Patents by Inventor Steven M. Shewchuk
Steven M. Shewchuk 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: 12275198Abstract: A method of manufacturing a composite structure includes accessing design data for the composite structure that is manufactured according to a process including forming a layup of plies of fibers using a machine tool. The method includes applying the design data to an ANN classifier to classify a localized inconsistency of a type of inconsistency on the composite structure, the localized inconsistency spatially referenced to a location on the composite structure. The method includes performing a root cause analysis to identify one or more of process parameters as a potential cause of the type of inconsistency, and modifying one or more of the geometric model, the layup design, or values of the one or more of the process parameters to address the potential cause.Type: GrantFiled: February 17, 2022Date of Patent: April 15, 2025Assignee: The Boeing CompanyInventors: Carla E. Reynolds, Dustin D. Fast, Andrew L. Bauer, Troy Winfree, Steven M. Shewchuk, Alexander M. Rubin, Samuel J. Tucker
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Patent number: 11999116Abstract: A composite forming apparatus includes an end effector, a forming feature, and a non-contact heater. The forming feature is coupled to the end effector. The end effector moves the forming feature relative to a composite ply to form the composite ply over a forming tool or a prior formed composite ply. The non-contact heater heats to a portion of the composite ply before the portion of the composite ply is formed over the forming tool or the prior formed composite ply.Type: GrantFiled: August 30, 2021Date of Patent: June 4, 2024Assignee: The Boeing CompanyInventors: Kurtis S. Willden, Brian G. Robins, Steven M. Shewchuk, Brice A. Johnson
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Publication number: 20230060932Abstract: A composite forming apparatus includes an end effector, a forming feature, and a non-contact heater. The forming feature is coupled to the end effector. The end effector moves the forming feature relative to a composite ply to form the composite ply over a forming tool or a prior formed composite ply. The non-contact heater heats to a portion of the composite ply before the portion of the composite ply is formed over the forming tool or the prior formed composite ply.Type: ApplicationFiled: August 30, 2021Publication date: March 2, 2023Applicant: The Boeing CompanyInventors: Kurtis S. Willden, Brian G. Robins, Steven M. Shewchuk, Brice A. Johnson
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Patent number: 11485096Abstract: A composite manufacturing system and method are provided. The composite manufacturing system comprises a press and a bladder. The press has an upper portion having a desired shape for a composite structure and a lower portion configured to receive layers of composite material. The bladder is associated with the upper portion of the press and is configured to reach a superplastic state when heated such that the bladder forms to the composite structure by applying heat and pressure to the layers of composite material. The bladder cools without appreciable shrinkage, applying a desired amount of pressure to the composite structure during the entire cooling cycle. Once one composite structure is formed using the bladder, the bladder may be reused to form similar structures.Type: GrantFiled: May 17, 2019Date of Patent: November 1, 2022Assignee: The Boeing CompanyInventors: Steven M. Shewchuk, Justin Joseph Schell, Michael Palmore Matlack, Ravi Verma
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Publication number: 20220299975Abstract: A method of manufacturing a composite structure includes accessing design data for the composite structure that is manufactured according to a process including forming a layup of plies of fibers using a machine tool. The method includes applying the design data to an ANN classifier to classify a localized inconsistency of a type of inconsistency on the composite structure, the localized inconsistency spatially referenced to a location on the composite structure. The method includes performing a root cause analysis to identify one or more of process parameters as a potential cause of the type of inconsistency, and modifying one or more of the geometric model, the layup design, or values of the one or more of the process parameters to address the potential cause.Type: ApplicationFiled: February 17, 2022Publication date: September 22, 2022Inventors: Carla E. Reynolds, Dustin D. Fast, Andrew L. Bauer, Troy Winfree, Steven M. Shewchuk, Alexander M. Rubin, Samuel J. Tucker
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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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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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Publication number: 20200361162Abstract: A composite manufacturing system and method are provided. The composite manufacturing system comprises a press and a bladder. The press has an upper portion having a desired shape for a composite structure and a lower portion configured to receive layers of composite material. The bladder is associated with the upper portion of the press and is configured to reach a superplastic state when heated such that the bladder forms to the composite structure by applying heat and pressure to the layers of composite material. The bladder cools without appreciable shrinkage, applying a desired amount of pressure to the composite structure during the entire cooling cycle. Once one composite structure is formed using the bladder, the bladder may be reused to form similar structures.Type: ApplicationFiled: May 17, 2019Publication date: November 19, 2020Inventors: Steven M. Shewchuk, Justin Joseph Schell, Michael Palmore Matlack, Ravi Verma
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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: 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