Patents by Inventor Edward McMurray Fisher, JR.
Edward McMurray Fisher, 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).
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Patent number: 10919192Abstract: Methods provide for creating a three-dimensional random fiber orientation in a composite component. According to embodiments described herein, narrow flakes are created from a unidirectional composite fiber tape and poured into a reservoir of a mold, creating a three-dimensional random fiber orientation of the narrow flakes within the reservoir. At least a majority of the narrow flakes have an aspect ratio of length to width of at least 6:1. The narrow flakes are heated and compressed to fill the mold and create the composite component. The three-dimensional random fiber orientation of the narrow flakes within the reservoir is maintained as the narrow flakes are pushed through the mold, creating consistent, uniform strength characteristics throughout the resulting composite component.Type: GrantFiled: November 1, 2019Date of Patent: February 16, 2021Assignee: The Boeing CompanyInventors: Edward McMurray Fisher, Jr., Dennis Lynn Coad, Brian Allen Carter, Glenn David Hardin, Jon Paul Thurber, Douglas Eugene Bailey
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Patent number: 10919191Abstract: Methods provide for creating a three-dimensional random fiber orientation in a composite component. According to embodiments described herein, narrow flakes are created from a unidirectional composite fiber tape and poured into a reservoir of a mold, creating a three-dimensional random fiber orientation of the narrow flakes within the reservoir. At least a majority of the narrow flakes have an aspect ratio of length to width of at least 6:1. The narrow flakes are heated and compressed to fill the mold and create the composite component. The three-dimensional random fiber orientation of the narrow flakes within the reservoir is maintained as the narrow flakes are pushed through the mold, creating consistent, uniform strength characteristics throughout the resulting composite component.Type: GrantFiled: November 1, 2019Date of Patent: February 16, 2021Assignee: The Boeing CompanyInventors: Edward McMurray Fisher, Jr., Dennis Lynn Coad, Brian Allen Carter, Glenn David Hardin, Jon Paul Thurber, Douglas Eugene Bailey
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Patent number: 10603821Abstract: Methods provide for creating a three-dimensional random fiber orientation in a composite component. According to embodiments described herein, narrow flakes are created from a unidirectional composite fiber tape and poured into a reservoir of a mold, creating a three-dimensional random fiber orientation of the narrow flakes within the reservoir. At least a majority of the narrow flakes have an aspect ratio of length to width of at least 6:1. The narrow flakes are heated and compressed to fill the mold and create the composite component. The three-dimensional random fiber orientation of the narrow flakes within the reservoir is maintained as the narrow flakes are pushed through the mold, creating consistent, uniform strength characteristics throughout the resulting composite component.Type: GrantFiled: January 23, 2012Date of Patent: March 31, 2020Assignee: The Boeing CompanyInventors: Edward McMurray Fisher, Jr., Dennis Lynn Coad, Brian Allen Carter, Glenn David Hardin, Jon Paul Thurber, Douglas Eugene Bailey
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Publication number: 20200061881Abstract: Methods provide for creating a three-dimensional random fiber orientation in a composite component. According to embodiments described herein, narrow flakes are created from a unidirectional composite fiber tape and poured into a reservoir of a mold, creating a three-dimensional random fiber orientation of the narrow flakes within the reservoir. At least a majority of the narrow flakes have an aspect ratio of length to width of at least 6:1. The narrow flakes are heated and compressed to fill the mold and create the composite component. The three-dimensional random fiber orientation of the narrow flakes within the reservoir is maintained as the narrow flakes are pushed through the mold, creating consistent, uniform strength characteristics throughout the resulting composite component.Type: ApplicationFiled: November 1, 2019Publication date: February 27, 2020Applicant: The Boeing CompanyInventors: Edward McMurray Fisher,, JR., Dennis Lynn Coad, Brian Allen Carter, Glenn David Hardin, Jon Paul Thurber, Douglas Eugene Bailey
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Publication number: 20200061880Abstract: Methods provide for creating a three-dimensional random fiber orientation in a composite component. According to embodiments described herein, narrow flakes are created from a unidirectional composite fiber tape and poured into a reservoir of a mold, creating a three-dimensional random fiber orientation of the narrow flakes within the reservoir. At least a majority of the narrow flakes have an aspect ratio of length to width of at least 6:1. The narrow flakes are heated and compressed to fill the mold and create the composite component. The three-dimensional random fiber orientation of the narrow flakes within the reservoir is maintained as the narrow flakes are pushed through the mold, creating consistent, uniform strength characteristics throughout the resulting composite component.Type: ApplicationFiled: November 1, 2019Publication date: February 27, 2020Applicant: The Boeing CompanyInventors: Edward McMurray Fisher, JR., Dennis Lynn Coad, Brian Allen Carter, Glenn David Hardin, Jon Paul Thurber, Douglas Eugene Bailey
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Patent number: 10118351Abstract: A method of retaining a molded-in insert in a fiber reinforced thermoplastic composite material and forming a high strength mechanical locking mechanism is provided. The method includes fixing a molded-in insert in a mold cavity. The insert has a cylindrical body and at least one circumferential groove formed in the cylindrical body, and has a substantially concave configuration, and the groove has a groove radius of 0.025 inch or greater, and greater than or equal to a groove depth. The method includes introducing a fiber reinforced thermoplastic composite material into the mold cavity and around the molded-in insert, enclosing the mold cavity, heating and compressing the material in the mold cavity to consolidate the material around the molded-in insert and to form a consolidated fiber reinforced thermoplastic composite structure with the molded-in insert, cooling the structure, and removing the structure with the molded-in insert from the mold cavity.Type: GrantFiled: October 5, 2015Date of Patent: November 6, 2018Assignee: The Boeing CompanyInventors: Edward McMurray Fisher, Jr., Brian Allen Carter
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Publication number: 20160023410Abstract: A method of retaining a molded-in insert in a fiber reinforced thermoplastic composite material and forming a high strength mechanical locking mechanism is provided. The method includes fixing a molded-in insert in a mold cavity. The insert has a cylindrical body and at least one circumferential groove formed in the cylindrical body, and has a substantially concave configuration, and the groove has a groove radius of 0.025 inch or greater, and greater than or equal to a groove depth. The method includes introducing a fiber reinforced thermoplastic composite material into the mold cavity and around the molded-in insert, enclosing the mold cavity, heating and compressing the material in the mold cavity to consolidate the material around the molded-in insert and to form a consolidated fiber reinforced thermoplastic composite structure with the molded-in insert, cooling the structure, and removing the structure with the molded-in insert from the mold cavity.Type: ApplicationFiled: October 5, 2015Publication date: January 28, 2016Inventors: Edward McMurray Fisher, JR., Brian Allen Carter
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Patent number: 9180631Abstract: In an embodiment of the disclosure, there is provided a molded-in insert for high strength retention in a fiber reinforced thermoplastic composite structure. The insert has a cylindrical body and at least one circumferential groove formed in the cylindrical body, the groove having a substantially concave configuration, having a groove radius of 0.025 inch or greater, and having the groove radius greater than or equal to a groove depth.Type: GrantFiled: July 22, 2011Date of Patent: November 10, 2015Assignee: The Boeing CompanyInventors: Edward McMurray Fisher, Jr., Brian Allen Carter
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Publication number: 20130189478Abstract: Methods provide for creating a three-dimensional random fiber orientation in a composite component. According to embodiments described herein, narrow flakes are created from a unidirectional composite fiber tape and poured into a reservoir of a mold, creating a three-dimensional random fiber orientation of the narrow flakes within the reservoir. At least a majority of the narrow flakes have an aspect ratio of length to width of at least 6:1. The narrow flakes are heated and compressed to fill the mold and create the composite component. The three-dimensional random fiber orientation of the narrow flakes within the reservoir is maintained as the narrow flakes are pushed through the mold, creating consistent, uniform strength characteristics throughout the resulting composite component.Type: ApplicationFiled: January 23, 2012Publication date: July 25, 2013Inventors: Edward McMurray Fisher, JR., Dennis Lynn Coad, Brian Allen Carter, Glenn David Hardin, Jon Paul Thurber, Douglas Eugene Bailey
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Publication number: 20130022391Abstract: In an embodiment of the disclosure, there is provided a molded-in insert for high strength retention in a fiber reinforced thermoplastic composite structure. The insert has a cylindrical body and at least one circumferential groove formed in the cylindrical body, the groove having a substantially concave configuration, having a groove radius of 0.025 inch or greater, and having the groove radius greater than or equal to a groove depth.Type: ApplicationFiled: July 22, 2011Publication date: January 24, 2013Applicant: The Boeing CompanyInventors: Edward McMurray Fisher, JR., Brian Allen Carter