Patents Assigned to SAFRAN ENGINEERING SERVICES
  • Patent number: 9598178
    Abstract: A method for monitoring a degradation in an on-board device of an aircraft, comprising a step of comparing an abnormality score obtained for a given flight of said aircraft with a decision threshold (S) and a step of transmitting an alert in the event of said decision threshold (S) being exceeded, said decision threshold (S) being automatically determined for a given probability of alert Pa, corresponding to the probability of an alert being transmitted during the monitoring method when said on-board device is healthy, by means of a plurality of steps, including a step of reading the antecedent of the continuous adjusted division function for the value 1?Peac, said antecedent corresponding to said decision threshold (S), with Peac being the elementary probability of exceeding the threshold for confirmation per k exceedances of threshold during n consecutive flights and being a function of the probability of alert Pa.
    Type: Grant
    Filed: September 5, 2014
    Date of Patent: March 21, 2017
    Assignees: SNECMA, SAFRAN ENGINEERING SERVICES, UNIVERSITE DE TECHNOLOGIE DE TROYES
    Inventors: Jean-Remi Andre Masse, Ouadie Hmad, Edith Grall-Maes, Pierre Jean Emile Beauseroy
  • Publication number: 20150073650
    Abstract: A method for monitoring a degradation in an on-board device of an aircraft, comprising a step of comparing an abnormality score obtained for a given flight of said aircraft with a decision threshold (S) and a step of transmitting an alert in the event of said decision threshold (S) being exceeded, said decision threshold (S) being automatically determined for a given probability of alert Pa, corresponding to the probability of an alert being transmitted during the monitoring method when said on-board device is healthy, by means of a plurality of steps, including a step of reading the antecedent of the continuous adjusted division function for the value 1?Peac, said antecedent corresponding to said decision threshold (S), with Peac being the elementary probability of exceeding the threshold for confirmation per k exceedances of threshold during n consecutive flights and being a function of the probability of alert Pa.
    Type: Application
    Filed: September 5, 2014
    Publication date: March 12, 2015
    Applicants: SNECMA, SAFRAN ENGINEERING SERVICES, UNIVERSITE DE TECHNOLOGIE DE TROYES
    Inventors: Jean-Remi Andre MASSE, Ouadie HMAD, Edith GRALL-MAES, Pierre Jean Emile BEAUSEROY