Patents by Inventor Luc Brunel

Luc Brunel 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).

  • Peptide-Silica Hybrid Materials
    Publication number: 20160096865
    Abstract: The invention relates to novel peptide-silane “hybrid block” molecules, to the synthesis thereof and to the use of same for producing novel peptide-silica hybrid materials that can be used in various applications.
    Type: Application
    Filed: June 24, 2013
    Publication date: April 7, 2016
    Applicant: Universite de Montpellier I
    Inventors: Jean MARTINEZ, Gilles SUBRA, Ahmad MEHDI, Said JEBORS, Christine ENJALBAL, Luc BRUNEL, Francois FAJULA
  • FADEC and avionic component distributed architecture
    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
  • FADEC AND AVIONIC COMPONENT DISTRIBUTED ARCHITECTURE
    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