曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

A - As a regulating valve.
B - As an ON/OFF valve.
C - A and B.
How does the APIC APU Bleed valve operate ?
A - Pneumatically.
B - Fuel operated
TMUPNEC01 LEVEL 3
EFFECTIVITY 36-12-00 Page 4
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 28
ALL
36 - PNEUMATIC
36-11-34 BMC INTERFACES
CONTENTS:
Inputs
Outputs
TMUPNEV02 LEVEL 3
EFFECTIVITY 36-11-34 Page 1
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 29
ALL
BMC INTERFACES
INPUTS
Each Bleed Monitoring Computer has three types of
inputs:
- DIGITAL INPUTS via ARINC 429 buses, from
opposite BMC, corresponding EIU and CFDIU.
- ANALOG INPUTS from the bleed sensors.
- DISCRETE INPUTS from valve position switches,
BMC and overhead panel.
28 Volts Direct Current power is supplied for
energization of the Bleed Pressure Regulated Valve
Control Solenoid (CTS).
TMUPNEV02-T01 LEVEL 3
EFFECTIVITY 36-11-34 Page 2
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 30
ALL
TMUPNEV02-P01 LEVEL 3
BMC INTERFACES(INPUTS)
EFFECTIVITY 36-11-34 Page 3
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 31
ALL
BMC INTERFACES
OUTPUTS
Each Bleed Monitoring Computer has two types of
outputs:
- DIGITAL OUTPUTS via ARINC 429 buses to the
SDACs (for ECAM warnings and indications), the
CFDIUs (for maintenance purposes), and the
opposite BMC (for bleed monitoring purposes).
- DISCRETE OUTPUTS to APU Electronic Control Box
for APU availability, to overhead panel for
bleed faults, to Cross Bleed Valve, CTS and
Zone Controller.
NOTE: In case of BMC failure, the monitoring of main
parameters (HPV and PRV, Heat Exchanger Outlet
Temperature Sensor, Pr) is kept, but the
automatic control of the PRV is lost.
TMUPNEV02-T02 LEVEL 3
EFFECTIVITY 36-11-34 Page 4
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 32
ALL
BMC INTERFACES(OUTPUTS)
TMUPNEV02-P02 LEVEL 3
EFFECTIVITY 36-11-34 Page 5
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 33
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMUPNEV02 LEVEL 3
EFFECTIVITY 36-11-34 Page 6
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 34
ALL
36 - LEAK DETECTION
36-22-00 LEAK DETECTION
CONTENTS:
Routing
Warning Logic
Fault Logic
Leak Consequence
Self Examination
TMUPNED01 LEVEL 3
EFFECTIVITY 36-22-00 Page 1
Nov 30/95
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 35
ALL
LEAK DETECTION
ROUTING
The leak detection system is used to detect leaks in
the vicinity of the packs, wings, pylons and APU hot
air ducts.
Each wing is monitored by a double loop.
The pylon and APU hot air ducts are monitored by a
single loop.
A continuous monitoring system detects ambient
overheat in the vicinity of the hot air ducts.
Protected areas:
Double loop for:
- RH wing and pack 2
- LH wing, pack 1 and mid fuselage APU duct.
Single loop for:
- LH and RH pylons
- Aft fuselage APU duct
NOTE: Each loop consists of sensing elements connected
in series.
TMUPNED01-T01 LEVEL 3
EFFECTIVITY 36-22-00 Page 2
Nov 30/95
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 36
ALL
LEAK DETECTION - ROUTING
TMUPNED01-P01 LEVEL 3
EFFECTIVITY 36-22-00 Page 3
Nov 30/95
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 37
ALL
LEAK DETECTION
WARNING LOGIC
Both Bleed Monitoring Computers receive signals from
the leak detection loops.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：ATA 36 PNEUMATIC(6)