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Z-14 extrapolation

 
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CBarber(at)TexasAttorney.
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PostPosted: Fri Dec 26, 2008 1:48 am    Post subject: Z-14 extrapolation Reply with quote

Pardon my sophmoric ignorance on this question (sophmore = wise fool) but I
have installed my Z-14 system in my Velocity with a Mazda Rotary. I am
using two standard/stock alternators for this engine rated at 80 amps each.
The Z drawing uses two 40 amp alternators and mostly 20 awg wire. Do I need
to increase the wire size to perhaps 10 awg for my larger alternators? This
is becoming an issue as after finally seeming to get my system to "work"
mostly properly after having my EE friend come out and figure out some basic
switch functioning that I missed I am having my two Bat circuit breakers
trip whenever the engine is running and the crossover toggle is in the NON
crossover mode.

My friend, Blain (who formed and owns the company who supplies air
conditioner units for smaller airplanes such as Cirus, Moody,
Columbia/Cessna and now developing for the EXP market, namely Velocity) is
very versed in electrics but was unable to stick around once this issue came
up. He had already spent the day helping me get things right and had a
family to tend to for the holidays. He did suggest that I may need to change
the 5 amp CB to 7.5 but cautioned to find out more before going too much
further by simply adding higer CB's ect.

Back to my problem. As mentioned, when in the "crossover mode", ie both
alternators acting together the CB's do NOT trip. However, when I put the
toggle in the center position (from down) having the systems act
indipendently, both trip. It happens only when the engine is running thus
the alternator, well, alternating...so to speak. I did change to the 7.5
amp CB's but when I tested it tonight, they both tripped as well. My
thought is since I used the 20 awg wire as in the Z drawing, but am using
higher output alternators that my system is not up to the task and that I
may need to beef things up with larger wire. Again, pardon my
ingonrance...even though the fog lifts a bit every day.

So, thoughts, concerns, insight???? All is appreciated.

Thank you.

All the best,

Chris Barber
Houston
www.LoneStarVelocity.com


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nuckolls.bob(at)aeroelect
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PostPosted: Fri Dec 26, 2008 7:04 am    Post subject: Z-14 extrapolation Reply with quote

At 03:45 AM 12/26/2008, you wrote:
Quote:

<CBarber(at)texasattorney.net>

Pardon my sophmoric ignorance on this question (sophmore = wise
fool) but I have installed my Z-14 system in my Velocity with a
Mazda Rotary. I am using two standard/stock alternators for this
engine rated at 80 amps each. The Z drawing uses two 40 amp
alternators and mostly 20 awg wire. Do I need to increase the wire
size to perhaps 10 awg for my larger alternators? This is becoming
an issue as after finally seeming to get my system to "work" mostly
properly after having my EE friend come out and figure out some
basic switch functioning that I missed I am having my two Bat
circuit breakers trip whenever the engine is running and the
crossover toggle is in the NON crossover mode.

The Z-figures are to illustrate architectures and
are not intended to drive alternator size, wire
sizes, fuse/breaker sizes. Nor are they intended
to drive the selection of what devices are fed
from which bus.

Quote:
My friend, Blain (who formed and owns the company who supplies air
conditioner units for smaller airplanes such as Cirus, Moody,
Columbia/Cessna and now developing for the EXP market, namely
Velocity) is very versed in electrics but was unable to stick around
once this issue came up. He had already spent the day helping me
get things right and had a family to tend to for the holidays. He
did suggest that I may need to change the 5 amp CB to 7.5 but
cautioned to find out more before going too much further by simply
adding higer CB's ect.

The very FIRST thing you do in crafting an
electrical system is make a list of every device
that needs DC power to function and you decide
what that device's position is in the hierarchy
of necessity. If it's functionality is highly
desirable for comfortable completion of flight,
then you have TWO of those devices fed from
separate power sources. Design goals for achieving
comfortable termination of flight after some
component failure are outlined in Chapter 17
of the 'Connection.

Next you select an architecture that mitigates
the effect on outcome of flight for having lost
one of the devices. Unless you plan on boring
long holes in the most marginal kinds of weather
AND you're planning on full-up capability of
flight in IMC on both sides of the panel, it's
not clear that the features offered by Z-14 is
really all that useful to you.

However, if you're already a long way down that
path, so be it.

Have you conducted a load analysis on your proposed
system and filled out forms like:
http://www.aeroelectric.com/PPS/Load_Analysis/Blank_Form.pdf

Fill out one sheet for each bus in your proposed
design with the goal of deducing what your electrical
system load are for each flight condition AND insuring
separate power sources for systems that back each other
up.

Or you can take advantage of the load analysis exercises
conducted by a number of List members and offered in
Excel spread sheets. You can download those for study
or modification to your needs in this director from
my website:

http://www.aeroelectric.com/PPS/Load_Analysis

After ALL the electrico-whizzies in your airplane
have been identified, quantified and assigned functionality,
then you pick fuse/breakers and wire sizes to accomModate
the needs of each system.

Quote:
Back to my problem. As mentioned, when in the "crossover mode", ie
both alternators acting together the CB's do NOT trip. However,
when I put the toggle in the center position (from down) having the
systems act indipendently, both trip. It happens only when the
engine is running thus the alternator, well, alternating...so to
speak. I did change to the 7.5 amp CB's but when I tested it
tonight, they both tripped as well. My thought is since I used the
20 awg wire as in the Z drawing, but am using higher output
alternators that my system is not up to the task and that I may need
to beef things up with larger wire. Again, pardon my
ingonrance...even though the fog lifts a bit every day.

So, thoughts, concerns, insight???? All is appreciated.

There are no positions of switches in Z-14 or
any other Z-figure that would cause a breaker
to trip. The cross-feed contactor is there to
(1) PERMIT running both sides from one alternator
should one alternator become inoperable and (2)
using both batteries to crank the engine. But
if the crossfeed is closed during normal operations,
no untoward behaviors should be expected. One
alternator (with the higher voltage setting) will
hog the load but no breakers will pop.

I'm not sure of the 20AWG wire reference. Wires
this small are used in power distribution and
control downstream of the appropriately sized
fuse or breaker. The wire is selected to meet
requirements for carrying current in that particular
task and the PROTECTED by the appropriate size
fuse or breaker.

If you've strung a lot of 20AWG wire into your
airplane without having evaluated each of those
wires with respect to their current carrying
function, then you've not conducted the load
analysis exercise suggested above.

Bob . . .


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