曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
NORMAL CONFIGURATION
Normal flight Configuration.
TMUELE104-T04 LEVEL 1
EFFECTIVITY 24-00-00 Page 8
Sep 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 16
ALL
ELECTRICAL SYSTEM DIAGRAM DESCRIPTION - MAIN ELEC CONFIGURATIONS (NORMAL CONFIGURATION)
TMUELE104-P04 LEVEL 1
EFFECTIVITY 24-00-00 Page 9
Sep 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 17
ALL
MAIN ELEC CONFIGURATIONS (CONT’D)
GROUND SERVICES
For ground service only, the AC and the DC ground
flight buses can be supplied independently from the
normal circuit.
TMUELE104-T05 LEVEL 1
EFFECTIVITY 24-00-00 Page 10
Sep 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 18
ALL
ELECTRICAL SYSTEM DIAGRAM DESCRIPTION - MAIN ELEC CONFIGURATIONS (GROUND SERVICES)
TMUELE104-P05 LEVEL 1
EFFECTIVITY 24-00-00 Page 11
Sep 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 19
ALL
MAIN ELEC CONFIGURATIONS (CONT’D)
LOSS OF MAIN GENERATORS
In flight, in case of total loss of all the main
generators, and before the emergency generator
connection, batteries 1 and 2 supply the AC and DC ESS
buses. This is a transient configuration, during Ram
Air Turbine extension or no emergency generator
available.
When its parameters are correct, the emergency
generator comes on line and supplies the AC and DC ESS
buses.
When the speed is lower than 100 knots, the emergency
generator is deactivated. The batteries supply the
A.C. and D.C. ESS buses. The D.C. battery bus is
recovered.
When the speed drops below 50 knots, the A.C. essential
bus disconnects from the static inverter.
TMUELE104-T06 LEVEL 1
EFFECTIVITY 24-00-00 Page 12
Sep 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 20
ALL
ELECTRICAL SYSTEM DIAGRAM DESCRIPTION - MAIN ELEC CONFIGURATIONS (LOSS OF MAIN GENERATORS)
TMUELE104-P06 LEVEL 1
EFFECTIVITY 24-00-00 Page 13
Sep 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 21
ALL
SELF EXAMINATION
The static inverter operates:
A - permanently
B - when on batteries only
C - when one engine generator fails
AC ESS BUS is normally supplied by the:
A - AC BUS 1
B - AC BUS 2
C - Emergency Generator
DC BAT BUS can be supplied by the:
A - DC BUS 1 or batteries
B - DC BUS 1, DC BUS 2 or batteries
C - DC BUS 2 or batteries
AC transfers enable AC buses:
A - to be connected in parallel
B - to be supplied by any generator or
external power
C - to be supplied by APU GEN or EXT PWR only
TMUELE104 LEVEL 1
EFFECTIVITY 24-00-00 Page 14
Sep 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 22
ALL
24 - ELECTRICAL POWER
24-00-00 ELECTRICAL SYSTEM MAIN CONTROL
PANEL PRESENTATION
CONTENTS:
IDG 1/2 Pushbuttons
GEN 1/2 Pushbuttons
APU GEN Pushbutton
EXT PWR Pushbutton
BUS TIE Pushbutton
AC ESS FEED Pushbutton
BAT 1/2 Pushbuttons
GALY & CAB Pushbutton
MAINT BUS Switch
TMUELE202 LEVEL 1
EFFECTIVITY 24-00-00 Page 1
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 23
ALL
ELECTRICAL SYSTEM MAIN CONTROL PANEL PRESENTATION
IDG 1/2 PUSHBUTTONS
When the IDG pushbutton is momentarily pressed, the
Integrated Drive Generator is disconnected from its
drive shaft.
It can only be reconnected by maintenance.
GEN 1/2 PUSHBUTTONS
In normal operation:
the generator is energized and the line contactor
closes, when electrical parameters are correct.
When OFF:
the generator is de-energized and the line contactor
opens.
APU GEN PUSHBUTTON
In normal operation:
the APU generator is energized and the line contactor
closes, if electrical parameters are correct and if
the APU generator has priority.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
ATA 24 ELECTRICAL POWER(4)
