Patents by Inventor Frédéric PATARD

Frédéric PATARD 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: 11585236
    Abstract: A bearing support designed to be secured to a stationary turbojet element for supporting a journal, including a cone which widens from a central portion for supporting the journal to a portion for securing to the stationary element, a cylindrical body extending the portion for securing to the stationary element while surrounding the cone, an upstream skirt carried by the cone for defining an upstream enclosure for the central portion, and at least one downstream revolution element carried by the cone for defining a downstream enclosure for the central portion. The bearing support can be made as a single part produced by additive manufacturing.
    Type: Grant
    Filed: March 20, 2019
    Date of Patent: February 21, 2023
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Dimitri Daniel Gabriel Marquie, Adrien Jacques Philippe Fabre, Frédéric Patard, Pierre Jean-Baptiste Metge
  • Patent number: 11261754
    Abstract: The invention relates to a turbojet bearing housing including a fixed envelope traversed by a rotor, this envelope including a cylindrical end surrounding a seal ensuring the leak tightness of the cylindrical end of the envelope with the rotor, this envelope being equipped with a shell screwed onto the cylindrical end thereof, this shell including radial channels emerging opposite the seal while being arranged so that an air stream traversing the seal towards the housing mainly comes from these radial channels.
    Type: Grant
    Filed: February 5, 2018
    Date of Patent: March 1, 2022
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Frédéric Patard, Antoine Jean-Philippe Beaujard, Philippe Pierre Vincent Bouiller, Christophe Caplain, Maxime Aurélien Rotenberg
  • Publication number: 20210062679
    Abstract: A bearing support designed to be secured to a stationary turbojet element for supporting a journal, including a cone which widens from a central portion for supporting the journal to a portion for securing to the stationary element, a cylindrical body extending the portion for securing to the stationary element while surrounding the cone, an upstream skirt carried by the cone for defining an upstream enclosure for the central portion, and at least one downstream revolution element carried by the cone for defining a downstream enclosure for the central portion. The bearing support can be made as a single part produced by additive manufacturing.
    Type: Application
    Filed: March 20, 2019
    Publication date: March 4, 2021
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Dimitri Daniel Gabriel MARQUIE, Adrien Jacques Philippe FABRE, Frédéric PATARD, Pierre Jean-Baptiste METGE
  • Publication number: 20200032672
    Abstract: The invention relates to a turbojet bearing housing including a fixed envelope traversed by a rotor, this envelope including a cylindrical end surrounding a seal ensuring the leak tightness of the cylindrical end of the envelope with the rotor, this envelope being equipped with a shell screwed onto the cylindrical end thereof, this shell including radial channels emerging opposite the seal while being arranged so that an air stream traversing the seal towards the housing mainly comes from these radial channels.
    Type: Application
    Filed: February 5, 2018
    Publication date: January 30, 2020
    Inventors: Frédéric PATARD, Antoine Jean-Philippe BEAUJARD, Philippe Pierre Vincent BOUILLER, Christophe CAPLAIN, Maxime Aurélien ROTENBERG
  • Patent number: 9163662
    Abstract: An installation for calibration of a stress gauge for an external bearing block of a turbomachine roller bearing, the bearing block including a radially internal roller bearing race. The installation includes a support table on which the bearing block is attached; an internal roller bearing ring mounted coaxial with the bearing block; a drive shaft driving the ring. The installation also includes a device for applying an axial stress to the bearing block including a support drum on which the internal ring is removably fixed and a connection with the device for applying the axial stress.
    Type: Grant
    Filed: April 7, 2014
    Date of Patent: October 20, 2015
    Assignee: SNECMA
    Inventors: Stephane Rousselin, Pascal Brunel, Sylvie Charles, Frederic Patard
  • Publication number: 20140307992
    Abstract: An installation for calibration of a stress gauge for an external bearing block of a turbomachine roller bearing, the bearing block including a radially internal roller bearing race. The installation includes a support table on which the bearing block is attached; an internal roller bearing ring mounted coaxial with the bearing block; a drive shaft driving the ring. The installation also includes a device for applying an axial stress to the bearing block including a support drum on which the internal ring is removably fixed and a connection with the device for applying the axial stress.
    Type: Application
    Filed: April 7, 2014
    Publication date: October 16, 2014
    Applicant: SNECMA
    Inventors: Stephane ROUSSELIN, Pascal Brunel, Sylvie Charles, Frederic Patard