Patents by Inventor Aurelie Piat

Aurelie Piat 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).

  • Oblique panel at the rear of a central box of an aircraft fuselage
    Patent number: 8672268
    Abstract: An aircraft structure includes a wing spar (10), with orbital frames (24, 24?, 24?) arranged in transverse planes, right and left horizontal spars (26) connected to the wing spar (10) at the upper panel (14) of the spar respectively to the right and to the left of the spar, and for each right or left horizontal spar (26), a triangular panel (50) that includes a wall (60), a first edge arranged at the horizontal spar (26), a second side arranged at the wing spar (10), and a third side at which a first rectilinear oblique reinforcement (62) connecting the horizontal spar (26) and the wing spar (10) is provided, characterized in that the triangular panel (50) includes at least one second rectilinear oblique reinforcement (64) that connects the horizontal spar (26) and the wing spar (10).
    Type: Grant
    Filed: November 30, 2011
    Date of Patent: March 18, 2014
    Assignee: Airbus Operations S.A.S.
    Inventors: Julien Guillemaut, Aurelie Piat, Jerome Comagro, Frederic Fort, Dominique Guittard, Jean Marc Durand
  • OBLIQUE PANEL AT THE REAR OF A CENTRAL BOX OF AN AIRCRAFT FUSELAGE
    Publication number: 20120138746
    Abstract: An aircraft structure includes a wing spar (10), with orbital frames (24, 24?, 24?) arranged in transverse planes, right and left horizontal spars (26) connected to the wing spar (10) at the upper panel (14) of the spar respectively to the right and to the left of the spar, and for each right or left horizontal spar (26), a triangular panel (50) that includes a wall (60), a first edge arranged at the horizontal spar (26), a second side arranged at the wing spar (10), and a third side at which a first rectilinear oblique reinforcement (62) connecting the horizontal spar (26) and the wing spar (10) is provided, characterized in that the triangular panel (50) includes at least one second rectilinear oblique reinforcement (64) that connects the horizontal spar (26) and the wing spar (10).
    Type: Application
    Filed: November 30, 2011
    Publication date: June 7, 2012
    Applicant: AIRBUS OPERATIONS (SAS)
    Inventors: Julien GUILLEMAUT, Aurélie PIAT, Jerome COMAGRO, Frederic FORT, Dominique GUITTARD, Jean Marc DURAND