A method of determining an operating condition of a valve of an aircraft system includes obtaining a first time period associated with actuating the valve, and a second time period associated with actuating the valve. The method includes providing an indication of an altered operating condition associated with actuation of the valve based on the first and second time periods.


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    Title :

    A METHOD OF DETERMINING AN OPERATING CONDITION OF A VALVE OF AN AIRCRAFT SYSTEM


    Additional title:

    VERFAHREN ZUR BESTIMMUNG EINES BETRIEBSZUSTANDS EINES VENTILS EINES FLUGZEUGSYSTEMS
    PROCÉDÉ DE DÉTERMINATION D'UNE CONDITION DE FONCTIONNEMENT D'UNE VANNE D'UN SYSTÈME D'AÉRONEF


    Contributors:

    Publication date :

    2024-01-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16K VALVES , Ventile / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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    MANARAS PETROS / SEGER BRIAN | European Patent Office | 2024

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    A method of determining an operating condition of a valve of an aircraft system

    PETROS MANARAS / BRIAN SAGAR | European Patent Office | 2022

    Free access