The invention relates to a valve (10) for a hydraulic circuit (51) for an aircraft (50), said valve being adapted to unit or separate multiple circuit portions (31, 32, 33, 34) in at least two configurations. More particularly the valve allows to create one hydraulic circuit or two independent hydraulic circuits in order to circulate a coolant in two distinct manners and thus to adapt the function of the hydraulic circuit (51) to any of two distinct phases of the functioning of an engine of the aircraft.


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    Title :

    VALVE FOR DIVIDING A HYDRAULIC CIRCUIT AND HYDRAULIC CIRCUIT COMPRISING SAID VALVE


    Additional title:

    VENTIL ZUM TEILEN EINES HYDRAULIKKREISLAUFS UND HYDRAULIKKREISLAUF MIT DIESEM VENTIL
    SOUPAPE POUR DIVISER UN CIRCUIT HYDRAULIQUE ET CIRCUIT HYDRAULIQUE COMPRENANT LADITE SOUPAPE


    Contributors:

    Publication date :

    2023-06-07


    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



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