Patents by Inventor Matthieu Della NAVE

Matthieu Della NAVE 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: 9969378
    Abstract: A method of determining the integrity of an electric or hydraulic braking control system. A reduction rate of a voltage or hydraulic pressure in the braking control system is determined, and the integrity of the braking control system is determined by comparing the reduction rate with a threshold. The braking control system may be an aircraft braking control system, and the method may be performed during flight of the aircraft—typically during cruise.
    Type: Grant
    Filed: July 17, 2015
    Date of Patent: May 15, 2018
    Assignee: AIRBUS OPERATIONS LIMITED
    Inventors: George Howell, Matthieu Della Nave
  • Patent number: 9580058
    Abstract: A method of determining the integrity of an electric or hydraulic energy source of a braking control system. The energy source is charged or discharged, and two or more measurements of voltage or hydraulic pressure are taken from the braking control system. A difference between at least two of the measurements is determined in order to determine a change or rate of change in voltage or hydraulic pressure caused by the charging or discharging of the energy source. The integrity of the energy source is determined by checking whether the change or rate of change in voltage or hydraulic pressure meets predetermined criteria. The check may comprise comparing the change or rate of change of the voltage or hydraulic pressure to a threshold—for instance checking whether the change exceeds a threshold, or falls between an upper threshold and a lower threshold.
    Type: Grant
    Filed: July 17, 2015
    Date of Patent: February 28, 2017
    Assignee: AIRBUS OPERATIONS LIMITED
    Inventors: George Howell, Matthieu Della Nave
  • Publication number: 20160016576
    Abstract: A method of determining the integrity of an electric or hydraulic braking control system. A reduction rate of a voltage or hydraulic pressure in the braking control system is determined, and the integrity of the braking control system is determined by comparing the reduction rate with a threshold. The braking control system may be an aircraft braking control system, and the method may be performed during flight of the aircraft—typically during cruise.
    Type: Application
    Filed: July 17, 2015
    Publication date: January 21, 2016
    Inventors: George HOWELL, Matthieu Della NAVE
  • Publication number: 20160016575
    Abstract: A method of determining the integrity of an electric or hydraulic energy source of a braking control system. The energy source is charged or discharged, and two or more measurements of voltage or hydraulic pressure are taken from the braking control system. A difference between at least two of the measurements is determined in order to determine a change or rate of change in voltage or hydraulic pressure caused by the charging or discharging of the energy source. The integrity of the energy source is determined by checking whether the change or rate of change in voltage or hydraulic pressure meets predetermined criteria. The check may comprise comparing the change or rate of change of the voltage or hydraulic pressure to a threshold—for instance checking whether the change exceeds a threshold, or falls between an upper threshold and a lower threshold.
    Type: Application
    Filed: July 17, 2015
    Publication date: January 21, 2016
    Inventors: George HOWELL, Matthieu Della NAVE