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Buses

Also from: Electrical Buses


Can be supplied by the engine driven generators (GEN 1 and GEN 2), APU generator (APU GEN), external A or B (EXT A and EXT B), and emergency generator (EMER GEN) powered by the green hydraulic system.


Both EXT A and EXT B are required to power all buses and galleys.


The emergency generator is in the main wheel well. If required, it takes a few seconds to come online, during which time the batteries power the buses.


AC 1 → AC ESS (via a contactor)

AC 1 → TR 1 → DC 1, DC BAT

AC 2 → TR 2 → DC 2

AC 1 → ESS TR → DC ESS


AC 1

Supplies AC ESS, TR 1, DC 1, DC BAT. If AC 1 fails, there is an automatic reconfiguration leading to AC 2 supplying AC ESS.


AC 2

Supplies TR 2, DC 2, APU TR, DC APU.


AC ESS

Supplies ESS TR, DC ESS.


DC BAT

Charges the batteries. Can supply DC ESS in a failure of AC ESS.


DC APU

Charges the APU battery which is dedicated to starting the APU.


Other buses

  • AC ESS SHED, DC ESS SHED: shed when insufficient power exists
  • AC LAND REC, DC LAND REC: buses that power systems required for an approach and landing
  • SHED LAND REC: a bus that is shed when the landing recovery buses are energised
  • HOT 1, HOT 2: hot battery buses from battery 1 and 2

ECAM

/wiki/wikis/a330/bin/elecdcpage.jpg

Figure: ELEC DC ECAM page


/wiki/wikis/a330/bin/elecacpage.jpg

Figure: ELEC AC ECAM page


Controls

AC ESS FEED pb swchanges feed for AC ESS bus from AC 1 to AC 2

Failures

ELEC AC ESS BUS FAULT- FWC 1 is lost
- the E/WD is displayed on the lower ECAM
- to call the ELEC AC page, hold the key down

Categories: Airbus A330 | Electrical System



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