Patents by Inventor Joseph Paul Giesing

Joseph Paul Giesing 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).

  • Modular fuselage assemblies for aircraft, aircraft including modular fuselage assemblies, and MEl'hods of assembling modular fuselage assemblies
    Patent number: 11383817
    Abstract: Modular fuselage assemblies for aircraft, aircraft including modular fuselage assemblies, and methods of assembling modular fuselage assemblies. A modular fuselage assembly includes a plurality of fuselage lobes that may extend along a longitudinal axis of the modular fuselage assembly. Each fuselage lobe includes a plurality of frame members and a lobe skin that is operatively attached to the plurality of frame members and defines an external surface of the fuselage lobe. The modular fuselage assembly also includes a plurality of longerons extending along a longitudinal axis of the modular fuselage assembly. At least two fuselage lobes are operatively attached to each longeron and the plurality of fuselage lobes and the plurality of longerons at least partially bound a cargo hold defined within the modular fuselage assembly. The methods include methods of assembling the modular fuselage assemblies.
    Type: Grant
    Filed: July 19, 2019
    Date of Patent: July 12, 2022
    Assignee: The Boeing Company
    Inventors: Robert Erik Grip, Joseph Paul Giesing
  • MODULAR FUSELAGE ASSEMBLIES FOR AIRCRAFT, AIRCRAFT INCLUDING MODULAR FUSELAGE ASSEMBLIES, AND METHODS OF ASSEMBLING MODULAR FUSELAGE ASSEMBLIES
    Publication number: 20210016868
    Abstract: Modular fuselage assemblies for aircraft, aircraft including modular fuselage assemblies, and methods of assembling modular fuselage assemblies. A modular fuselage assembly includes a plurality of fuselage lobes that may extend along a longitudinal axis of the modular fuselage assembly. Each fuselage lobe includes a plurality of frame members and a lobe skin that is operatively attached to the plurality of frame members and defines an external surface of the fuselage lobe. The modular fuselage assembly also includes a plurality of longerons extending along a longitudinal axis of the modular fuselage assembly. At least two fuselage lobes are operatively attached to each longeron and the plurality of fuselage lobes and the plurality of longerons at least partially bound a cargo hold defined within the modular fuselage assembly. The methods include methods of assembling the modular fuselage assemblies.
    Type: Application
    Filed: July 19, 2019
    Publication date: January 21, 2021
    Inventors: Robert Erik Grip, Joseph Paul Giesing