Auxiliary power control Unit
Control system of the various valves corresponding to start-up of the engine by monitoring analog and discrete signals from the aircraft. The operation sequence is fully software programmable and supports real-time monitoring of operation status by an external PC (RS-422 communication).
Features
- Supporting various interfaces (various bus, analog, discrete)
- High reliability with redundancy system
- Customizable for enclosure shape, input/output signals, connector and redundancy configurations
Standard Configuration
Digital Interface | 1553B/RS-422, etc |
---|---|
Analog Signal Input | DC Voltage/DC Voltage/ Frequency etc. |
Discrete Signal Input | 28VDC / OPEN / GND etc. |
Redundancy Design | Double Redundant Internal Circuits |
Power Input | +28VDC(MIL-STD-704) |
Power Consumption | 50W or Less |
Environmental Conditions | MIL-HDBK-5400 Class 1 |
Dimensions, Mass | 300(W)*100(D)*120(H)mm, 3.0kg or Less |
EMI | MIL-STD-461 |
*Please contact us for the detailed specification.