4.2 Electrical Systems Flashcards

1
Q

What forms of electrical power are they?

A

3-Phase AC, AC, DC

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2
Q

Name types of Power Sources on an aircraft

A

Engine Driven AC Generators
Auxiliary Power Unit (APU) - power to start the engines, for backup
External Power - Ground power only, AC provided by a Ground Power Unit (GPU) through external plug
Ram Air Turbine (RAT) - emergency
Battery - backup or emergency power for typically 30mins, 28V DC and 1154AC (40Hz)

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3
Q

What electrical loads are on aircraft?

A

Motors and actuation, Lighting services, Heating services, Subsystem Controllers, Avionics Systems, Environmental Control System

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4
Q

Electrical Design Drivers:

A

total electrical load
power quality
safety
reliability

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5
Q

Electrical Design issues

A

Engine Power Off-takes
Generator and generator control
Power Switching
Wiring and Connectors

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6
Q

Whats the formula for the Engine Electrical Power Index?

A

EPI = Electrical Power / Number of Engines * Thrust/MTOW
in kW
EPI = Main Electrical Power per Engine * Thrust/Weight ratio

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7
Q

What backup systems for electrical Power are there?

A

Ram Air Turbine
Backup Generators and converters - variable frequency
Permanent Magnet Generators - used to generate 28V DC emergency power for high integrity systems (e.g. Flight control system)

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8
Q

What system configurations for power distribution exist?

A

Parallel Bus Systems - total electrical system load is shared on equally by all active generators in parallel
+ Generator load distribution
- High effort of controls (voltage, phase, frequency)
Split Bus Power Systems (standard)
each generator supplies power separately from the other generator
+ independent systrems
- more complex systems
Split Parallel bus systems ?

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9
Q

What are the primary functions of an electrical system?

A

Power generation
Power conversion and regulation
Power distribution and protection

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10
Q

What makes up the Constant frequency integrated drive generator?

A

the Integrated Drive Generator (idg) consists of a
Constant Speed Drive (CSD)
AC generator

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11
Q

How does the Generation Control Unit (GCU) work?

A

regulated the output voltage and provides portection
controls the Generator Control Breaker (GCB):
- GCB close: when all operation params are ok
- GCB open: when fault conditions prevail
monitoring and protection functions:
under/over voltage
under/over excitation
under/over frequency
differential current position
correct phase rotation

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12
Q

What conversion and chargers are there?

A

Inverters: VDC -> VAC single or three phase power
Transformer Recifier Units (TRUs): VAC -> 28VDC
Auto transformer units (ATUs): AC voltage -> another AC voltage
Auto transformer rectifier untis (ATRUs) - >conver unregulated VAC -> 270VDC power
Battery charger: like TRU, but dedicated unit for a controlled charge without overheating

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13
Q

What categories of wiring routes are there?

A

Non-customized routes: identical for all aircraft within family: power feeders and power distribution, flight control system
wiring segregated in differeing wiring routes -> important functions are not carried in the same routing,
redundant routes (flight critical routes are doubled)
Customized routes: customer/airline dependent routes for board electronics, galley systems, in flgiht entertainment

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14
Q

Whats a digital mock up?

A

A Digital Mock-Up (DMU) is a virtual computer-generated model of the aircraft which is being
used as the “master” reference for the entire development team:
* A highly detailed DMU helps to speed up development: Everyone can work as a virtual
team and shares the latest information during each phase of development/manufacturing.
* Beginning with the concept phase, the utilization of the DMU will extend throughout the
aircraft’s entire lifecycle (Airbus)

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