Patents by Inventor Scott L. Smotherman

Scott L. Smotherman 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: 11931845
    Abstract: In an example, a system is disclosed. The system comprises a one-piece mandrel, a fuselage coupled to the one-piece mandrel, and a strongback apparatus positioned on the fuselage. The strongback apparatus comprises an arcuate central body comprising a front end, a rear end, and a plurality of elongated members that connect the front end to the rear end, and actuators mounted to the plurality of elongated members. The actuators are configured to move in a radially outward direction from extended positions to retracted positions and comprise (i) proximal ends mounted to the plurality of elongated members and (ii) distal ends having vacuum suction cups. In the extended positions, the vacuum suction cups engage the fuselage on which the strongback apparatus is positioned. As the actuators moves from the extended positions to the retracted positions, the vacuum suction cups pull the fuselage away from the one-piece mandrel.
    Type: Grant
    Filed: December 13, 2021
    Date of Patent: March 19, 2024
    Assignee: The Boeing Company
    Inventors: Byron James Autry, David Raines, Scott L. Smotherman, David M. Petka
  • Patent number: 11459124
    Abstract: An apparatus for mounting a splice component for joining two or more workpieces includes a base plate and one or more bias assemblies. The base plate includes one or more passageways extending through the base plate and one or more barrier elements mounted proximate to the passageway(s). Each barrier element and associated passageway are configured to freely receive a protrusion of a splice component. The bias assembly includes a bias element that extends proximate to the passageway and is configured to move resiliently to urge the protrusion against the barrier element. The passageway, the barrier element, and the bias assembly are configured to allow movement of the splice component relative to the base plate transverse to a direction of force applied by the bias element on the protrusion.
    Type: Grant
    Filed: February 21, 2020
    Date of Patent: October 4, 2022
    Assignee: The Boeing Company
    Inventors: David Howard Curry, III, David Raines, Scott L. Smotherman, Paul Gabriel Werntges, Dennis Ray Mathis, Charlie E. Branyon, III, Daniel B. Freeman
  • Publication number: 20220184760
    Abstract: In an example, a system is disclosed. The system comprises a one-piece mandrel, a fuselage coupled to the one-piece mandrel, and a strongback apparatus positioned on the fuselage. The strongback apparatus comprises an arcuate central body comprising a front end, a rear end, and a plurality of elongated members that connect the front end to the rear end, and actuators mounted to the plurality of elongated members. The actuators are configured to move in a radially outward direction from extended positions to retracted positions and comprise (i) proximal ends mounted to the plurality of elongated members and (ii) distal ends having vacuum suction cups. In the extended positions, the vacuum suction cups engage the fuselage on which the strongback apparatus is positioned. As the actuators moves from the extended positions to the retracted positions, the vacuum suction cups pull the fuselage away from the one-piece mandrel.
    Type: Application
    Filed: December 13, 2021
    Publication date: June 16, 2022
    Inventors: Byron James Autry, David Raines, Scott L. Smotherman, David M. Petka
  • Publication number: 20210261231
    Abstract: An apparatus for mounting a splice component for joining two or more workpieces includes a base plate and one or more bias assemblies. The base plate includes one or more passageways extending through the base plate and one or more barrier elements mounted proximate to the passageway(s). Each barrier element and associated passageway are configured to freely receive a protrusion of a splice component. The bias assembly includes a bias element that extends proximate to the passageway and is configured to move resiliently to urge the protrusion against the barrier element. The passageway, the barrier element, and the bias assembly are configured to allow movement of the splice component relative to the base plate transverse to a direction of force applied by the bias element on the protrusion.
    Type: Application
    Filed: February 21, 2020
    Publication date: August 26, 2021
    Applicant: The Boeing Company
    Inventors: David Howard Curry, III, David Raines, Scott L. Smotherman, Paul Gabriel Werntges, Dennis Ray Mathis, Charlie E. Branyon, III, Daniel B. Freeman