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blues750
Joined: 06 Jun 2015 Posts: 56
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Posted: Sun May 03, 2020 7:20 am Post subject: DC clamp meter |
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Looking for recommendations on a suitable DC clamp meter to do capacity checks on my EarthX batteries. Prices seem to be all over the place. Am curious what kind others might be having good experience with. Thanks all!
Dave
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nuckolls.bob(at)aeroelect Guest
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Posted: Sun May 03, 2020 6:27 pm Post subject: DC clamp meter |
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At 10:20 AM 5/3/2020, you wrote:
Quote: | --> AeroElectric-List message posted by: "blues750" <den_beaulieu(at)yahoo.com>
Looking for recommendations on a suitable DC clamp meter to do capacity
checks on my EarthX batteries. Prices seem to be all over the place.
Am curious what kind others might be having good experience with. Thanks all!
Dave |
Help us out with your mission. A 'capacity test' is
a measured depletion and recharge of a battery
to deduce its contained energy.
This could be accomplished at a prescribed discharge
rate commensurate with your anticipated 'endurance
loads' (useful capacity of a battery varies with
load).
In the attached chart you can see how a battery
rated at 18Ah under a 20Hr discharge rate
delivers only 12Ah if discharge over 1Hr rate.
2/3rds of its capacity is tossed off as internal
heating of the battery.
To accomplish a capacity test, you need a means
for establishing a constant current load at
some selected rate while recording the battery's
output voltage until it falls below some
artfully selected cut-off voltage.
Alternatively, consider a device like
this:
https://tinyurl.com/moaoaus
I have used these on numerous projects
over the years. I'm thinking of upgrading
my 20+ year old device. The newer ones
have some really nice software features.
I'm wondering if you're interested in the
battery's cranking (load bearing) characteristics.
This is a different test that quantifies the
battery's internal resistance -and- state of
the chemistry under heavy load.
For this you need a critter like this
https://tinyurl.com/yag4529y
I have a couple of these HF testers . . .
got a $high$ AutoMeter tester too but
the el-cheeso works just fine for our
purposes.
You hook this to your battery under test.
Just before you crank up the load such that
battery voltage falls to 9V, push the 15
second timer button. Adjust load
during the 15 second interval
to maintain 9V reading. Take note of
the CURRENT delivered by the battery
at the end of 15 seconds.
Acquire this benchmark value for a new
battery. Note the value with a sharpie
on the battery case along with date.
At any later time, should the battery
perform to less than 80% (*) of new,
consider replacing the battery. Same
thing goes with capacity checks 80%
is the 'retirement' value for
batteries in TC, flight-for-hire aircraft.
(*) Of course, you CAN establish your own
benchmarks if some other numbers make
more sense for how you operate your airplane.
But pick other numbers based on understanding,
not because your trying to squeeze more
service out of the battery.
EARTHX batteries (and all other LIFePO4
batteries) are special cases. Your load
test value will probably be more than
9V . . . internal resistance of these
batteries is very low and you probably
can't load it down to 9v without
tripping internal current limits.
If you want to capcheck your EARTHX,
fire up your airplane's anticipated
endurance mode accessories and measure
the time before auto-disconnect. Make
note of that time for the new battery.
Think about replacing the battery when
those minutes fall by 25% or so.
As for DC clamp-on ammeters, they've
been around for some time. I have
a Fluke meter I bought about 20 years
ago . . . hall-effect device . . . works
mostly okay for large measurements
(10+ amps) but flakiness typical of
contemporary technology at low current
levels.
I have one like this
https://tinyurl.com/y9gb4cgs
. . . but haven't had much occasion to
exercise it's capability. It has a
ZERO read function on DC amps that
wipes out most of the variability
in the hall-sensor at low current
readings. Seems to work well. Will follow
up when I've learned more . . . but
the price/performance numbers are
certainly attractive.
Bob . . .
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blues750
Joined: 06 Jun 2015 Posts: 56
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Posted: Mon May 04, 2020 9:12 am Post subject: Re: DC clamp meter |
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"Help us out with your mission."
Hi Bob, I simply want to put a typical inflight load on the fuly charged battery and perform the below method /test as my benchmark for battery capacity check and/or replacement. When at 80% of the benchmark, replace battery. I was going to use old style truck headlight bulbs for a resistive load. Cranking capacity is not a significant concern for my style of flying operation... (famous last words?) Thanks for input and reply so far!!
From the Earth FAQ's listing...
Test Method #2 (with timer and DC current meter):
a. Fully charge the battery with an appropriate charger.
b. Turn on all electrical loads and start a timer. The same load must be used in subsequent years for accuracy.
c. Measure and record the battery’s discharge amps using a DC clamp-on current meter at the positive terminal of the battery.
d. Using the measured amps in the previous step and the battery’s nameplate rated capacity (in Ah), calculate the time to discharge the battery to 80%.
Time to Discharge 80% (Hours)=Rated Capacity in Ah * .8Measured Discharge Amps
For Example (16 Ah Rated Capacity, 5 amp measured discharge rate)
Time to Discharge 80%=16 Ah * .85= 2.56 hours
e. Terminate the test after the number of hours calculated in the previous step has expired or if the battery is over-discharged (shuts off discharge current). If the battery is still supplying power at the termination of the test, then the battery’s capacity is greater than 80%. If the battery’s capacity is greater than 80% of it rated or capable of supporting the aircraft’s emergency load for the required amount of time, then the battery has passed the test.
f. Fully charge the battery with an appropriate charger.[/i]
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nuckolls.bob(at)aeroelect Guest
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Posted: Tue May 05, 2020 8:56 am Post subject: DC clamp meter |
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At 12:12 PM 5/4/2020, you wrote:
Quote: | --> AeroElectric-List message posted by: "blues750" <den_beaulieu(at)yahoo.com>
"Help us out with your mission."
Hi Bob, I simply want to put a typical inflight load on the fuly charged battery and perform the below method /test as my benchmark for battery capacity check and/or replacement. When at 80% of the benchmark, replace battery. I was going to use old style truck headlight bulbs for a resistive load. Cranking capacity is not a significant concern for my style of flying operation... (famous last words?)
>From the Earth FAQ's listing...
Test Method #2 (with timer and DC current meter):
a. Fully charge the battery with an appropriate charger.
b. Turn on all electrical loads and start a timer. The same load must be used in subsequent years for accuracy.
c. Measure and record the battery’s discharge amps using a DC clamp-on current meter at the positive terminal of the battery.
d. Using the measured amps in the previous step and the battery’s nameplate rated capacity (in Ah), calculate the time to discharge the battery to 80%.
Time to Discharge 80% (Hours)=Rated Capacity in Ah * .8Measured Discharge Amps
For Example (16 Ah Rated Capacity, 5 amp measured discharge rate)
Time to Discharge 80%=16 Ah * .85= 2.56 hours |
If one is going to test the battery in-situ, i.e.
on the airplane with plan-b endurance loads running,
then the exact current demand is somewhat irrelevant
to the test. Just time the interval until electro-
whizzies shut down. That time represents the present
capacity-at-plan-b-load. You can do that with a
new battery to benchmark T1. The replacement
milestone would be at T0.80 of the as-new value.
You should measure or accurately calculate plan-b
loads to (1) predict plan-b endurance based on
battery specifications and (2) verify the battery's
capabilities at the time of your benchmark
test on a new battery.
You can easily measure plan-b loads by inserting
an ammeter in series with your battery lead and
turning on the plan-b compliment of electro-
whizzies. This is a good thing to do to verify
your load analysis values.
Quote: | e. Terminate the test after the number of hours calculated in the previous step has expired or if the battery is over-discharged (shuts off discharge current). If the battery is still supplying power at the termination of the test, then the battery’s capacity is greater than 80%. If the battery’s capacity is greater than 80% of it rated or capable of supporting the aircraft’s emergency load for the required amount of time, then the battery has passed the test.
f. Fully charge the battery with an appropriate charger.[/i] |
The Earth-X testing is okay but I think
overly complicated. YOUR primary interest
as the guy sitting in the left seat is
"how long will the panel stay lit up"?
Doing the in-situ test tells you what the
battery will do right now. The 80% value
is a somewhat arbitrary number established
by convention and experience with rechargeable
batteries (when a battery drops to 80% of
as new capacity, it's on the down-hill-slide
toward useless).
Your multimeter probably has a 10 amp DC
current measurement capability that can be
used to quantify your real, plan-b loads.
You don't need to buy a special instrument
for this measurement.
Bob . . .
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blues750
Joined: 06 Jun 2015 Posts: 56
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Posted: Wed May 06, 2020 5:17 pm Post subject: Re: DC clamp meter |
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Bob, I cannot imagine how to go about doing the voltmeter method with an electrical dependent engine running...hence my plan...
Once batteries are charged my normal inflight electrical load is approx 20 amps when not using pitot heat. This is consistent with my predicted load analysis. I have a dual ECU electrically dependent engine which requires approx 13 amps to keep me flying (derived from the engine manufacturer's chart). By shutting down one ECU and a few other items I can safely continue flight and recover to an airfield or suitable airstrip (day VMC) with about the same electrical load of 13 amps.
My plan was to test each battery separately with a 15 amp load (hence the need for a DC clamp meter) and see how long I got energy from the battery before the voltages dropped off below 10V (ECU/engine quitting time) or the EarthX BMS shuts down due to over discharge. As I've already got a few flying seasons on the batteries, I can only compare my discharge amp-hrs to the battery specs and then use the 80% factor for battery changeout.
Does this sound like a reasonable way to do a meaningful capacity check? It does to me, but what the heck may I be missing? Seems like the hardest thing to do will be rigging up the resistive dummy load (open for ideas) so I can consistently do the load test per battery year to year.
Thanks again for the insight and ideas!!
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gilles(at)elixir-aircraft Guest
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Posted: Wed May 06, 2020 5:41 pm Post subject: DC clamp meter |
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Le 07/05/2020 à 03:17, blues750 a écrit :
Quote: |
Bob, I cannot imagine how to go about doing the voltmeter method with an electrical dependent engine running...hence my plan...
Once batteries are charged my normal inflight electrical load is approx 20 amps when not using pitot heat. This is consistent with my predicted load analysis. I have a dual ECU electrically dependent engine which requires approx 13 amps to keep me flying (derived from the engine manufacturer's chart).
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Performing actual voltage and current measurements at cruise power would
be interesting.
It can safely be done on the ground.
FWIW,
--
Best regards,
Gilles
http://contrails.free.fr
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nuckolls.bob(at)aeroelect Guest
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Posted: Fri May 08, 2020 6:04 pm Post subject: DC clamp meter |
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Quote: | Does this sound like a reasonable way to do a meaningful capacity check? It does to me, but what the heck may I be missing? Seems like the hardest thing to do will be rigging up the resistive dummy load (open for ideas) so I can consistently do the load test per battery year to year.\ |
Okay, got a tighter box around your goal. Probably
doesn't need to be that complicated. You know your
endurance loads to a reasonable degree of accuracy.
The really cool thing about Li batteries is their
very FLAT discharge curve as a consequence of low
internal resistance. This means that energy delivered
to the terminals is relatively constant irrespective
of load. So consider getting some of these.
https://tinyurl.com/ydg62u2r
an order of 5 pcs is about 8 bux delivered to your
door. Mount 4 of these to a chunk of aluminum say
6 x 6 inches or so. .06 or more thick. Space them
out over the surface. Hook all four in parallel
to make a robust, 1.0 ohm resistor.
This resistor connected to one of your batteries
will discharge right at 12.5 amps. Time the interval
to discharge limit with this load.
Since you have quite a bit of time on these
batteries, you don't have an as-new benchmark
but you now have as-is benchmark.
Maybe the a.h. number isn't really that
useful. Rather, it's time to trip
the discharge limiter. That's pretty close
to your as-is endurance value. When
that number is below design goals, change
the battery.
Bob . . .
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racerjerry
Joined: 15 Dec 2009 Posts: 202 Location: Deer Park, NY
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blues750
Joined: 06 Jun 2015 Posts: 56
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Posted: Mon May 11, 2020 4:54 pm Post subject: Re: DC clamp meter |
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Bob, finally able to do the calculation on how you get a 1 OHM equivalent resistor out of the four resistors rated at 4 ohms in parallel along with power dissipation through the resistors...what a blast from the past! Thank you so much for the help and interest. I can't wait to get some data!
Dave (most appreciative novice experimentalist)
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nuckolls.bob(at)aeroelect Guest
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Posted: Mon May 11, 2020 7:20 pm Post subject: DC clamp meter |
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At 07:54 PM 5/11/2020, you wrote:
Quote: | --> AeroElectric-List message posted by: "blues750" <den_beaulieu(at)yahoo.com>
Bob, finally able to do the calculation on how you get a 1 OHM equivalent resistor out of the four resistors rated at 4 ohms in parallel. What a blast from the past! I'll take your word on the Power rating being suitable!! Thank you so much for the help and interest. I can't wait to get some data!
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Yup . ..
1
RT = ====================================
1 1 1 1
____ _____ _____ ______
R1 R2 R3 Rx
Rtotal equals the reciprocal of the SUM
of reciprocals of all resistors in the
array . . . no matter how many resistors.
It just so happened that your target current
worked out close to a 1-ohm load . . . so
the array of 4 x 4 ohms works nicely.
The total wattaged needed is much less than
to total ratings of thsoe four resistors.
They're offered as 100W devices . . . but
in practice, they're closer to 50W when
adequately heat-sinked. So the sum total
of the 4 is comfortably good for 200W.
You only need 13A x 13v is 169W.
This bucket-o-resistors technique is
very versatile. For example, a couple
years ago I crafted a portable, 750
watt, variable load bank for the purpose
of airborne cooling tests on alternators.
An array of 21 resistors not unlike the
ones I suggested plus a handful of components
and a fan made for a device that would
offer loads from 0 to approx 50A fan
cooled.
I've used this technique to craft load banks
up to 2800 watts (28v, 100A) . . . with
a lot more resistors and a bigger fan . . .
but knob-adjusted at the control panel.
Bob . . .
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blues750
Joined: 06 Jun 2015 Posts: 56
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Posted: Wed May 13, 2020 10:02 am Post subject: Re: DC clamp meter |
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Bob, that's pretty clever. In my case how "fancy" should I go? For connections to the load from the battery, I was thinking of simply using two leads of #10 wire with alligator clips on both ends and having an inline fuseholder on one lead with a 15A fuse. Or...do I fabricate a switched/fused platform, with ring terminals for connections, etc? User preference?
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