Wikiposts
Search
Tech Log The very best in practical technical discussion on the web

737 APU ?

Thread Tools
 
Search this Thread
 
Old 9th Mar 2001, 02:40
  #1 (permalink)  
Barbers Pole
Guest
 
Posts: n/a
Question 737 APU ?

Can some one explain to me why, if you turn the battery switch off on the ground it shutdowns the APU but if you do the same inflight it dosn't?

Many thanks
 
Old 9th Mar 2001, 02:51
  #2 (permalink)  
spannerhead
Guest
 
Posts: n/a
Post

You switch the battery off in flight..Why?
 
Old 9th Mar 2001, 03:26
  #3 (permalink)  
Barbers Pole
Guest
 
Posts: n/a
Post

We don't, it's a technical question on the system I'm asking!

PS, you might consider it if the battery was your only power source left, to consevre it.
Bad day at the office!
 
Old 9th Mar 2001, 11:53
  #4 (permalink)  
HighSpeed
Guest
 
Posts: n/a
Post

Barbers Pole,

Thats because fire detection on the B737 comes from the battery bus thus switching off the battery switch will disable the fire detection therefore the APU auto shuts down.

HS
 
Old 9th Mar 2001, 14:47
  #5 (permalink)  
cossack
Guest
 
Posts: n/a
Question

As a slight aside:
Would an unserviceable APU require fire service attendance inbound on an A321 if this unseviceability was brought about by a battery problem. Said aircraft was towed off stand with no lights later.
BTW fire cover was asked for by handling agent prior to landing and ATC found out from fire service as aircraft was approaching stand!
 
Old 10th Mar 2001, 02:23
  #6 (permalink)  
Barbers Pole
Guest
 
Posts: n/a
Thumbs up

Thanks HS

So inflight if you turned the battery off, the bat bus would still be powered via the No.2 gen/TR3, therefore it wouldn't cause a APU shutdown? As you would still have fire detection. Logic would have to work via a air/ground sensor??
 
Old 10th Mar 2001, 12:25
  #7 (permalink)  
QAVION
Guest
 
Posts: n/a
Post

Looking at the Boeing electrical schematics for the 737 (Ref 49-62-11), I see that there are several 28v dc inputs going into the APU controller. If the APU fire handle is pulled, a 28vdc signal is sent to the APUC. If a fire is detected, a 28vdc signal is sent to the APUC. If the APU is switched off, a 28vdc signal is sent to the APUC. If the battery switch is switched off, 28vdc is sent to the APUC. Presumably all these 28vdc signals are shutdown commands.

In the latter example, the signal goes through an air/ground relay ("R38" on the particular schematic I have). The contacts of the relay are opened in the air, so the "battery off" shutdown signal cannot get to the APU.

This explains the how. I'm still not sure of the why. All that battery circuit seems to be doing is providing you with less ways to switch off the APU in the air.

Rgds.
Q.
 
Old 13th Mar 2001, 22:27
  #8 (permalink)  
Canuck_AV8R
Guest
 
Posts: n/a
Lightbulb

Because Boeing wired it that way

But seriously:

The APU on the -200 shuts down on the ground when the battery is shut off because you have lost APU fire DETECTION capability which comes from the Battery Bus. The Battery Bus is powered inflight by TR3.

Why you would turn off the battery in flight I am not sure but on e situation that comes to mind would be a suspected overcharging of the battery or a looming thermal runaway.
 

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are Off
Refbacks are Off



Contact Us - Archive - Advertising - Cookie Policy - Privacy Statement - Terms of Service

Copyright © 2024 MH Sub I, LLC dba Internet Brands. All rights reserved. Use of this site indicates your consent to the Terms of Use.