Patents by Inventor Matthieu Savarit

Matthieu Savarit 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: 8408864
    Abstract: A device for regulating the flow rate of air feeding a turbine ventilation cavity of a turbomachine turbine section is disclosed. The device includes at least one tubular duct opening into a take-off cavity and leading into a turbine ventilation cavity, the pressure inside the take-off cavity being higher than the pressure inside the turbine ventilation cavity; an air flow rate regulation valve disposed in the tubular duct, the valve being suitable for moving under the effect of the pressure difference between the take-off cavity and the turbine ventilation cavity; and a mechanical return device for holding the valve in a maximum closure position for the duct so long as the pressure difference between the take-off cavity and the turbine ventilation cavity remains below a predetermined threshold pressure.
    Type: Grant
    Filed: November 10, 2009
    Date of Patent: April 2, 2013
    Assignee: SNECMA
    Inventors: Ion Fintescu, Laurent Gille, Jean-Pierre Andre Joseph Mourlan, Matthieu Savarit
  • Publication number: 20100119356
    Abstract: The invention relates to a device for regulating the flow rate of air feeding a turbine ventilation cavity of a turbomachine turbine section, the device comprising at least one tubular duct opening into a take-off cavity and leading into a turbine ventilation cavity, the pressure inside the take-off cavity being higher than the pressure inside the turbine ventilation cavity, an air flow rate regulation valve disposed in the tubular duct, the valve being suitable for moving under the effect of the pressure difference between the take-off cavity and the turbine ventilation cavity, and mechanical return means for holding the valve in a maximum closure position for the duct so long as the pressure difference between the take-off cavity and the turbine ventilation cavity remains below a predetermined threshold pressure.
    Type: Application
    Filed: November 10, 2009
    Publication date: May 13, 2010
    Applicant: SNECMA
    Inventors: Ion FINTESCU, Laurent Gille, Jean-Pierre Andre Joseph Mourlan, Matthieu Savarit