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92 Cards in this Set
- Front
- Back
|
What are the advantages of using transformers
and transformer rectifiers vice inverters and dynamotors for supplying aircraft power? |
Lightweight, more reliable, and simple to maintain
|
|
What power system requirements do modern
naval aircraft have? |
120-/208-volt ac, 3 phase and 400 Hz
|
|
What determines the voltage frequency of an
ac generator? |
The number of magnetic poles and the rotor rpm
|
|
What are the two types of ac generators?
|
Brush and brushless
|
|
What supplies the output ac power of a generator?
|
The stator
|
|
How many phases is an ac generator?
|
Three
|
|
What are the advantages of a brushless generator
over a brush-type generator? |
Increased reliability and greater operating time between overhaul
|
|
What is a prime mover?
|
A device that provides the driving force for a generator
|
|
What is the purpose of a CSD?
|
Convert variable engine speed to a constant speed output
|
|
What are inverters?
|
An emergency source of ac power when normal ac power fails
|
|
In an inverter, what converts electrical energy
to mechanical energy? |
The dc motor
|
|
On what does the rating of an aircraft inverter
depend? |
The equipment that it will supply
|
|
What is the purpose of a transformer?
|
To convert an input ac voltage into a usable ac output voltage by either stepping
up or stepping down that voltage |
|
What is the function of a transformer
rectifier? |
To convert ac input voltage to a dc output voltage
|
|
What is the only moving part in a transformer
rectifier? |
The cooling fan
|
|
What is the difference between an autotransformer
and an ordinary transformer? |
An autotransformer has one winding that is common to both primary and
secondary windings. |
|
Autotransformers offer savings in both size
and costs over conventional units. When are these savings greatest? |
When the turns ratio is less than 2:1
|
|
What are the two general types of instrument
transformers? |
Current and potential
|
|
What are the ways in which emergency power
is supplied to naval aircraft? |
Aircraft storage batteries, auxiliary power units, and hydraulic motor driven
generator |
|
What components maintain the aircraft (a/c)
storage battery in a charged state? |
Ac generator and transformer rectifier
|
|
What are the two most common types of a/c
storage batteries in use today and what are the colors of each? |
Lead-acid which have a red case and nickel-cadmium which have a blue case
|
|
What manual is used for information on
securing, storing, servicing, and handling a/c storage batteries? |
NAVAIR 17-15BAD-1
|
|
On a VLAB, what is the purpose of the vent
nozzles? |
The upper nozzle is connected to a tube that supplies definite pressure on the
battery while in flight. The lower nozzle is connected to a negative pressure tube, allowing battery acid to drain without damaging the aircraft |
|
The sump jar of a VLAB system contains a felt
pad moistened with what? |
Sodium bicarbonate
|
|
In a VLAB system, what is the purpose of the
sump jar and the felt pad? |
To neutralize the gases and excess battery solution
|
|
What type of electrolyte is used in a SLAB?
|
A mixture of sulfuric acid and water
|
|
In a SLAB, how is electrolyte immobilization
accomplished? |
By using a gel or special mats to absorb electrolyte
|
|
What is considered the fundamental unit of a
NICAD battery? |
The cell
|
|
What are the types of cells used in NICAD
batteries? |
Vented and sealed
|
|
What is the nominal value of a NICAD battery
cell? |
1.26 volts dc
|
|
Why can the hydraulic driven emergency
generator only power a small number of circuits? |
The kVA rating is too low
|
|
What causes the rotor in the generator to
turn? |
The hydraulic motor
|
|
What helps to maintain generator output frequency?
|
The motor converts 3000 pounds per square inch of fluid to a constant speed
rotation |
|
How is the generator cooled?
|
By the hydraulic fluid
|
|
What is the purpose of the motor-generator
control? |
It provides voltage regulation and fault detection of the generator output
|
|
What is the function of the solenoid control
valve? |
It is de-energized when primary electrical power is lost and allows hydraulic
fluid to be routed to the hydraulic motor to drive the generator |
|
What is the function of an APU?
|
To supply pneumatic power for starting engines and operating air conditioning
systems, electrical power for in-flight emergencies, and ground maintenance |
|
What is needed for APU starting?
|
Aircraft battery and fuel
|
|
On a GTCP-95, what drives the generator?
|
Shaft power at the main output drive pad
|
|
What are the two main sections of an APU?
|
Accessory assembly and compressor/turbine assembly
|
|
The electrical system of an APU consists of
what components? |
Holding relays, oil pressure switch, centrifugal switch assembly, hour meter, and
wiring harness |
|
APU ignition cuts out at what rpm?
|
95%
|
|
What is the purpose of the centrifugal speed
switch assembly? |
It controls the sequence of operation of various electrical components
|
|
How many sub-switches make up the
centrifugal speed switch assembly? |
Three
|
|
How are the centrifugal speed switches
adjusted? |
By using an adjustment screw to apply spring tension to the lever arm
|
|
What are the functions of each switch?
|
35%—shuts the starter down; 95%—arms load control circuit, starts hour meter,
and shuts off ignition; 106%—overspeed protection (shuts down the APU during an overspeed condition) |
|
Changing the setting of the 35% switch also
affects what? |
The settings of the 95% and 106% switches
|
|
How does the 106% switch shut down the
APU? |
When the switch is actuated it cuts off fuel flow, causing the APU to shut down
|
|
At what rpm is the starter disengaged?
|
35%
|
|
What could happen to the starter if the
dropout relay fails? |
The starter may fail internally due to an overheat or overspeed condition
|
|
Why do we use external electrical power on
aircraft? |
It provides ground crews with electrical power for servicing, fueling, and
performing maintenance actions |
|
What is the most common method of voltage
regulation for ac generators? |
Varying the current to the field windings
|
|
Why would we use a permanent magnet on the
generator rotor in place of exciter windings? |
It helps to maintain a constant load on the generator and simplifies generator
construction |
|
What happens when magnetic fields of
alternating polarity pass across the armature windings? |
Ac voltage induction occurs
|
|
What controls the voltage induced into the
armature windings? |
1. The number of turns of conductor per winding
2. Generator rpm 3. Magnetic field strength |
|
What must ac generator control systems
protect against? |
1. Over- or undervoltage
2. Over- or underfrequency 3. Improper phase sequence |
|
What is the purpose of the rotating
three-phase rectifier in a brushless generator? |
Change the rotating ac output voltages of the exciter to dc voltages
|
|
What is the chief advantage of having dc
exciter units integrated into ac generators? |
Each generator has its own independent source of excitation so no external
source of electrical power is necessary |
|
What is the only moving mechanical part in a
solid state voltage regulator? |
Exciter control relay
|
|
What happens if the output of the control
amplifier section of a voltage regulator is too low? |
Regulator circuitry increases the field strength of the ac exciter
|
|
In a solid-state voltage regulator, what component
supplies the power to the bridge circuit? |
CR1
|
|
What prevents the generator from receiving
excitation voltages when the frequency is too low? |
Underspeed switch
|
|
Why is controlling the rotor rpm the only
means of fine-tuning the output frequency of a generator? |
The generator has a fixed number of poles
|
|
What two components are joined by the CSD?
|
Engine and generator
|
|
List the components of the CSD.
|
Hydraulic pump, hydraulic motor, governing system, gear pump, charge pump,
replenishing pump, and scavenge pump |
|
When the input engine rpm is too low, what
happens to the CSD hydraulic pump? |
The pump supplies more oil to the hydraulic motor causing it to increase rpm
|
|
How is the CSD/generator system protected
during underspeed conditions? |
An underspeed pressure switch is used to break the electrical circuit
|
|
What component provides circuit protection
for an ac generator? |
Supervisory panel
|
|
A supervisory panel will disconnect the generator
from the load under what conditions? |
Over-/underfrequency
Over-/undervoltage Feeder fault |
|
What is the required output frequency of the
PMG? |
600 Hz
|
|
How many amperes are required through the
exciter coil to generate a 120-/208-volt, 60-kilovolt ampere (kVA) load? |
1.7 amps
|
|
During an undervoltage condition, at what
voltage will the generator be dropped off line? |
When one or more phases drops to 90 volts or less
|
|
At what voltage will the generator be dropped
off line during an overvoltage condition? |
When one or more phases is 129 volts or greater
|
|
What is feeder fault?
|
A condition where the current leaving the generator does not pass through the
load |
|
In an electrical system, what is a “bus?”
|
A primary power distribution point that is connected to the main power source
Usually holds systems of like priority |
|
How are buses identified?
|
By the priority of the equipment it powers
|
|
What are the types of output protection devices
used by buses? |
Circuit breakers, fuses, or current limiters
|
|
What are the two basic types of power contactors?
|
Single coil and double coil
|
|
What are the four power sources available to
the F-14 aircraft? |
Left main generator, right main generator, emergency power, and external power
|
|
List the three-phase buses of the F-14 aircraft.
|
Left and right main ac buses, number one and two ac essential buses, and the ac
monitor bus |
|
What dc bus willNOT be powered in the event
of one TR failure in the F-14 aircraft? |
Dc monitor bus
|
|
In an F-14 aircraft, what is the purpose of the
GPM? |
It prevents external power from being applied if it is not within specified
tolerances |
|
How will the pilot of an F-14 know if external
power is applied to or disconnected from his aircraft? |
Hand signals from the plane captain
|
|
What is the purpose for jumping pins E and F
on the external power receptacle? |
It energizes the external power contactor
|
|
In an F-14 aircraft, with both main generators
on line, which buses does the left main generator power? |
All 115-Vac essential and instrument buses, and 26-Vac instrument and navigation
buses |
|
With both generators on line, 115-Vac essential
bus number two fails to be powered. Which components could be faulty? |
Power contactor K3
|
|
External power is applied to the aircraft, the
right generator comes on line, and only the main ac bus loses power. What component could be faulty? |
Power contactor K2
|
|
If the right TR fails, what bus, if any, will be
lost? |
None
|
|
What will cause the monitor bus to lose
power? |
If both TRs fail
|
|
What ac bus does the emergency generator
supply power to? |
Essential bus
|
|
What is the main advantage of a grounded
system? |
It alleviates an extra conductor
|
|
What are the disadvantages of ungrounded
systems? |
Added weight, cost, and space
|