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.
VALVE FOR DIVIDING A HYDRAULIC CIRCUIT AND HYDRAULIC CIRCUIT COMPRISING SAID VALVE
VENTIL ZUM TEILEN EINES HYDRAULIKKREISLAUFS UND HYDRAULIKKREISLAUF MIT DIESEM VENTIL
SOUPAPE POUR DIVISER UN CIRCUIT HYDRAULIQUE ET CIRCUIT HYDRAULIQUE COMPRENANT LADITE SOUPAPE
07.06.2023
Patent
Elektronische Ressource
Englisch
Valve for dividing a hydraulic circuit and hydraulic circuit comprising said valve
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