Electrical power systems: generation, distribution and protection
Generators, conversion, batteries, bus architecture, circuit protection and EWIS on transport aeroplanes, under CS-25 and 14 CFR Part 25
What you will be able to do
- ✓ Describe the architecture of an aircraft electrical power system under ATA 24, the AC and DC supplies used, and the CS-25 and 14 CFR Part 25 paragraphs that certify it.
- ✓ Explain how integrated drive and variable-frequency generators, control units, APU and external power, batteries and the ram air turbine supply power in normal and emergency conditions.
- ✓ Compare lead-acid, nickel-cadmium and lithium-ion batteries, their thermal runaway hazards and special conditions, using the NTSB findings on the 2013 Boeing 787 APU battery fire.
- ✓ Analyse bus architecture and load shedding, and calculate bus loads and battery-only endurance for normal and failure cases.
- ✓ Apply circuit protection, EWIS and bonding requirements, including continuity and insulation-resistance checks and protect-clean-as-you-go practice.
- ✓ Apply safe isolation, wiring-diagram troubleshooting and MEL relief to make sound maintenance and dispatch decisions on electrical defects.
Course content
Session 1 · Aircraft electrical power: the system and its rules
1.1
- Electrical power on a modern aeroplane · free preview
- AC and DC: the voltages aircraft use
- The certification basis
- Worked example: a load analysis on two DC buses
Session 2 · Generating the power: IDG, VFG, APU and emergency sources
1.2
- Engine-driven generators: IDG and variable frequency
- Control, protection and the other sources
- Emergency power: RAT, batteries and the rules
- Worked example: IDG high oil temperature, service or replace?
Session 3 · Converting and storing: TRUs, inverters and batteries
1.3
- Transformer rectifiers, inverters and converters
- Lead-acid and nickel-cadmium batteries
- Lithium-ion batteries and special conditions
- From the investigation file: the Boeing 787 APU battery fire, Boston 2013
Session 4 · Distribution: bus architecture, load shedding and emergency power
1.4
- Bus architecture: who feeds what
- Load management and load shedding
- The emergency configuration
- Worked example: how long will the batteries last?
Session 5 · Circuit protection, wiring and bonding: EWIS in practice
1.5
- Circuit breakers, fuses and arc-fault protection
- EWIS: wiring as a system
- Bonding, connectors and the faults wiring causes
- Worked example: continuity and insulation-resistance check
Session 6 · Working safely, troubleshooting and MEL relief
1.6
- Working safely: de-energising and lock-out
- Troubleshooting with wiring diagrams
- MEL relief for electrical items
- Worked example: dispatching with one generator inoperative
Who this course is for
Course content © Aerospace Garage Limited. All rights reserved.