• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-24 11:22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

Cables connect to the forward end of the stabilizer structure and mechanically transmit stabilizer movement to the stabilizer position modules.
The STCMs are immediately aft of the pressure bulkhead near the ceiling of the stabilizer compartment.
EFFECTIVITY BEJ ALL  27-41-00 
Page 10 
D633W101-BEJ  Sep 05/2002 

 


HORIZONTAL STABLIZER CONTROL -COMPONENT LOCATIONS -TAIL

EFFECTIVITY BEJ ALL  27-41-00 
Page 11 
D633W101-BEJ  Sep 05/2002 

 

HORIZONTAL STABILIZER CONTROL -ANALOG AND DISCRETE INTERFACES

General

All the analog interfaces for the stabilizer pitch control within the PFCS go through the ACEs. Each ACE has interfaces with these components:
*
Alternate pitch trim lever switches

*
Control wheel pitch trim switches

*
Stabilizer position indicators

*
Auto shutdown relays

*
Stabilizer trim control modules (STCM)

*
Stabilizer position modules.


Alternate Pitch Trim Lever Switches

The alternate pitch trim lever switches on the alternate pitch trim forward quadrants send discrete signals to the AIMS. The signals represent pitch up or pitch down commands.
Control Wheel Pitch Trim Switch Modules

The pitch trim switches on each control wheel send pitch up, pitch down or off discrete signals to the ACEs.
Stabilizer Position Indicators

The two stabilizer position indicators receive analog signals from the AIMS that show stabilizer position.
Stabilizer Cutout Switches
Each stabilizer cutout switch controls a motor-operated shutoff valve in an STCM.
Auto Shutdown Relays
The ACEs can send discrete signals to the auto shutdown relays to close the motor-operated shutoff valves in the STCMs.
Stabilizer Trim Control Modules
Each of the two STCMs receive discrete signals from the ACEs and the auto shutdown relays. The discrete signals are for the:
*
Control and arm trim solenoids

*
Rate control solenoids

*
Motor operated shutoff valves.


The pressure switches send discrete signals back to the ACEs.
Stabilizer Position Module
Three stabilizer position modules contain a position RVDT and limit switches.
The RVDTs send an analog signal to the ACEs that represents the stabilizer position.
The ACEs send discrete signals through the limit switches to the STCMs.

EFFECTIVITY BEJ ALL  27-41-00 
Page 12 
D633W101-BEJ  Sep 05/2002 

 


HORIZONTAL STABILIZER CONTROL -ANALOG AND DISCRETE INTERFACES

EFFECTIVITY BEJ ALL  27-41-00 
Page 13 
D633W101-BEJ  Sep 05/2002 

 

HORIZONTAL STABILIZER CONTROL -PITCH TRIM SWITCHES

Purpose

The pitch trim switches electrically command stabilizer movement.
Physical Description

Each switch has three positions: pitch up, pitch down, and off. It is spring loaded to the off position.
Location

Two pitch trim switch pairs are on the outboard side of each control column.
Functional Description

One switch of the pair sends an arm signal and the other sends a control signal to the ACEs.
The pilot moves both switches in the up position to command nose down trim. In the down position, the switches command nose up trim.
EFFECTIVITY BEJ ALL  27-41-00 
Page 14 
D633W101-BEJ  Sep 05/2002 

 


HORIZONTAL STABILIZER CONTROL -PITCH TRIM SWITCHES

EFFECTIVITY BEJ ALL  27-41-00 
Page 15 
D633W101-BEJ  Sep 05/2002 

 


777 AIRCRAFT MAINTENANCE MANUAL


THIS PAGE IS INTENTIONALLY LEFT BLANK

27-41-00


Page 16 D633W101-BEJ Sep 05/2002


HORIZONTAL STABILIZER CONTROL -ALTERNATE PITCH TRIM LEVERS AND FORWARD QUADRANT ASSEMBLY

Purpose

The alternate pitch trim levers give the pilots mechanical control of pitch trim. The forward quadrant assembly transmits the movement from the levers to the control cables.
Physical Description

Two alternate pitch trim levers supply arm and control mechanical commands to the STCMs. The two levers are independent of each other. Springs move the levers back to the center position. Each lever connects by rod to its own forward quadrant.
Each quadrant has three alternate pitch trim lever switches. Cams on the quadrants operate the switches. A pair of cables connects each quadrant to the aft control module in the stabilizer compartment.
Location

The two alternate pitch trim levers are on the captain’s side of the P10 control stand. The forward quadrant assembly is just below the levers in the aisle stand.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:777 AMM 飞机维护手册 飞行操纵 Flight Controls 2(16)