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时间:2011-04-02 15:00来源:蓝天飞行翻译 作者:航空
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GROUND SERVICE
REVERSER REVERSER  EDGE FLAPS
DISCONNECT GROUND SERVICE
SYSTEM ADISCONNECT
PRESSURE MODULESYSTEM BFLIGHT
CONTROLMODULE FLT SPOILERS
SYSTEM A
FLIGHT2 & 7
CONTROL
FLT SPOILERSMODULE
3 & 6

ELEVATORS  ELEVATORSELEVATORRUDDER ANDAILERONS AILERONSAUTOPILOT FEEL YAW DAMPER AUTOPILOT GROUND
SPOILERS
LANDING
GEAR

BRAKES 1 CHECK VALVE LOCATIONS ARE DIFFERENT FOR DIFFERENT AIRPLANE CONFIGURATIONS (AMM 29-22-00/001)
Simplified Hydraulic System Schematic
Figure 2

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F42828
A

737-300/400/500
MAINTENANCE MANUAL

SEE  A  1 
MOUNTING PAD 
CLAMP QAD 
PUMP DEPRESSURIZATION VALVE  CASE DRAIN LINE 
ELECTRICAL CONNECTOR 

PRESSURE LINE 
SUPPLY LINE  FWD 
VICKERS EDP 
1  NO. 1 ENGINE SHOWN NO. 2 ENGINE SIMILAR  A 
Engine-Driven Pump (EDP) Figure 3 

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 4.  Standby Electric Motor-Driven Pump (EMDP) (Fig. 7 and 8)
_________________________________________
 A.  The motor/pump assembly is mounted behind the standby reservoir on the keel beam.
 B.  The standby EMDP supplies a maximum of 3 gpm regulated to a nominal 3000 psi. The pump is a variable delivery, positive displacement pump driven by a 3-phase, 115-volt motor and controlled by 28 volt dc relays (Fig. 8).
 C.  A compensator within the pump reacts to discharge pressures and varies the ratio of fluid delivered to the system to fluid recirculated within the pump. Case drain fluid for cooling and lubrication is discharged to the return line through piston bypass holes.
 5.  Hydraulic Reservoir (Fig. 9)
___________________
 A.  The hydraulic reservoir for each system supplies hydraulic fluid for the flow demands of the user systems. The reservoirs for systems A and B are in the center and right main wheel wells, respectively. The standby system reservoir is mounted on the keel beam between the wheel wells and is attached by a balance line to the system B reservoir. The balance line permits filling and pressurizing the standby and system B reservoirs.

YOKE ASSEMBLY

INPUT SHAFT
NO. 1 ENG PUMP
DEPRESS VALVE

28V DC BUS NO. 2

ENG 1
P6


NO. 1 EDP SHOWN NO. 2 SIMILAR
Engine Driven Pump (EDP) Control
1 Figure 4
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500MAINTENANCE MANUAL
SYSTEM A EMDP SEE A
FWD 
SYSTEM B EMDP 
SEE  A 
KEEL BEAM 
(REF) 
WHEEL WELL 
ELECTRICAL 
CONNECTOR 
ABEX EMDP 

GROUNDING STRAP CASE DRAIN LINE
(TYPICAL) PRESSURE LINEACOUSTIC FILTER
SUPPLY LINE 1
SYSTEM B EMDP SHOWN
A1
SYSTEM A EMDP SIMILAR
Hydraulic Systems A and B Electric Motor-Driven Pump (EMDP) Figure 5
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 ALL  ú ú 02 Page 6 ú Feb 25/85
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

(SYSTEM B EQUIVALENT)
Hydraulic Systems A and B Electric Motor-Driven Pump (EMDP) Control
 
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