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VM-1000 current sensor question

 
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dean.psiropoulos(at)veriz
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PostPosted: Thu Jul 06, 2006 9:46 pm    Post subject: VM-1000 current sensor question Reply with quote

I've been looking at this VM1000 current sensor (it looks like some sort of
hall effect sensor with 4 terminals, it's a coil you slide over the wire, no
connection needed). Originally I had it on the feed line from the alternator
but realized that I would only get readings of zero and greater than zero on
the display if I did that. So I thought I'd put it around the fat wire that
connects to the battery positive terminal and get both discharge and charge
readings. But....re-reading the VM-1000 manual and looking at their display
silk-screening, it appears that the display is only designed to read a
positive rate of charge from the alternator (0 to +60 amps). I don't have
everything connected yet so I can't actually fire it up and test it.

You VM1000 users, is this true? Does it NOT read and display negative
amperes when the battery is discharging and the alternator is not running
(or failed)? Is everyone installing this sensor on the alternator feed line
or are some of you doing something else??? if so what???? and why? Thanks.
Dean Psiropoulos
RV-6A N197DM
Plodding along to blissful completion.


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recapen(at)earthlink.net
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PostPosted: Fri Jul 07, 2006 3:01 am    Post subject: VM-1000 current sensor question Reply with quote

I'm in a similar situation as Dean - except I have most of my electrical
system up and functioning. My amp sensor is in the equivalent place of the
feed line and could only show current being generated by the alternators.
My instruction manual shows the 'minus' bar on the display page implying
that the unit could display current draw and supply - but I can't figure out
how to wire it so both situations would be discernable to the
transducer......the only solutions that I have come up with involve A) two
wires passing throught the transducer - one 'flowing' in each
direction...under normal operation one would carry generated current - under
failure operation (of the alternators) the other would carry drawn current
or B) two transducers with a switch to select which one is being
displayed...one transducer would show the generated current and the other
would show drawn current.

The VM1000 instruction manual indicates that the transducer is to be placed
to measure generated current from what I remember reading and does not
provide for reading of drawn current - even though the unit is implied to be
able to display either mode.

Maybe we need to get Vision Microsystems to weigh in n this one.....I'll
send out a note to them.....

Ralph Capen
---


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jlinga(at)mchsi.com
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PostPosted: Fri Jul 07, 2006 4:27 am    Post subject: VM-1000 current sensor question Reply with quote

Guys,
    When I installed my VM1000C, I had the same question and called the company.  The display will not show negative numbers.  The current sensor is designed to be used as a loadmeter and not a battery ammeter.  The voltage will generally give you a good indication whether or not the battery is charging.
 
Jerry
 
 
--> AeroElectric-List message posted by: "Ralph E. Capen" <recapen(at)earthlink.net ([email]recapen(at)earthlink.net?subject=Re:%20VM-1000%20current%20sensor%20question&replyto=003801c6a1b2$0a00a8c0(at)CAPENFAMILY.ORG[/email])>

I'm in a similar situation as Dean - except I have most of my electrical
system up and functioning.  My amp sensor is in the equivalent place of the
feed line and could only show current being generated by the alternators.
My instruction manual shows the 'minus' bar on the display page implying
that the unit could display current draw and supply - but I can't figure out
how to wire it so both situations would be discernable to the
transducer......the only solutions that I have come up with involve A) two
wires passing throught the transducer - one 'flowing' in each
direction...under normal operation one would carry generated current - under
failure operation (of the alternators) the other would carry drawn current
or B) two transducers with a switch to select which one is being
displayed...one transducer would show the generated current and the other
would show drawn current.

The VM1000 instruction manual indicates that the transducer is to be placed
to measure generated current from what I remember reading and does not
provide for reading of drawn current - even though the unit is implied to be
able to display either mode.

Maybe we need to get Vision Microsystems to weigh in n this one.....I'll
send out a note to them.....

Ralph Capen
---


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nuckollsr(at)cox.net
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PostPosted: Fri Jul 07, 2006 5:19 am    Post subject: VM-1000 current sensor question Reply with quote

At 01:43 AM 7/7/2006 -0400, you wrote:

Quote:

<dean.psiropoulos(at)verizon.net>

I've been looking at this VM1000 current sensor (it looks like some sort of
hall effect sensor with 4 terminals, it's a coil you slide over the wire, no
connection needed). Originally I had it on the feed line from the alternator
but realized that I would only get readings of zero and greater than zero on
the display if I did that.

Correct. It becomes an alternator LOADMETER
Quote:
. . . So I thought I'd put it around the fat wire that
connects to the battery positive terminal and get both discharge and charge
readings.

That becomes a BATTERY AMMETER which is less useful. While
it was the ONLY instrumentation in most automobiles and many
airplanes, it wasa system health instrument that required
interpretation and flight to flight trend monitoring. It met
FAA requirements for electrical system health monitoring.

The problem with a battery ammeter is that it "sorta" tells you if
the bus voltage is okay when the recharge current ultimately goes
back to zero AFTER it sorta tells you that the battery is okay when
it accepts a healthy recharge after engine start. Battery ammeters
are better than nothing but not much. Given that the VM-1000 provides
voltage readings and low volts warning, then using the ammeter function
to watch alternator load is the most definitive use of the instrument
for troubleshooting.
Bob . . .
---------------------------------------------------------
< What is so wonderful about scientific truth...is that >
< the authority which determines whether there can be >
< debate or not does not reside in some fraternity of >
< scientists; nor is it divine. The authority rests >
< with experiment. >
< --Lawrence M. Krauss >
---------------------------------------------------------


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bakerocb



Joined: 15 Jan 2006
Posts: 727
Location: FAIRFAX VA

PostPosted: Fri Jul 07, 2006 7:34 am    Post subject: VM-1000 current sensor question Reply with quote

7/7/2006

Responding to an AeroElectric-List message previously posted by: "DEAN
PSIROPOULOS" <dean.psiropoulos(at)verizon.net>

Hello Dean, Why don't you just shoot an email to Vision Microsystems
support(at)visionmicrosystems.com <support(at)visionmicrosystems.com> or, better
yet, call them on the phone, (360-714-8203) ask for a technician and ask
him. I have found them great people to deal with. Please tell us what you
learn.

My sensor is on the output (B lead) from the alternator. My visual
electrical information consists of that VM 1000 display reading of amperage
being put out by the alternator, the VM 1000 display of bus voltage, and a
low voltage warning light from a B&C LR3 voltage regulator. The VM 1000
display amperage reading is zero until the alternator comes on line.

Isn't the above a sufficient display of electrical information?

I guess it would be nice to be able to know at all times what amount of the
electrical supply to the aircraft systems was coming from the battery and
what amount was coming from the alternator, but I don't know just exactly
how one would go about configuring a system to obtain that information or
how one would use that information.

I think that after the engine is started and the alternator is on line that
all of the aircraft's electrical system needs are being supplied by the
alternator and if the battery needs charging as determined by the voltage
regulator then the alternator is also supplying the amperage that flows into
the battery.The only time the battery should be discharging is if the total
amperage required by aircraft systems and battery charging needs is greater
than the output capacity of the alternator. Can some one help me here?

OC

PS: I did find the VM hall effect sensor difficult to mount. Their
directions to put it into some sort of protective box was too awkward for me
so mine is just bolted to a bracket on the forward side of the fire wall.
Has worked OK for 144 hours.

"DEAN PSIROPOULOS WRITES"

Quote:
I've been looking at this VM1000 current sensor (it looks like some sort
of
hall effect sensor with 4 terminals, it's a coil you slide over the wire,
no
connection needed). Originally I had it on the feed line from the
alternator
but realized that I would only get readings of zero and greater than zero
on
the display if I did that. So I thought I'd put it around the fat wire
that
connects to the battery positive terminal and get both discharge and
charge
readings. But....re-reading the VM-1000 manual and looking at their
display
silk-screening, it appears that the display is only designed to read a
positive rate of charge from the alternator (0 to +60 amps). I don't have
everything connected yet so I can't actually fire it up and test it.

You VM1000 users, is this true? Does it NOT read and display negative
amperes when the battery is discharging and the alternator is not running
(or failed)? Is everyone installing this sensor on the alternator feed
line
or are some of you doing something else??? if so what???? and why?
Thanks.
Dean Psiropoulos
RV-6A N197DM
Plodding along to blissful completion.


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recapen(at)earthlink.net
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PostPosted: Fri Jul 07, 2006 8:42 am    Post subject: VM-1000 current sensor question Reply with quote

I sent a note to Vision Microsystems....

I'll post the response.....

BTW, My understanding matches yours....about the alternator supplying required current etc.....

Ralph
--


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flyboy.bob(at)gmail.com
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PostPosted: Fri Jul 07, 2006 2:00 pm    Post subject: VM-1000 current sensor question Reply with quote

So Bob,

I hope this isn't too redundant, in this scenario, where is the best
(most useful) place to locate the hall effect sensor?

Thanks,
Bob Christensen
in SE Iowa - RV-8 Bldr
On 7/7/06, Robert L. Nuckolls, III <nuckollsr(at)cox.net> wrote:
Quote:


At 01:43 AM 7/7/2006 -0400, you wrote:

>
><dean.psiropoulos(at)verizon.net>
>
>I've been looking at this VM1000 current sensor (it looks like some sort of
>hall effect sensor with 4 terminals, it's a coil you slide over the wire, no
>connection needed). Originally I had it on the feed line from the alternator
>but realized that I would only get readings of zero and greater than zero on
>the display if I did that.

Correct. It becomes an alternator LOADMETER
> . . . So I thought I'd put it around the fat wire that
>connects to the battery positive terminal and get both discharge and charge
>readings.

That becomes a BATTERY AMMETER which is less useful. While
it was the ONLY instrumentation in most automobiles and many
airplanes, it wasa system health instrument that required
interpretation and flight to flight trend monitoring. It met
FAA requirements for electrical system health monitoring.

The problem with a battery ammeter is that it "sorta" tells you if
the bus voltage is okay when the recharge current ultimately goes
back to zero AFTER it sorta tells you that the battery is okay when
it accepts a healthy recharge after engine start. Battery ammeters
are better than nothing but not much. Given that the VM-1000 provides
voltage readings and low volts warning, then using the ammeter function
to watch alternator load is the most definitive use of the instrument
for troubleshooting.
Bob . . .
---------------------------------------------------------
< What is so wonderful about scientific truth...is that >
< the authority which determines whether there can be >
< debate or not does not reside in some fraternity of >
< scientists; nor is it divine. The authority rests >
< with experiment. >
< --Lawrence M. Krauss >
---------------------------------------------------------




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nuckollsr(at)cox.net
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PostPosted: Fri Jul 07, 2006 2:42 pm    Post subject: VM-1000 current sensor question Reply with quote

At 04:54 PM 7/7/2006 -0500, you wrote:

Quote:


So Bob,

I hope this isn't too redundant, in this scenario, where is the best
(most useful) place to locate the hall effect sensor?

Thanks,
Bob Christensen
in SE Iowa - RV-8 Bldr

If it were my airplane (and I chose to have any ammeters
at all) they would be alternator loadmeters. This is the
most useful current measurement location for troubleshooting
a misbehaving alternator system.

Bob . . .


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brian



Joined: 02 Jan 2006
Posts: 643
Location: Sacramento, California, USA

PostPosted: Fri Jul 07, 2006 4:03 pm    Post subject: VM-1000 current sensor question Reply with quote

On Jul 7, 2006, at 5:54 PM, Bob C. wrote:

Quote:

<flyboy.bob(at)gmail.com>

So Bob,

I hope this isn't too redundant, in this scenario, where is the best
(most useful) place to locate the hall effect sensor?

In the average electrical system there are three places to measure
current. If measure two you can calculate the third. The three places
are:

1. output of the alternator (B-lead);

2. battery positive terminal;

3. input to the main distribution bus.

If you know what is coming out of the alternator and what is going
into the loads then the difference is what is going into or coming
out of the battery.

If you know what is coming out of the alternator and what is going
into the battery, the difference is going into your loads.

If you know what is going into the battery and what is going into
your loads, add them together to figure out alternator load.

If I could only measure one I would measure alternator load and, of
course, system voltage. You will quickly learn what your loads draw
and what the battery draws will drop near to zero. Any excess load on
the alternator indicates a problem.

Brian Lloyd 361 Catterline Way
brian-yak AT lloyd DOT com Folsom, CA 95630
+1.916.367.2131 (voice) +1.270.912.0788 (fax)

I fly because it releases my mind from the tyranny of petty things . . .
— Antoine de Saint-Exupéry


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PostPosted: Mon Jul 10, 2006 11:29 am    Post subject: VM-1000 current sensor question Reply with quote

This conversation has run far-afield . . .

Consider that as long as your low-volts warning light is OFF,
there is nothing helpful for aviating or navigating offered by any
display of amps in any part of the system. When the low volts
light does come on, it's wise to have "plan-b" in the hip pocket
for comfortable termination of flight, preferably at the airport
of intended destination. Again, whatever the amps display is saying
is not useful to the task at hand.

When it comes time to troubleshoot the system, there is no
single measurement point for amps that will minimize the efforts
needed to troubleshoot the system. The repair task almost always
requires probing the system for a LOT more data than what is
offered by panel displays.

I'll suggest there is no right, better, wrong, or best place to
put an ammeter sense point. Every one of the classic locations offers
some data that is useful only if you know the significance of the
data and how to interpret it. But using any such data in flight
for diagnosis is not a useful thing to do . . . it's never helpful
for comfortably completing the flight. No matter where you choose
to put the sense point(s), they will be only the beginning of a
future troubleshooting effort.

Bob . . .


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AdventureD



Joined: 13 Jan 2021
Posts: 16

PostPosted: Wed Mar 10, 2021 11:37 am    Post subject: Re: VM-1000 current sensor question Reply with quote

Resurrecting this old thread.

Suppose the hall effect sensor is on the fat wire from battery 2 in Z-14 with a 70 amp alternator 1 and a 20 amp alternator 2. Here are my questions (recognizing that this is not debugging done in the airplane -- its for understanding how this stuff works).

1. Under normal conditions, when both alternators and batteries are on and the crossfeed is not closed, what will the gauge connected to the hall effect sensor show? Will it show the voltage of the #2 battery and zero amps since the current on the number 2 bus is being drawn from the alternator rather than from the battery? Something else?

2. Suppose the #2 alternator craps out and the low voltage light comes on. If I shut down the #2 alternator and leave the crossfeed open, what will the gauge show? Will it show the same voltage for the #2 battery and the current draw of the instruments on the #2 bus? Something else?

3. Suppose I close the cross feed contactor after the #2 alternator goes kaput and is shut down. Does the gauge now show the voltage of the #2 battery and zero current if the #1 alternator is sufficient to supply both buses?

4. Suppose I shut down both alternators, turn on both batteries, and close the crossfeed. Since battery 1 and battery 2 are now connected, what will the gauge show?

This is all by way of trying to understand what these volts/amps meters do.


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user9253



Joined: 28 Mar 2008
Posts: 1921
Location: Riley TWP Michigan

PostPosted: Wed Mar 10, 2021 4:39 pm    Post subject: Re: VM-1000 current sensor question Reply with quote

Hall effect sensors only measure current, not voltage.
If the hall effect sensor is located to measure current into or out of a battery,
then once the battery is recharged, the current into the battery will be near zero.
If the hall effect sensor is located to measure alternator output current, the
ammeter will show the combination of aircraft load current and battery recharge current.
If the hall effect sensor is located to measure aircraft load current, then it will
not be known if that current is coming from the battery or from an alternator.
Some builders elect to not install an ammeter. As long as the voltage is above
13.5 VDC, then the alternator must be working.


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