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时间:2011-04-20 07:56来源:蓝天飞行翻译 作者:航空
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

 (f)  
Reservoirs can be pressure filled or manually filled. A hand pump and reservoir fill valve (selector) allow filling of the selected reservoir.


 G. Left and Right Hydraulic System Components (Fig. 6)
 (1)  
The left and right hydraulic systems each have one engine driven pump (EDP) and one alternating current motor pump (ACMP). The EDP is attached to the engine gearbox on the under side of the engine. The pump is a line replaceable unit (LRU) with a rated output of 37 gpm.

 (2)  
The ACMPs are in the left and right mainwheel forward fairings. The associated filters, valves, and reservoir are also located in that area. The electric motor is powered by 115 vac using 45 amps at rated output. The pump is a LRU with a rated hydraulic output of 7 gpm.


 H. Center Hydraulic Systems Components (Fig. 7)
 (1)  The two ACMP primary sources are on the left side of the airplane in the fairing aft of the main wheel well. They are mounted on shelves on the keel structure. The associated filters, valves, and reservoir are also in that area. The center ACMPs are identical to the left and right ACMPs.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL

SYSTEM R RESERVOIR
SYSTEM L  SYSTEM R
RETURN PRESSURIZATION
SYSTEM C RESERVOIRPRESSURIZATIONRESERVOIR SYSTEM LPRESSURIZATION RETURN
SYSTEM
C
RETURN

HEAT
HEAT
HEAT
EXCHANGER

TO PTU
EXCHANGER
EXCHANGER EDP ACMP EDP
ACMP ACMP ACMP RAT
L L RR
RESERVOIRFILL SELVALVE
12
ENGINE
ALTERNATING
DRIVEN

CURRENT RAM AIRMOTOR PUMP
PUMP TURBINEDIVEN RAT HAND PUMP
PUMP RETRACTION SPOILER
PCAs (12)
AILERONS
PCAs (4) ELEVATORS
PCAs (6) THRUST
REVERSERS RUDDERPCAs (3)
ALTERNATE BRAKES
STAB TRIM CONTMODULES (2)
NORMAL BRAKES
LEADING EDGE
TRAILING EDGESLAT PDUs (2)
AUTOPILOTSERVOS (9)FROM SYS L RESERVOIR
FLAP PDU (1)
YAW DAMPER
ACTUATION

LANDING GEARSERVOS (2)
POWER TRANSFER
UNIT PUMP/
MOTOR

NOSE GEAR
STEERING
Hydraulic System - Simplified
Figure 5

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL

PRESSURE(OUT)
SUPPLY(IN)
PUMP
SEE ACASEDRAINSEE C (OUT)
SEE B SEE E UP FWD MOTOR
ENGINEB
SUPPLY(IN)
PRESSURE(OUT)
POWER TRANSFER UNITA
ELECTRICALCONNECTOR
INLET
DEPRESSURIZATION
SUPPLY
SOLONOID
PORT ELECTRICRETURNMOTOR
FILTER
MODULE

EMHP
UP FILTERMODULE
FWD PRESSURE(OUT)
INBD
CASEDRAINELECTRIC MOTOR
FWD
(OUT) HYDRAULIC PUMP
OUTLETPRESSUREPORTSUPPLY
(IN)
SEE D CASE
PUMP
DRAIN
LEFT MAIN WHEEL WELL (RIGHT SIDE SIMILAR)
ALTERNATING CURRENT MOTOR PUMP PORT ENGINE DRIVEN PUMPC
E Left and Right Hydraulic System ComponentsFigure 6
D
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL

RESERVOIR ACMP (2)
DEPLOY/STOWACTUATOR
FILTERMODULE STRUTHOUSING DOOR
FILTER GROUND FLUIDMODULE SERVICE SERVICE CONNECTION
RETURN TURBINE PUMP
LEFT WHEEL WELL FAIRINGRAM AIR TURBINE (DEPLOYED)
Center Hydraulic System Components
Figure 7

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