Patents by Inventor Robert Anthony Godlasky

Robert Anthony Godlasky 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).

  • VERTICAL TAKEOFF AND LANDING AIRCRAFT
    Publication number: 20180273168
    Abstract: An aircraft for use in fixed wing flight mode and rotor flight mode while maintaining a horizontal fuselage is provided. The aircraft can include a fuselage, wings, rotor, and a plurality of engines. The rotor can comprise a wing attachment assembly further comprising a rotating support. A rotating section can comprise a central support and the wings, with a plurality of engines attached to the rotating section. In a rotor flight mode, the rotating section can rotate around a longitudinal axis of the rotor providing lift for the aircraft similar to the rotor of a helicopter. In a fixed wing flight mode, the rotating section does not rotate around a longitudinal axis of the rotor, providing lift for the aircraft similar to a conventional airplane. The same engines that provide torque to power the rotor in rotor flight mode also power the aircraft in fixed-wing flight mode.
    Type: Application
    Filed: March 21, 2018
    Publication date: September 27, 2018
    Applicant: DZYNE Technologies, Inc.
    Inventors: Mark Allan Page, Matthew Robert McCue, Robert Anthony Godlasky
  • Long endurance vertical takeoff and landing aircraft
    Patent number: 9688398
    Abstract: An aircraft for use in fixed wing flight mode and rotor flight mode is provided. The aircraft can include a fuselage, wings, and a plurality of engines. The fuselage can comprise a wing attachment region further comprising a rotating support. A rotating section can comprise a rotating support and the wings, with a plurality of engines attached to the rotating section. In a rotor flight mode, the rotating section can rotate around a longitudinal axis of the fuselage providing lift for the aircraft similar to the rotor of a helicopter. In a fixed wing flight mode, the rotating section does not rotate around a longitudinal axis of the fuselage, providing lift for the aircraft similar to a conventional airplane. The same engines that provide torque to power the rotor in rotor flight mode also power the aircraft in fixed wing flight mode.
    Type: Grant
    Filed: March 10, 2015
    Date of Patent: June 27, 2017
    Assignee: DZYNE Technologies, INC.
    Inventors: Mark Allan Page, Matthew Robert McCue, Robert Anthony Godlasky
  • LONG ENDURANCE VERTICAL TAKEOFF AND LANDING AIRCRAFT
    Publication number: 20150183514
    Abstract: An aircraft for use in fixed wing flight mode and rotor flight mode is provided. The aircraft can include a fuselage, wings, and a plurality of engines. The fuselage can comprise a wing attachment region further comprising a rotating support. A rotating section can comprise a rotating support and the wings, with a plurality of engines attached to the rotating section. In a rotor flight mode, the rotating section can rotate around a longitudinal axis of the fuselage providing lift for the aircraft similar to the rotor of a helicopter. In a fixed wing flight mode, the rotating section does not rotate around a longitudinal axis of the fuselage, providing lift for the aircraft similar to a conventional airplane. The same engines that provide torque to power the rotor in rotor flight mode also power the aircraft in fixed wing flight mode.
    Type: Application
    Filed: March 10, 2015
    Publication date: July 2, 2015
    Applicant: DZYNE Technologies, Inc.
    Inventors: MARK ALLAN PAGE, MATTHEW ROBERT MCCUE, ROBERT ANTHONY GODLASKY
  • Long endurance vertical takeoff and landing aircraft
    Patent number: 8991751
    Abstract: An aircraft for use in fixed wing flight mode and rotor flight mode is provided. The aircraft can include a fuselage, wings, and a plurality of engines. The fuselage can comprise a wing attachment region further comprising a rotating support. A rotating section can comprise a rotating support and the wings, with a plurality of engines attached to the rotating section. In a rotor flight mode, the rotating section can rotate around a longitudinal axis of the fuselage providing lift for the aircraft similar to the rotor of a helicopter. In a fixed wing flight mode, the rotating section does not rotate around a longitudinal axis of the fuselage, providing lift for the aircraft similar to a conventional airplane. The same engines that provide torque to power the rotor in rotor flight mode also power the aircraft in fixed wing flight mode.
    Type: Grant
    Filed: March 23, 2012
    Date of Patent: March 31, 2015
    Assignee: DZYNE Technologies, Inc.
    Inventors: Mark Allan Page, Matthew Robert McCue, Robert Anthony Godlasky
  • LONG ENDURANCE VERTICAL TAKEOFF AND LANDING AIRCRAFT
    Publication number: 20120248259
    Abstract: An aircraft for use in fixed wing flight mode and rotor flight mode is provided. The aircraft can include a fuselage, wings, and a plurality of engines. The fuselage can comprise a wing attachment region further comprising a rotating support. A rotating section can comprise a rotating support and the wings, with a plurality of engines attached to the rotating section. In a rotor flight mode, the rotating section can rotate around a longitudinal axis of the fuselage providing lift for the aircraft similar to the rotor of a helicopter. In a fixed wing flight mode, the rotating section does not rotate around a longitudinal axis of the fuselage, providing lift for the aircraft similar to a conventional airplane. The same engines that provide torque to power the rotor in rotor flight mode also power the aircraft in fixed wing flight mode.
    Type: Application
    Filed: March 23, 2012
    Publication date: October 4, 2012
    Inventors: Mark Allan Page, Matthew Robert McCue, Robert Anthony Godlasky