Patents by Inventor Matthew Senesac

Matthew Senesac 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: 11142326
    Abstract: An aircraft nacelle is disclosed and includes a first fan cowl and a second fan cowl. An opening is defined in an exterior surface of the first fan cowl. The aircraft nacelle also includes a blade, a latch mechanism, an arm, and a linkage assembly operably connecting the arm to the blade. The blade is moveable along between a stowed position and a deployed position. The latch mechanism is moveable between a latched position an unlatched position where a portion of the latch mechanism obstructs a path of movement of the blade. The arm is unable to move from an extended position where a portion of the arm extends through the opening in the exterior surface of the aircraft nacelle into a retracted position within an interior volume of the aircraft nacelle when the blade is in the deployed position and the latch mechanism is in the unlatched position.
    Type: Grant
    Filed: July 27, 2018
    Date of Patent: October 12, 2021
    Assignee: The Boeing Company
    Inventors: Kyle A. Thomas, Rhoda Rebecca Toliver, Michael Roethle, Matthew Joseph Woerly, Matthew Senesac, Kushy Sachdeva
  • Publication number: 20200031484
    Abstract: An aircraft nacelle is disclosed and includes a first fan cowl and a second fan cowl. An opening is defined in an exterior surface of the first fan cowl. The aircraft nacelle also includes a blade, a latch mechanism, an arm, and a linkage assembly operably connecting the arm to the blade. The blade is moveable along between a stowed position and a deployed position. The latch mechanism is moveable between a latched position an unlatched position where a portion of the latch mechanism obstructs a path of movement of the blade. The arm is unable to move from an extended position where a portion of the arm extends through the opening in the exterior surface of the aircraft nacelle into a retracted position within an interior volume of the aircraft nacelle when the blade is in the deployed position and the latch mechanism is in the unlatched position.
    Type: Application
    Filed: July 27, 2018
    Publication date: January 30, 2020
    Inventors: Kyle A. Thomas, Rhoda Rebecca Toliver, Michael Roethle, Matthew Joseph Woerly, Matthew Senesac, Kushy Sachdeva