Patents by Inventor Emilie Luche

Emilie Luche 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).

  • Tool for simultaneously holding several attachment clips in contact with an aircraft fuselage frame element
    Patent number: 9789948
    Abstract: A system with attachment clips designed to fix an attachment element of an aircraft fuselage frame onto a fuselage skin and/or to stiffeners fitted onto this fuselage skin is provided. The system includes tooling elements arranged alternately with the clips such that they connect to each other, in order to reduce the fabrication time and cost of an aircraft fuselage.
    Type: Grant
    Filed: July 31, 2014
    Date of Patent: October 17, 2017
    Assignee: Airbus Operations (S.A.S.)
    Inventors: Yannick Marin, Emilie Luche
  • Aircraft fuselage frame element integrating tabs for the fastening of stiffeners
    Patent number: 9745043
    Abstract: In order to reduce the time and the cost of manufacturing an aircraft fuselage, the subject matter disclosed herein provide an aircraft fuselage frame element comprising a core provided with at least one through-opening intended for the passing of a fuselage stiffener, and further comprising, associated with each opening, a tab for the fastening of the frame element onto the fuselage stiffener, with the tab being a single piece with the core and connected to the latter by a fold that delimits the opening.
    Type: Grant
    Filed: July 31, 2014
    Date of Patent: August 29, 2017
    Assignee: Airbus Operations (S.A.S.)
    Inventors: Yannick Marin, Damien Guilloteau, Emilie Luche
  • TOOL FOR SIMULTANEOUSLY HOLDING SEVERAL ATTACHMENT CLIPS IN CONTACT WITH AN AIRCRAFT FUSELAGE FRAME ELEMENT
    Publication number: 20150034766
    Abstract: The subject matter disclosed herein discloses a system with attachment clips designed to fix an attachment element of an aircraft fuselage frame onto a fuselage skin and/or to stiffeners fitted onto this fuselage skin, the system also comprising tooling elements arranged alternately with the clips that they connect to each other, in order to reduce the fabrication time and cost of an aircraft fuselage.
    Type: Application
    Filed: July 31, 2014
    Publication date: February 5, 2015
    Inventors: Yannick MARIN, Emilie LUCHE
  • AIRCRAFT FUSELAGE FRAME ELEMENT INTEGRATING TABS FOR THE FASTENING OF STIFFENERS
    Publication number: 20150034763
    Abstract: In order to reduce the time and the cost of manufacturing an aircraft fuselage, the subject matter disclosed herein provide an aircraft fuselage frame element comprising a core provided with at least one through-opening intended for the passing of a fuselage stiffener, and further comprising, associated with each opening, a tab for the fastening of the frame element onto the fuselage stiffener, with the tab being a single piece with the core and connected to the latter by a fold that delimits the opening.
    Type: Application
    Filed: July 31, 2014
    Publication date: February 5, 2015
    Inventors: Yannick Marin, Damien Guilloteau, Emilie Luche