Patents by Inventor Thomas Peter Joseph

Thomas Peter Joseph 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).

  • Publication number: 20210253260
    Abstract: An aircraft and propulsion system are provided. The aircraft includes an airframe including one or more of a fuselage, a wing, or an empennage. The aircraft includes an aircraft propulsion system including a front frame and an aft frame. A front mount link is connected to the airframe and the front frame, and the aft frame is selectively connected to the airframe by an aft mount link.
    Type: Application
    Filed: February 19, 2020
    Publication date: August 19, 2021
    Inventors: Timothy Leo Schelfaut, Anthony Michael Metz, Jonathan Edward Coleman, Thomas Peter Joseph, Brian Michael Dixon
  • Patent number: 11077954
    Abstract: A connection assembly for mounting an engine to a mounting structure. The engine is rotatable about an axis of rotation and defines an axial direction extending along the axis of rotation from a forward end to an aft end. The engine has a center of gravity. The connection assembly includes: an engine coupling piece coupled to the engine; and a connection piece connecting the engine coupling piece and the mounting structure, the connection piece being inclined toward the axial direction. A mounting system including the connection assembly is also described.
    Type: Grant
    Filed: December 20, 2017
    Date of Patent: August 3, 2021
    Assignee: General Electric Company
    Inventors: Timothy Leo Schelfaut, Lawrence Jerome Meyer, Anthony Michael Metz, Jonathan Edward Coleman, Thomas Peter Joseph
  • Publication number: 20190185170
    Abstract: A connection assembly for mounting an engine to a mounting structure. The engine is rotatable about an axis of rotation and defines an axial direction extending along the axis of rotation from a forward end to an aft end. The engine has a center of gravity. The connection assembly includes: an engine coupling piece coupled to the engine; and a connection piece connecting the engine coupling piece and the mounting structure, the connection piece being inclined toward the axial direction. A mounting system including the connection assembly is also described.
    Type: Application
    Filed: December 20, 2017
    Publication date: June 20, 2019
    Inventors: Timothy Leo SCHELFAUT, Lawrence Jerome MEYER, Anthony Michael METZ, Jonathan Edward COLEMAN, Thomas Peter JOSEPH
  • Patent number: 6330985
    Abstract: A link for use in an aircraft engine mounting system includes a span section having a first connector formed (at one end thereof and a second connector formed at another end thereof. A lumped mass is disposed on the span section for placing the resonant frequency of the link away from engine excitation frequencies.
    Type: Grant
    Filed: June 30, 2000
    Date of Patent: December 18, 2001
    Assignee: General Electric Company
    Inventors: John Alan Manteiga, Cornelius Harm Dykhuizen, Thomas Peter Joseph, Christopher James Wilusz, Robert Eugene Troup, Ethan Boger, Anthony John Franceschelli