Patents by Inventor Denis Millepied

Denis Millepied 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).

  • Composite structuring panel for the trailing edge of an aircraft element
    Patent number: 8936216
    Abstract: The invention relates to a composite structuring panel (1) for the trailing edge of an aircraft element, having: an upper surface (3); a lower surface (5); an edge (7) connecting said upper (3) and lower (5) surfaces; the upper surface (3) and the lower surface (5) being connected by transverse stiffeners (9) and the structuring panel being made of a unitary part forming the upper surface (3), the lower surface (5), the edge (7), and the transverse stiffeners (9). The invention also relates to a method for manufacturing such a panel (1), and to an aircraft element comprising such a panel (1).
    Type: Grant
    Filed: May 28, 2010
    Date of Patent: January 20, 2015
    Assignee: Societe Lorraine de Construction Aeronautique
    Inventors: Didier Remene, Denis Millepied, Paulo Francisco, Valérian Montagne, Jean-Luc Pacary, Arnaud Bertrand
  • METHOD FOR THE PRODUCTION OF A COMPOSITE TRAILING EDGE PANEL FOR AN AIRCRAFT ELEMENT
    Publication number: 20120267479
    Abstract: The invention relates to a method for producing a structural composite trailing edge panel (1) for an aircraft element having: an upper surface (3), a lower surface (5), and a trailing edge (7) connecting said upper (3) and lower (5) surfaces, the upper surface (3) and the lower surface (5) being connected by transverse stiffeners (9), at least one longitudinal spar (10) being positioned in such a way that the directrix (?10) of each longitudinal spar (10) and the directrix (?9) of the transverse stiffeners (9) are not collinear and the structuring panel (1) being made up of a one-piece component forming the upper surface (3), the lower surface (5), the trailing edge (7), the transverse stiffeners (9) and the spar or spars (10).
    Type: Application
    Filed: December 14, 2010
    Publication date: October 25, 2012
    Applicant: SOCIETE LORRAINE DE CONSTRUCTION AERONAUTIQUE
    Inventors: Denis Millepied, Jean-Luc Pacary, Arnaud Bertrand, Valerian Montagne
  • COMPOSITE STRUCTURING PANEL FOR THE TRAILING EDGE OF AN AIRCRAFT ELEMENT
    Publication number: 20120061515
    Abstract: The invention relates to a composite structuring panel (1) for the trailing edge of an aircraft element, having: an upper surface (3); a lower surface (5); an edge (7) connecting said upper (3) and lower (5) surfaces; the upper surface (3) and the lower surface (5) being connected by transverse stiffeners (9) and the structuring panel being made of a unitary part forming the upper surface (3), the lower surface (5), the edge (7), and the transverse stiffeners (9). The invention also relates to a method for manufacturing such a panel (1), and to an aircraft element comprising such a panel (1).
    Type: Application
    Filed: May 28, 2010
    Publication date: March 15, 2012
    Applicant: SOCIETE LORRAINE DE CONSTRUCTION AERONAUTIQUE
    Inventors: Didier Remene, Denis Millepied, Paulo Francisco, Valérian Montagne, Jean-Luc Pacary, Arnaud Bertrand