Aircraft Electrical Power Generation Systems

021-09-03Pablo Asensio Martínez2026-03-242 min

AC Generation

Large aircraft typically require High Voltage AC power (115/200V, 400Hz, 3-phase).

  • Brushless AC Generators: Use a set of permanent magnets for initial excitation.
    • Exciter Generator: Mounted on the same shaft.
    • Permanent Magnet Generator (PMG): Specifically used for initial excitation current and powering the generator control.
  • Voltage Regulation: The Voltage Regulator controls the output voltage (keeps it constant at varying loads/speeds) by adjusting the excitation current to the field coil.
    • Wired in series with the field coil.
    • If electrical load increases -> Voltage drops -> Regulator increases excitation current -> Voltage returns to normal.

Constant Speed Drive (CSD) & IDG

AC generators must spin at a constant speed to maintain a constant frequency (400Hz), despite the engine's varying RPM.

  • CSD (Constant Speed Drive): A hydromechanical unit that converts variable engine speed to constant generator speed.
    • Monitors/Adjusts: Output Frequency.
    • Has its own independent oil system for lubrication and cooling.
    • Faults: High oil temperature, low oil pressure.
  • IDG (Integrated Drive Generator): Combines the CSD and the Generator into one single unit.
    • Disconnect: In case of a fault (e.g., high oil temp, low pressure), the pilot operates the IDG disconnect switch.
    • Consequence: The drive shaft is mechanically disconnected. The generator is unusable for the rest of the flight.
    • Reset: Can ONLY be reconnected on the ground by maintenance with the engine stopped.

Frequency Wild

  • Frequency Wild Generators: Generators where the frequency varies with engine speed (no CSD/IDG).
  • Application: Only suitable for resistive loads (e.g., anti-icing mats/heaters) because inductance/reactance are frequency-dependent.

DC Generation & Conversion

  • TRU (Transformer Rectifier Unit):
    • Combines a Transformer and a Rectifier.
    • Function: Converts AC (115V) to DC (28V).
    • Used to power DC buses and charge batteries from the main AC supply.
    • Often includes a smoothing/filter circuit to minimize output fluctuation.
  • Inverter:
    • Function: Converts DC (28V) to AC (115V, 400Hz).
    • Static Inverter: Solid-state device (no moving parts) used for essential AC loads if main AC fails.
  • Starter-Generator:
    • Combines starter motor and generator functions (common on turbine engines).
    • Acts as a starter motor to spool the engine up to self-sustaining speed.
    • Switches to become a DC generator once the engine is running.

Protection & Control

  • GCU (Generator Control Unit):
    • Checks for faults (over-voltage, over-excitation).
    • Controls the Generator Circuit Breaker (GCB) and Exciter Control Relay.
  • Split Bus System: If a generator fails, GCBs/BTBs (Bus Tie Breakers) reconfigure to ensure essential loads are powered.
Written and reviewed by

Pablo Asensio

Aeronautical engineer. Passed the thirteen EASA ATPL(A) theoretical knowledge exams studying from these very notes. Writes and reviews each topic against the Part-FCL Learning Objectives.