Patents by Inventor Benjamin FAURE

Benjamin FAURE 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: 20250367640
    Abstract: The present invention relates to a suspension of oxygenated cerium compound particles, said particles having a D50 of from 10 to 200 nm and a D90 below 1000 nm, determined by laser particle size analysis, in a liquid medium, preferably an aqueous liquid medium, including at least one carboxylic acid containing from 3 to 9 carbon atoms, or at least one functionalized carboxylic acid having 2 carbon atoms or any mixture thereof. The present invention also relates to the process for preparing such a suspension.
    Type: Application
    Filed: June 16, 2023
    Publication date: December 4, 2025
    Inventors: Benjamin Faure, Simon Ifrah, Virginie Harle
  • Patent number: 11964255
    Abstract: Disclosed are a mixed oxide composition based on zirconium and cerium exhibiting a high reducibility, the process for preparing it and its use in the field of catalysis.
    Type: Grant
    Filed: September 23, 2019
    Date of Patent: April 23, 2024
    Assignee: RHODIA OPERATIONS
    Inventors: Simon Ifrah, Laure Jeanne Simone Bisson, Benjamin Faure, Rui Miguel Jorge Coelho Marques, Wei Li, Ling Zhu
  • Publication number: 20220401921
    Abstract: The present invention relates to a suspension of nanoparticles of a mixed oxide based on cerium and zirconium. It also relates to the use of said suspension for the preparation of a catalysed gasoline particulate filter.
    Type: Application
    Filed: September 28, 2020
    Publication date: December 22, 2022
    Applicant: RHODIA OPERATIONS
    Inventors: Virginie Harle, Simon Ifrah, Boris Chabert, Benjamin Faure, Olivier Larue
  • Publication number: 20210354111
    Abstract: Disclosed are a mixed oxide composition based on zirconium and cerium exhibiting a high reducibility, the process for preparing it and its use in the field of catalysis.
    Type: Application
    Filed: September 23, 2019
    Publication date: November 18, 2021
    Inventors: Simon IFRAH, Laure, Jeanne, Simone BISSON, Benjamin FAURE, Rui Miguel JORGE COELHO MARQUES, Wei LI, Ling ZHU
  • Patent number: 10612493
    Abstract: A system allowing for the tilting of the rocket motor such that, in the tilted position, the centre of the nozzle is located at least approximately on the neutral orientation axis of said rocket motor.
    Type: Grant
    Filed: April 22, 2014
    Date of Patent: April 7, 2020
    Assignee: ArianeGroup SAS
    Inventors: Fabrice Ruffino, Benjamin Faure
  • Patent number: 10046868
    Abstract: A spaceplane suitable for aeronautical flight comprising a body and a wing defining a lower airfoil surface in addition to attitude control means that comprise one or a plurality of shutters disposed under the lower airfoil surface of same and maneuverable between a stowed position and an inclined extended position for aerodynamic braking during the transition from a phase of space flight to a phase of aeronautical flight of the aircraft.
    Type: Grant
    Filed: March 28, 2014
    Date of Patent: August 14, 2018
    Assignee: AIRBUS DEFENCE AND SPACE SAS
    Inventors: Eugénio Ferreira, Angélique Santerre, Benjamin Faure, Samuel Chevrollier, Pierre Parpaite, Christophe Favre
  • Patent number: 9938025
    Abstract: A device for mounting and supporting a generally cylindrical or tapered tank, having a main axis X, that includes a pair of first retaining rods for retaining the tank along a vertical axis Z on each of a first and second end of the tank, a second retaining rod for retaining the tank along a horizontal axis Y, perpendicular to the main axis, on the first end of the tank, and a third retaining rod for retaining in a ball-and-socket joint, the means being located around the vertical axis and connected to the second end of the tank.
    Type: Grant
    Filed: February 4, 2014
    Date of Patent: April 10, 2018
    Assignee: AIRBUS DEFENCE & SPACE SAS
    Inventors: Benjamin Faure, Jérôme Bertrand, Yohann Coraboeuf, Samuel Chevrollier, Robert Abadie-La-Haille, Pascal Mezieres, Angélique Santerre
  • Publication number: 20160069299
    Abstract: A system allowing for the tilting of the rocket motor such that, in the tilted position, the centre of the nozzle is located at least approximately on the neutral orientation axis of said rocket motor.
    Type: Application
    Filed: April 22, 2014
    Publication date: March 10, 2016
    Applicant: AIRBUS DEFENCE AND SPACE SAS
    Inventors: Fabrice Ruffino, Benjamin Faure
  • Publication number: 20160052650
    Abstract: A spaceplane suitable for aeronautical flight comprising a body and a wing defining a lower airfoil surface in addition to attitude control means that comprise one or a plurality of shutters disposed under the lower airfoil surface of same and maneuverable between a stowed position and an inclined extended position for aerodynamic braking during the transition from a phase of space flight to a phase of aeronautical flight of the aircraft.
    Type: Application
    Filed: March 28, 2014
    Publication date: February 25, 2016
    Inventors: Eugénio FERREIRA, Angélique SANTERRE, Benjamin FAURE, Samuel CHEVROLLIER, Pierre PARPAITE, Christophe FAVRE
  • Publication number: 20150360792
    Abstract: The present invention relates to a device for mounting and supporting a generally cylindrical or tapered tank, having a main axis X, that includes a pair of first means for retaining the tank along a vertical axis Z on each of a first and second end of the tank, a second means for retaining the tank along a horizontal axis Y, perpendicular to the main axis, on the first end of the tank, and a third means for retaining in a ball-and-socket joint, the means being located around the vertical axis and connected to the second end of the tank.
    Type: Application
    Filed: February 4, 2014
    Publication date: December 17, 2015
    Inventors: Benjamin FAURE, Jérôme BERTRAND, Yohann CORABOEUF, Samuel CHEVROLLIER, Robert ABADIE-LA-HAILLE, Pascal MEZIERES, Angélique SANTERRE
  • Publication number: 20150360791
    Abstract: The invention concerns a tank retainer for retaining a tank in the fuselage of an aircraft which includes, between the tank and a frame rigidly connected to the fuselage of the aircraft, a hinged retaining means and a fastening rod on which said hinged retaining means is mounted. Advantageously, the hinged retaining means is intended to be connected to a rear end of the tank and the fastening rod is suitable for being mounted on the frame rigidly connected to the fuselage of the aircraft and, preferably, the hinged retaining means comprises a ball joint.
    Type: Application
    Filed: February 4, 2014
    Publication date: December 17, 2015
    Inventors: Samuel CHEVROLLIER, Robert ABADIE-LAHAILLE, Pascal MEZIERES, Benjamin FAURE, Jérôme BERTRAND, Yohann CORABOEUF, Angélique SANTERRE
  • Patent number: D762157
    Type: Grant
    Filed: August 5, 2014
    Date of Patent: July 26, 2016
    Assignee: AIRBUS DEFENCE AND SPACE SAS
    Inventors: Benjamin Faure, Angélique Santerre, Jean Philippe Dutheil, Christophe Chavagnac, Eugénio Ferreira, Thierry Pichard
  • Patent number: D762548
    Type: Grant
    Filed: August 5, 2014
    Date of Patent: August 2, 2016
    Assignee: AIRBUS DEFENCE AND SPACE SAS
    Inventors: Benjamin Faure, Angélique Santerre, Jean Philippe Dutheil, Christophe Chavagnac, Eugénio Ferreira, Thierry Pichard
  • Patent number: D778803
    Type: Grant
    Filed: August 5, 2014
    Date of Patent: February 14, 2017
    Assignee: AIRBUS DEFECE AND SPACE SAS
    Inventors: Benjamin Faure, Angélique Santerre, Jean Philippe Dutheil, Christophe Chavagnac, Eugénio Ferreira, Thierry Pichard