Patents by Inventor Gilian Thierry ANTONIO

Gilian Thierry ANTONIO 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: 11346750
    Abstract: ABSTRACT A control method of a measurement supplied by a first turbomachine sensor by a first channel, and by a second turbomachine sensor by a second communication channel includes: acquiring the first signal from the first communication channel and the second signal from the second communication channel; determining of a validity status of each of the acquired signals; and transmitting of a signal to be processed.
    Type: Grant
    Filed: December 19, 2018
    Date of Patent: May 31, 2022
    Assignee: Safran Aircraft Engines
    Inventors: Gwenael Thierry Esteve, Gilian Thierry Antonio
  • Patent number: 11300427
    Abstract: The invention relates to a method for checking a measurement supplied by a sensor (2) of a turbine engine, said method being implemented by a computer (5) of the turbine engine. The method comprises the processing steps of: acquiring a first value of the measurement; comparing an increment with an increment threshold; and transmitting a measurement to be processed to the processing interface (6), said measurement being selected so as to be: equal to the value of an estimation model for the received measurement, if the increment is higher than the increment threshold, or equal to the acquired first value of the measurement if the increment is lower than the increment threshold, the method then comprising additional processing steps.
    Type: Grant
    Filed: December 14, 2018
    Date of Patent: April 12, 2022
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Gilian Thierry Antonio, Gwenael Thierry Esteve
  • Publication number: 20210088362
    Abstract: The invention relates to a method for checking a measurement supplied by a sensor (2) of a turbine engine, said method being implemented by a computer (5) of the turbine engine. The method comprises the processing steps of: acquiring a first value of the rl measurement; comparing an increment with an increment threshold; and transmitting a measurement to be processed to the processing interface (6), said measurement being selected so as to be: equal to the value of an estimation model for the received measurement, if the increment is higher than the increment threshold, or equal to the acquired first value of the measurement if the increment is lower than the increment threshold, the method then comprising additional processing steps.
    Type: Application
    Filed: December 14, 2018
    Publication date: March 25, 2021
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Gilian Thierry ANTONIO, Gwenael Thierry ESTEVE