Main electrical Components Flashcards

1
Q

Electrical components

A

Two engine driven generators
Two back ups
APU
AC needs two sources for normal ops

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2
Q

Electrical load management system

A

Comes into play when only one source available

Automatically shuts down low priority items, such as the galleys

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3
Q

Schematic

A

Left and right buses distribute AC power to all systems

Bus tie and and two isolation relays ensure both main buses remain powered at all times

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4
Q

All electrical power switched off

A

Main battery still continues to power a few important items through the hot battery bus even with battery switch off
Fire eq bottles
APU eq bottles
And the ADIRU as long as it is switched on

When AC shutdown main battery if on will power
Standby power systems
Captains display
Left AIMS

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5
Q

Primary external power

A

If Available light on this indicates primary external power is connected to the airplane and is useable quality

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6
Q

Secondary external power

A

Gives full electrical load capacity for most ground situations

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7
Q

Both primary and secondary power on

A

Primary powers right main bus

Secondary powers left main bus

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8
Q

APU POWER WHEN ON

A

APU powers left main bus and secondary light will annunciate available

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9
Q

APU ON and primary and secondary off

A

APU powers both buses

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10
Q

Each main engine generator

A

Housed in a single case
Share common oil supply
Combined unit called a IDG
Integrated drive generator

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11
Q

IDG

A

controlled by a general control unit (see schematic)

Which provides automatic control functions and system protection

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12
Q

Generator off switches

A

Breaker open and on means armed if off light is visible

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13
Q

Starting engine

A

IDG begins to rotate at operating speed
Breaker closes
Generator off and drive lights extinguish
This generator will now power its applicable bus (right engine start=right bus)

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14
Q

When generator comes on line

A

Primary and secondary external power automatically disconnect from the main buses and the applicable side generator will power both buses
After a few seconds APU will power left main bus until the left engine is started

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15
Q

Each main AC bus powers

A

One utility bus (see schematic)

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16
Q

Priority power order

A

Keep buses powered

  1. Associated engine generator
  2. APU Generator
  3. Opposite engine generator
17
Q

ELMS if only one power source

A

First galleys
Galley chiller
Then left and right utility buses

18
Q

Shut down of left engine example

A
Fuel control switch moved to cutoff
The IDG synchronises with the bus tie
The left tie breaker closes
Engine generator breaker opens
APU powers that bus