Patents by Inventor Jocelyn Be

Jocelyn Be 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).

  • Aerodynamic measurement probe
    Patent number: 12618864
    Abstract: An aerodynamic measurement probe intended to measure a local angle of attack of an air stream flowing along the fuselage of an aircraft, includes a support and a shaft that is able to rotate about a longitudinal axis with respect to the support, the support and the shaft being configured to form between them a gap, passing around an annular tab at the end of the shaft in the support, making it possible to maintain a functional clearance to allow one end of the shaft to pivot freely in the support, and communicating with an impurity discharge circuit, the gap comprising an inner annular groove about the axis of rotation, made in the support, and opening out away from the axis directly onto the end part of the annular tab, the profile of the inner groove being rounded.
    Type: Grant
    Filed: May 20, 2022
    Date of Patent: May 5, 2026
    Assignee: THALES
    Inventors: Natacha Szulga, François Perez, Eric Loil, Frédéric Sadrin, Jocelyn Be, Jean-Luc Vallee, Tristan Guillabeau
  • Angle-of-attack sensor, in particular for an aircraft
    Publication number: 20240308682
    Abstract: This angle-of-attack sensor, in particular for an aircraft, of the type including a sensor body (11) on which a wind vane (12) is mounted movable in rotation by a flow, is characterized in that the wind vane (12) includes at least one deflector (13, 14) extending from the leading edge of this wind vane over at least part of the intrados and/or extrados thereof.
    Type: Application
    Filed: July 7, 2022
    Publication date: September 19, 2024
    Inventors: Jocelyn BE, Jean-Philippe PINEAU
  • AERODYNAMIC MEASUREMENT PROBE
    Publication number: 20240241150
    Abstract: An aerodynamic measurement probe intended to measure a local angle of attack of an air stream flowing along the fuselage of an aircraft, includes a support and a shaft that is able to rotate about a longitudinal axis with respect to the support, the support and the shaft being configured to form between them a gap, passing around an annular tab at the end of the shaft in the support, making it possible to maintain a functional clearance to allow one end of the shaft to pivot freely in the support, and communicating with an impurity discharge circuit, the gap comprising an inner annular groove about the axis of rotation, made in the support, and opening out away from the axis directly onto the end part of the annular tab, the profile of the inner groove being rounded.
    Type: Application
    Filed: May 20, 2022
    Publication date: July 18, 2024
    Inventors: Natacha SZULGA, François PEREZ, Eric LOIL, Frédéric SARDIN, Jocelyn BE, Jean-Luc VALLEE, Tristan GUILLABEAU
  • Aerodynamic measurement probe for measuring a local incidence of airflow
    Patent number: D972950
    Type: Grant
    Filed: September 9, 2020
    Date of Patent: December 20, 2022
    Assignee: THALES
    Inventors: Frédéric Sadrin, Jocelyn Be, Eric Loil, Jean-Luc Vallee, François Perez