Avionics Module Design (AMT)

Avionics Module Design (AMT)

The main objective of the Avionics Power Module is to convert the standard voltage produced in aircraft to the 28VDC voltage, which is the supply of the subsystems of aircraft, in high efficiency in accordance with military aviation standards. In cases where more output power is needed in a product with an output power of 500 W, it is possible to increase the power capacity by running identical products in parallel. The minimum efficiency of the Avionics Power Module is %90. The converter unit produced as a module aims to reduce the special design costs at these power levels thanks to its high power density, parallel connectivity, and cooling features from the body.


Input Features

  • Input Voltage
    270 VDC
  • Input Voltage Range
    180-400 VDC
  • No-load Power Consumption
    <0,5 A

Output Features

  • Output Voltage
    28,0±0,5 VDC
  • Rated Output Power
    500 W
  • Output Voltage Fluctuation
    ±0.5 VDC
  • Output Current
    19 A

Environmental Characteristics

  • Operating Temperature
    −40°C ~ +70°C
  • Storage Temperature
    −40°C ~ +85°C
  • Temperature Shock

    MIL-STD-810G, Method 503.5, Procedure I

    −40°C ~ +70°C

  • Mechanical Shock

    MIL-STD-810G, Method 516.6, Procedure I

    (Functional, 40g 11ms)

  • Vibration
    MIL-STD-810G, Metot 514.8
  • Altitude
    MIL-STD-810G (20.000 feet)
  • Humidity
    MIL-STD-810G, Metot 507.6