Patents by Inventor Yannick Wattier

Yannick Wattier 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: 10633073
    Abstract: The invention relates to a device for assembling a plurality of panels of an aircraft fuselage, said device comprising at least one anvil body, comprising a surface for supporting the said plurality of panels, the said anvil body comprising at least one anvil rail mounted movably in a cavity of the anvil body and configured to move between a top position in which the upper surface of the anvil rail extends into the extension of the support surface and a bottom position in which a workspace is created between the upper surface of the anvil rail and the support surface so as to allow a machining and/or stripping tool to pass through.
    Type: Grant
    Filed: December 19, 2014
    Date of Patent: April 28, 2020
    Assignee: AEROLIA
    Inventors: Franck Darras, Yannick Wattier
  • Publication number: 20170001734
    Abstract: The invention relates to a device for assembling a plurality of panels of an aircraft fuselage, said device comprising at least one anvil body, comprising a surface for supporting the said plurality of panels, the said anvil body comprising at least one anvil rail mounted movably in a cavity of the anvil body and configured to move between a top position in which the upper surface of the anvil rail extends into the extension of the support surface and a bottom position in which a workspace is created between the upper surface of the anvil rail and the support surface so as to allow a machining and/or stripping tool to pass through.
    Type: Application
    Filed: December 19, 2014
    Publication date: January 5, 2017
    Inventors: Franck Darras, Yannick Wattier
  • Publication number: 20170001735
    Abstract: The invention relates to a system for assembling a plurality of panels of an aircraft fuselage, said system comprising at least one anvil body, at least one first panel and one second panel, and movement means mounted on the said anvil body, the said movement means being arranged to move the first panel in relation to the second panel between a first machining position in which one edge of the first panel and one edge of the second panel are spaced a machining distance apart so as to allow a machining tool to pass between the said edges in order to machine them simultaneously and a second welding position in which the said edge of the first panel and the said edge of the second panel are adjacent and resting on the said anvil body.
    Type: Application
    Filed: December 19, 2014
    Publication date: January 5, 2017
    Inventors: Franck Darras, Yannick Wattier