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11-04-2007, 05:44 AM
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Join Date: Oct 2006
Location: Hardin, KY
Posts: 62
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Ammeter shunt
I have an RV7-A. Where physically are you installing the ammeter shunt?
__________________
Carl Nank
Western Kentucky
RV7A, firewall forward
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11-04-2007, 05:59 AM
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Join Date: Jul 2005
Location: Fern Park, Florida
Posts: 37
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Carl,
I mounted mine right below the battery box and above the gascolator.
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Dick
N797RV - KSFB
RV-7A Flying
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11-04-2007, 06:20 AM
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Join Date: Jan 2005
Location: Tulsa, OK
Posts: 1,014
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11-04-2007, 06:56 AM
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Join Date: Jan 2005
Posts: 4,283
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Depends on type of ammeter and wiring
Quote:
Originally Posted by cbnank
I have an RV7-A. Where physically are you installing the ammeter shunt?
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Yea firewall side near BAT is fine, but what kind of ammeter do you have? (LOAD or BAT CHRG/DISCHRG)
Do you have a LOAD METER or CHARGE/DISCHARGE METER? Either way, shunt mounting location is somewhat dictated by your wiring. A better location may be near the the buss on the cockpit side of the firewall to make the wire runs to the gauge shorter and reducing wires penetrating the firewall.
If you are using a LOAD METER (total aircraft electical load monitored all the time the alternator is running) any where on the B-lead is fine. If you B-lead runs all the way to the main buss inside the cockpit, than the SHUNT should can go near the buss, to simplify running the wires to the gauge.
If you are using a BAT CHG/DISCHG METER anywhere on the main feed from the POS side of the BAT to the Buss[/b]. Again if running the BAT FEED to the BUSS, locating the shunt near the buss simplifys (shortens) gauge wiring.
Here are the previous discussions of what is better: Load or Bat Chg/Dischg monitoring. I vote for Load ammeter.
http://www.vansairforce.com/communit...ighlight=shunt
http://www.vansairforce.com/communit...ighlight=shunt
__________________
George
Raleigh, NC Area
RV-4, RV-7, ATP, CFII, MEI, 737/757/767
2020 Dues Paid
Last edited by gmcjetpilot : 11-04-2007 at 07:06 AM.
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11-04-2007, 04:16 PM
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Join Date: Oct 2006
Location: Hardin, KY
Posts: 62
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Shunt placement
Sorry, I should have elaborated.
I have a Dynon system and I will be placing the shunt on wire P1 (Van's basic wireing harness) between the buss bar & the copper connector between the master relay & starter relay. I believe Dynon calls it the "A" position.
This would make the position beside the battery a perfect location for the shunt. I was originally thinking about the instrument sub panel, but I think I like the firewall better.
What do some others think?
Thanks
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Carl Nank
Western Kentucky
RV7A, firewall forward
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11-25-2007, 08:05 AM
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Join Date: Jan 2005
Location: Cincinnati, OH
Posts: 1,551
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Shunt
Bob Nucholls (Aeroelectric Connection) doesn't recommend the 'A' position. This makes it a battery monitor - charge/discharge. If you loose your alternator, this info is useless.....and when the alternator is working, it's almost useless. You should get an idea of how long your battery will last on it's own and land within that time - or have a back-up battery if flying IFR. All of Bob's wiring schematics has the shunt it the 'B' location, functioning as a loadmeter. This also makes it useful if configuring any kind of diagnostics to check/monitor your alternator/regulator health.
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11-25-2007, 06:10 PM
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Join Date: Apr 2005
Location: KSLC
Posts: 4,021
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Quote:
Originally Posted by Scott Hersha
Bob Nucholls (Aeroelectric Connection) doesn't recommend the 'A' position. This makes it a battery monitor - charge/discharge. If you loose your alternator, this info is useless.....and when the alternator is working, it's almost useless. You should get an idea of how long your battery will last on it's own and land within that time - or have a back-up battery if flying IFR. All of Bob's wiring schematics has the shunt it the 'B' location, functioning as a loadmeter. This also makes it useful if configuring any kind of diagnostics to check/monitor your alternator/regulator health.
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Happily, I don't always agree with Bob. He does not like "Cessna type" battery/alt switches. I do.
However, I've used his essential buss feed with the diode setup, as well as other ideas.
With a charge/discharge setup, I can easily see the load that different equipment is taking (and if they work), before I start the plane. Once it's running, at a quick glance, it's easy to see that the alternator is doing it's job of handling the load.
If there is an alternator failure, then it's my blinking alt warning light & volt meter, that let's me know exactly what's going on. Needless to say, I prefer "A", which is the same as Van's schematics.
L.Adamson -- RV6A
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11-25-2007, 09:10 PM
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Join Date: Jan 2005
Location: 57AZ - NW Tucson area
Posts: 10,011
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Just as easy...
L. I'm confused...everything you say can be easily seen (easier?) with the loadmeter (Dynon B) set-up...
With a charge/discharge setup, I can easily see the load that different equipment is taking (and if they work), before I start the plane.
OK... switch stuff on... get a negative amps reading.. more stuff, more amps...
Once it's running, at a quick glance, it's easy to see that the alternator is doing it's job of handling the load.
OK.. a zero reading in flight says alternator is working... battery charges pretty quickly, but a short positive reading says charging is OK as soon as engine starts...
If there is an alternator failure, then it's my blinking alt warning light & volt meter, that let's me know exactly what's going on. Needless to say, I prefer "A", which is the same as Van's schematics.
Alternator failure in flight is easily seen as a negative reading...
L.Adamson -- RV6A
Seems to me like it is a "different strokes for different folks issue"....
Both work equally well with quite clear readings....
gil A
__________________
Gil Alexander
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
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