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View Poll Results: Where did you put your Ammeter Shunt?
A) Monitor Battery Load Only 9 47.37%
B) Monitor Total Load Consumed 10 52.63%
c) Monitor Aircraft Load Only 0 0%
Voters: 19. You may not vote on this poll

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  #1  
Old 07-20-2007, 12:03 AM
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RudiGreyling RudiGreyling is offline
 
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Default Where did you put your Ammeter Shunt?

Hi Guys,

Busy with wiring, (some noticed from my recent posts), got a good diagram from Dynon manual below for this discussion.

I have gone back and forth on my decision on where to install the shunt.
As I see it you can either ONLY check what goes in or out of your battery (A) OR how much your airplane ONLY is drawing (C). Position (B) gives you the total draw but not the split.

See the Dilemma? What is more important, What did you guys do and why?

Thanks in advance, Kind Regards
Rudi

http://www.dynonavionics.com/downloa...on%20Guide.pdf
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Last edited by RudiGreyling : 07-20-2007 at 12:07 AM.
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  #2  
Old 07-20-2007, 07:47 AM
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Default

Rudi, I am not there yet, but I am giving it some thought. I am considering adding a second shunt with a DPDT switch to select which one the monitor is getting the info from. I would have the A and C position. B could be determined by the difference in A and C. ( battery is showing 2 positive, A/C load is 30 => alternator is 32 amps)

But then again, I could put it at C and know that my battery is charging by looking at the voltage.
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Last edited by AltonD : 07-20-2007 at 08:24 AM.
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  #3  
Old 07-20-2007, 08:43 AM
chris mitchell chris mitchell is offline
 
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Default

Surely the important thing is to know whether the battery is overall being charged or discharged? I don't think you are much interested in what the aircraft load is? I'd have thought position A? That's what I'm planning to do, but I'm still only halfway through AeroElectric Connection so plenty to learn!! Hopefully Ironflight will be along shortly!

Chris
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  #4  
Old 07-20-2007, 09:48 AM
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Default

I also am just at the point of making this decision.

At this time, I am leaning on monitoring the battery, as my voltage regulator has a warning light to tell me if there is a problem there.

In reading the above posts, it seems folks are trying to follow what the electrical system is doing when things are working properly. I am looking at setting things up so as to find out what is going on when there is a problem.

It will be interesting to hear from folks already flying, and read the poll results, as so far all 4 of the posts have been from folks still building.
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  #5  
Old 07-20-2007, 10:05 AM
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az_gila az_gila is offline
 
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Question Confusing .. a bit...

Rudi,
You have them labeled as....

A Monitor Battery Load Only
B Monitor Total Load Consumed
C Monitor Aircraft Load Only

but in reality A is not battery load, but battery charge/load, and does check that the alternator has an output.

and B is not Total load, but is actually Alternator Output

I prefer A, since it measures load with the alternator off, and checks that the battery is charging when in normal flight. In cruise, all should be close to zero....

Perhaps you should relabel choices A and B?....

gil in Tucson
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  #6  
Old 07-20-2007, 10:57 AM
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Default EI has good reference. Same considerations as Dynon

The EI MVP-50 installation manual has a good explanation of pro's and con's of where the Shunt should be installed. If you download the MVP-50P (Piston Engine) Installation Manual from http://www.buy-ei.com/Downloads.htm and go to page 21 & 22, you will find a good explanation and diagram.
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  #7  
Old 07-20-2007, 11:06 AM
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az_gila az_gila is offline
 
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Exclamation Only A an B...

Quote:
Originally Posted by Rick_A
The EI MVP-50 installation manual has a good explanation of pro's and con's of where the Shunt should be installed. If you download the MVP-50P (Piston Engine) Installation Manual from http://www.buy-ei.com/Downloads.htm and go to page 21 & 22, you will find a good explanation and diagram.
Interesting, they only use A and B, and don't mention C....

gil A
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  #8  
Old 07-20-2007, 12:33 PM
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Default Is there a difference between B & C ?

When I look at the diagram that Rudi posted, B & C appear to be electrical equivalent. I am missing something?
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  #9  
Old 07-20-2007, 01:19 PM
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Yes, B will only show alternator output. If the alternator dies, Zero while there is now a load on your battery.
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?The secret of getting ahead is getting started. The secret of getting started is breaking your complex overwhelming tasks into small manageable tasks, and then starting on the first one.?

?Mark Twain
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  #10  
Old 07-20-2007, 04:21 PM
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Exclamation Trace paths...

Quote:
Originally Posted by Rick_A
When I look at the diagram that Rudi posted, B & C appear to be electrical equivalent. I am missing something?
You can trace out the current paths.
Only two exist for current sources...
1. The Alternator can generate current (one direction only)
2. The Battery can charge or discharge (two directions... both a source and a sink.)

The aircraft load is a sink in one direction only.

Use these options, and every possible circuit path can be traced... But ignore the starter, it's current is too high to be measured anyway...

gil A
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EAA Technical Counselor, Airframe Mechanic
Half completed RV-10 QB purchased
RV-6A N61GX - finally flying
Grumman Tiger N12GA - flying
La Cholla Airpark (57AZ) Tucson AZ

Last edited by az_gila : 07-20-2007 at 04:22 PM. Reason: Quoted wrong person...
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