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charging system problems

 
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collin



Joined: 19 Sep 2006
Posts: 6

PostPosted: Sun Oct 08, 2006 5:19 pm    Post subject: charging system problems Reply with quote

I am still trying to figure this thing out. The bus voltage is a constant 14.5 volts. On the last two flights I made (1hr each) I had to reset the system twice in the first 10 min or so. The rest of the flight everything seemed to work fine.

Collin,

Bearhawk (N370CC)


Quote:
Let me try to describe the problem as best I can. I am using a Van's 35
amp alt. a VR-371 voltage/over-voltage protector, and a Electronics
International (VA-1) guage installed in the alt lead. Also using a Odyssey
680 battery.

The problem is this: Everything seems to work just fine until maybe 10-15
minutes into the flight when the discharge light on the VA-1 comes on. I
can reset the system by recyling the field breaker and everything goes
back to normal--charging again. This will last maybe another 10-15
minutes and the whole process repeats itself. I have checked all my
conections, replaced the battery, and now am beginning to suspect the
alternator or even the regulator. But I need some advice before I go
replacing stuff that doesn't need replacing. (been there done that before!)

If your system needs "reset", then the symptoms suggest
that the OV protection system in your voltage regulator
is being tripped. This becomes a problem of deducing whether
a real OV condition existed -or- the circuit is being nuisance
tripped.

It's a rational component of troubleshooting to suspect
any component. But it's much better to do measurements
to determine the physics behind the difficulty before embarking
on a swaptronics excursion where one can only hope to pick
the right component . . . with the attendant risk that NONE
of the components replaced will fix the problem.

What are your bus voltages when the system is operating
normally? I'm curious as to how you integrated the VR-371
voltage regulator with a Van's alterantor. I was under the
impression that Van's sold only internally regulated machines.
Let's do the detective work before you pull out any hardware.

Bob . . .

[quote][b]


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collin



Joined: 19 Sep 2006
Posts: 6

PostPosted: Fri Oct 13, 2006 3:20 pm    Post subject: charging system problems Reply with quote

I am still trying to figure out the glitch in my charging system. I wrote about this a couple of weeks ago, I am new to this group, haven't figured out how to include all the past discussion without retyping it all over again. I beg your patience.

To rehash the problem. Everything seems to work fine until five or so minuites into the flight when the system begins to discharge. I can reset the system by recycling the field breaker and everything goes back to normal, for another few minutes. After I recycle the system the second time, I can continue the rest of the flight with no problems. The bus voltage is a constant 14.5 volts. I am using a Van's 35 amp alt, VR-371 regulator, Electronics Int. VA-1 guage installed in the alt. lead. This is a "Bearhawk" aircraft. (tubing fuselage, metal wings) I didn't discover this group until I had already wired the plane so I know I have done some things that I would do differently if I had it to do over again. My battery (Odyssey 680) is grounded to the engine mount. Engine is grounded to the mount via a bolt on the oil sump. I know, I know... there is a better way, just that I copied what I saw on numerous other planes. My wiring diagram is one that I borrowed from one of Tony Bengelis' books.

Still hoping someone out there can shed some light on this..

Collin
[quote][b]


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mprather(at)spro.net
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PostPosted: Fri Oct 13, 2006 4:55 pm    Post subject: charging system problems Reply with quote

Hello Collin,

I am not clear how you know that the system is "discharging".. If the bus
voltage is solid at 14.5V, then the alternator is regulating, and keeping
up with system demands. Or, what's the bus voltage during the discharge?

If you go to the archive search engine:

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

And enter "Collin", you can see everything you have posted to the
Aeroelectric list (be sure to select that Archive as the thing to
search)..
Regards,

Matt-

Quote:
I am still trying to figure out the glitch in my charging system. I wrote
about this a couple of weeks ago, I am new to this group, haven't figured
out how to include all the past discussion without retyping it all over
again. I beg your patience.

To rehash the problem. Everything seems to work fine until five or so
minuites into the flight when the system begins to discharge. I can reset
the system by recycling the field breaker and everything goes back to
normal, for another few minutes. After I recycle the system the second
time, I can continue the rest of the flight with no problems. The bus
voltage is a constant 14.5 volts. I am using a Van's 35 amp alt, VR-371
regulator, Electronics Int. VA-1 guage installed in the alt. lead. This
is a "Bearhawk" aircraft. (tubing fuselage, metal wings) I didn't
discover this group until I had already wired the plane so I know I have
done some things that I would do differently if I had it to do over again.
My battery (Odyssey 680) is grounded to the engine mount. Engine is
grounded to the mount via a bolt on the oil sump. I know, I know... there
is a better way, just that I copied what I saw on numerous other planes.
My wiring diagram is one that I borrowed from one of Tony Bengelis' books.

Still hoping someone out there can shed some light on this..

Collin


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collin



Joined: 19 Sep 2006
Posts: 6

PostPosted: Fri Oct 13, 2006 5:56 pm    Post subject: charging system problems Reply with quote

Matt,

Ok, I forgot to mention that the discharge light comes on. The amp reading
goes to "0" and the voltage drops to 12.8 (a fully charged battery)

Thanks for the reply

Collin
---


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nuckollsr(at)cox.net
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PostPosted: Sat Oct 14, 2006 5:06 am    Post subject: charging system problems Reply with quote

At 08:55 PM 10/13/2006 -0500, you wrote:

Quote:

<collinc(at)alltel.net>

Matt,

Ok, I forgot to mention that the discharge light comes on. The amp
reading goes to "0" and the voltage drops to 12.8 (a fully charged battery)

Thanks for the reply

Collin


Given that the alternator in question is externally regulatred,
the system lends itself to rudimentary trouble shooting techniques.
I believe I referred you to Note 8 on page Z-8 of

http://aeroelectric.com/articles/Rev11/AppZ_R11J.pdf

as a guide for chasing out the bugs. It would be useful
to know what field voltage the alternator is seeing during
a failure. This means that you need to bring a wire into
the cockpit from the alternator's field terminal and watch
it with a voltmeter so you can observe and report the
readings during normal and failed operations.

Bob . . .


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