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).

  • Patent number: 10919192
    Abstract: 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: Grant
    Filed: November 1, 2019
    Date of Patent: February 16, 2021
    Assignee: The Boeing Company
    Inventors: Edward McMurray Fisher, Jr., Dennis Lynn Coad, Brian Allen Carter, Glenn David Hardin, Jon Paul Thurber, Douglas Eugene Bailey
  • Patent number: 10919191
    Abstract: 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: Grant
    Filed: November 1, 2019
    Date of Patent: February 16, 2021
    Assignee: The Boeing Company
    Inventors: Edward McMurray Fisher, Jr., Dennis Lynn Coad, Brian Allen Carter, Glenn David Hardin, Jon Paul Thurber, Douglas Eugene Bailey
  • Patent number: 10603821
    Abstract: 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: Grant
    Filed: January 23, 2012
    Date of Patent: March 31, 2020
    Assignee: The Boeing Company
    Inventors: Edward McMurray Fisher, Jr., Dennis Lynn Coad, Brian Allen Carter, Glenn David Hardin, Jon Paul Thurber, Douglas Eugene Bailey
  • Publication number: 20200061881
    Abstract: 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: Application
    Filed: November 1, 2019
    Publication date: February 27, 2020
    Applicant: The Boeing Company
    Inventors: Edward McMurray Fisher,, JR., Dennis Lynn Coad, Brian Allen Carter, Glenn David Hardin, Jon Paul Thurber, Douglas Eugene Bailey
  • Publication number: 20200061880
    Abstract: 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: Application
    Filed: November 1, 2019
    Publication date: February 27, 2020
    Applicant: The Boeing Company
    Inventors: Edward McMurray Fisher, JR., Dennis Lynn Coad, Brian Allen Carter, Glenn David Hardin, Jon Paul Thurber, Douglas Eugene Bailey
  • Patent number: 10118351
    Abstract: 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: Grant
    Filed: October 5, 2015
    Date of Patent: November 6, 2018
    Assignee: The Boeing Company
    Inventors: Edward McMurray Fisher, Jr., Brian Allen Carter
  • Publication number: 20160023410
    Abstract: 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: Application
    Filed: October 5, 2015
    Publication date: January 28, 2016
    Inventors: Edward McMurray Fisher, JR., Brian Allen Carter
  • Patent number: 9180631
    Abstract: 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: Grant
    Filed: July 22, 2011
    Date of Patent: November 10, 2015
    Assignee: The Boeing Company
    Inventors: Edward McMurray Fisher, Jr., Brian Allen Carter
  • Publication number: 20130189478
    Abstract: 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: Application
    Filed: January 23, 2012
    Publication date: July 25, 2013
    Inventors: Edward McMurray Fisher, JR., Dennis Lynn Coad, Brian Allen Carter, Glenn David Hardin, Jon Paul Thurber, Douglas Eugene Bailey
  • Publication number: 20130022391
    Abstract: 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: Application
    Filed: July 22, 2011
    Publication date: January 24, 2013
    Applicant: The Boeing Company
    Inventors: Edward McMurray Fisher, JR., Brian Allen Carter