Patents by Inventor Paul L. Gooch

Paul L. Gooch 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: 8973241
    Abstract: A method and apparatus for forming a joint between a first composite structure and a second composite structure. A number of tab sections may be formed at an end of the first composite structure. The first composite structure may comprise a first skin, a second skin, and a core located between the first skin and the second skin. A tab section in the number of tab sections may comprise a first skin section of the first skin, a second skin section of the second skin, and a core section of the core. A portion of the core section may be removed from each tab section to form a number of tabs at the end of the first composite structure. The first composite structure may be attached to the second composite structure using the number of tabs to form the joint between the first composite structure and the second composite structure.
    Type: Grant
    Filed: September 6, 2012
    Date of Patent: March 10, 2015
    Assignee: The Boeing Company
    Inventor: Paul L. Gooch
  • Patent number: 8961059
    Abstract: A method of fabricating a self-locking joint in a panel structure. The method provides a panel structure having at least two face sheets and a core portion sandwiched therebetween. The method further fabricates in a first portion of the panel structure at least one mortice opening having self-locking end portions. The method further fabricates on a second portion of the panel structure at least one tenon extension having flexible self-locking members. The method further interlocks the flexible self-locking members of the at least one tenon extension with the self-locking end portions of the at least one mortice opening to form a self-locking joint in the panel structure.
    Type: Grant
    Filed: September 6, 2012
    Date of Patent: February 24, 2015
    Assignee: The Boeing Company
    Inventors: Brad J. Reeves, Paul L. Gooch
  • Publication number: 20140064833
    Abstract: There is provided in an embodiment a method of fabricating a self-locking joint in a panel structure. The method provides a panel structure having at least two face sheets and a core portion sandwiched therebetween. The method further fabricates in a first portion of the panel structure at least one mortise opening having self-locking end portions. The method further fabricates on a second portion of the panel structure at least one tenon extension having flexible self-locking members. The method further interlocks the flexible self-locking members of the at least one tenon extension with the self-locking end portions of the at least one mortise opening to form a self-locking joint in the panel structure.
    Type: Application
    Filed: September 6, 2012
    Publication date: March 6, 2014
    Applicant: The Boeing Company
    Inventors: Brad J. Reeves, Paul L. Gooch