Patents by Inventor Philippe Feuillard

Philippe Feuillard 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).

  • Method and device for implementing the thrust reversers of an aircraft
    Patent number: 8733698
    Abstract: Method and device for implementing the thrust reversers of an aircraft. According to the invention, the following successive steps are carried out automatically: • deployment (E3) of the previously armed thrust reversers of the aircraft; • application (E5) of a predetermined engine speed; reduction (E6) of the engine speed; —re-furling (E7) of the thrust reversers of the aircraft.
    Type: Grant
    Filed: April 30, 2009
    Date of Patent: May 27, 2014
    Assignee: Airbus Operations (SAS)
    Inventors: Philippe Abrial, Philippe Feuillard
  • METHOD AND DEVICE FOR IMPLEMENTING THE THRUST REVERSERS OF AN AIRCRAFT
    Publication number: 20110108665
    Abstract: Method and device for implementing the thrust reversers of an aircraft. According to the invention, the following successive steps are carried out automatically: deployment (E3) of the previously armed thrust reversers of the aircraft; application (E5) of a predetermined engine speed; reduction (E6) of the engine speed; re-furling (E7) of the thrust reversers of the aircraft.
    Type: Application
    Filed: April 30, 2009
    Publication date: May 12, 2011
    Applicant: AIRBUS OPERATIONS (SAS)
    Inventors: Philippe Abrial, Philippe Feuillard
  • Chevron-type primary exhaust nozzle for aircraft turbofan engine, and aircraft comprising such a nozzle
    Patent number: 7469529
    Abstract: A primary exhaust nozzle for a turbofan engine of the double, separated air-flow type for aircraft comprises: an inner coat, within which there circulates a primary air flow (FP), comprising chevrons at an external end and an outer coat at least partially surrounding the inner coat and along which there flows a secondary air flow (FS), the outer coat being mobile along the inner coat. Also disclosed is an aircraft comprising such an exhaust nozzle.
    Type: Grant
    Filed: March 24, 2005
    Date of Patent: December 30, 2008
    Assignee: Airbus France
    Inventors: Philippe Feuillard, Philippe Hemeury, Christian Gerri
  • Chevron-type primary exhaust nozzle for aircraft turbofan engine, and aircraft comprising such a nozzle
    Publication number: 20060053769
    Abstract: A primary exhaust nozzle for a turbofan engine of the double, separated air-flow type for aircraft comprises: an inner coat, within which there circulates a primary air flow (FP), comprising chevrons at an external end and an outer coat at least partially surrounding the inner coat and along which there flows a secondary air flow (FS), the outer coat being mobile along the inner coat. Also disclosed is an aircraft comprising such an exhaust nozzle.
    Type: Application
    Filed: March 24, 2005
    Publication date: March 16, 2006
    Inventors: Philippe Feuillard, Philippe Hemeury, Christian Gerri