Matronics Email Lists Forum Index Matronics Email Lists
Web Forum Interface to the Matronics Email Lists
 
 Get Email Distribution Too!Get Email Distribution Too!    FAQFAQ   SearchSearch   MemberlistMemberlist   UsergroupsUsergroups   RegisterRegister 
 ProfileProfile   Log in to check your private messagesLog in to check your private messages   Log inLog in 

Dancing ammeter and alternator drop outs

 
Post new topic   Reply to topic    Matronics Email Lists Forum Index -> AeroElectric-List
View previous topic :: View next topic  
Author Message
thomas.n.gautier(at)jpl.n
Guest





PostPosted: Fri Dec 05, 2008 2:12 pm    Post subject: Dancing ammeter and alternator drop outs Reply with quote

Bob,

Our club Arrow IV has recently experienced a spate of alternator and
related electrical system maintenance issues. The symptoms that the club
members complained about centered on alternator drop outs which could often,
if not always, be cured by turning the alternator off and then back on.
There may have been an outright alternator failure of some sort as well. I
haven't followed the maintenance in detail since I haven't, until today,
flown the plane in the last month.

The upshot of all the maintenance is that first the voltage regulator
and then the alternator were replaced. The symptom reported after voltage
regulator replacement but before alternator replacement was that the
alternator was dropping out every 10 minutes in the last half hour of a
cross country trip. I was the first to fly the plane after the alternator
replacement and I found the system to still be misbehaving.

In my flight immediately upon starting the engine and switching on the
alternator the alternator ammeter (a load meter, I think) showed 70 amps,
pretty steady, recharging the battery I presume. Then, in less than a minute
the ammeter began swinging from 30A to 70A 2 or 3 times a second. I've read
your dancing ammeter posts so I assumed this was not particularly
troublesome (except that these swings were larger than I had seen before).
Then, after my first turn around the pattern, I noticed that the alternator
had dropped off line. It came back after cycling the alternator switch,
however the ammeter dancing was now as large as 0A to 70A. This behavior
continued for a couple more turns around the pattern, with full stop
landings, as I watched what was going on. I had to reset the alternator
twice more over the span of 20 minutes.

So, the plane's electrical problems are not solved and I'm trying to
help the owner and his mechanic figure out what is really wrong. I dug some
of your posts about dancing ammeters out of the archive and I'm ready to
show them to the plane's owner. However I'd like to get your opinion as to
whether I'm on the right track. Can the aging wiring problem that causes
dancing ammeters also cause the alternator to frequently drop off line?

Regards,
Nick Gautier


- The Matronics AeroElectric-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

http://www.matronics.com/Navigator?AeroElectric-List
Back to top
nuckolls.bob(at)aeroelect
Guest





PostPosted: Sat Dec 06, 2008 6:48 am    Post subject: Dancing ammeter and alternator drop outs Reply with quote

At 04:11 PM 12/5/2008, you wrote:
Quote:

<thomas.n.gautier(at)jpl.nasa.gov>

Bob,

Our club Arrow IV has recently experienced a spate of alternator and
related electrical system maintenance issues. The symptoms that the club
members complained about centered on alternator drop outs which could often,
if not always, be cured by turning the alternator off and then back on.
There may have been an outright alternator failure of some sort as well. I
haven't followed the maintenance in detail since I haven't, until today,
flown the plane in the last month.

By "drop out" do you mean that the alternator shuts down completely?
Do you get a low voltage warning or does the ammeter go to zero
and stay there?

Quote:
The upshot of all the maintenance is that first the voltage regulator
and then the alternator were replaced. The symptom reported after voltage
regulator replacement but before alternator replacement was that the
alternator was dropping out every 10 minutes in the last half hour of a
cross country trip. I was the first to fly the plane after the alternator
replacement and I found the system to still be misbehaving.

In my flight immediately upon starting the engine and switching on the
alternator the alternator ammeter (a load meter, I think) showed 70 amps,
pretty steady, recharging the battery I presume. Then, in less than a minute
the ammeter began swinging from 30A to 70A 2 or 3 times a second. I've read
your dancing ammeter posts so I assumed this was not particularly
troublesome (except that these swings were larger than I had seen before).
Then, after my first turn around the pattern, I noticed that the alternator
had dropped off line. It came back after cycling the alternator switch,
however the ammeter dancing was now as large as 0A to 70A. This behavior
continued for a couple more turns around the pattern, with full stop
landings, as I watched what was going on. I had to reset the alternator
twice more over the span of 20 minutes.

I'm trying to deduce if you're speaking to an intermittent operation.
A lack of ability for the alternator to deliver any power at all . . . or
an unstable condition where the alternator is always developing some
power but the regulation is unstable.

Quote:
So, the plane's electrical problems are not solved and I'm trying to
help the owner and his mechanic figure out what is really wrong. I dug some
of your posts about dancing ammeters out of the archive and I'm ready to
show them to the plane's owner. However I'd like to get your opinion as to
whether I'm on the right track. Can the aging wiring problem that causes
dancing ammeters also cause the alternator to frequently drop off line?

You use the words "dancing ammeter". Go to

http://www.matronics.com/searching/ws_script.cgi

Search the AeroElectric List archive using search string . . .

dancing & ammeter

You will unearth a lot of conversation about a phenomenon
common to older airplanes where the voltage regulator senses
bus voltage through the same wire that supplies field current.
This sets up the possibility for a "negative resistance" (read
oscillation) of voltage regulator stability that can be
anything from barely noticeable to quite severe.

It has nothing to do with the alternator or the regulator and
everything to do with condition of ALL wires, components and
joints between the bus and the regulator. The 30-year fix is to
replace ALL these components.

If you're describing an oscillating voltage condition, then
the discussions and recommended fixes described in the archives
are the road to Nirvana. If you're describing an intermittent
functionality where the alternator output goes to zero and
stays there for some observable time interval . . . you're
chasing a loose connection.

Bob . . .


- The Matronics AeroElectric-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

http://www.matronics.com/Navigator?AeroElectric-List
Back to top
thomas.n.gautier(at)jpl.n
Guest





PostPosted: Sun Dec 07, 2008 7:31 am    Post subject: Dancing ammeter and alternator drop outs Reply with quote

Bob,

Thanks for your reply. I'm sorry I was not more specific.

The current symptom of the airplane is that the alternator will shut
down and produce no current. The load meter goes to zero and the voltage
drops to the battery voltage, a little over 12v on my flight. Turning the
alternator half of the split master off and then back on restores alternator
output, the load meter goes to 70A briefly and then starts dancing. I
carelessly did not observe the voltage with the alternator working. After
ten or 15 minutes the alternator output will again go to zero. Cycling the
alternator half of the master will again restore the load meter indication.
The 5A alternator field breaker does not pop during this process. I am
unsure how long I left the alternator off line before cycling the split
master.

I did search the archives for 'dancing & ammeter' and I understand the
issue of excessive resistance in the voltage sense/field current wire. Looks
to me like this plane has that problem. You seem to be saying that the
alternator drop out I describe is not related to the dancing ammeter symptom
but that the drop outs are probably caused by a loose connection. But why
would cycling the alternator half of the master reliably restore operation
if there was a loose connection?

Are there any more tests you would suggest?

Thanks much for your attention.

Nick Gautier
You wrote:
Time: 06:48:48 AM PST US
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Dancing ammeter and alternator drop outs
At 04:11 PM 12/5/2008, you wrote:
Quote:
<thomas.n.gautier(at)jpl.nasa.gov>

Bob,

Our club Arrow IV has recently experienced a spate of alternator and
related electrical system maintenance issues. The symptoms that the club
members complained about centered on alternator drop outs which could often,
if not always, be cured by turning the alternator off and then back on.
There may have been an outright alternator failure of some sort as well. I
haven't followed the maintenance in detail since I haven't, until today,
flown the plane in the last month.

By "drop out" do you mean that the alternator shuts down completely?
Do you get a low voltage warning or does the ammeter go to zero
and stay there?

Quote:
The upshot of all the maintenance is that first the voltage regulator
and then the alternator were replaced. The symptom reported after voltage
regulator replacement but before alternator replacement was that the
alternator was dropping out every 10 minutes in the last half hour of a
cross country trip. I was the first to fly the plane after the alternator
replacement and I found the system to still be misbehaving.

In my flight immediately upon starting the engine and switching on the
alternator the alternator ammeter (a load meter, I think) showed 70 amps,
pretty steady, recharging the battery I presume. Then, in less than a minute
the ammeter began swinging from 30A to 70A 2 or 3 times a second. I've read
your dancing ammeter posts so I assumed this was not particularly
troublesome (except that these swings were larger than I had seen before).
Then, after my first turn around the pattern, I noticed that the alternator
had dropped off line. It came back after cycling the alternator switch,
however the ammeter dancing was now as large as 0A to 70A. This behavior
continued for a couple more turns around the pattern, with full stop
landings, as I watched what was going on. I had to reset the alternator
twice more over the span of 20 minutes.

I'm trying to deduce if you're speaking to an intermittent operation.
A lack of ability for the alternator to deliver any power at all . . . or
an unstable condition where the alternator is always developing some
power but the regulation is unstable.

Quote:
So, the plane's electrical problems are not solved and I'm trying to
help the owner and his mechanic figure out what is really wrong. I dug some
of your posts about dancing ammeters out of the archive and I'm ready to
show them to the plane's owner. However I'd like to get your opinion as to
whether I'm on the right track. Can the aging wiring problem that causes
dancing ammeters also cause the alternator to frequently drop off line?

You use the words "dancing ammeter". Go to

http://www.matronics.com/searching/ws_script.cgi

Search the AeroElectric List archive using search string . . .

dancing & ammeter

You will unearth a lot of conversation about a phenomenon
common to older airplanes where the voltage regulator senses
bus voltage through the same wire that supplies field current.
This sets up the possibility for a "negative resistance" (read
oscillation) of voltage regulator stability that can be
anything from barely noticeable to quite severe.

It has nothing to do with the alternator or the regulator and
everything to do with condition of ALL wires, components and
joints between the bus and the regulator. The 30-year fix is to
replace ALL these components.

If you're describing an oscillating voltage condition, then
the discussions and recommended fixes described in the archives
are the road to Nirvana. If you're describing an intermittent
functionality where the alternator output goes to zero and
stays there for some observable time interval . . . you're
chasing a loose connection.

Bob . . .


- The Matronics AeroElectric-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

http://www.matronics.com/Navigator?AeroElectric-List
Back to top
thomas.n.gautier(at)jpl.n
Guest





PostPosted: Mon Dec 08, 2008 8:48 am    Post subject: Dancing ammeter and alternator drop outs Reply with quote

Bob,

Thanks. I'll send your comments along to the owner and mechanic and
I'll try to get the switch carcass if its replaced.

Nick Gautier

You Wrote:

Time: 09:47:56 AM PST US
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Re: Dancing ammeter and alternator drop
outs

At 09:28 AM 12/7/2008, you wrote:
Quote:
<thomas.n.gautier(at)jpl.nasa.gov>

Bob,

Thanks for your reply. I'm sorry I was not more specific.

Not a problem . . .
Quote:
The current symptom of the airplane is that the alternator will shut
down and produce no current. The load meter goes to zero and the voltage
drops to the battery voltage, a little over 12v on my flight. Turning the
alternator half of the split master off and then back on restores alternator
output, the load meter goes to 70A briefly and then starts dancing. I
carelessly did not observe the voltage with the alternator working. After
ten or 15 minutes the alternator output will again go to zero. Cycling the
alternator half of the master will again restore the load meter indication.
The 5A alternator field breaker does not pop during this process. I am
unsure how long I left the alternator off line before cycling the split
master.

These split-rocker switches are close cousins to the S700 series
Carling toggle switches offered by B&C and described here:

http://aeroelectric.com/Mfgr_Data/Switches/Carling_G-series.pdf

http://aeroelectric.com/Pictures/Switches/Carling_Cutaway.jpg

http://aeroelectric.com/Pictures/Switches/Split_Rocker_Front.jpg

http://aeroelectric.com/Pictures/Switches/Split_Rocker_Rear.jpg

I used to have a plastic bag in my desk drawer that contained
two split-rockers removed from TC aircraft that were plagued
with some form of alternator recalcitrance . . . teardown inspection
showed that the contacts on the alternator were badly degraded
due to combinations of corrosion exacerbated by time, and current
draw thorough the switch's rising contact resistance. Next
time I put my hands on them, I'll get them photographed for the
rogue's gallery of switch failures.
Quote:
I did search the archives for 'dancing & ammeter' and I understand the
issue of excessive resistance in the voltage sense/field current wire. Looks
to me like this plane has that problem.

It's quite possible . . .
Quote:
You seem to be saying that the
alternator drop out I describe is not related to the dancing ammeter symptom
but that the drop outs are probably caused by a loose connection. But why
would cycling the alternator half of the master reliably restore operation
if there was a loose connection?

You're very close to answering your own question with
a high probability of accuracy . . . what gets "wiggled"
when you cycle the switch?
Quote:
Are there any more tests you would suggest?

Sure, take a voltmeter along and do the divide/conquer study.
Connect a test lead at half-way between bus and alternator
field terminal. See if you can get the problem to repeat.
If symptom repeats and voltage disappears during alternator
misbehavior, move test point toward the bus 1/4 of the way
and test again. If you're feeling really confident about the
switch, just probe the downstream side of the switch.

Now, if there's alternator ammeter wiggle when things are
working "normally", then perhaps you can get the folks to
do the bus-to-regulator refurbishment cited in the aforementioned
articles . . . most likely, this will fix both the dancing
ammeter -AND- the alternator drop out. If you do replace the
switch for any reason, I'd like to have the carcass.

Bob . . .


- The Matronics AeroElectric-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

http://www.matronics.com/Navigator?AeroElectric-List
Back to top
Display posts from previous:   
Post new topic   Reply to topic    Matronics Email Lists Forum Index -> AeroElectric-List All times are GMT - 8 Hours
Page 1 of 1

 
Jump to:  
You cannot post new topics in this forum
You cannot reply to topics in this forum
You cannot edit your posts in this forum
You cannot delete your posts in this forum
You cannot vote in polls in this forum
You cannot attach files in this forum
You can download files in this forum


Powered by phpBB © 2001, 2005 phpBB Group