Aircraft Electrical System Trainer

The system is laid out to depict a typical aircraft electrical system, and contains standard aircraft components and wiring. This is a complete functional simulation of adual-engine 28 V DC electrical system of a typical turbine aircraft. The aircraft electrical system trainer is an ideal resource to teach about an aircraft multi engine electrical system. By using this trainer, students not only learn the functionality of each component, but they also develop logical and systematic approach to perform troubleshooting tasks.

Generator:
Aircraft DC generator rated 28 VDC at the rate 40A/ 50A at 3600 rpm, driven by 230 VAC/50 HzMotor.
Battery:
Aircraft sealed, 24V battery
Starters:
Aircraft Starter 24 VDC
Generator Controls:
Electronic Controlled Generator Build-up
Reverse Current Protection
Paralleling /Equalizing
GCU induced Over Voltage (OV) Protected
Voltage Regulation: 28.4V + 0.4V
Max Field Current: 3A.
Electronic Field Controller/Switching
Current Limiter.
AC Power:
Two Static Inverters, each rated 50VA minimum.
Two Auxiliary Bus-bars 28VDC
No.1 Generator Bus-bar 28VDC
No.2 Generator Bus-bar 28VDC
Ground Bus-bar
Battery Bus-bar.