11.6 Electrical Power Flashcards
(88 cards)
What are the two main subsystems of the aircraft electrical power system?
A) Power and Control
B) Generation and Distribution
C) Storage and Monitoring
B) Generation and Distribution
Which two sources provide electrical power on the ground?
A) Engine generators and TRUs
B) Batteries and APU
C) APU and GPU
C) APU and GPU
Which of the following is NOT one of the three DC power sources used for generation?
A) AC alternator
B) DC battery
C) DC generators
A) AC alternator
What are two typical uses for the aircraft battery system?
A) Flight data storage and lighting
B) Emergency power and APU start
C) Cabin entertainment and flight control
B) Emergency power and APU start
In an emergency, how long must the battery supply electrical power to all consumers?
A) 10 minutes
B) 20 minutes
C) 30 minutes
C) 30 minutes
What are the two common types of main aircraft batteries?
A) Ni-Cd and Lithium-ion
B) Ni-Cd and Lead-acid
C) Lead-acid and Gel-cell
B) Ni-Cd and Lead-acid
What is the nominal voltage of a fully assembled aircraft battery made of cells in series?
A) 12V
B) 24V
C) 36V
B) 24V
What voltage does a battery cell typically reach when fully charged?
A) 1.2V
B) 1.5V
C) 2.0V
B) 1.5V
What is a major safety concern associated with batteries?
A) Static discharge
B) Electromagnetic interference
C) Thermal runaway
C) Thermal runaway
Which method is NOT used to charge nickel-cadmium batteries?
A) Constant voltage
B) Constant current
C) Pulse discharge
C) Pulse discharge
How can line maintenance personnel monitor the charge level of Ni-Cd batteries?
A) By weighing the battery
B) By checking voltage and current during charging
C) By using infrared scanning
B) By checking voltage and current during charging
What voltage is used from the DC distribution to recharge batteries via TRUs?
A) 12V
B) 24V
C) 28V
C) 28V
Which of the following is NOT one of the three possible DC power sources used in modern aircraft?
A) DC battery
B) DC inverter
C) DC generator
B) DC inverter
What is the primary role of the Ground Power Unit (GPU) or External Power Unit (EPU)?
A) To regulate onboard battery voltage
B) To supply power to the aircraft while on the ground
C) To boost engine performance during takeoff
B) To supply power to the aircraft while on the ground
What component is responsible for automatically maintaining a generator’s voltage within a set limit?
A) Power control unit
B) Load shed relay
C) Voltage regulator
C) Voltage regulator
Which unit converts AC voltage from the generator into DC voltage?
A) Inverter
B) Transformer Rectifier Unit (TRU)
C) Voltage regulator
B) Transformer Rectifier Unit (TRU)
What are the typical DC output voltages provided by TRUs?
A) 115 Vdc and 230 Vdc
B) 28 Vdc and 14 Vdc
C) 24 Vdc and 48 Vdc
B) 28 Vdc and 14 Vdc
What is the main function of a Transformer Rectifier Unit (TRU)?
A) To convert DC to AC power
B) To rectify and transform AC voltage to DC at a usable level
C) To synchronize generator frequencies
B) To rectify and transform AC voltage to DC at a usable level
What is one key advantage of parallel DC systems in aircraft?
A) They are lighter in weight
B) They reduce the voltage requirement
C) They allow buses to remain connected if a generator fails
C) They allow buses to remain connected if a generator fails
What is the purpose of the synchronising or sync bus in a DC system?
A) To increase generator voltage output
B) To isolate the TRUs
C) To connect the generators during flight
C) To connect the generators during flight
How are the main DC buses normally switched into parallel operation?
A) Automatically by the GPU
B) Through “DC BUS” switching
C) Using the inverter relay
B) Through “DC BUS” switching
What are the primary sources of AC power on an aircraft?
A) AC batteries, solar panels, fuel cells
B) Static inverters, rotary inverters, AC generators
C) Fuel pumps, CSDs, hydraulic motors
B) Static inverters, rotary inverters, AC generators
What are the standard voltage and frequency values for modern aircraft AC systems?
A) 230V, 60Hz
B) 115V/200V, 400Hz, three-phase
C) 28V, 400Hz, single-phase
B) 115V/200V, 400Hz, three-phase
In a rotating field alternator, what remains stationary?
A) Field
B) Rotor
C) Armature
C) Armature