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trigo(at)mail.telepac.pt Guest
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Posted: Fri Aug 29, 2008 7:05 am Post subject: Avionics Back-Up Power |
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Bob and the group
Since I had to put some weight in the tail of my RV-9A, I decided to install a battery as back-up power to some avionics, the EFIS, the COMM Radio and the Transponder.
My GRT EFIS has 2 power inputs, which are internally controlled (EFIS uses the electrons from the highest source), so this is easy to wire.
However, the Radio (SL-30) and the Transponder (GTX-330) only have 1 power input, therefore the question:
- How should I wire power, both from Main Battery and Back-Up Battery, to the COMM Radio and the Transponder?
Help appreciated
Carlos
[quote][b]
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nuckolls.bob(at)cox.net Guest
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Posted: Fri Aug 29, 2008 7:28 am Post subject: Avionics Back-Up Power |
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At 04:04 PM 8/29/2008 +0100, you wrote:
Quote: | Bob and the group
Since I had to put some weight in the tail of my RV-9A, I decided to
install a battery as back-up power to some avionics, the EFIS, the COMM
Radio and the Transponder.
My GRT EFIS has 2 power inputs, which are internally controlled (EFIS uses
the electrons from the highest source), so this is easy to wire.
However, the Radio (SL-30) and the Transponder (GTX-330) only have 1 power
input, therefore the question:
- How should I wire power, both from Main Battery and Back-Up Battery,
to the COMM Radio and the Transponder?
|
How big a battery is it? How many batteries does the airplane
carry already . . . in other words do you already have an
AUX battery?
Bob . . .
----------------------------------------)
( . . . a long habit of not thinking )
( a thing wrong, gives it a superficial )
( appearance of being right . . . )
( )
( -Thomas Paine 1776- )
----------------------------------------
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trigo(at)mail.telepac.pt Guest
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Posted: Fri Aug 29, 2008 8:18 am Post subject: Avionics Back-Up Power |
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Quote: | >
>Since I had to put some weight in the tail of my RV-9A, I decided to
>install a battery as back-up power to some avionics, the EFIS, the COMM
>Radio and the Transponder.
>
>
>My GRT EFIS has 2 power inputs, which are internally controlled (EFIS uses
>the electrons from the highest source), so this is easy to wire.
>
>However, the Radio (SL-30) and the Transponder (GTX-330) only have 1 power
>input, therefore the question:
>
>
> - How should I wire power, both from Main Battery and Back-Up Battery,
> to the COMM Radio and the Transponder?
How big a battery is it? How many batteries does the airplane
carry already . . . in other words do you already have an
AUX battery?
Bob . . .
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I don't know exactly, because I still don't know the exact weight I need for W & B, but I am planning for a battery around 10Ah
I do have 2 other batteries, Main and AUX, since my engine is an electron-dependant Subaru.
Carlos
[quote][b]
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nuckolls.bob(at)cox.net Guest
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Posted: Sat Aug 30, 2008 5:06 am Post subject: Avionics Back-Up Power |
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> How big a battery is it? How many batteries does the airplane
> carry already . . . in other words do you already have an
> AUX battery?
>
> Bob . . .
I don't know exactly, because I still don't know the exact weight I need
for W & B, but I am planning for a battery around 10Ah I do have 2 other
batteries, Main and AUX, since my engine is an electron-dependant Subaru.
Hmmmm . . . this is a bit problematic. Battery installation
philosophy in A/C calls for local disconnect (battery contactor
or relay). We also need to size the wiring so expected loads
and recharge currents do not experience too large voltage
drop. Finally, all wires need to be properly protected against
faults.
A 10 a.h. battery is good for about 10# of 'ballast'. If
you went further back on the airframe, could you get down
to say 5# of ballast? The reason for asking is that my present
image of this system suggests a plastic battery relay (one
of those 70A plastic things). A local fuse (use MAXI fuse
holder to make the battery(+) to battery relay jumper. Run
the battery feeder forward to the battery bus that runs
the panel during alternator out operations. We don't
want to leave that feeder hot while the airplane is
shut down . . . you need another relay at the forward
end of the feeder too and protect that end with another
MAXI fuse. The wire probably wants to be 10AWG and the
fuses at both ends are MAX30. Now you need a third battery
switch that closes both relays during flight operations.
This is electrically messy . . . not much better from
the pilot workload perspective either. As I mentioned
earlier, it might be better to minimize total added weight
by moving it as far back on the airframe as possible . . .
an letting it be dead-weight thus avoiding the bow-
of-spaghetti-wiring.
Bob . . .
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trigo(at)mail.telepac.pt Guest
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Posted: Sat Aug 30, 2008 6:48 am Post subject: Avionics Back-Up Power |
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Bob
Thanks for your explanation and suggestions.
Anyway, which is the reason you say "we don't want to leave that feeder hot while the airplane is shut down” ?
If it’s not so important, 2 relays and 1 switch could be avoided, and pilot workload as well…
Carlos
Quote: | -----Original Message-----
From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-
server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III
Sent: sábado, 30 de Agosto de 2008 14:05
To: aeroelectric-list(at)matronics.com
Subject: RE: Avionics Back-Up Power
--> AeroElectric-List message posted by: "Robert L. Nuckolls, III"
<nuckolls.bob(at)cox.net>
> How big a battery is it? How many batteries does the airplane
> carry already . . . in other words do you already have an
> AUX battery?
>
> Bob . . .
I don't know exactly, because I still don't know the exact weight I need
for W & B, but I am planning for a battery around 10Ah I do have 2 other
batteries, Main and AUX, since my engine is an electron-dependant Subaru.
Hmmmm . . . this is a bit problematic. Battery installation
philosophy in A/C calls for local disconnect (battery contactor
or relay). We also need to size the wiring so expected loads
and recharge currents do not experience too large voltage
drop. Finally, all wires need to be properly protected against
faults.
A 10 a.h. battery is good for about 10# of 'ballast'. If
you went further back on the airframe, could you get down
to say 5# of ballast? The reason for asking is that my present
image of this system suggests a plastic battery relay (one
of those 70A plastic things). A local fuse (use MAXI fuse
holder to make the battery(+) to battery relay jumper. Run
the battery feeder forward to the battery bus that runs
the panel during alternator out operations. We don't
want to leave that feeder hot while the airplane is
shut down . . . you need another relay at the forward
end of the feeder too and protect that end with another
MAXI fuse. The wire probably wants to be 10AWG and the
fuses at both ends are MAX30. Now you need a third battery
switch that closes both relays during flight operations.
This is electrically messy . . . not much better from
the pilot workload perspective either. As I mentioned
earlier, it might be better to minimize total added weight
by moving it as far back on the airframe as possible . . .
an letting it be dead-weight thus avoiding the bow-
of-spaghetti-wiring.
Bob . . .
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[quote][b]
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nuckolls.bob(at)cox.net Guest
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Posted: Sat Aug 30, 2008 1:35 pm Post subject: Avionics Back-Up Power |
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At 03:47 PM 8/30/2008 +0100, you wrote:
Quote: | Bob
Thanks for your explanation and suggestions.
Anyway, which is the reason you say "we don't want to leave that feeder
hot while the airplane is shut down ?
If it s not so important, 2 relays and 1 switch could be avoided, and
pilot workload as well&
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It's just not done (at least in the TC aircraft world) both for maintenance
and crash safety. How would you propose to wire it?
Bob . . .
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trigo(at)mail.telepac.pt Guest
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Posted: Sun Aug 31, 2008 8:49 am Post subject: Avionics Back-Up Power |
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Quote: | --> AeroElectric-List message posted by: "Robert L. Nuckolls, III"
<nuckolls.bob(at)cox.net>
At 03:47 PM 8/30/2008 +0100, you wrote:
>Bob
>
>Thanks for your explanation and suggestions.
>
>
>
>Anyway, which is the reason you say "we don't want to leave that feeder
>hot while the airplane is shut down ?
>
>If it s not so important, 2 relays and 1 switch could be avoided, and
>pilot workload as well&
It's just not done (at least in the TC aircraft world) both for maintenance
and crash safety. How would you propose to wire it?
Bob . . .
|
I am thinking in installing the battery in the tail deck (under the RV-9A tail fairing), in order to obtain the longest arm to help with the Balance of the aircraft.
The (-) terminal will be connected to a local Ground (which is the same I used for the tail light), and the (+) terminal connected to a 16A fuse located near the battery. (Is this fuse adequate to protect the wire and the battery from any inadvertent short along the hot wire?)
By the way, regarding your observation that the wire should not be hot after shutdown, because of maintenance and crash safety, my humble opinion is that, in case of maintenance it is easy to disconnect the battery or pull out the fuse, and in case of crash I do have many hot wires around…
From the fuse I will run an AWG#14 wire to a buss behind the instrument panel. Actually I’m planning this “buss” to be the “out” terminal of a diode, and I am thinking to connect the Main Battery to the “In” terminal of the Diode, to charge the Back-Up Battery.
From that “buss” (the “out” terminal of the diode) I would run wires to each of the Avionics to be fed with back-up power.
And that’s where I come back to my initial question:
How do I wire from this back-up “buss”, which is permanently hot, to each of the Avionics (Comm Radio and Transponder) which only have one power input?
I am prepared to be technically fustigated but please be gentle….
Carlos
[quote][b]
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nuckolls.bob(at)cox.net Guest
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Posted: Sun Aug 31, 2008 4:51 pm Post subject: Avionics Back-Up Power |
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I am thinking in installing the battery in the tail deck (under the RV-9A
tail fairing), in order to obtain the longest arm to help with the Balance
of the aircraft.
The (-) terminal will be connected to a local Ground (which is the same I
used for the tail light), and the (+) terminal connected to a 16A fuse
located near the battery. (Is this fuse adequate to protect the wire and
the battery from any inadvertent short along the hot wire?).
Sure, fuses are fast and tend to limit energy in
the fault to the lowest practical values.
By the way, regarding your observation that the wire should not be hot
after shutdown, because of maintenance and crash safety, my humble opinion
is that, in case of maintenance it is easy to disconnect the battery or
pull out the fuse, and in case of crash I do have many hot wires around…
If this meets your design goals, then go for it!
From the fuse I will run an AWG#14 wire to a buss behind the instrument
panel. Actually I’m planning this “buss” to be the “out” terminal of a
diode, and I am thinking to connect the Main Battery to the “In” terminal
of the Diode, to charge the Back-Up Battery.
From that “buss” (the “out” terminal of the diode) I would run wires to
each of the Avionics to be fed with back-up power.
And that’s where I come back to my initial question:
How do I wire from this back-up “buss”, which is permanently hot, to each
of the Avionics (Comm Radio and Transponder) which only have one power input?
Okay, you already have two batteries and you've
suggested that the always hot wire does not violate
your design goals. You've also stated a desire not
to add switches.
I am prepared to be technically fustigated but please be gentle….
Not a problem. If I understand your design goals
accurately, then how about simply adding the second
battery in parallel to the battery that is already
tasked with running the panel when the alternator is
off line. Fuses at both ends protects the wire,
minimized parts count and avoids voltage drops
associated with diodes.
There's much M-Squared (mythology and misunderstanding)
about paralleling batteries. It is true that any number
of batteries may be paralleled for the purpose of
charging them on a constant voltage source. All
batteries will accept what ever energy they are capable
of holding. Any number of batteries may be paralleled
for the purpose of discharging them and aside from
shorted-cell failures (exceedingly rare in RG batteries)
all paralleled batteries will deliver all their contained
energy to the load irrespective of their size or condition.
Energy storage abilities of the tail-battery will
be seamlessly added to those of the existing panel-
battery if you simply parallel them.
For the purposes of supporting good recharging times
on the tail battery and minimizing voltage drop on that
long run, I'll suggest 10AWG wire and 20A MAXI fuses at both
ends.
Bob . . .
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mrspudandcompany(at)veriz Guest
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Posted: Mon Sep 01, 2008 8:45 am Post subject: Avionics Back-Up Power |
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Hmmmm . . . this is a bit problematic. Battery installation
philosophy in A/C calls for local disconnect (battery contactor
or relay). We also need to size the wiring so expected loads
and recharge currents do not experience too large voltage
drop. Finally, all wires need to be properly protected against
faults.
Bob . . .
Bob,
Quote: | From one of your recent postings, you mentioned that battery install
philosophy calls for a local disconnect. In the Z19RB the wires off the
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busses at the 2 batteries are always hot. Are you saying that the fat wires
must be short or disconnected and it is OK to have small fused wires, always
hot going to the instrument panel and elsewhere?
Thanks,
Roger
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trigo(at)mail.telepac.pt Guest
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Posted: Mon Sep 01, 2008 10:05 am Post subject: Avionics Back-Up Power |
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Bob
As usual you've been very useful.
Thanks for your help
Carlos
[quote] --
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wilenius(at)sympatico.ca Guest
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Posted: Tue Sep 02, 2008 5:11 am Post subject: Avionics Back-Up Power |
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Carlos,
You've probably thought of this but ... could you not move the 2nd battery backwards into the tail? Too much W&B shift?
regards,
Dave
[quote] --
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trigo(at)mail.telepac.pt Guest
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Posted: Tue Sep 02, 2008 5:42 am Post subject: Avionics Back-Up Power |
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Hi Dave
I did thought of that but
1 - my Aux Batt is also an Odissey PC625 which doesn’t fit under the tail fairing, and if I decided to put it somewhere between the baggage area and the tail tip, I would not be able to service/replace it
2 – I need the Aux battery to be an exclusive back-up to my electron-dependant engine, in case of alternator death and Main Battery is out of electrons
I know that 3 batteries look really overkill, mainly to Total Weight ….
Thanks anyway
Carlos
From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Dave Wilenius
Sent: terça-feira, 2 de Setembro de 2008 14:09
To: aeroelectric-list(at)matronics.com
Subject: RE: AeroElectric-List: Avionics Back-Up Power
Carlos,
You've probably thought of this but .. could you not move the 2nd battery backwards into the tail? Too much W&B shift?
regards,
Dave
[quote]
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