Patents by Inventor Aurélien GONZALEZ

Aurélien GONZALEZ 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).

  • System for installing and removing a propulsion unit on a pylon of an aircraft
    Patent number: 11186379
    Abstract: The present disclosure concerns a system for installing and removing a propulsion unit on a pylon of an aircraft, a propulsion unit of the type including a nacelle and a turbojet engine, the turbojet engine being linked on the pylon by at least one front suspension and one rear suspension. The system includes a supporting structure which is adapted to support a thrust reverser device, a front suspension of the turbojet engine, which carries a front part of the supporting structure, and which is removably fastened on a front part of the pylon, and a rear suspension of the turbojet engine which carries a rear part of the supporting structure, and which is removably fastened on a rear part of the pylon, and the disengagement of said suspensions of the pylon allowing removing the propulsion unit mounted on the pylon.
    Type: Grant
    Filed: July 19, 2017
    Date of Patent: November 30, 2021
    Assignee: Safran Nacelles
    Inventors: Patrick Boileau, Olivier Kerbler, Julien Lezerac, Aurélien Gonzalez, Loïc Grall, Ludovic Toupet
  • SYSTEM FOR INSTALLING AND REMOVING A PROPULSION UNIT ON A PYLON OF AN AIRCRAFT
    Publication number: 20170313432
    Abstract: The present disclosure concerns a system for installing and removing a propulsion unit on a pylon of an aircraft, a propulsion unit of the type including a nacelle and a turbojet engine, the turbojet engine being linked on the pylon by at least one front suspension and one rear suspension. The system includes a supporting structure which is adapted to support a thrust reverser device, a front suspension of the turbojet engine, which carries a front part of the supporting structure, and which is removably fastened on a front part of the pylon, and a rear suspension of the turbojet engine which carries a rear part of the supporting structure, and which is removably fastened on a rear part of the pylon, and the disengagement of said suspensions of the pylon allowing removing the propulsion unit mounted on the pylon.
    Type: Application
    Filed: July 19, 2017
    Publication date: November 2, 2017
    Applicant: SAFRAN NACELLES
    Inventors: Patrick BOILEAU, Olivier KERBLER, Julien LEZERAC, Aurélien GONZALEZ, Loïc GRALL, Ludovic TOUPET