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

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 hydra...

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Bibliographic Details
Main Author CALDERON GOMEZ, Pablo Manuel
Format Patent
LanguageEnglish
French
German
Published 07.06.2023
Subjects
ACTUATING-FLOATS
AIR INTAKES FOR JET-PROPULSION PLANTS
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
COCKS
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
COSMONAUTICS
DEVICES FOR VENTING OR AERATING
ENGINEERING ELEMENTS AND UNITS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GAS-TURBINE PLANTS
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
PARACHUTES
PERFORMING OPERATIONS
TAPS
THERMAL INSULATION IN GENERAL
TRANSPORTING
VALVES
WEAPONS
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Summary: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.
Bibliography:Application Number: EP20210383094