Patents Assigned to Proxflyer AS
  • Patent number: 8336809
    Abstract: An aircraft that is enabled to turn in a desired direction, and a method for controlling the flight direction of an aircraft, by employing differential drag on the respective wings. A control means that receives a control signal indicating a left turn increases the incidence angle on the left wing and reduces it on the right wing. For a right turn the opposite action is performed. The aircraft comprises airfoils that have increased drag as the incidence angle increases but have a generally constant lift.
    Type: Grant
    Filed: September 10, 2007
    Date of Patent: December 25, 2012
    Assignee: Proxflyer AS
    Inventor: Petter Muren
  • Patent number: 7204453
    Abstract: The present invention discloses a rotor that enables an aircraft to be passively stable in hover. The rotor, having a generally fixed geometry is tiltably connected to its rotor shaft. The outer part of the rotor blades have a pitch fixed relative to the rotational plane, whereas the inner part of the rotor blades have a pitch fixed relative to a reference plane perpendicular to the rotor shaft.
    Type: Grant
    Filed: April 15, 2004
    Date of Patent: April 17, 2007
    Assignee: Proxflyer AS
    Inventor: Petter Muren