Fluidic valve
A fluid valve is suitable for use with a hydraulic circuit of an item of aircraft equipment. The fluid valve includes a valve body having one inlet, two outlets and a communication channel with an external pressure source. The fluid valve further includes an electric solenoid actuator located in the valve body and having a movable ferromagnetic pilot. A valve member is movable inside valve body to at least partially block a passage between said inlet and one of the two outlets. The valve member at least partially defines first and second cavities. A fixed limiter is disposed within the communication channel such that a displacement of the movable pilot causes a variation in pressure in one of the first and second cavities to produce a force for moving the valve member.
1. A fluid valve for a hydraulic circuit in an item of aircraft equipment, comprising:
a hollow valve body comprising one inlet, two outlets and a communication channel with an external pressure source;
an electric solenoid actuator located in the hollow of the hollow valve body and including a movable ferromagnetic pilot;
a valve member movable inside the valve body to at least partially block a passage between said inlet and one of the two outlets, said valve member at least partially defining a first and a second cavity located on either side of said valve member in the hollow of valve body, and
a fixed limiter in said communication channel such that a displacement of said movable pilot causes a variation in pressure in one of said first and second cavities to produce a force for moving said valve member to vary a flow rate of a fluid between the inlet and the two outlets,
wherein at least a section of said member contains a ferromagnetic material, and that said electric solenoid actuator is configured to exert a magnetic displacement force on said ferromagnetic section of the valve member.
2. The fluid valve according to claim 1 , wherein the fluid valve is configured such that a displacement of said movable pilot causes a pressure variation to produce a force on said pilot in the opposite direction to said displacement.
3. The fluid valve according to claim 1 , wherein said fixed limiter comprises a passage between the pilot and a cylindrical wall that surrounds it.
4. The fluid valve according to claim 1 , wherein said pilot is connected to a spring.
5. The fluid valve according to claim 1 , wherein said valve member is perforated by a longitudinal hole to establish communication between said first and second cavities when it is not blocked, and that said pilot is configured to block said longitudinal hole in the valve member.
6. A hydraulic circuit in an item of aircraft equipment, comprising a fluid valve according to claim 1 .
7. An aircraft comprising a fluid valve according to claim 1 .