Patents by Inventor George E. Bible

George E. Bible 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: 12521946
    Abstract: A method for preparing a bond assembly jig (BAJ) includes forming a cutter relief groove in the BAJ, filling the cutter relief groove of the BAJ with a material, and curing the material after said filling.
    Type: Grant
    Filed: December 6, 2023
    Date of Patent: January 13, 2026
    Assignee: The Boeing Company
    Inventors: George E. Bible, Peter M. Winzek
  • Publication number: 20240190090
    Abstract: A method for preparing a bond assembly jig (BAJ) includes forming a cutter relief groove in the BAJ, filling the cutter relief groove of the BAJ with a material, and curing the material after said filling.
    Type: Application
    Filed: December 6, 2023
    Publication date: June 13, 2024
    Applicant: THE BOEING COMPANY
    Inventors: George E. Bible, Peter M. Winzek
  • Patent number: 11338480
    Abstract: A method including steps of (1) heating, with a heating system, an apparatus comprising an enclosure assembly and a temperature emulation assembly positioned within said enclosure assembly; (2) thermally isolating said temperature emulation assembly from said heating system with said enclosure assembly; (3) permitting conductive heat transfer to said temperature emulation assembly only through an enclosure assembly-leading end of said enclosure assembly; and (4) representing a hottest temperature and a coldest temperature of an article being emulated by said apparatus with said temperature emulation assembly.
    Type: Grant
    Filed: September 9, 2020
    Date of Patent: May 24, 2022
    Assignee: The Boeing Company
    Inventors: John M. Griffith, Steven M. Shewchuk, George E. Bible, Steven J. Plummer, Ryan M. Trella, Ronald J. Byington
  • Patent number: 11181887
    Abstract: A method and system provide for reducing gaps between two mating parts. Either or both parts may be nondestructively inspected at a plurality of locations on a surface to gather a data set relating to the part thickness. The data set may be used to calculate a set of as-built thickness values for the part and a set of deviations from a design model. A mating area may be determined for mating surfaces of the parts. One or more layers of sacrificial material in the mating area may be prepared for any deviations greater than a design allowance. The system may include a ply cutting device and an additive manufacturing device coupled to a computer to receive the sacrificial material layer data and shim data and to cut the one or more layers of sacrificial material and to construct the shim. A shim may be constructed for any deviations equal to or greater than a minimum shim thickness. The one or more layers of sacrificial material may be applied to the part, cured, and machined to a desired thickness.
    Type: Grant
    Filed: December 14, 2018
    Date of Patent: November 23, 2021
    Assignee: The Boeing Company
    Inventors: Roger W. Engelbart, James L. Scherer, Christopher M. Vaccaro, Brian Stutzman, George E. Bible, Jeffrey J. Kilwin
  • Publication number: 20210039283
    Abstract: A method including steps of (1) heating, with a heating system, an apparatus comprising an enclosure assembly and a temperature emulation assembly positioned within said enclosure assembly; (2) thermally isolating said temperature emulation assembly from said heating system with said enclosure assembly; (3) permitting conductive heat transfer to said temperature emulation assembly only through an enclosure assembly-leading end of said enclosure assembly; and (4) representing a hottest temperature and a coldest temperature of an article being emulated by said apparatus with said temperature emulation assembly.
    Type: Application
    Filed: September 9, 2020
    Publication date: February 11, 2021
    Applicant: The Boeing Company
    Inventors: John M. Griffith, Steven M. Shewchuk, George E. Bible, Steven J. Plummer, Ryan M. Trella, Ronald J. Byington
  • Patent number: 10800072
    Abstract: An apparatus includes a enclosure assembly including an enclosure assembly-leading end and an opposed enclosure assembly-lagging end, and a temperature emulation assembly mounted within the enclosure assembly and including a temperature emulation assembly-leading end located proximate to the enclosure assembly-leading end and a temperature emulation assembly-lagging end spaced away from the enclosure assembly-lagging end. The enclosure assembly thermally isolates the temperature emulation assembly. The enclosure assembly permits conductive heat transfer to the temperature emulation assembly only through the enclosure assembly-leading end.
    Type: Grant
    Filed: April 24, 2017
    Date of Patent: October 13, 2020
    Assignee: The Boeing Company
    Inventors: John M. Griffith, George E. Bible, Steven M. Shewchuk, Steven J. Plummer, Ryan M. Trella, Ronald J. Byington
  • Publication number: 20200192331
    Abstract: A method and system provide for reducing gaps between two mating parts. Either or both parts may be nondestructively inspected at a plurality of locations on a surface to gather a data set relating to the part thickness. The data set may be used to calculate a set of as-built thickness values for the part and a set of deviations from a design model. A mating area may be determined for mating surfaces of the parts. One or more layers of sacrificial material in the mating area may be prepared for any deviations greater than a design allowance. The system may include a ply cutting device and an additive manufacturing device coupled to a computer to receive the sacrificial material layer data and shim data and to cut the one or more layers of sacrificial material and to construct the shim. A shim may be constructed for any deviations equal to or greater than a minimum shim thickness. The one or more layers of sacrificial material may be applied to the part, cured, and machined to a desired thickness.
    Type: Application
    Filed: December 14, 2018
    Publication date: June 18, 2020
    Applicant: The Boeing Company
    Inventors: Roger W. Engelbart, James L. Scherer, Christopher M. Vaccaro, Brian Stutzman, George E. Bible, Jeffrey J. Kilwin
  • Patent number: 10139808
    Abstract: A method and a system are provided for predicting and creating a shim for use in a joint where two parts, such as a skin and a substructure, are assembled together. Digital models for the skin and the substructure may be used as nominal maps of the outlines and profiles of the parts. The skin may be inspected, e.g., by nondestructive means, such as ultrasound, to determine as-built thickness profile for comparison to the skin's digital model of the thickness profile. Mating areas of the skin and substructure may be determined from their digital models of their outlines. Deviations in the mating areas of the as-built thickness of the skin from the digital model of the skin may be used to generate a digital model of a shim. The shim may be constructed from its digital model by additive manufacturing techniques that may involving machining or 3D printing.
    Type: Grant
    Filed: September 7, 2016
    Date of Patent: November 27, 2018
    Assignee: The Boeing Company
    Inventors: Roger W. Engelbart, George E. Bible, James Leonard Scherer, Brian Stutzman, Jeffrey J. Kilwin, Christopher M. Vaccaro
  • Publication number: 20180304501
    Abstract: An apparatus includes a enclosure assembly including an enclosure assembly-leading end and an opposed enclosure assembly-lagging end, and a temperature emulation assembly mounted within the enclosure assembly and including a temperature emulation assembly-leading end located proximate to the enclosure assembly-leading end and a temperature emulation assembly-lagging end spaced away from the enclosure assembly-lagging end. The enclosure assembly thermally isolates the temperature emulation assembly. The enclosure assembly permits conductive heat transfer to the temperature emulation assembly only through the enclosure assembly-leading end.
    Type: Application
    Filed: April 24, 2017
    Publication date: October 25, 2018
    Applicant: The Boeing Company
    Inventors: John M. Griffith, George E. Bible, Steven M. Shewchuk, Steven J. Plummer, Ryan M. Trella, Ronald J. Byington
  • Publication number: 20180067476
    Abstract: A method and a system are provided for predicting and creating a shim for use in a joint where two parts, such as a skin and a substructure, are assembled together. Digital models for the skin and the substructure may be used as nominal maps of the outlines and profiles of the parts. The skin may be inspected, e.g., by nondestructive means, such as ultrasound, to determine as-built thickness profile for comparison to the skin's digital model of the thickness profile. Mating areas of the skin and substructure may be determined from their digital models of their outlines. Deviations in the mating areas of the as-built thickness of the skin from the digital model of the skin may be used to generate a digital model of a shim. The shim may be constructed from its digital model by additive manufacturing techniques that may involving machining or 3D printing.
    Type: Application
    Filed: September 7, 2016
    Publication date: March 8, 2018
    Applicant: The Boeing Company
    Inventors: Roger W. Engelbart, George E. Bible, James Leonard Scherer, Brian Stutzman, Jeffrey J. Kilwin, Christopher M. Vaccaro