Patents Assigned to PEGASUS AERONAUTICS CORPORATION
  • Patent number: 12168396
    Abstract: A hybrid powertrain system and method includes a prime mover driving a generator/motor to produce an AC power output. The AC power output is applied to a rectifier which is controlled to transform the applied AC power to DC power to supply a DC Power bus at a selected voltage and current. An energy storage device is also connected to the DC power bus and the current flow between the energy storage device and the DC power bus is monitored and compared to preselected values and the results of that comparison are used to alter the operation of the rectifier to increase or decrease, as needed, the current provided to the DC power bus as electrical loads on the DC power bus change.
    Type: Grant
    Filed: June 9, 2023
    Date of Patent: December 17, 2024
    Assignee: PEGASUS AERONAUTICS CORPORATION
    Inventors: Matthew McRoberts, Joseph Kinsella, John Biskey, Carl Engelmann
  • Patent number: 12113472
    Abstract: A system and method are disclosed for determining the mechanical angular position of a rotating member of a prime mover which is connected, directly, or indirectly, to an electric machine, such as a permanent magnet synchronous machine or an induction machine. The electrical angular position of the rotor of the electric machine is determined by a sensorless AC motor control system, such as a Field Oriented Control System or back EMF control system, and is used in turn to determine the mechanical angular position of the rotating member.
    Type: Grant
    Filed: June 3, 2020
    Date of Patent: October 8, 2024
    Assignee: PEGASUS AERONAUTICS CORPORATION
    Inventors: Matthew Mcroberts, Joseph Kinsella
  • Patent number: 11697350
    Abstract: A hybrid powertrain system and method includes a prime mover driving a generator/motor to produce an AC power output. The AC power output is applied to a rectifier which is controlled to transform the applied AC power to DC power to supply a DC Power bus at a selected voltage and current. An energy storage device is also connected to the DC power bus and the current flow between the energy storage device and the DC power bus is monitored and compared to preselected values and the results of that comparison are used to alter the operation of the rectifier to increase or decrease, as needed, the current provided to the DC power bus as electrical loads on the DC power bus change.
    Type: Grant
    Filed: September 1, 2021
    Date of Patent: July 11, 2023
    Assignee: PEGASUS AERONAUTICS CORPORATION
    Inventors: Matthew McRoberts, Joseph Kinsella, John Biskey, Carl Engelmann
  • Patent number: 11130411
    Abstract: A hybrid powertrain system and method includes a prime mover driving a generator/motor to produce an AC power output. The AC power output is applied to a rectifier which is controlled to transform the applied AC power to DC power to supply a DC Power bus at a selected voltage and current. An energy storage device is also connected to the DC power bus and the current flow between the energy storage device and the DC power bus is monitored and compared to preselected values and the results of that comparison are used to alter the operation of the rectifier to increase or decrease, as needed, the current provided to the DC power bus as electrical loads on the DC power bus change.
    Type: Grant
    Filed: June 8, 2020
    Date of Patent: September 28, 2021
    Assignee: PEGASUS AERONAUTICS CORPORATION
    Inventors: Matthew McRoberts, Joseph Kinsella, John Biskey, Carl Engelmann
  • Patent number: 10696178
    Abstract: A hybrid powertrain system and method includes a prime mover driving a generator/motor to produce an AC power output. The AC power output is applied to a rectifier which is controlled to transform the applied AC power to DC power to supply a DC Power bus at a selected voltage and current. An energy storage device is also connected to the DC power bus and the current flow between the energy storage device and the DC power bus is monitored and compared to preselected values and the results of that comparison are used to alter the operation of the rectifier to increase or decrease, as needed, the current provided to the DC power bus as electrical loads on the DC power bus change.
    Type: Grant
    Filed: August 10, 2017
    Date of Patent: June 30, 2020
    Assignee: PEGASUS AERONAUTICS CORPORATION
    Inventors: Matthew McRoberts, Joseph Kinsella, John Biskey, Carl Engelmann