Passive fluidic valve for fixed flow rate distribution

A passive fluidic valve for a hydraulic circuit of an equipment of an aircraft comprising:

• a hollow valve body comprising:
• an inlet;
• a first outlet comprising a first restriction delimiting an upstream cavity of first outlet and a downstream cavity of first outlet;
• a second outlet comprising a second restriction delimiting an upstream cavity of second outlet and a downstream cavity of second outlet;
• a first cavity;
• and
• a second cavity,
• a valve member movable in the valve body configured to at least partially block a passage between said inlet and one of the two outlets, comprising:
• a first end located in the first cavity so as to at least partially delimit a first and a third chambers in said first cavity,
• a second end located in the second cavity so as to at least partially delimit a second and a fourth chambers in said second cavity,
• a first fluid communication between said first chamber and said upstream cavity of first outlet;
• a second fluid communication between said third chamber and said downstream cavity of first outlet;
• a third fluid communication between said second chamber and said upstream cavity of second outlet;
• and
• a fourth fluid communication between said fourth chamber and said downstream cavity of second outlet.