Patents by Inventor Philippe Gaucheron

Philippe Gaucheron 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 for determining the total temperature of an airflow surrounding an aircraft
    Patent number: 7974812
    Abstract: A method for determining the total temperature of the air stream surrounding an aircraft, including the following operations; measuring a parameter of static temperature, measuring a parameter of total temperature, determining a value of speed of the air stream, determining a total temperature computed from the parameters of measured static temperature and measured total temperature as a function of the speed of the air stream.
    Type: Grant
    Filed: February 1, 2007
    Date of Patent: July 5, 2011
    Assignee: Airbus France
    Inventors: Valerie Brivet, Philippe Gaucheron, Stephane Saint-Aroman
  • METHOD FOR DETERMINING THE TOTAL TEMPERATURE OF AN AIRFLOW SURROUNDING AN AIRCRAFT
    Publication number: 20090306927
    Abstract: A method for determining the total temperature of the air stream surrounding an aircraft, including the following operations; measuring a parameter of static temperature, measuring a parameter of total temperature, determining a value of speed of the air stream, determining a total temperature computed from the parameters of measured static temperature and measured total temperature as a function of the speed of the air stream.
    Type: Application
    Filed: February 1, 2007
    Publication date: December 10, 2009
    Applicant: AIRBUS FRANCE
    Inventors: Valerie Brivet, Philippe Gaucheron, Stephane Saint-Aroman
  • Process and device for detecting the failure of a pressure sensor of an air data system of an aircraft
    Patent number: 6993419
    Abstract: Detection of the failure of a pressure sensor of an air data system of an aircraft having at least two pressure sensors includes measuring first and second pressure values with the aid of the two pressure sensors, respectively. The deviation between the first and second pressure values is calculated, and this deviation is compared with a predetermined threshold value. If the deviation is greater than the threshold value, a failure cue relating to the air data system is displayed on a display device that is mounted in the aircraft.
    Type: Grant
    Filed: November 12, 2003
    Date of Patent: January 31, 2006
    Assignee: Airbus France
    Inventors: Arnaud D'Ouince, Bruno Ley, Philippe Gaucheron, Arnaud Bellier