Patents by Inventor Xavier Lamoussiere

Xavier Lamoussiere 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).

  • POWER CONTROL UNIT, HYDRAULIC SYSTEM AND AIRCRAFT USING THE SAME
    Publication number: 20220306285
    Abstract: A power control unit configured to supply hydraulic pressure and mechanical torque. To this end, the power control unit includes an electric motor coupled to a differential output transmission and a hydraulic pump. A switchable transmission device allows the torque of the motor to be redirected either to the output transmission, e.g., to drive high-lift devices, or to the hydraulic pump, e.g., to extend or retract landing gears.
    Type: Application
    Filed: March 22, 2022
    Publication date: September 29, 2022
    Inventors: Andreas FLEDDERMANN, Xavier LAMOUSSIERE, Arnaud DIDEY
  • Method and system for deactivating a steering system of an aircraft'S front landing gear
    Patent number: 8660711
    Abstract: A method for deactivating a steering system of a front landing gear of an aircraft, including detecting an activated status of the steering system, detecting a pilot control unit in neutral position, detecting towing conditions of the aircraft, detecting a rotational movement of the nose gear, and deactivating the steering system when operations to are verified. The disclosed embodiments also concern a system for implementing this method.
    Type: Grant
    Filed: November 7, 2008
    Date of Patent: February 25, 2014
    Assignee: Airbus Operations (SAS)
    Inventors: Noelle Bailbe, Xavier Lamoussiere
  • METHOD AND SYSTEM FOR DEACTIVATING A STEERING SYSTEM OF AN AIRCRAFT'S FRONT LANDING GEAR
    Publication number: 20110046819
    Abstract: A method for deactivating a steering system of a front landing gear of an aircraft, including detecting an activated status of the steering system, detecting a pilot control unit in neutral position, detecting towing conditions of the aircraft, detecting a rotational movement of the nose gear, and deactivating the steering system when operations to are verified. The disclosed embodiments also concern a system for implementing this method.
    Type: Application
    Filed: November 7, 2008
    Publication date: February 24, 2011
    Applicant: AIRBUS OPERATIONS (S.A.S.)
    Inventors: Noelle Bailbe, Xavier Lamoussiere
  • BRAKING PROCESS FOR AN AIRPLANE
    Publication number: 20100076623
    Abstract: An aircraft braking adaptation process is used to prevent rapid derotation of an aircraft causing damage to the front landing gear by formulating a braking command, applying the command to at least one brake, adapting the braking command by acquiring the aircraft trim and modifying the braking commands as a function of the aircraft trim. This process limits the derotation speed and preserves the front landing gear.
    Type: Application
    Filed: March 24, 2009
    Publication date: March 25, 2010
    Applicant: AIRBUS FRANCE
    Inventor: Xavier Lamoussiere