Patents by Inventor Bilal Youssef

Bilal Youssef 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: 9556780
    Abstract: The invention relates to a method for diagnosing a particulate filter by means of a soot sensor, the method being based on the direct analysis of the temporal signal supplied by the soot sensor (CAP) and the use of the available quantities (PAR) in the control unit of the heat engine. These data allow for a classification (CLA) of an indicator correlated to the cumulative quantity of soot (RES) in a multidimensional space (GRA). Based on the classification (CLA), the existence of a failure of the particulate filter is determined.
    Type: Grant
    Filed: January 16, 2014
    Date of Patent: January 31, 2017
    Assignees: IFP ENERGIES NOUVELLES, ELECTRICFIL AUTOMOTIVE
    Inventors: Bilal Youssef, Yann Creff
  • Publication number: 20150361859
    Abstract: The invention relates to a method for diagnosing a particulate filter by means of a soot sensor, the method being based on the direct analysis of the temporal signal supplied by the soot sensor (CAP) and the use of the available quantities (PAR) in the control unit of the heat engine. These data allow for a classification (CLA) of an indicator correlated to the cumulative quantity of soot (RES) in a multidimensional space (GRA). Based on the classification (CLA), the existence of a failure of the particulate filter is determined.
    Type: Application
    Filed: January 16, 2014
    Publication date: December 17, 2015
    Inventors: Bilal YOUSSEF, Yann CREFF
  • Patent number: 8082091
    Abstract: A method for controlling a turbocharger using a physical model of the turbocharger speed is disclosed with an application for controlling an internal-combustion engine. A setpoint pressure corresponding to a fluid pressure in the engine intake manifold is converted to a desired speed value. A physical relation connecting the turbocharger speed to a pressure ratio of the fluid flowing into and out of the turbine is then defined. A desired pressure ratio for the fluid flowing into and out of the turbine is deduced therefrom. A turbine actuator control law is estimated by mapping the turbine, from a measurement of the fluid flow rate flowing into the turbine and from the desired ratio of the pressures in the turbine. Finally, the control law is applied to the turbine actuator so that the pressure in the intake manifold is equal to the setpoint pressure.
    Type: Grant
    Filed: September 26, 2008
    Date of Patent: December 20, 2011
    Assignee: IFP
    Inventors: Bilal Youssef, Philippe Moulin
  • Publication number: 20100217498
    Abstract: A method of extracting useful information for control of an internal-combustion engine, based on graphic signatures is disclosed. A signal carrying at least information relative to engine operation is acquired. This signal is then converted, for each engine cycle, to a graphic signature translating a set of characteristic features of the signal in a form of a graph which is simple to analyze. At least one attribute of this signature is then determined, from which the pertinent information is estimated by a predetermined relation between the attribute and the information.
    Type: Application
    Filed: October 24, 2008
    Publication date: August 26, 2010
    Inventors: Bilal Youssef, Gilles Corde
  • Publication number: 20090090107
    Abstract: A method for controlling a turbocharger using a physical model of the turbocharger speed is disclosed with an application for controlling an internal-combustion engine. A setpoint pressure corresponding to a fluid pressure in the engine intake manifold is converted to a desired speed value. A physical relation connecting the turbocharger speed to a pressure ratio of the fluid flowing into and out of the turbine is then defined. A desired pressure ratio for the fluid flowing into and out of the turbine is deduced therefrom. A turbine actuator control law is estimated by mapping the turbine, from a measurement of the fluid flow rate flowing into the turbine and from the desired ratio of the pressures in the turbine. Finally, the control law is applied to the turbine actuator so that the pressure in the intake manifold is equal to the setpoint pressure.
    Type: Application
    Filed: September 26, 2008
    Publication date: April 9, 2009
    Inventors: Bilal Youssef, Philippe Moulin