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).
- Supporting various interfaces (various bus, analog, discrete)
- High reliability with redundancy system
- Customizable for enclosure shape, input/output signals, connector and redundancy configurations
|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 Consumption||50W or Less|
|Environmental Conditions||MIL-HDBK-5400 Class 1|
|Dimensions, Mass||300(W)*100(D)*120(H)mm, 3.0kg or Less|
*Please contact us for the detailed specification.