Search Patents
  • Patent number: 10315760
    Abstract: An aerial vehicle adapted for vertical takeoff and landing using pivoting thrust producing elements for takeoff and landing. An aerial vehicle which is adapted to takeoff with thrust units providing vertical thrust and then transitioning to a horizontal flight path. An aerial vehicle with pivoting thrust units with propellers, wherein some or all of the propellers are able to be stowed and fully nested during forward flight.
    Type: Grant
    Filed: March 17, 2015
    Date of Patent: June 11, 2019
    Assignee: Joby Aero, Inc.
    Inventors: JoeBen Bevirt, Alex Stoll
  • Patent number: 9694911
    Abstract: An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements and a set of tail mounted rotors for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle uses different configurations of its wing mounted rotors and propellers to reduce drag in all flight modes.
    Type: Grant
    Filed: March 18, 2014
    Date of Patent: July 4, 2017
    Assignee: Joby Aviation, Inc.
    Inventors: Joeben Bevirt, Alex Stoll
  • Patent number: 10625852
    Abstract: An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements and a set of tail mounted rotors for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle uses different configurations of its wing mounted rotors and propellers to reduce drag in all flight modes.
    Type: Grant
    Filed: March 17, 2015
    Date of Patent: April 21, 2020
    Assignee: Joby Aero, Inc.
    Inventors: Joeben Bevirt, Alex Stoll
  • Patent number: 10046855
    Abstract: An aerial vehicle adapted for vertical takeoff and landing using pivoting thrust producing elements for takeoff and landing. An aerial vehicle which is adapted to takeoff with thrust units providing vertical thrust and then transitioning to a horizontal flight path. An aerial vehicle with pivoting thrust units with propellers, wherein some or all of the propellers are able to be stowed and fully nested during forward flight. An aerial vehicle adapted to withstand impacts upon its propellers. An aerial vehicle able to quickly alter the thrust of its propellers.
    Type: Grant
    Filed: March 18, 2015
    Date of Patent: August 14, 2018
    Assignee: Joby Aero, Inc.
    Inventors: JoeBen Bevirt, Alex Stoll