Aero Engine Fuel Control Unit

Aero Engine Fuel Control Unit

AEFCU is a backup control unit for FADEC designed to regulate the fuel flow to aero engine in case of emergency. The control unit is built around Xilinx, Zynq 7020 processor on a customized carrier board where required peripherals/signal conditioner circuits are implemented. The unit has 512 MB DDR3 RAM and 256 MB QSPI flash where the application program reside.

Features:

  • RS422 Interface
  • Discrete I/O
  • Isolated thermocouple interface
  • Isolated RTD interface
  • 16 Bit resolver interface
  • LVDT Interface
  • Two (NH/NL) Speed sensor interface
  • Pressure Sensor Interface
  • Stepper motor with quadrature encoder interface
  • Servo valve interface
  • Conduction cooled
  • Operating Temp : -40 °C to +85 °C
  • Operating Voltage : 12-36 VDC
  • Meets MIL-861 and MIL -461 standards