Patents by Inventor Audrey Benaben

Audrey Benaben 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).

  • Publication number: 20230082125
    Abstract: A spacer element serving to obtain a spacer washer positioned between first and second parts of an assembly. The spacer element includes a body having the same geometry as the spacer washer that is to be obtained and a circular score line whose diameter is equal to the internal diameter of the spacer washer that is to be obtained, this score line being configured to break upon insertion of a shank of a connection element, and a centering pad configured to center the score line with respect to the through-orifices of the first and second parts that are configured to accommodate the shank of a connection element when the centering pad is inserted into one of the through-orifices.
    Type: Application
    Filed: September 7, 2022
    Publication date: March 16, 2023
    Inventors: Clément CHIROL, Audrey BENABEN, Guillaume PICHON
  • Patent number: 10800549
    Abstract: A method for assembling a primary structure of an aircraft pylon, includes a step of fixing an angle bracket to each of the first and second lateral panels such as to obtain an L form for each of the first and second lateral panels prior to a placement of said L forms each placed against two sides of each transverse frame. This assembly technique makes it possible to reduce the mounting clearances such that it is unnecessary to fit shims, resulting in a reduction of mounting time and manufacturing costs.
    Type: Grant
    Filed: October 2, 2018
    Date of Patent: October 13, 2020
    Assignees: Airbus Operations S.A.S., AIRBUS OPERATIONS LTD
    Inventors: Stéphane Dostes, Thierry Theron, Audrey Benaben, Thomas Deforet, Julien Moulis, Joel Dedieu, Robert Whiffen, François Martinel
  • Publication number: 20200231294
    Abstract: A method for assembling an aircraft pylon having a primary structure and at least one internal system at least partially positioned within the primary structure, wherein the internal system is positioned inside the primary structure before the last lateral panel of the primary structure is attached. The absence of one of the lateral panels facilitates the installation of the internal systems.
    Type: Application
    Filed: January 10, 2020
    Publication date: July 23, 2020
    Applicants: Airbus Operations S.A.S., AIRBUS OPERATIONS LTD
    Inventors: François Martinel, Joel Dedieu, Thierry Theron, Julien Moulis, Thomas Deforet, Audrey Benaben, Robert Whiffen
  • Publication number: 20190112074
    Abstract: A method for assembling a primary structure of an aircraft pylon, includes a step of fixing an angle bracket to each of the first and second lateral panels such as to obtain an L form for each of the first and second lateral panels prior to a placement of said L forms each placed against two sides of each transverse frame. This assembly technique makes it possible to reduce the mounting clearances such that it is unnecessary to fit shims, resulting in a reduction of mounting time and manufacturing costs.
    Type: Application
    Filed: October 2, 2018
    Publication date: April 18, 2019
    Applicants: Airbus Operations S.A.S., AIRBUS OPERATIONS LTD
    Inventors: Stéphane Dostes, Thierry Theron, Audrey Benaben, Thomas Deforet, Julien Moulis, Joel Dedieu, Robert Whiffen, François Martinel