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When is a Good Ground Not?
November 18, 1999
Bob Nuckolls
6936 Bainbridge Road
Wichita, KS 67226-1006
Voice/Fax: 316-685-8617
E-mail: nuckolls@aeroelectric.com
When is a Good Ground Not?
Poor performance in high current carrying conductors
(especially grounds) can be difficult to diagnose. Investi-
gations into poor alternator voltage regulation or starter
performance always begin with conductors other than
grounds. Ground pathways are often overlooked as a
contributor to poor system performance . . . especially in
metal airplanes where the whole airframe is ground.
It's important to remember that for every electron that
leaves the battery another electron has to return via the
other terminal; the same currents that flow in the power
distribution wiring also flow in ground return conduc-
tors. Lets take a look at how a small resistance in
wiring and electrical system components can stack up to
trash what might otherwise be satisfactory performance
of an electrical system.
A Few Milliohms Go a Long Way
A pretty decent flooded (wet), lead-acid battery will have
an internal resistance of about 10 milliohms. It's difficult
to make a joint between any two conductors that's much
better than 0.5 milliohms per joint without welding.
Consider 2AWG wire with a resistance of .156 milliohms
per foot. In a Long-Ez the path from nose to tail can be
about 20 feet round trip so 20 x .156 = 3.22 milliohms
resistance in the wire alone. How about the contactors?
Hmmmmm . . . two contacts in series held together by an
energized electromagnet might be 1 milliohm per contact
so there's another 4 milliohms total. Add 'em up . . .
Battery resistance . . . . . . . . . . . 10.0 milliohms
2 Contactors . . . . . . . . . . . . . . .
4.0 milliohms
15' of 2AWG wire . . . . . . . . . . . 3.2 milliohms
Bolted Joints (4 wire
segments with 2 joints
at 0.5 milliohms each) . . . . . 8.0 milliohms
____________
Total resistance . . . . . . . . . . . . . 25.2 milliohms
It is difficult to imagine how so small a resistance can
make any difference. Consider that for all but the small-
est engines, a starter can easily draw over 200 amps!
Ohm's law says that for every ampere of current pushed
through 1 ohm of resistance, there will be 1 volt of drop
across the resistor or Volts = Amps x Ohms. 25.2 Milli-
ohms time 200 Amps equal 5040 Millivolts or 5.04 volts of
drop. If we started with a 12.5 volt battery, we'll now see
about 12.5 minus 5.04 or 7.46 volts at the starter terminals.
We've lost over 1/3 of our cranking energy in the trip from
battery to motor! On a cold morning, the engine is stiffer
and battery resistance goes up. Just when the engine would
benefit from more cranking energy, the battery's ability to
deliver it lessens.
The resistance of wire, contactors and battery are fixed, we
have no control over them and they are never zero. Also
note that bolted joints make up a significant percentage of
total drop. Even minimizing wire length has a rather small
effect compared to reduction in number of bolted joints.
Numbers in real life may vary quite a bit from those Ive
used in the example. The point to be made is that while the
resistance values were discussing are tiny; pushing
electrons through the system at 200+ amps makes every
milliohm count. Some care in selection and assembly of
parts can reduce the over all resistance numbers.
In Figure 1, I've illustrated the most important wires in the
airplane. The first wire I install is from battery minus to a
firewall ground block thru-bolt.. The second wire runs from
ground block thrubolt to crankcase. For canard-pushers
with forward batteries, a instrument panel ground block is
wired to battery minus lead in the nose as shown. Ground
points for equipment in the rear are provided with a second
ground block mounted on one or both sides of the firewall.
Some of the worst performing starters are found on metal
airplanes where battery ground lead is bonded locally to
airframe. Engine is bonded to mount by jumpers around the
vibration isolators and the mount is "grounded" to airframe
through its mounting bolts. New airframes and other
structures holding engines on are pretty good substitutes for
wires when new. A few decades of age and improper
maintenance can drive ground path resistance up dramati-
cally from that which left the factory. Figure 1. The Most Important Wires in the Airplane.
Engine mounts should be used for attaching engines to
airplanes. They are not good substitutes for an electrical
bond strap connecting the crankcase to a firewall ground
stud.. This grounding architectures I recommend here
optimizes engine cranking performance and minimizes
ground loop problems which may degrade alternator
voltage regulation, cause noises in an audio system or
radios and affect the accuracy or stability of engine
instruments.
If the battery and engine are on opposite ends of a
composite airplane it's important to run battery (+) and
(-) cables right next to each other as they traverse the
cockpit and instrument panel areas. Tie-wrap them
together every 6 inches or so. Some Ez builders have run
(+) and ground down opposite sides of the fuselage with
some bizarre results.
Several kit manuals suggest that a couple of studs on a
firewall ground block are sufficient for termination of all
system grounds. This is poor practice. As single stud is
responsible for many grounds . . . a broken bolt or loose
nut causes problems in multiple systems. The ground
block I've illustrated is a special product I designed and
asked B&C Specialty products to manufacture. 0.25"
wide, fast-on tabs are sweat soldered to a piece of sheet
brass. A 5/16" BRASS stud is used to carry a good
electrical ground from the cockpit area to the engine
compartment. There are sufficient ground points to give
each system all the structurally independent grounds it
needs without having to share. I highly recommend its use.
Minimizing high-current path resistance has another
benefit: Many airplane designs don't need a lot of battery
capacity but some builders find that a larger battery (lower
internal resistance) improves cranking performance. A
number of single-engine Pipers have 35 ampere-hour
batteries in the tail . . they didn't need the extra capacity but
the lower internal resistance improved cold weather
cranking operations. B&C holds STCs for replacing a 35
ampere-hour, 30 pound battery in many Pipers with a 25
ampere-hour, RG (recombinant gas) battery. The new
battery has a 5 milliohm internal resistance and 22.5
pounds weight. Cranking performance is greatly improved
in spite of the new battery's small and lighter package.
Keeping wiring and component resistance down allows a
builder to consider very light batteries that might otherwise
be unsuitable if theyre sandbagged with unnecessarily high
cranking path resistance.
Introducing the 4-Wire Ohmmeter
Measuring the quality of any low resistance conductor path
would appear to be difficult. Common multimeters do not
read out in fractions of milliohms. A few years ago I was
investigating an accident where electrical ground Figure 2. Poor Mans 4-Wire Milliohmmeter
.
Figure 3. 4-Wire Ohmmeter Schematic.
conductivity was in question; measurements in the milli-
ohms were need. I visited a local Radio Shack and
bought two digital multimeters. One needed a capability
of reading current on the order of 10 amperes or more.
The other was for reading millivolts; hopefully to the
nearest 0.1 millivolt.
I also purchased a D-size alkaline cell, some 18 gauge
lamp cord, test probes and banana plugs. The man
behind the counter loaned me a soldering iron and I built
the rig shown in Figures 2 and 3; a poor-man's 4-wire
milliohm meter. You may be tempted to construct this
fixture using spring-loaded battery holder for the D-cell.
I recommend soldering leads right to the cell; battery
holders are not designed to carry the 5-10 amp currents
that will flow while this text fixture is in use. Clean the
cell end areas to be soldered. Get on and off quick with
a hot iron.
When I touch the two probes together I've placed a dead
short on the D-cell . . . well, almost a dead short.
Obviously, the cell has an internal impedance which
limits the current that a shorted cell will deliver. The
wire between cell and probes has some resistance too. As
it turned out, when the two probes were touched together,
multimeter M1 indicated about 7 amps.
Figure 3 shows how one multimeter is set up to measure
the voltage between the two probes through a path that is
independent of the D-cell current
path. The operative feature here is
that no voltage drop will occur along
the voltage sense leads and multimet-
er M2 will read the voltage between
the two probes irrespective of the
voltage dropped along the D-cells
current path.
W h e n m a k i n g r e s i s t a n c e
measurements between a tailcone
mounted battery and a nose mounted
engines crankcase, the task may
require two people. The accident case
I was working questioned the qu