Patents by Inventor Jean-François Belkadi

Jean-François Belkadi 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: 8825227
    Abstract: A device for a motorized aircraft includes at least one avionic component positioned in the aircraft, at least one engine interface positioned in the aircraft and at least one engine controller positioned in or near an engine of the aircraft. The at least one engine interface is designed to exchange data between the at least one avionic component and the at least one engine controller. The at least one engine interface is generic and able to communicate with engine controllers of various types that may be mounted on the aircraft. The at least one engine controller is specific to a particular engine.
    Type: Grant
    Filed: August 20, 2008
    Date of Patent: September 2, 2014
    Assignee: Airbus Operations S.A.S.
    Inventors: Laurent Saint-Marc, Luc Brunel, Patrick Zaccaria, Matthieu Alexandre, Julien Feau, Frédéric Leborgne, Thierry Immordino, Jean-François Belkadi, Nathalie Durand
  • Patent number: 8480037
    Abstract: A device for determining a position of a throttle lever includes position sensors each connected to a primary flight control computer, position sensors each connected to an engine management computer, the position sensors being split into at least three groups of sensors with no common simple failure mode, and at least one interface computer, that includes at least one input to receive measurement information emitted by the computers connected to the position sensors and outputs leading to the engine management computer.
    Type: Grant
    Filed: July 10, 2009
    Date of Patent: July 9, 2013
    Assignee: Airbus Operations
    Inventors: Jean-Francois Belkadi, Richard Ambroise
  • Publication number: 20110093140
    Abstract: A device for determining a position of a throttle lever includes position sensors each connected to a primary flight control computer, position sensors each connected to an engine management computer, the position sensors being split into at least three groups of sensors with no common simple failure mode, and at least one interface computer, that includes at least one input to receive measurement information emitted by the computers connected to the position sensors and outputs leading to the engine management computer.
    Type: Application
    Filed: July 10, 2009
    Publication date: April 21, 2011
    Applicant: Airbus Operations(S. A. S.)
    Inventors: Jean-Francois Belkadi, Richard Ambroise
  • Publication number: 20100292870
    Abstract: The invention relates to a device for motorized aircraft comprising at least one avionic component (300) positioned in the said aircraft, at least one engine interface (310) positioned in the said aircraft and at least one engine controller (315) positioned in or near an engine (320) of the said aircraft. According to the device of the invention, the said at least one engine interface (310) is designed to exchange data between the said at least one avionic component (300) and the said at least one engine controller (315). The said at least one engine interface (310) is generic and able to communicate with engine controllers (315) of various types that may be mounted on said aircraft. The said at least one engine controller is specific to a particular engine.
    Type: Application
    Filed: August 20, 2008
    Publication date: November 18, 2010
    Applicant: AIRBUS OPERATIONS (inc as a Societe par Act Simpl)
    Inventors: Laurent Saint Marc, Luc Brunel, Patrick Zaccaria, Matthieu Alexandre, Julien Feau, Frederic Leborgne, Thierry Immordino, Jean-Francois Belkadi, Nathalie Durand