Patents by Inventor Fabien Latourelle

Fabien Latourelle 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).

  • Electric propulsion system of an aircraft
    Patent number: 11866185
    Abstract: A propulsion system includes a system for producing electricity that supplies electricity to at least one electric motor to which is mechanically coupled a propeller situated near a first longitudinal end of a nacelle that houses at least the system for producing electricity and the at least one electric motor. An air circulation channel, which receives a heat exchanger provided to allow the system for producing electricity to be cooled, extends inside the nacelle from a first end of the air circulation channel situated at the first longitudinal end of the nacelle. A part of the air circulation channel that is contiguous with its first end is delimited by an outer surface of cylindrical shape that surrounds the longitudinal axis of the nacelle.
    Type: Grant
    Filed: March 23, 2022
    Date of Patent: January 9, 2024
    Assignees: AIRBUS SAS, AIRBUS OPERATIONS SAS
    Inventors: Christophe Labarthe, Franck Alvarez, Fabien Latourelle, Olivier Verseux, Pascal Pome, Jean Francois Allias, Olivier Ciet, Olivier Raspati, Anthony Roux, Benedikt Bammer
  • ELECTRIC PROPULSION SYSTEM OF AN AIRCRAFT
    Publication number: 20220306306
    Abstract: A propulsion system includes a system for producing electricity that supplies electricity to at least one electric motor to which is mechanically coupled a propeller situated near a first longitudinal end of a nacelle that houses at least the system for producing electricity and the at least one electric motor. An air circulation channel, which receives a heat exchanger provided to allow the system for producing electricity to be cooled, extends inside the nacelle from a first end of the air circulation channel situated at the first longitudinal end of the nacelle. A part of the air circulation channel that is contiguous with its first end is delimited by an outer surface of cylindrical shape that surrounds the longitudinal axis of the nacelle.
    Type: Application
    Filed: March 23, 2022
    Publication date: September 29, 2022
    Inventors: Christophe LABARTHE, Franck ALVAREZ, Fabien LATOURELLE, Olivier VERSEUX, Pascal POME, Jean Francois ALLIAS, Olivier CIET, Olivier RASPATI, Anthony ROUX, Benedikt BAMMER
  • Aircraft comprising fairings for correcting its dissymmetry or lateral asymmetry
    Publication number: 20130240667
    Abstract: An aircraft having an asymmetry or a lateral geometric dissymmetry and comprising at least one pair of wings to each of which are fixed at least one fairing, each fairing comprising a surface connected to the lower surface of the wing and extending longitudinally in the direction of a longitudinal axis of the fuselage. The surface of at least one of the fairings has at least one local geometric deformation which is suitable for producing a corrective rolling moment to compensate for the undesirable rolling moment produced by the asymmetry or the lateral dissymmetry of the aircraft.
    Type: Application
    Filed: March 11, 2013
    Publication date: September 19, 2013
    Applicant: AIRBUS OPERATIONS (SAS)
    Inventors: Cyril Guichot, Fabien Latourelle