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[24电源] 飞机通外电时备用液压为什么会运转4秒钟

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TAECO实名认证

发表于 2018-8-14 20:53:25 | 显示全部楼层 |阅读模式
大家好,刚接触B737NG的飞机,今天看了飞机接通外接电源的手册,发现手册里有段警告的注意事项:WHEN APPLYING 115V AC, 400HZ EXTERNAL OR APU GENERATOR POWER, THE STANDBY HYDRAULIC PUMP CAN OPERATE FOR APPROX 4  SECONDS AND MAY MOVE THE RUDDER AND THRUST REVERSERS. TO PREVENT POSSIBLE INJURY, MAKE SURE THE RUDDER AND THRUST REVERSERS ARE CLEAR OF PERSONNEL BEFORE APPLYING POWER.现在想请教一下大伙,B737NG通外电为什么备用液压会运转4秒钟?这个实际操作中有没有很大危险性,rudder会突然偏摆很厉害吗?

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西安航空学院

发表于 2018-8-15 23:10:08 | 显示全部楼层
好像跟飞机构型有关吧!
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发表于 2018-8-16 02:00:51 | 显示全部楼层
也有同样的问题
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发表于 2018-8-16 21:06:44 | 显示全部楼层
你可以去看下备用液压的自动工作条件,飞机刚上电PSEU会自测试,如果构型符合自动工作条件,就会工作
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 楼主| 发表于 2018-8-16 21:26:49 | 显示全部楼层
一叶知厦 发表于 2018-8-16 21:06
你可以去看下备用液压的自动工作条件,飞机刚上电PSEU会自测试,如果构型符合自动工作条件,就会工作
...

是有可能,可能会有短暂的air mode状态
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东航中国民航大学

发表于 2018-8-18 11:32:04 | 显示全部楼层
737NG-FTD-29-05001

Momentary Operation of Standby Hydraulic Pump When Electrical Ground Power is Applied

Description   
A number of operators have reported that the Standby hydraulic pump operates for several seconds following application of external electrical power. This is a normal system response and not a cause for concern.

However, operators should take note of the warning in AMM TASK 24-22-00-860-813 related to this issue.  

Background   
The phenomenon is related to the auto-standby system, which can be seen in System Schematic Manual (SSM) 27-23-11 and 29-22-11 Flagnote 1. Auto-standby turns on the Standby hydraulic pump and opens the Standby rudder shutoff valve under the following condition:

Flaps "NOT UP" switch actuated
--AND--
MLG wheel speed > 60KT ---OR--- Air-ground in AIR mode
--AND--
Either /A/ or /B/ flight control hydraulic pressure < 1200 PSI --OR-- Yaw damper coupler turns on System A Flight Control Low Pressure Light L3 (airplanes with rudder pressure reducers)

On airplanes with the Rudder System Enhancement Program (RSEP) incorporated, the rudder Force Fight Monitor (FFM) can also turn on the Standby pump if a rudder force fight (greater than 3600 psi difference in delta-P between A and B sides of Rudder PCU) is detected.  

Status   
The Standby pump may run momentarily when hydraulic system pressures (S142 & S141) are less than 1200 psi and the flaps are extended (flaps switch S1051 is "NOT UP"). The momentary running occurs when external ground power is applied.

If the Reverse Thrust Lever is not STOWED or if the Speed Brake Lever is not DOWN, then upon application of electrical power to the airplane, relay R591 (AIR/GND) moves to the GROUND position. As part of a self-test, the auto speed brake module (ASM)(M980) then closes an internal wheel speed relay for four seconds, connecting pins 47 and 49 in connector D2586A. This provides a "WHEEL SPEED GREATER THAN 60 KT" signal to the auto-standby system, and the Standby pump comes on. After 4 seconds, the ASM wheel speed relay opens, the "WHEEL SPEED GREATER THAN 60 KT" input goes away, and the Standby pump turns off. The circuits may be seen in SSM 27-23-11 and 27-62-11.

This is all normal operation, and is not cause for concern.  

Interim Action   
No interim action; this article published for information only.  

Final Action   
A warning was added to AMM TASK 24-22-00-860-813, Supply External Power, to warn maintenance personnel of the possibility of this happening. The warning reads:

WARNING: WHEN APPLYING 115V AC, 400HZ EXTERNAL OR APU GENERATOR POWER, THE STANDBY HYDRAULIC PUMP CAN OPERATE FOR APPROX 4 SECONDS AND MAY MOVE THE RUDDER AND THRUST REVERSERS. TO PREVENT POSSIBLE INJURY, MAKE SURE THE RUDDER AND THRUST REVERSERS ARE CLEAR OF PERSONNEL BEFORE APPLYING POWER.  

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 楼主| 发表于 2018-9-13 20:53:22 | 显示全部楼层
codyplane 发表于 2018-8-18 11:32
737NG-FTD-29-05001

Momentary Operation of Standby Hydraulic Pump When Electrical Ground Power is A ...

真是太感谢了,这个解释非常详细
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