Patents Assigned to Supersonie Aerospace International, LLC
  • Canard position and dihedral for boom reduction and pitch/directional control
    Patent number: 7416155
    Abstract: A supersonic aircraft comprises a fuselage extending forward and aft, wings coupled to lateral sides of the fuselage, and canards coupled to lateral sides of the fuselage forward of the wings. The individual canards are configured to generate shocks that wrap around the fuselage and intersect with wing leading edges on opposing sides of the fuselage.
    Type: Grant
    Filed: June 7, 2005
    Date of Patent: August 26, 2008
    Assignee: Supersonie Aerospace International, LLC
    Inventors: Robert S. Cuccias, John M. Morgenstern, Alan E. Arslan, Howard Lee