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tim2542(at)sbcglobal.net Guest
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Posted: Wed Oct 20, 2010 5:40 pm Post subject: AUX Battery |
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I'm designing my system using a small AUX Battery and single Alt. I want to charge the aux battery with a Schottkey diode. The AUX battery will power the avionics during start to prevent brown out and can be used as clearance delivery and/or a backup bus for the EFIS/430W GPS/Comm. Others I know of who have done it this way also used a 50 ohm resistor in series with the diode for reasons no one can really explain to me. The battery is a small 7ah sealed unit and I plan to charge it thru the diode and a 7.5 amp fuse. Is there any reason to use a resistor in this configuration?
Thanks, Tim Andres
(rnbraud(at)yahoo.com)
[quote][b]
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user9253
Joined: 28 Mar 2008 Posts: 1922 Location: Riley TWP Michigan
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Posted: Thu Oct 21, 2010 6:07 am Post subject: Re: AUX Battery |
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Quote: | Is there any reason to use a resistor in this configuration? |
No, I see no reason to use a resistor. If someone else used a resistor, they should be able to explain why. Just because some other builder wired their plane wrong is no reason to do it the same way. There have been arguments on this forum about what type of diode to use to minimize voltage drop. Using a resistor does not minimize voltage drop.
If there is a reason for using a resistor, it would be interesting to know how and why it was used.
Joe
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_________________ Joe Gores |
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nuckolls.bob(at)aeroelect Guest
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Posted: Thu Oct 21, 2010 6:30 am Post subject: AUX Battery |
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At 08:34 PM 10/20/2010, you wrote:
Quote: | I'm designing my system using a small AUX Battery and single Alt. I want to charge the aux battery with a Schottkey diode. The AUX battery will power the avionics during start to prevent brown out and can be used as clearance delivery and/or a backup bus for the EFIS/430W GPS/Comm. Others I know of who have done it this way also used a 50 ohm resistor in series with the diode for reasons no one can really explain to me. The battery is a small 7ah sealed unit and I plan to charge it thru the diode and a 7.5 amp fuse. Is there any reason to use a resistor in this configuration? |
No. In fact the ideal aux battery charging circuit
has a MINIMUM of voltage drop. The Shottky diode
offers the closest solid state solution with drops
averaging 0.3 to 0.5 volts. You can acquire these
devices packaged for user-friendly installations
from
https://matronics.com/aeroelectric/Catalog/AEC/9001/IM9001-700A.pdf
or
http://www.periheliondesign.com/powerschottkydiodesfiles/PowerSchottky%20Manual.pdf
or loose parts from electronics suppliers of various
sorts
http://search.digikey.com/scripts/DkSearch/dksus.dll?Detail&name=MBRF40250TGOS-ND
Alternatively, you can achieve essentially zero-volts
drop for the charging circuit with incorporation of
an Aux Battery Management Module that closes a relay
between the two batteries only when the alternator is
running (bus rises above 13.0 volts).
Bob . . . [quote][b]
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nuckolls.bob(at)aeroelect Guest
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Posted: Fri Oct 22, 2010 8:14 am Post subject: AUX Battery |
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At 09:07 AM 10/21/2010, you wrote:
Quote: |
> Is there any reason to use a resistor in this configuration?
No, I see no reason to use a resistor. If someone else used a
resistor, they should be able to explain why. Just because some
other builder wired their plane wrong is no reason to do it the same
way. There have been arguments on this forum about what type of
diode to use to minimize voltage drop. Using a resistor does not
minimize voltage drop.
If there is a reason for using a resistor, it would be
interesting to know how and why it was used.
|
An excellent point. A series resistor
in a small battery charging circuit is
indicated for one purpose only and under
a narrow set of circumstances.
If the small battery is at risk for
ever becoming totally discharged one might
improve on battery performance by limiting
the magnitude of recharge current when the
system comes back up at normal voltages.
The batteries I used in the recovery parachute
controllers for HBC
http://www.aeroelectric.com/Pictures/Misc/Recovery_Parachute_Controller.jpg
were 1.2 a.h. devices intended to be charged by and
as back-up for ship's power. If ship's power was
brought on with completely discharged batteries,
the inrush to the little batteries would not be
conducive to a long service lift. Hence, the charge
loop included a 3 ohm resistor that would limit
initial current flows to about 8 amps. This also
prevented the initial recharge current to a dead
battery from popping the 10A breaker on the ship's
bus.
Of course, this would mean that getting the batteries
fully recharged would take longer. It also means that
the charging loop could not be depended upon for
power to run the system. That task was covered by
a separate circuit.
The decision for including such resistors depends
on an assessment (and preventative maintenance
program) for circumstances that might totally
discharge the battery . . . and what you would
do about it if such an event were discovered.
I built a battery maintainer into the parachute
controller intended to be plugged into AC mains
for a minimum of two hours within the week prior
to a flight where the parachute was to be armed.
Further, preflight testing by ground
crews before launch included a load test of the
batteries. Hence, probability of the resistor ever
being functionality tasked was very low.
Joe's assessment is quite correct that inclusion
of a resistor in the charge path of a battery demands
a full understanding of it's purpose and the effect
on system functionality under all anticipated
conditions. 99% of the time, you don't need them.
Bob . . .
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tim2542(at)sbcglobal.net Guest
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Posted: Fri Oct 22, 2010 8:52 am Post subject: AUX Battery |
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Thanks Bob, Joe. The idea as I understood it was in regard to limiting the charge current just as you surmised.
The Diode I'm using is a 9amp wire diode. I'll install it using your homeless components methods from the site, no resistor.
Thanks,Tim
Sent from my iPhone
On Oct 22, 2010, at 9:13 AM, "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> wrote:
Quote: |
At 09:07 AM 10/21/2010, you wrote:
>
>
>
> > Is there any reason to use a resistor in this configuration?
>
> No, I see no reason to use a resistor. If someone else used a resistor, they should be able to explain why. Just because some other builder wired their plane wrong is no reason to do it the same way. There have been arguments on this forum about what type of diode to use to minimize voltage drop. Using a resistor does not minimize voltage drop.
> If there is a reason for using a resistor, it would be interesting to know how and why it was used.
An excellent point. A series resistor
in a small battery charging circuit is
indicated for one purpose only and under
a narrow set of circumstances.
If the small battery is at risk for
ever becoming totally discharged one might
improve on battery performance by limiting
the magnitude of recharge current when the
system comes back up at normal voltages.
The batteries I used in the recovery parachute
controllers for HBC
http://www.aeroelectric.com/Pictures/Misc/Recovery_Parachute_Controller.jpg
were 1.2 a.h. devices intended to be charged by and
as back-up for ship's power. If ship's power was
brought on with completely discharged batteries,
the inrush to the little batteries would not be
conducive to a long service lift. Hence, the charge
loop included a 3 ohm resistor that would limit
initial current flows to about 8 amps. This also
prevented the initial recharge current to a dead
battery from popping the 10A breaker on the ship's
bus.
Of course, this would mean that getting the batteries
fully recharged would take longer. It also means that
the charging loop could not be depended upon for
power to run the system. That task was covered by
a separate circuit.
The decision for including such resistors depends
on an assessment (and preventative maintenance
program) for circumstances that might totally
discharge the battery . . . and what you would
do about it if such an event were discovered.
I built a battery maintainer into the parachute
controller intended to be plugged into AC mains
for a minimum of two hours within the week prior
to a flight where the parachute was to be armed.
Further, preflight testing by ground
crews before launch included a load test of the
batteries. Hence, probability of the resistor ever
being functionality tasked was very low.
Joe's assessment is quite correct that inclusion
of a resistor in the charge path of a battery demands
a full understanding of it's purpose and the effect
on system functionality under all anticipated
conditions. 99% of the time, you don't need them.
Bob . . .
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nuckolls.bob(at)aeroelect Guest
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Posted: Fri Oct 22, 2010 1:50 pm Post subject: AUX Battery |
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At 11:49 AM 10/22/2010, you wrote:
Quote: |
Thanks Bob, Joe. The idea as I understood it was in regard to
limiting the charge current just as you surmised.
The Diode I'm using is a 9amp wire diode. I'll install it using your
homeless components methods from the site, no resistor.
|
What's the capacity of your aux battery?
Bob . . .
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tim2542(at)sbcglobal.net Guest
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Posted: Fri Oct 22, 2010 3:11 pm Post subject: AUX Battery |
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7ah
Tim
Sent from my iPhone
On Oct 22, 2010, at 2:48 PM, "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com> wrote:
Quote: |
At 11:49 AM 10/22/2010, you wrote:
>
>
> Thanks Bob, Joe. The idea as I understood it was in regard to limiting the charge current just as you surmised.
> The Diode I'm using is a 9amp wire diode. I'll install it using your homeless components methods from the site, no resistor.
What's the capacity of your aux battery?
Bob . . .
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nuckolls.bob(at)aeroelect Guest
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Posted: Sat Oct 23, 2010 9:21 am Post subject: AUX Battery |
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What's the capacity of your aux battery?
At 06:08 PM 10/22/2010, you wrote:
AeroElectric-List message posted by: tim2542(at)sbcglobal.net
7ah
Tim
Okay, it's not one of those "tiny" things and
will probably be okay with the simple diode in
the charging feeder.
CAUTION
Any builders on the List who are relatively new
or perhaps were not paying close attention to battery
discussions in past years, I advise a review of the
following publications:
Chapters 2 and 17 of the AeroElectric Connection
http://www.aeroelectric.com/articles/neveragain/neveragain.html
http://www.aeroelectric.com/articles/neveragain/neveragain_1.html
http://www.aeroelectric.com/articles/neveragain/neveragain_2.html
http://www.aeroelectric.com/articles/battery.pdf
http://www.aeroelectric.com/articles/rg_bat.html
http://www.aeroelectric.com/articles/Batteries/Multiple_Battery_Myths_A.pdf
http://www.aeroelectric.com/articles/bat_iso2.pdf
http://www.aeroelectric.com/articles/Batteries/Deltran_Odyssey_Floobydust.html
http://www.aeroelectric.com/articles/WestMountain_CBAII.pdf
Bottom line is that if you are carrying ANY
number of battery(ies) on board for the purpose
of alternator failure mitigation, then
you need to SIZE the task - how much time to do
you EXPECT any battery to perform as back-up power?
Then you need A PLAN to make sure those requirements
will be met.
This is especially important for so-called AUX
batteries that are not NORMALLY expected to
do anything. If the battery doesn't crank the
engine . . . nor is it occasionally used to
supply some noteworthy run-time for ground maintenance,
then HOW DO YOU KNOW the thing is even useful?
The heavy iron guys periodically capacity test
all ship's batteries and replace them when they
fall below established limits for meeting
s/b power needs.
With out A PLAN, it's a high order risk that
the battery won't be there for you at such
time you DO need it.
If no plan, then depending on an AUX battery (or
even the ship's main battery) to bail you
out is problematic. You're may be investing
$acquisition$, space, weight and fuel to wrap
yourself in a lead-acid security blanket.
Cap meters like . . .
http://www.westmountainradio.com/content.php?page=cba
are excellent pieces of test equipment that will load
the battery exactly like you'll expect to load it
during S/B service in your airplane. If not this
class of device, then
http://www.aeroelectric.com/articles/Poor_Man%27s_Cap_Tester.pdf
or just put a new battery in every two years. But
have requirements assured by a plan.
Bob . . .
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