Airbus A330 Flight Deck and Systems Briefing for Pilots

Page 33

A330 electrical system Distribution - normal configuration AC distribution network

ELEC DC

• In normal configuration, each engine-driven generator supplies its associated AC BUS. • The AC ESS BUS is normally supplied from AC BUS 1.

DC BAT BAT 1 25 V 5A

DC 1

DC APU BAT 2 26 V 0A

DC ESS

APU BAT 25 V 5A DC 2

STAT INV

DC distribution network • In normal configuration, normal DC systems are split into two networks : DC BUS 1 in parallel with DC BAT BUS and DC BUS 2.

TR 1 28 V 50 A

ESS TR 28 V 50 A

TR 2 28 V 50 A

APU TR 25 V 100 A

AC1

AC1

AC2

AC2

• Each DC network is supplied by its own TR. • More specifically, ESS TR systematically feeds DC ESS BUS, which allows a better segregation between DC 1 and DC 2. • Two batteries are connected to the DC BAT BUS via the Battery Charge Limiter (BCL). • Each battery has its own HOT BUS bar (engine/APU fire squib, ADIRS, CIDS, PRIM and SEC computers, slide warnings, parking brake, etc). • The third battery is dedicated to APU starting.

STL 472.755/92 Issue 4

3.3


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Airbus A330 Flight Deck and Systems Briefing for Pilots by SkyhawkSS - Issuu