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).
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Patent number: 12521946Abstract: 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: GrantFiled: December 6, 2023Date of Patent: January 13, 2026Assignee: The Boeing CompanyInventors: George E. Bible, Peter M. Winzek
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Publication number: 20240190090Abstract: 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: ApplicationFiled: December 6, 2023Publication date: June 13, 2024Applicant: THE BOEING COMPANYInventors: George E. Bible, Peter M. Winzek
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Patent number: 11338480Abstract: 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: GrantFiled: September 9, 2020Date of Patent: May 24, 2022Assignee: The Boeing CompanyInventors: John M. Griffith, Steven M. Shewchuk, George E. Bible, Steven J. Plummer, Ryan M. Trella, Ronald J. Byington
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Patent number: 11181887Abstract: 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: GrantFiled: December 14, 2018Date of Patent: November 23, 2021Assignee: The Boeing CompanyInventors: Roger W. Engelbart, James L. Scherer, Christopher M. Vaccaro, Brian Stutzman, George E. Bible, Jeffrey J. Kilwin
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Publication number: 20210039283Abstract: 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: ApplicationFiled: September 9, 2020Publication date: February 11, 2021Applicant: The Boeing CompanyInventors: John M. Griffith, Steven M. Shewchuk, George E. Bible, Steven J. Plummer, Ryan M. Trella, Ronald J. Byington
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Patent number: 10800072Abstract: 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: GrantFiled: April 24, 2017Date of Patent: October 13, 2020Assignee: The Boeing CompanyInventors: John M. Griffith, George E. Bible, Steven M. Shewchuk, Steven J. Plummer, Ryan M. Trella, Ronald J. Byington
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Publication number: 20200192331Abstract: 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: ApplicationFiled: December 14, 2018Publication date: June 18, 2020Applicant: The Boeing CompanyInventors: Roger W. Engelbart, James L. Scherer, Christopher M. Vaccaro, Brian Stutzman, George E. Bible, Jeffrey J. Kilwin
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Patent number: 10139808Abstract: 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: GrantFiled: September 7, 2016Date of Patent: November 27, 2018Assignee: The Boeing CompanyInventors: Roger W. Engelbart, George E. Bible, James Leonard Scherer, Brian Stutzman, Jeffrey J. Kilwin, Christopher M. Vaccaro
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Publication number: 20180304501Abstract: 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: ApplicationFiled: April 24, 2017Publication date: October 25, 2018Applicant: The Boeing CompanyInventors: John M. Griffith, George E. Bible, Steven M. Shewchuk, Steven J. Plummer, Ryan M. Trella, Ronald J. Byington
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Publication number: 20180067476Abstract: 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: ApplicationFiled: September 7, 2016Publication date: March 8, 2018Applicant: The Boeing CompanyInventors: Roger W. Engelbart, George E. Bible, James Leonard Scherer, Brian Stutzman, Jeffrey J. Kilwin, Christopher M. Vaccaro