FUEL CONTROL VALVE


The Fuel Control Valve is a motorized valve that allows the user to select or shut off the flow path.

Fuel control valves have double reduntant position control electronics and they are operatable with aviation fuels in between -55°C to +60°C.

Position control and monitoring can be done by discrete signals, CAN bus and RS485 commnunication.

Fuel control valve provides lightweight solution where solenoid valves are not preferred.


TECHNICAL SPECIFICATIONS

Operating Temperature: -55°C to +60°C
Fuel: Jet A-1, JP-8
Supply Voltage: 28 V Nominal (Vnom), 36 V Max., 12 V Min.
Standby Current: 10 mA, Heater ON: Max. 200 mA
Current Consumption: Max. 2.5 A
Communication: CAN 2.0A, RS485 Full Duplex, Independent I/O pins, Quick Reference Led

Working Pressure: 200 kPa, Max. 500 kPa, Burst 1000 kPa
Pressure Drop: TBC 10 mbar at 1000 lph
Internal Leakage: 0
External Leakage: 0
Time Between Overhauls TBC: 1000 Cycles, 1000 Flight Hours, 1 Year
Service Life TBC: 4000 Cycles, 4000 Flight Hours, 4 Years