Patents by Inventor Thibault Xavier Alexis Berranger

Thibault Xavier Alexis Berranger 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).

  • Device for measuring at least one parameter of an aerodynamic flow of a turbine engine equipped with a vibratory damping means and turbine engine duct equipped with such a device
    Patent number: 10907507
    Abstract: A measuring device for measuring at least one parameter of an aerodynamic flow of a turbine engine. The device operates to collect parameters of the flow. A body extends along a radial axis (L). A connecting part is fastened to a first end of the body and designed to secure the measuring device to a radially outer wall of the turbine engine. A stud is inserted and mounted on a second end of the body radially opposite the first end. The stud includes at least a portion of a rubberlike material designed to come into contract with a radially inner wall of the turbine engine.
    Type: Grant
    Filed: October 8, 2018
    Date of Patent: February 2, 2021
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Jeremy Giordan, Thibault Xavier Alexis Berranger, Guillaume Jose Rodrigues, Stephane Rousselin, Mathieu Raymond Paul Sezeur
  • Device for measuring the characteristics of an air flow
    Patent number: 10871402
    Abstract: A device for measuring the characteristics of an air flow intended to be mounted in an annular duct having a longitudinal axis in a turbine engine, comprising supporting means which support means for measuring the characteristics of an air flow. According to the invention, the supporting means comprise at least one first support including a main branch supporting first measuring means and a second support, structurally independent of the first support and including a main branch supporting second measuring means, with the first support and the second support being so formed that the main branch of the first support extends over a distance greater than the main branch of the second support in a common direction of extension of the branches.
    Type: Grant
    Filed: March 29, 2018
    Date of Patent: December 22, 2020
    Assignee: Safran Aircraft Engines
    Inventors: Jérémy Giordan, Florian Joseph Bernard Kockenpo, Thibault Xavier Alexis Berranger, Pascal Léon Georges Beilvert
  • DEVICE FOR MEASURING AT LEAST ONE PARAMETER OF AN AERODYNAMIC FLOW OF A TURBINE ENGINE EQUIPPED WITH A VIBRATORY DAMPING MEANS AND TURBINE ENGINE DUCT EQUIPPED WITH SUCH A DEVICE
    Publication number: 20190107008
    Abstract: A measuring device for measuring at least one parameter of an aerodynamic flow of a turbine engine. The device operates to collect parameters of the flow. A body extends along a radial axis (L). A connecting part is fastened to a first end of the body and designed to secure the measuring device to a radially outer wall of the turbine engine. A stud is inserted and mounted on a second end of the body radially opposite the first end. The stud includes at least a portion of a rubberlike material designed to come into contract with a radially inner wall of the turbine engine.
    Type: Application
    Filed: October 8, 2018
    Publication date: April 11, 2019
    Inventors: Jeremy GIORDAN, Thibault Xavier Alexis BERRANGER, Guillaume Jose RODRIGUES, Stephane ROUSSELIN, Mathieu Raymond Paul SEZEUR
  • DEVICE FOR MEASURING THE CHARACTERISTICS OF AN AIR FLOW
    Publication number: 20180283960
    Abstract: A device for measuring the characteristics of an air flow intended to be mounted in an annular duct having a longitudinal axis in a turbine engine, comprising supporting means which support means for measuring the characteristics of an air flow. According to the invention, the supporting means comprise at least one first support including a main branch supporting first measuring means and a second support, structurally independent of the first support and including a main branch supporting second measuring means, with the first support and the second support being so formed that the main branch of the first support extends over a distance greater than the main branch of the second support in a common direction of extension of the branches.
    Type: Application
    Filed: March 29, 2018
    Publication date: October 4, 2018
    Applicant: Safran Aircraft Engines
    Inventors: Jérémy Giordan, Florian Joseph Bernard Kockenpo, Thibault Xavier Alexis Berranger, Pascal Léon Georges Beilvert