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EFIS backup battery switch wiring

 
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messydeer



Joined: 13 Feb 2006
Posts: 214
Location: Bellingham, WA

PostPosted: Tue Nov 17, 2009 10:26 am    Post subject: EFIS backup battery switch wiring Reply with quote

Hello Smile

I have an MGL Enigma EFIS and will put in a backup battery. In regular operation, both the main and backup battery are to be wired to the EFIS. The Enigma automatically switches to backup when it senses a main battery low voltage.

I was thinking of maybe some wiring of a 2-10 that would do the following:

Down position: main buss to EFIS.

Middle position: backup battery to EFIS (for backup battery check)

Up position: both batteries to EFIS.

Or maybe just a two position switch, one position would be for both batteries, the other just to the backup. The backup check position could be a momentary on, I suppose, that just takes the main battery offline. Hold it in this position and see if the EFIS still works, then release.


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messydeer



Joined: 13 Feb 2006
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Location: Bellingham, WA

PostPosted: Tue Nov 17, 2009 10:47 am    Post subject: Re: EFIS backup battery switch wiring Reply with quote

Well, I got one possibility figured out using a 2-10. Figure attached.

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Enigma EFIS backup switch wiring with 2-10.pdf
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edleg



Joined: 11 Jun 2009
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PostPosted: Tue Nov 17, 2009 11:47 am    Post subject: Re: EFIS backup battery switch wiring Reply with quote

With one switch you are putting all your eggs (and faith) in a single point of failure. What use is having emergency backup power if you can not use it if the only switch is broken?

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PostPosted: Tue Nov 17, 2009 12:25 pm    Post subject: EFIS backup battery switch wiring Reply with quote

Dan,
Turn the master on, turn the EFIS on . Turn the master off. If EFIS remains on the systemn works.
Don VS RV7 flying
---- messydeer <messydeer(at)yahoo.com> wrote:
Quote:


Well, I got one possibility figured out using a 2-10. Figure attached.

--------
Dan




Read this topic online here:

http://forums.matronics.com/viewtopic.php?p 73310#273310




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http://forums.matronics.com//files/enigma_efis_backup_switch_wiring_with_2_10_162.pdf









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messydeer



Joined: 13 Feb 2006
Posts: 214
Location: Bellingham, WA

PostPosted: Tue Nov 17, 2009 12:56 pm    Post subject: Re: EFIS backup battery switch wiring Reply with quote

Turns out I had the wiring to the EFIS wrong. There are separate terminals for the backup and main power inputs, so I've redrawn it. It looks like if I forgot to turn off the EFIS switch, my backup battery would run dead. But I suppose I otta notice that my screen is still powered up. I would think that would be pretty obvious.

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Enigma EFIS backup switch wiring with 2-10.pdf
 Description:

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 Filename:  Enigma EFIS backup switch wiring with 2-10.pdf
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PostPosted: Tue Nov 17, 2009 3:55 pm    Post subject: EFIS backup battery switch wiring Reply with quote

Quote:
I have an MGL Enigma EFIS and will put in a backup battery. In
regular operation, both the main and backup battery are to be wired
to the EFIS. The Enigma automatically switches to backup when it
senses a main battery low voltage.

I was thinking of maybe some wiring of a 2-10 that would do the
following . . .


What does the manufacturer of the EFIS system
recommend?
Bob . . .

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messydeer



Joined: 13 Feb 2006
Posts: 214
Location: Bellingham, WA

PostPosted: Tue Nov 17, 2009 4:28 pm    Post subject: Re: EFIS backup battery switch wiring Reply with quote

Thanks, Bob.

From the manual:

"...One power switch for the main incoming 12 or 24 V feed (switch in positive supply lead),
another for the backup battery.
In flight, both switches would be “on” allowing the charging of the backup battery.
Preflight check would involve switching main power on, then battery power on. Check of
battery power would involve switching main power off and verifying that Enigma continues
to operate. Voltage on the backup battery should be measured by means of the backup
voltage readouts which can be placed on any display..."

Imaged referred to attached.


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MGL Enigma Odyssey installation.bmp
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MGL Enigma Odyssey installation.bmp



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edleg



Joined: 11 Jun 2009
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PostPosted: Tue Nov 17, 2009 7:11 pm    Post subject: Re: EFIS backup battery switch wiring Reply with quote

In simple terms... if the backup battery is not on its own switch it won't charge. Two switches is simple. Trying to find a special switch to do all things at once leaves you with a non-common fix if it fails away from your home airport.....

Two switches lets you troubleshoot power problems, and lets the EFIS be powered fully during a voltage drop, like during an engine start.


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messydeer



Joined: 13 Feb 2006
Posts: 214
Location: Bellingham, WA

PostPosted: Tue Nov 17, 2009 7:36 pm    Post subject: Re: EFIS backup battery switch wiring Reply with quote

Thanks, E., for bringing up the issue of single point of failure. Hadn't thought about that, which makes me ask some questions about DPDT vs SPST switches.

Looking at the schematic of a DPDT switch it looks like there are two circuits, an upper and a lower. Their terminals are separate but contained in the same housing. They also use the same lever and the mechanism the lever connects to that makes and brakes the contacts.

If the only way a switch failed was through these shared components, then a DPDT would have the same reliability as a SPST, so there would be a single point of failure.

And if DPDT's never failed at these shared components, then having one DPDT would be just as reliable as having two SPST's, and there wouldn't be a single point of failure.

I'm sure the truth lies somewhere between these two extremes. If it turns out that a DPDT has 90% of the reliabilty as two SPST's, I might stick with just one DPDT. If it has only 20% of the reliabilty of two SPST's, I might consider going with two switches.


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PostPosted: Tue Nov 17, 2009 8:09 pm    Post subject: EFIS backup battery switch wiring Reply with quote

The issue is not so much about what the relative reliability is. The
issue is that if the DPDT switch fails you may not be able to connect to
either source of electrons. If one of the SPST switches fails, you
always have the other one.

Dick Tasker

messydeer wrote:
Quote:


Thanks, E., for bringing up the issue of single point of failure. Hadn't thought about that, which makes me ask some questions about DPDT vs SPST switches.

Looking at the schematic of a DPDT switch it looks like there are two circuits, an upper and a lower. Their terminals are separate but contained in the same housing. They also use the same lever and the mechanism the lever connects to that makes and brakes the contacts.

If the only way a switch failed was through these shared components, then a DPDT would have the same reliability as a SPST, so there would be a single point of failure.

And if DPDT's never failed at these shared components, then having one DPDT would be just as reliable as having two SPST's, and there wouldn't be a single point of failure.

I'm sure the truth lies somewhere between these two extremes. If it turns out that a DPDT has 90% of the reliabilty as two SPST's, I might stick with just one DPDT. If it has only 20% of the reliabilty of two SPST's, I might consider going with two switches.

--------
Dan


Read this topic online here:

http://forums.matronics.com/viewtopic.php?p 73392#273392




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khorton01(at)rogers.com
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PostPosted: Tue Nov 17, 2009 8:49 pm    Post subject: EFIS backup battery switch wiring Reply with quote

What are the consequences of failure of both poles in that switch,
given how you will operate the aircraft (day/night and VFR/IFR) and
the backups you have installed? If you are certain that you will be
able to safely get the aircraft on the ground with an acceptable
workload, then the potential single point failure is acceptable.

Kevin Horton

Sent from my iPod

On 2009-11-17, at 10:36 PM, "messydeer" <messydeer(at)yahoo.com> wrote:

Quote:

>

Thanks, E., for bringing up the issue of single point of failure.
Hadn't thought about that, which makes me ask some questions about
DPDT vs SPST switches.

Looking at the schematic of a DPDT switch it looks like there are
two circuits, an upper and a lower. Their terminals are separate but
contained in the same housing. They also use the same lever and the
mechanism the lever connects to that makes and brakes the contacts.

If the only way a switch failed was through these shared components,
then a DPDT would have the same reliability as a SPST, so there
would be a single point of failure.

And if DPDT's never failed at these shared components, then having
one DPDT would be just as reliable as having two SPST's, and there
wouldn't be a single point of failure.

I'm sure the truth lies somewhere between these two extremes. If it
turns out that a DPDT has 90% of the reliabilty as two SPST's, I
might stick with just one DPDT. If it has only 20% of the reliabilty
of two SPST's, I might consider going with two switches.

--------
Dan


Read this topic online here:

http://forums.matronics.com/viewtopic.php?p 73392#273392




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jay(at)horriblehyde.com
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PostPosted: Tue Nov 17, 2009 10:36 pm    Post subject: EFIS backup battery switch wiring Reply with quote

There is one quite important thing to note, no matter how one wires the
switches (I used two DPST switches in the Sling - one for the power to the
Enigmas and one to the backup batteries)- that is that the backups will not
charge unless the voltage to them is sufficiently high. Obvious of course,
but where this becomes a problem is if you have a diode between your main
bus and the e-bus. You get a 0.7v drop across it and then there are some
voltage drops inside the Enigma and the backup batt gets a voltage of
between 12.5 -13v.

To solve this we now run the aircraft with the e-bus alt feed permanently
on, which boosts the e-bus voltage back up sufficiently to charge the backup
battery.

Jay

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PostPosted: Wed Nov 18, 2009 7:04 am    Post subject: EFIS backup battery switch wiring Reply with quote

When crafting your project's electrical system architecture
it would be helpful to be aware of the marketplace for
to which avionics suppliers deliver most of their products.
99.9% of all light aircraft built feature an architecture
that has not changed materially in 40+ years when the
avionics bus and master switch was added to protect
transistors from will-o'-the-wisp spikes.

Those same aircraft are largely owned and operated
by individuals who know little if any more about their
airplanes than they do about their cars. Further, even
if they knew and understood a great deal about them,
they would not be permitted by regulation to make
any meaningful improvements upon them. Phrases
like "failure tolerance", "meeting design goals",
and "artful preventative maintenance for maintenance
of system reliability" might just as well be spoken
in Swahili.

Now we have the starry-eyed entrepreneur who
tailors a product for best-fit into spam-can/
FAA-trained aviation. Not only is the product marketed
and sold as the greatest accessory since sliced bread,
it may include a suite of "back up" features designed
to ward of a host of failures uncomfortable to contemplate.

Internal back up batteries are popular. Keep in
mind that internal batteries MIGHT make sense in
the spam-can/FAA-trained world of flight . . . but
we're OBAM aviation. We can craft power sources that
are exceedingly robust. In fact so robust that
flight-critical systems are more likely to become
unavailable due to internal failure than for lack of
ship's power.

Staying true to our design goals for failure tolerance:
If your are PLANNING for any accessory to be critical
to comfortable completion of flight, then your plan-B
for failure of that device needs to go BEYOND any
need for ship's power. If you have a system like Z-13/8
(and assuming further that you exercise due diligence for
battery maintenance) then the probability of the E-bus
ever becoming un-powered in flight is on the same
order as prop bolt failure.

At the same time, probability of some flight critical
system going down for for reasons OTHER than power
failure is decidedly higher.

With that reasoning in mind I'll suggest that fussing
over the optimum back-up battery installation for any
accessory is a distraction from the real task of
crafting a failure tolerant system.

If it were my airplane, I'd go for Z-13/8, ditch the
internal back-up batteries and figure out how I'm
going to comfortably deal with a failure of the LEDs
that light up the screen or a rate sensor that goes
south, etc. etc.
Bob . . .

---------------------------------------
( It's MATRONICS FUND RAISER MONTH! )
( Do your part to keep this marvelous )
( tool sharp and available to all our )
( brothers in the OBAM aviation )
( community. )
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