The DC power supply for test aircraft equipment, used standarts MIL-STD-704, RTCA/DO-160F
Products - Specialized projects
The DC power supply for test aircraft equipment, using standarts MIL-STD-704, RTCA/DO-160F.
Output parameters DC power supply: current load to 400A, output voltage to 80V, output power to 25 kW.
Functionally, the source consists of three blocks of KULON (power modules), electronic switch unit, built-in control panel and remote control.
Сontrol system of DC power supply synchronously controls the power modules and the switch unit.
Сontrol system of DC power supply supports three modes of operation:
- Manual mode - arbitrary connection of one of the power modules to load, manual control the output voltage during operation.
- Auto mode - control the power modules and switch in accordance with the parameters set previously from the control panel or remote control.
- Program mode - control the source via cyclograms, downloaded from a personal computer (PC).
The DC power supply for test aircraft equipment
mobile version
Structure of DC power supply for test aircraft equipment
Technical specification
| Parameter | Dimension | Value |
| Line voltage | V | 380±38 |
| Ouput current, up to | A |
400 |
| Ouput voltage, up to | V |
80 |
| Efficiency at rated parameters | % |
90 |
| cos φ | - |
0,85 |
| Resolution of voltage regulation | V |
0,1 |
| Resolution of current regulation | A |
1 |
| Current consumption of the network at full output | А |
65 |
| Own source consumption when idle and a maximum voltage of not more than | W | 750 |
| Cooling system | Air-forced | |
| Mass | kg | 230 |
| Dimensions - width х depth х height | mm | 1610х1050х1280 |
| Operation temperature | ºС |
1...+40 |
| Protection | IP21 |