Patents by Inventor Stephanie Dantin

Stephanie Dantin has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 8186619
    Abstract: A wing arrangement of an aircraft has a wing and at least one pylon for suspending an engine below the wing. The wing has a leading edge with a high-lift device, which is able to move between a deployed position in which the high-lift device projects forward of the leading edge, and which is interrupted in a forward intermediate region of the wing located at the leading edge, the pylon having a forward edge extending forward of the leading edge of the wing between a forward upper portion connected to the wing in the forward intermediate region and a forward lower portion connected to a nacelle of the engine. An element of narrow elongate shape protrudes longitudinally from the forward edge and, during flight at a high angle of attack of the aircraft, generates a vortex of aerodynamic flow that is propagated toward the forward intermediate region above the wing.
    Type: Grant
    Filed: March 13, 2009
    Date of Patent: May 29, 2012
    Assignee: Airbus Operations SAS
    Inventors: Cyril Bonnaud, Stephanie Dantin, Marjorie Defos, Thierry Fol
  • Patent number: 8006931
    Abstract: An aircraft wing arrangement including a wing and at least one strut for attaching the aircraft engine suspended under the wing and including a front zone situated projecting towards the front with respect to a leading edge of the wing. The front zone includes a lateral projection delimiting a lateral air flow channel while being projected towards a proximal end of the wing.
    Type: Grant
    Filed: March 28, 2007
    Date of Patent: August 30, 2011
    Assignee: AIRBUS France
    Inventors: Stephanie Dantin, Thierry Fol, Ludovic Gerard, Philippe Jimenez
  • Publication number: 20090230251
    Abstract: A wing arrangement of an aircraft has a wing and at least one pylon for suspending an engine below the wing. The wing has a leading edge with a high-lift device, which is able to move between a deployed position in which the high-lift device projects forward of the leading edge, and which is interrupted in a forward intermediate region of the wing located at the leading edge, the pylon having a forward edge extending forward of the leading edge of the wing between a forward upper portion connected to the wing in the forward intermediate region and a forward lower portion connected to a nacelle of the engine. An element of narrow elongate shape protrudes longitudinally from the forward edge and, during flight at a high angle of attack of the aircraft, generates a vortex of aerodynamic flow that is propagated toward the forward intermediate region above the wing.
    Type: Application
    Filed: March 13, 2009
    Publication date: September 17, 2009
    Applicant: AIRBUS FRANCE
    Inventors: Cyril Bonnaud, Stephanie Dantin, Marjorie Defos, Thierry Fol
  • Publication number: 20090032639
    Abstract: An aircraft wing arrangement including a wing and at least one strut for attaching the aircraft engine suspended under the wing and including a front zone situated projecting towards the front with respect to a leading edge of the wing. The front zone includes a lateral projection delimiting a lateral air flow channel while being projected towards a proximal end of the wing.
    Type: Application
    Filed: March 28, 2007
    Publication date: February 5, 2009
    Applicant: AIRBUS FRANCE
    Inventors: Stephanie Dantin, Thierry Fol, Ludovic Gerard, Philippe Jimenez