lower central orifice and the upper reflective surface.
    Type: Grant
    Filed: September 6, 2017
    Date of Patent: February 27, 2018
    Assignee: The Boeing Company
    Inventors: Paul H. Shelley, Jr., Gregory J. Werner, Milan Milosevic, Paul Vahey
  • Publication number: 20180017505
    Abstract: A system and method for internally inspecting a tubular composite part so as to identify and measure adhesive flow therewithin are provided, along with an endpoint adapter assembly of a near infrared (NIR) spectrometer. The system includes an end point adapter that fits within and maintains a consistent cross-sectional position within the tubular composite part. The system also includes a plurality of optical fibers extending radially outward from the end point adapter. The end point adapter moves longitudinally through the tubular composite part and receives light with the plurality of optical fibers following interaction of the light with the tubular composite part. The system further includes a NIR imaging spectrometer configured to disperse the light being collected by the plurality of optical fibers across an NIR spectrum and a NIR camera configured to generate images of the tubular composite part based on dispersed light.
    Type: Application
    Filed: July 14, 2016
    Publication date: January 18, 2018
    Inventors: Paul H. Shelley, JR., Christopher Wayne Fay
  • Patent number: 9863888
    Abstract: A multispectral imaging system and method and a system for composite layup are provided in order to detect foreign object debris during the fabrication of a composite structure. In the context of a method, a surface of a composite material is illuminated with near infrared light. The method also detects the near infrared light following interaction of the near infrared light with the composite material. Following detection, the method analyzes a spectrum of the near infrared light to detect foreign object debris upon the composite material. The method analyzes the spectrum of near infrared light by distinguishing between different types of foreign object debris as a result of comparing the spectrum of near infrared light to predefined spectral signatures of a plurality of different types of foreign object debris. The method may also determine the size and location of the foreign object debris.
    Type: Grant
    Filed: February 16, 2017
    Date of Patent: January 9, 2018
    Assignee: The Boeing Company
    Inventors: Paul H. Shelley, Jr., Paul G. Vahey, Gregory J. Werner, Robert Arthur Kisch
  • Publication number: 20170370846
    Abstract: A system for measuring thermal degradation of composites includes a cylindrical body; a bottom cover having a lower central aperture; an upper concave mirror facing the bottom cover with an upper central orifice concentric with a central axis of the body; a lower concave mirror facing the upper concave mirror with a lower central orifice concentric with the central axis; a source of actinic radiation between the upper concave mirror and the lower concave mirror on the central axis to direct actinic radiation through the lower central orifice and lower central aperture; and a camera with an image sensor positioned concentrically relative to the upper central orifice; wherein the bottom cover is adjustable relative to the cylindrical body to provide a focusing function for the image sensor by varying the distance from the lower central orifice and the upper reflective surface.
    Type: Application
    Filed: September 6, 2017
    Publication date: December 28, 2017
    Inventors: Paul H. Shelley, JR., Gregory J. Werner, Milan Milosevic, Paul Vahey
  • Patent number: 9791365
    Abstract: A system for measuring thermal degradation of composites, may include a housing having an interior with an opening shaped to expose a test area of the composite to be tested to the interior; a light-emitting diode that emits primarily ultraviolet radiation, the diode mounted on the housing to direct the ultraviolet radiation into the interior and through the opening; an image sensor mounted on the housing and open to the interior to receive radiation emitted from the test area passing through the opening into the interior; and an image processor connected to receive a signal from the image sensor, the image processor determining a presence or absence of thermal degradation of the test area in response to the signal.
    Type: Grant
    Filed: September 16, 2015
    Date of Patent: October 17, 2017
    Assignee: The Boeing Company
    Inventors: Paul H. Shelley, Jr., Gregory J. Werner, Milan Milosevic
  • Publication number: 20170160208
    Abstract: A multispectral imaging system and method and a system for composite layup are provided in order to detect foreign object debris during the fabrication of a composite structure. In the context of a method, a surface of a composite material is illuminated with near infrared light. The method also detects the near infrared light following interaction of the near infrared light with the composite material. Following detection, the method analyzes a spectrum of the near infrared light to detect foreign object debris upon the composite material. The method analyzes the spectrum of near infrared light by distinguishing between different types of foreign object debris as a result of comparing the spectrum of near infrared light to predefined spectral signatures of a plurality of different types of foreign object debris. The method may also determine the size and location of the foreign object debris.
    Type: Application
    Filed: February 16, 2017
    Publication date: June 8, 2017
    Inventors: Paul H. Shelley, JR., Paul G. Vahey, Gregory J. Werner, Robert Arthur Kisch
  • Patent number: 9606070
    Abstract: A multispectral imaging system and method and a system for composite layup are provided in order to detect foreign object debris during the fabrication of a composite structure. In the context of a method, a surface of a composite material is illuminated with near infrared light. The method also detects the near infrared light following interaction of the near infrared light with the composite material. Following detection, the method analyzes a spectrum of the near infrared light to detect foreign object debris upon the composite material. The method analyzes the spectrum of near infrared light by distinguishing between different types of foreign object debris as a result of comparing the spectrum of near infrared light to predefined spectral signatures of a plurality of different types of foreign object debris. The method may also determine the size and location of the foreign object debris.
    Type: Grant
    Filed: November 25, 2014
    Date of Patent: March 28, 2017
    Assignee: The Boeing Company
    Inventors: Paul H Shelley, Jr., Paul G Vahey, Gregory J Werner, Robert Arthur Kisch
  • Publication number: 20170074782
    Abstract: A system for measuring thermal degradation of composites, may include a housing having an interior with an opening shaped to expose a test area of the composite to be tested to the interior; a light-emitting diode that emits primarily ultraviolet radiation, the diode mounted on the housing to direct the ultraviolet radiation into the interior and through the opening; an image sensor mounted on the housing and open to the interior to receive radiation emitted from the test area passing through the opening into the interior; and an image processor connected to receive a signal from the image sensor, the image processor determining a presence or absence of thermal degradation of the test area in response to the signal.
    Type: Application
    Filed: September 16, 2015
    Publication date: March 16, 2017
    Inventors: Paul H. Shelley, JR., Gregory J. Werner, Milan Milosevic
  • Publication number: 20160146741
    Abstract: A multispectral imaging system and method and a system for composite layup are provided in order to detect foreign object debris during the fabrication of a composite structure. In the context of a method, a surface of a composite material is illuminated with near infrared light. The method also detects the near infrared light following interaction of the near infrared light with the composite material. Following detection, the method analyzes a spectrum of the near infrared light to detect foreign object debris upon the composite material. The method analyzes the spectrum of near infrared light by distinguishing between different types of foreign object debris as a result of comparing the spectrum of near infrared light to predefined spectral signatures of a plurality of different types of foreign object debris. The method may also determine the size and location of the foreign object debris.
    Type: Application
    Filed: November 25, 2014
    Publication date: May 26, 2016
    Inventors: Paul H. Shelley, JR., Paul G. Vahey, Gregory J. Werner, Robert Arthur Kisch
  • Patent number: 9103758
    Abstract: A method for manufacturing a test specimen assembly. A first material for the test specimen assembly and a witness coupon are positioned relative to each other. A surface treatment is applied onto a first surface of the first material and onto a surface of the witness coupon. An adhesive is applied onto the first surface of the first material. A second surface of a second material for the test specimen assembly is placed onto the first surface of the first material with the adhesive. The adhesive is cured to form the test specimen assembly.
    Type: Grant
    Filed: October 25, 2012
    Date of Patent: August 11, 2015
    Assignee: THE BOEING COMPANY
    Inventors: Douglas Allen Frisch, Richard H. Bossi, William Bruce Hopkins Grace, Marc Joel Piehl, Kay Youngdahl Blohowiak, Paul H. Shelley, Jr.
  • Patent number: 8853634
    Abstract: A method and apparatus for inspecting a composite structure. A resin inspection system comprises a housing having an open section, a movement system associated with the housing, a light source associated with the housing, an infrared measurement system associated with the interior of the housing, and a visible light sensor system. The movement system is configured to move the housing on a surface of a composite structure. The light source is configured to emit light. The infrared measurement system is configured to generate infrared measurement information from infrared light detected by the infrared measurement system through the open section. The visible light sensor system is configured to generate image information about the surface of the composite structure.
    Type: Grant
    Filed: March 12, 2012
    Date of Patent: October 7, 2014
    Assignee: The Boeing Company
    Inventors: Paul H. Shelley, Jr., Paul G. Vahey, Gregory James Werner, Gabor John Kemeny, Gard Groth, Gina Elaine Stuessy, Natalie Ann Crothers
  • Publication number: 20130234030
    Abstract: A method and apparatus for inspecting a composite structure. A resin inspection system comprises a housing having an open section, a movement system associated with the housing, a light source associated with the housing, an infrared measurement system associated with the interior of the housing, and a visible light sensor system. The movement system is configured to move the housing on a surface of a composite structure. The light source is configured to emit light. The infrared measurement system is configured to generate infrared measurement information from infrared light detected by the infrared measurement system through the open section. The visible light sensor system is configured to generate image information about the surface of the composite structure.
    Type: Application
    Filed: March 12, 2012
    Publication date: September 12, 2013
    Applicant: THE BOEING COMPANY
    Inventors: Paul H. Shelley, JR., Paul G. Vahey, Gregory James Werner, Gabor John Kemeny, Gard Groth, Gina Elaine Stuessy, Natalie Ann Crothers