Patents Assigned to Hybridskys Technology Pty Ltd
  • Publication number: 20190263519
    Abstract: A hybrid aircraft comprises at least three independent electric motors each arranged to drive a respective rotor; and an internal combustion engine arranged to drive at least two rotor, which are preferably horizontally spaced apart. There is also a controller for providing speed control signals to the electric motor driven rotors and a throttle control signal for controlling the throttle of the internal combustion engine, based on a flight control signal.
    Type: Application
    Filed: October 24, 2017
    Publication date: August 29, 2019
    Applicant: Hybridskys Technology Pty Ltd
    Inventor: Murray Argus