Electrical Flashcards

1
Q

System voltage & battery

A

28-VDC, dc power provided by one 34 amp-hr, air cooled, 20 cell, nickel cadmium battery & two 250 amp starter/generators connected in parallel

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2
Q

What bus is the battery always connected to?

A

Hot battery bus

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3
Q

How does the battery provide power to the whole system?

A

Battery switch closes a bus tie and a battery relay

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4
Q

The airplane utilizes a ________ system

A

Multi-Bus

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5
Q

How many buses are there? What are they?

A

5

L/R generator Bus, Center Bus, Triple-Fed Bus, and battery emergency bus

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6
Q

What is the triple fed bus powered from?

A

Battery and both generator buses

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7
Q

What is the center bus fed from?

A

Two generator buses and the battery, connecting both components when the bus ties are closed

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8
Q

What is provided to isolate a fault in the system?

A

High current (Hall Effect) sensors, bus tie relays, and current limiters

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9
Q

The DC power distribution is commonly called a _________ system

A

Triple-fed

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10
Q

What are the 3 DC power sources available?

A

One 24 volt, 34 amp-hr, nickel cadmium battery

Two 28 volt, 250 amp starter/generators

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11
Q

What happens when the battery switch is turned on?

A

Bus tie relays close

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12
Q

How is the battery power routed?

A

Battery relay to the triple fed bus, and through the battery bus tie relay to the center bus and to both starter relays

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13
Q

What 3 buses are tied together by the center bus?

A

Generator bus, hot battery bus, and the battery

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14
Q

How is the electrical system protected from excessively high current flow?

A

The bus tie system

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15
Q

With no power applied to the electrical system, how many bus tie relays are left open?

A

All 3

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16
Q

Why is the coil circuit of the bus tie relay latched open?

A

To prevent the bus tie relay from closing

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17
Q

When the bus tie relay has been opened by excessively high current flow through the Hall Effect sensor, how can it be reset?

A

Momentarily activating the BUS SENSE switch to RESET

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18
Q

Momentarily activating the BUS SENSE switch to TEST connects bus voltage to ________ current sensor test circuits.

A

All 3

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19
Q

Manually closing the generator bus tie relays will connect the generator buses to what bus?

A

The center bus, providing power to the whole system

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20
Q

Can a generator bus tie relay be manually closed if a fault opened the tie?

A

No, the BUS SENSE switch must be activated to RESET to reset the tie.

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21
Q

What is bypassed during a cross-generator engine start?

A

The high current sensors and current limiters

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22
Q

What happens if an over current situation causes a current limiter to open?

A

It causes bus isolation

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23
Q

What is the protection for the triple-fed bus?

A

60-amp current limiters

24
Q

When will triple-fed bus isolation occur?

A

If all 3 of the limiters are opened

25
Q

Why is load shedding beneficial?

A

Electrical system automatically will remove excess loads

26
Q

What happens, during load shedding, when both generators are offline?

A

The generator bus ties open and the bus loads are shed

27
Q

What is the best choice to make if load shedding occurs during flight?

A

To land as soon as practicable, unless it can be remedied, and one generator be brought back online.

28
Q

Is the lead acid battery air cooled?

A

No

29
Q

The starters are dual purpose, ________ units.

A

Engine driven

30
Q

A series starter winding is used during _________ operation and a shunt field winding is used during ________ operation.

A

Starter, generator

31
Q

What is the regulated output of the generator?

A

28.25 +- 0.25 volts with a maximum continuous load of 250 amps.

32
Q

During an engine start, the battery is connected to the _________ by the starter relay.

A

Starter/generator

33
Q

Normally one engine is started on ______ power, and the other is ______ started.

A

Battery, cross

34
Q

During a cross generator start, the generator control panel closes what relay?

A

Cross-start, which allows for a bypass of the generator bus, current limiter, and bus tie relay.

35
Q

When a starter is selected, what happens to the bus tie sensors?

A

They are disabled to prevent them from opening their respective bus tie relays.

36
Q

Is the generator system self exciting or require external power for operation?

A

Self-exciting

37
Q

How many generator control units is the generator operation controlled through?

A

2

38
Q

What are some functions of the Generator Control Unit (GCU)?

A

Voltage regulation, over voltage protection, paralleling/load sharing, reverse-current protection, cross-start relay activation

39
Q

What happens if the generator output voltage is within 0.5 volts of the aircraft bus voltage?

A

GCU sends a signal to the line contractor, which will close and connect the generator to the aircraft bus and will close both generator ties to connect the center bus and the generator buses.

40
Q

During single-generator operation, what does the GCU do to the line contractor?

A

Opens it and isolates the inoperative generator from its bus.

41
Q

What provides over voltage protection to prevent excessive generator voltage from being applied to aircraft equipment?

A

The GCU

42
Q

What is the max voltage of the generator output before being detected by the over-excitation circuits?

A

32 volts

43
Q

What happens during an over-excitation from a generator?

A

The GCU over-excitation circuit will disconnect generator from electrical system.

44
Q

What is paralleling/load sharing?

A

Averages the output of the both generators to equalize the loads

45
Q

When does paralleling of the GCU become operative?

A

When both generators are online

46
Q

What percentage are the GCUs designed to balance loads to?

A

2.5%

47
Q

What is reverse current protection provided by?

Ex: When shutting an engine down, enough power isn’t provided so it begins to pull from elsewhere.

A

The GCU.

48
Q

During cross-starts, what sensors are disabled to prevent bus isolation?

A

The Hall Effect sensors

49
Q

How is AC power provided to avionics and engine instruments?

A

By 2 inverters

50
Q

What are the 2 levels of power that inverters can provide?

A

115 volts, 400Hz for avionics and 26 volts, 400Hz for the engine instruments, and some avionics

51
Q

What is the standard rated output of an inverter?

A

250 volt-amps (optional: 300 amps)

52
Q

Where are the inverters located?

A

The wing, outboard of each nacelle

53
Q

What is the purpose of an inverter?

A

To change AC power to DC power

54
Q

What are indications of an inverted failure?

A

Getting INVERTER annunciator, erratic behavior, or loss of AC powered instruments (torque gage), or AC avionics

55
Q

Switches that have a white ring around them receive power from which buses?

A

The center bus and the triple-fed bus