Patents by Inventor Julien GARNIER

Julien GARNIER 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: 11959706
    Abstract: The invention relates to a heat exchanger (20) plate (1, 2a) intended to delimit at least one channel (30, 30a, 30b) for circulation of a fluid, the circulation plate (1) being provided with a bottom (3) and a raised rim (5, 5a-5h) that surrounds the bottom (3), the circulation plate (1) comprising at least one opening (7, 7a-7d) through which a fluid can enter the channel (30, 30a, 30b), characterized in that the opening (7, 7a-7d) is delimited by at least one at least partially rectilinear edge (9a). Application to the field of heat exchanges.
    Type: Grant
    Filed: September 25, 2019
    Date of Patent: April 16, 2024
    Assignee: VALEO SYSTEMES THERMIQUES
    Inventors: Julien Tissot, Kamel Azzouz, Michael Lissner, Cédric De Vaulx, Patrick Leblay, Sébastien Garnier
  • Patent number: 10921179
    Abstract: An assembly for a turbine engine, the assembly including a casing and an impeller rotatably movable inside the casing, the impeller including at least one blade having a tip edge opposite the casing, wherein the tip edge includes a magnet and wherein the casing includes an electrical conductor suitable for generating between the terminals thereof an electric voltage induced by the magnet of the tip edge opposite same and representing vibrations sustained by the tip edge of the blade when the impeller is rotated.
    Type: Grant
    Filed: December 22, 2014
    Date of Patent: February 16, 2021
    Assignee: SAFRAN HELICOPTER ENGINES
    Inventors: Arnaud Talon, Gilbert Arrouge, Jean-Yves Cazaux, Julien Garnier
  • Patent number: 10508948
    Abstract: A turbine engine assembly includes a housing and a bladed wheel rotatable within the housing. The bladed wheel includes a blade including a head opposite the housing. The head includes a magnet and the housing includes first and second electrical conductors. Each electrical conductor generates, across terminals thereof, an electrical voltage induced by the magnet of the head opposite the housing and that represents vibrations of the head of the blade when the bladed wheel is rotated. The first electrical conductor includes a first central portion extending around the rotational axis of the bladed wheel and includes two mutually facing ends, and the second electrical conductor includes a second central portion passing through a space left by the first central portion between the two ends thereof. The arrangement of the electrical conductors makes it possible to obtain two voltages for determining an axial vibration speed at the tip.
    Type: Grant
    Filed: December 22, 2014
    Date of Patent: December 17, 2019
    Assignee: SAFRAN HELICOPTER ENGINES
    Inventors: Arnaud Talon, Jean-Yves Cazaux, Guillaume Chauvin, Julien Garnier
  • Publication number: 20170131138
    Abstract: A turbine engine assembly including a housing and a bladed wheel rotatable within the housing. The bladed wheel includes at least one blade including a head opposite the housing. The head includes a magnet and the housing includes a first and second electrical conductor. Each electrical conductor is configured to generate, across terminals thereof, an electrical voltage induced by the magnet of the head opposite the housing and that represents vibrations to which the head of the blade is subjected when the bladed wheel is rotated. The first electrical conductor includes a first central portion extending around the rotational axis of the bladed wheel and includes two mutually facing ends, and the second electrical conductor includes a second central portion passing through a space left by the first central portion between the two ends thereof.
    Type: Application
    Filed: December 22, 2014
    Publication date: May 11, 2017
    Applicant: TURBOMECA
    Inventors: Arnaud TALON, Jean-Yves CAZAUX, Guillaume CHAUVIN, Julien GARNIER
  • Publication number: 20160320230
    Abstract: An assembly for a turbine engine, the assembly including a casing and an impeller rotatably movable inside the casing, the impeller including at least one blade having a tip edge opposite the casing, wherein the tip edge includes a magnet and wherein the casing includes an electrical conductor suitable for generating between the terminals thereof an electric voltage induced by the magnet of the tip edge opposite same and representing vibrations sustained by the tip edge of the blade when the impeller is rotated.
    Type: Application
    Filed: December 22, 2014
    Publication date: November 3, 2016
    Applicant: TURBOMECA
    Inventors: Arnaud TALON, Gilbert ARROUGE, Jean-Yves CAZAUX, Julien GARNIER