ELECTRICAL POWER SYSTEMS Flashcards
1
Q
- Describe the electrical system:
A
- Single-loop
- 28-volt DC
- Triple-fed system w/ a negative ground.
2
Q
- What supplies normal DC power?
A
during normal operation:
- 24-volt nickel-cadmium battery, or a 24-volt lead-acid battery
- two 28-volt
- 300-ampere starter-generators
3
Q
- Where is the battery located?
A
RH wing center section between the RH nacelle and fuselage
4
Q
- Battery power is connected to which buses?
A
- the battery bus,
- the center bus,
- the triple-fed bus.
5
Q
- What protects the five electrical buses?
A
The five primary buses are individually protected by:
- current sensors
- limiters
- diodes
- relays.
Load-shedding is accomplished by isolating a faulty bus from those that are still functional, thereby preventing a failure of the entire electrical system.
6
Q
- Which relays close when the Battery Switch is placed to ON?
A
- Battery relay
- Battery Bus Tie relay.
7
Q
- Describe Automatic Load Shedding?
A
Automatically sheds the generator busses as necessary to reduce excess loads.
8
Q
- What is on the Dual Fed Bus?
A
- L Engine Fire Ext
- R Engine Fire Ext
- Cabin Entry Lights
9
Q
- Explain the functions of the Generator Control Unit?
A
- Voltage regulation
- Overvoltage/over-excitation protection
- Reverse current protection;
- Paralleling/load sharing (within 10%)
- Isolates failed/Off gen from its bus.
- Cross-gen start current limiting;
10
Q
AC ELECTRICAL SYSTEM
- Describe the AC electrical system.
A
- 115-VAC and 26-VAC,
- single phase,
- It operates on 28 VDC and provides AC power to certain avionics and electrical equipment.
- 400 Hz system.
- The system consists of two static inverters, two bus-transfer relays, an AC power monitor circuit card and associated switches, circuit breakers, and annunciators.
11
Q
AC ELECTRICAL SYSTEM
- What will cause the red AC Bus annunciator light to illuminate?
A
- fault on the AC bus
- loss of AC power
12
Q
- Where are the AC Bus circuit breakers located?
A
On the fuel panel CB panel.
13
Q
A