Patents by Inventor Julien PERROT

Julien PERROT 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 and equipment for purging a reservoir and associated purge and assembly processes
    Patent number: 10994858
    Abstract: A system for purging an aircraft fuel reservoir includes a body (48) configured to be assembled on the aircraft fuel reservoir (16) and a valve (50), received in the body (48), and having a released configuration of an outlet channel (70) and a tight closed configuration of the outlet channel (70). The system further comprises a transport pipe (44) secured to the body (48), the transport pipe (44) being configured to be fluidly connected to a fuel supply pipe (20) configured to supply an energy producing device. The transport pipe (44) extends at least between a fuel suction inlet (52) and a discharge outlet (54), the suction inlet (52) being configured to emerge in the aircraft fuel reservoir (16) and the discharge outlet (54) being configured to emerge in the supply pipe (20) when the body (48) is mounted on the aircraft fuel reservoir (16).
    Type: Grant
    Filed: July 17, 2019
    Date of Patent: May 4, 2021
    Assignee: DASSAULT AVIATION
    Inventors: Teddy Dufaure, Jean- Philippe Dupont, Julien Perrot
  • SYSTEM AND EQUIPMENT FOR PURGING A RESERVOIR AND ASSOCIATED PURGE AND ASSEMBLY PROCESSES
    Publication number: 20200023990
    Abstract: A system for purging an aircraft fuel reservoir includes a body (48) configured to be assembled on the aircraft fuel reservoir (16) and a valve (50), received in the body (48), and having a released configuration of an outlet channel (70) and a tight closed configuration of the outlet channel (70). The system further comprises a transport pipe (44) secured to the body (48), the transport pipe (44) being configured to be fluidly connected to a fuel supply pipe (20) configured to supply an energy producing device. The transport pipe (44) extends at least between a fuel suction inlet (52) and a discharge outlet (54), the suction inlet (52) being configured to emerge in the aircraft fuel reservoir (16) and the discharge outlet (54) being configured to emerge in the supply pipe (20) when the body (48) is mounted on the aircraft fuel reservoir (16).
    Type: Application
    Filed: July 17, 2019
    Publication date: January 23, 2020
    Inventors: Teddy DUFAURE, Jean- Philippe DUPONT, Julien PERROT