Patents by Inventor Jean-Baptiste GOULARD

Jean-Baptiste GOULARD 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: 11401887
    Abstract: An improved thrust reverser for an aircraft propulsion assembly includes redirection of the air flow for performing the thrust reversal by one or more closure membranes, i.e. by thin and flexible structures deployed across the propulsion assembly. The improved thrust reverser includes at least one closure membrane arranged to deflect at least one portion of the air flow in the direction of the evacuation structure when the thrust reverser is in the reverse jet position and an intermediate structure movable in rotation relative to the fixed structure.
    Type: Grant
    Filed: July 16, 2020
    Date of Patent: August 2, 2022
    Assignee: Safran Nacelles
    Inventors: Patrick Gonidec, Olivier Kerbler, Alexandre Phi, Jean-Paul Rami, Stephane Tirel, Jean-Baptiste Goulard, Matthieu Vanderlinden, Arnaud Carles-Espiteau
  • Patent number: 11401866
    Abstract: An active device for attenuating the acoustic emissions of an aircraft turbojet engine includes circulation conduits for a pressurized air flow rate supplying rotary elements each having a pulsation system for the delivered air. The rotary elements are controlled in amplitude and phase and deliver, to outlet diffusers, a pulsed air flow rate with a pulsation at the frequency of the noise to be attenuated having an amplitude and a phase adjusted according to a local feedback law with microphones to attenuate the radiated acoustic power.
    Type: Grant
    Filed: September 8, 2020
    Date of Patent: August 2, 2022
    Assignee: Safran Nacelles
    Inventors: Jean-Paul Rami, Hervé Hurlin, Jean-Baptiste Goulard, Marc Versaevel, Philippe Micheau, Julien Drant, Ambre Allard, Alain Berry, Raymond Robert
  • Publication number: 20200400076
    Abstract: An active device for attenuating the acoustic emissions of an aircraft turbojet engine includes circulation conduits for a pressurized air flow rate supplying rotary elements each having a pulsation system for the delivered air. The rotary elements are controlled in amplitude and phase and deliver, to outlet diffusers, a pulsed air flow rate with a pulsation at the frequency of the noise to be attenuated having an amplitude and a phase adjusted according to a local feedback law with microphones to attenuate the radiated acoustic power.
    Type: Application
    Filed: September 8, 2020
    Publication date: December 24, 2020
    Applicant: Safran Nacelles
    Inventors: Jean-Paul RAMI, Hervé HURLIN, Jean-Baptiste GOULARD, Marc VERSAEVEL, Philippe MICHEAU, Julien DRANT, Ambre ALLARD, Alain BERRY, Raymond ROBERT
  • Publication number: 20200347800
    Abstract: An improved thrust reverser for an aircraft propulsion assembly includes redirection of the air flow for performing the thrust reversal by one or more closure membranes, i.e. by thin and flexible structures deployed across the propulsion assembly. The improved thrust reverser includes at least one closure membrane arranged to deflect at least one portion of the air flow in the direction of the evacuation structure when the thrust reverser is in the reverse jet position and an intermediate structure movable in rotation relative to the fixed structure.
    Type: Application
    Filed: July 16, 2020
    Publication date: November 5, 2020
    Applicant: Safran Nacelles
    Inventors: Patrick GONIDEC, Olivier KERBLER, Alexandre PHI, Jean-Paul RAMI, STEPHANE TIREL, Jean-Baptiste GOULARD, Matthieu VANDERLINDEN, Arnaud CARLES-ESPITEAU