Patents by Inventor Laurent RAVIER

Laurent RAVIER 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: 20230264054
    Abstract: Disclosed is a fire-fighting device, which includes a casing that delimits an inner cavity in which at least one dispersible fire-extinguishing agent is deposited, and pyrotechnics suitable for generating an explosion causing the casing to rupture and the fire-extinguishing agent to be dispersed. The pyrotechnics include at least one explosive charge, generating the explosion, and a detonator for triggering the explosion of the at least one explosive charge. The detonator includes an ignition device designed to trigger, when in an active state, the explosion of the at least one explosive charge, and an impact sensor designed to detect a mechanical impact received by the device and to bring the ignition device to the active state upon detection of the mechanical impact.
    Type: Application
    Filed: March 25, 2021
    Publication date: August 24, 2023
    Inventors: Jacques PITOUX, Aline BERTAGNE, Alec BERTAGNE, Pierrick DURET, Patrice Queiras, Bruno Jean Gilbert LIVERRGNE, Youcef DJANEH, Morgane RAVIER, Robin TOURNOUX, Jérôme LUPO, Laurent RAVIER, René Alphone Joseph Marie DURET, Marie-Renée Blanche Michèle DURET, Baptiste Sylvain Charly GADROY, Faustine LERAY, Jean-François KWASEK
  • Patent number: 10981644
    Abstract: An assembly for an aircraft including an aircraft wall in which a routing slit is formed. A drive shaft of a bearing surface passes through the slit while remaining free to move along the slit. A seal is provided to seal the slit.
    Type: Grant
    Filed: February 11, 2019
    Date of Patent: April 20, 2021
    Assignee: SONACA S.A.
    Inventors: Albert-Paul Gonze, Laurent Ravier
  • Publication number: 20190248470
    Abstract: The invention relates to an assembly for an aircraft comprising an aircraft wall in which a routing slit is formed, a drive shaft of a bearing surface that passes through the slit while remaining free to move along the slit, and a seal to seal this slit. According to the invention, the seal is formed in two parts, comprising a lower seal part and an upper seal part arranged facing each other on opposite sides of the slit, each of the two parts comprising a lip forming contact tracks between which the drive shaft is squeezed and moves while deforming them during a phase in which the bearing surface is moved, these lips being in the shape of rabbit ears so that they can wind around the shaft so as to limit parasite opening spaces, and to prevent misalignment.
    Type: Application
    Filed: February 11, 2019
    Publication date: August 15, 2019
    Inventors: Albert-Paul GONZE, Laurent RAVIER