BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
SHT 1 A SECONDARY SHUTOFF SOLENOID FUEL METERING UNIT
HIGH PRESSURE RELIEF VALVE METERING VALVE MINIMUM PRESSURE VALVE
SHT 1 B
SHT 1 C STEPPER MOTOR AND RESOLVER CONTROLLER TO APU FROM APU CONTROLLER
VALVE REGULATING PRESSURE SERVO REGULATOR SUPPLY
SOLENOID SHUTOFF PRIMARY FUEL FILTER CONTROL DIVERTER VALVE ACTUATOR AND PRESSURE TO IGV SERVO REGULATED
Figure 2 (Sheet 2) APU Fuel System Schematic
M32451
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
49-31-00
ALL ú ú 03 Page 6 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
A. APU fuel flow is controlled by the APU controller in conjunction with the fuel metering unit (FMU). Pressurized fuel from the fuel pump flows through an adapter plate to the FMU. The APU controller provides control signals to the stepper motor and metering valve, in the FMU, to regulate fuel flow in response to load demands. Metered fuel is supplied to the combustion chamber through a fuel flow divider and dump valve together with independent distribution manifolds radially arranged around the gas generator case. The flow divider distributes the flow between primary and secondary fuel nozzles projected into the combustion chamber. Any residual fuel after shutdown is drained by drain valves located at the bottom of the gas generator case. Pressurized fuel is supplied to the inlet guide vane (IGV) actuator control and the diverter valve control to be used as hydraulic fluid. Fuel through the fuel cooled oil cooler (FCOC) maintains oil temperature in the lubrication system feed line within operating limits by heat exchange with high pressure fuel.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
49-31-00
ALL ú ú 01 Page 7 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL
APU ENGINE FUEL SYSTEM
COMPONENT 102 SHT FIG. QTY ACCESS/AREA AMM REFERENCE
ADAPTER - FUEL METERING 1 317AL, 318AR/310 (APU COMPARTMENT) 49-31-02
ADAPTER - NOZZLE 14 317AL, 318AR/310 (APU COMPARTMENT) 49-31-04
FILTER - FUEL PUMP OUTLET 1 317AL, 318AR/310 (APU COMPARTMENT) 49-31-00
INDICATOR - FUEL FILTER BYPASS 1 317AL, 318AR/310 (APU COMPARTMENT) 49-31-05
MANIFOLD - PRIMARY FUEL 1 317AL, 318AR/310 (APU COMPARTMENT) 49-31-04
MANIFOLD - SECONDARY FUEL 1 317AL, 318AR/310 (APU COMPARTMENT) 49-31-04
PLUG - FUEL PUMP COVER 1 317AL, 318AR/310 (APU COMPARTMENT) 49-31-00
PUMP- FUEL 1 317AL, 318AR/310 (APU COMPARTMENT) 49-31-03
SCREEN - FUEL PUMP INLET 1 317AL, 318AR/310 (APU COMPARTMENT) 49-31-00
UNIT - FUEL METERING, M3374 1 317AL, 318AR/310 (APU COMPARTMENT) 49-31-01
VALVE - FLOW DIVIDER AND DUMP 1 317AL, 318AR/310 (APU COMPARTMENT) 49-31-00
APU Engine Fuel System - Component Index
Figure 101
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
49-31-00
ALL ú ú 01 Page 101 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
FAULT ISOLATION/MAINT MANUAL
FUEL COOLED
317AL, 318AR FWD OIL COOLER
APU COMPT (REF)
SEE A
FUEL PUMP,
FUEL METERING UNIT,
FUEL METERING ADAPTER
FUEL MANIFOLDS,
FUEL NOZZLES, SEE B
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 機載輔助動力 2(30)
