Electrical Flashcards

1
Q

How many generators are there?

A

Four (GEN 1, GEN 2, APU, EMER GEN)

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2
Q

How many batteries are there?

A

2

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3
Q

What do the batteries provide?

A

DC, 28V

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4
Q

What do the Generators provide?

A

AC: 115/200V, 400Hz, 3 phase

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5
Q

Why do the batteries need to be 25.5V or higher during Cockpit Preparation? (2 reasons)

A

1) 25.5V is the minimum charge required for APU FIRE TEST / APU START.
2) A voltage at or below 25.5V may result in the discharge of the APU FIRE extinguisher bottle.

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6
Q

What does a TR do and how many are there?

A

Convers AC to DC
3 (TR 1, TR 2, ESS TR)

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7
Q

What is a SI and what does it do?

A

A Static Inverter and it converts DC to AC

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8
Q

What type of electricity do the Generators produce?

A

AC

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9
Q

What type of electricity do the batteries produce?

A

DC

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10
Q

What is the IDG and how does it work?

A

Integrated Drive Generator. It regulates the rotational energy of the engine. It is connected by a shaft from the Accessory Gear Box to the Generator. If it is INOP, you loose the Generator

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11
Q

How many kVa do the Generators produce?

A

90kVa, enough to run the whole plane.

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12
Q

What does the Accessory Gearbox do?

A

It takes the rotational energy of the engine and slows it down for the engine driven accessories e.g. IDGs, HYD ENG pumps.

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13
Q

Why is there no IDG on the APU?

A

Because the N% is constant, it is a fixes value.

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14
Q

In a normal configuration, with both engines running, how is each bus powered?

A

GEN 1 - AC BUS 1 - TR 1 - DC BUS 1 - DC ESS BUS - DC BAT BUS

GEN 2 - AC BUS 2 - TR 2 - DC BUS 2

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15
Q

What is the role of the BUS TIE?

A

The BUS TIE connects both sides of the electrical system together. When it is turned off, the sides are isolated from each other.

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16
Q

When GEN 1 fails, what happens and how is each bus supplied?

A

GEN 2 - AC BUS 2 - TR 2 - DC BUS 2

GEN 2 - AC BUS 1 - AC ESS BUS and TR 1 - DC BUS 1 - DC ESS BUS - DC BAT BUS