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70.90 CONTROLS AND INDICATORS
- PEDESTAL
- OVERHEAD PANEL
- MAINTENANCE PANEL
- ECAM
- WARNINGS AND CAUTIONS
- MEMO DISPLAY
70.98 ELECTRICAL SUPPLY
.1
.4
.4
.5
13
15
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┃J -~ A318 ┃POWER PLANT ┃1.70.10 P 1 ┃
┃ .-,,.8, ,, ~e~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lli,~ A320 ┃ ┃SEQ 120 I ┃J REV 28 ┃
┃ A~7-~'M" A321 ┃ ENGINE ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━━┻━━━━━┛
R The CFM 56-5B engine is a high bypass ratio turbofan
Low-pressure (LP) compressor/turbine
The low-speed rotor (N1) consists of a front fan (single-stage) and a four-stage LP
compressor connected to a four-stage LP turbine.
High-pressure (HP) compressor/turbine
The high-speed rotor (N2) consists of a nine-stage HP compressor connected to a
single-stage HP turbine.
Combustion chamber
The annular combustion chamber is fitted with 40 fuel nozzles and 2 igniters
Accessory gearbox
The accessory gearbox, located at the bottom of the fan case, receives torque from
horizontal HP rotor drive shaft and drives gearbox mounted accessories.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━━━┓
┃J -~ A318 ┃POWER PLANT ┃1.70.20 P 1 ┃
┃ .*,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lli,~ A320 ┃ ┃SEQ 005 J ┃J REV 23 ┃
┃ A~7-~'M" A321 ┃ FADEC ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━━┻━━━━━┛
Each powerplant has a FADEC (Full Authority Digital Engine Control) system.
FADEC, also called the Electronic Control Unit (ECU), is a digital control system that
performs complete engine management.
FADEC has two-channel redundancy, with one channel active and one in standby.
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual5(152)
