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trigo(at)mail.telepac.pt Guest
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Posted: Thu Oct 03, 2013 10:58 am Post subject: Electric System architecture (was Charging the Aux Battery) |
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Please see answers below
-----Mensagem original-----
De: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] Em nome de Robert L. Nuckolls, III
Enviada: 1 de outubro de 2013 22:18
Para: aeroelectric-list(at)matronics.com
Assunto: RE: Charging the Aux Battery
--> AeroElectric-List message posted by: "Robert L. Nuckolls, III"
--> <nuckolls.bob(at)aeroelectric.com (nuckolls.bob(at)aeroelectric.com)>
At 11:41 AM 10/1/2013, you wrote:
Quote: | --> AeroElectric-List message posted by: "Carlos Trigo"
<trigo(at)mail.telepac.pt (trigo(at)mail.telepac.pt)>
Bob
Thank you for the dissertation about the theme I had proposed.
I confess that I still didn't read it thoroughly, so I will have to
digest it conveniently.
Meanwhile, I can confirm that my question was not academic, I am
building an
RV-10 and did consider the Dual battery, One main Alternator - one Aux
alternator system.
So far, I am considering a variation of the Z-14 architecture, but
still didn't reach the "end of the line" in what regards the final
schematic, so would appreciate all suggestions.
Regards
Carlos
|
Understand. I presume your airplane will
be Lycoming powered and has a accessory
pad that will NOT be occupied with a vacuum
pump.
Correct
Do you plan to fly a significant portion of
your use under instrument flight rules, over
mountainous terrain or at night?
Not a significant portion.
But it would be nice to be able to fly IFR and at night.
Do you plan to have a gps aided wing-leveler
or better?
Better, planning an auto-pilot.
Engine electrically dependent in any way?
It is a IO-540
You need to compile a list of every currently
anticipated electro-whizzy. If you have actual
running current for each device, record that value
along. Peak currents too even if intermittent.
Already done an excel table with A consumptions
Do any of these accessories feature built in
back up batteries and/or connections brought
out for dual power sourcing?
Yes, the EFIS will be dual power sourcing.
I am using a VP-X Pro box.
How do you rate yourself for competence/confidence
that under total loss of panel instrumentation,
you could get to where you originally intended to
go with flight bag back-ups?
Well, not so sure, but I do like to fly with the old paper map over my knee…
And I suppose an iPad with electronic charts will also travel in the glove box
Since this is a 4-seated airplane, your approach
toward risk mitigation is understandably more
conservative. It's not necessary that your self-
assessments be shared with the List but do put
some thought into the skill set you plan to have
in your bag of tricks by the time you're ready
to launch with all the seats occupied.
Yeah, right
……….
If this were MY airplane, I'd be trading off
cost of ownership and practical utility of
every installed accessory while maintaining
the notion that under the worst case conditions,
I might have to dig the hand held radios out
of the flight bag. A very tiny risk to be sure
but it's your personal confidence level for making
plan-C . . . D or whatever save your buns.
I also like to have an hand-held radio in the bag of tricks
Hence the real driver for choosing how much stuff
you hang on the panel has more to do with how
well you think you can do without it. If your
confidence level is low, then a plan-b for loss
of any particular item gets elevated in priority.
THESE mental exercises will drive how many
alternators, batteries, busses and kilobux worth
of hardware will fly with you every flight whether
routinely useful or not. So mission profiles,
skill sets, FMEA and load analysis is where the
planning starts.
Ok, now what do you think?
Carlos
[quote][b]
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michaelrorth
Joined: 04 Feb 2011 Posts: 65
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Posted: Thu Oct 03, 2013 12:35 pm Post subject: Electric System architecture (was Charging the Aux Battery) |
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Bob & Carlos,
What a great, and insightful, exchange of information and facts.
Clear, concise, and easily readable.
Keep it up,
Michael
From: Carlos Trigo (trigo(at)mail.telepac.pt)
Sent: Thursday, October 3, 2013 12:00 PM
To: aeroelectric-list(at)matronics.com (aeroelectric-list(at)matronics.com)
Subject: RE: Electric System architecture (was Charging the Aux Battery)
Please see answers below
-----Mensagem original-----
De: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] Em nome de Robert L. Nuckolls, III
Enviada: 1 de outubro de 2013 22:18
Para: aeroelectric-list(at)matronics.com
Assunto: RE: Charging the Aux Battery
--> AeroElectric-List message posted by: "Robert L. Nuckolls, III"
--> <nuckolls.bob(at)aeroelectric.com (nuckolls.bob(at)aeroelectric.com)>
At 11:41 AM 10/1/2013, you wrote:
Quote: | --> AeroElectric-List message posted by: "Carlos Trigo"
<trigo(at)mail.telepac.pt (trigo(at)mail.telepac.pt)>
Bob
Thank you for the dissertation about the theme I had proposed.
I confess that I still didn't read it thoroughly, so I will have to
digest it conveniently.
Meanwhile, I can confirm that my question was not academic, I am
building an
RV-10 and did consider the Dual battery, One main Alternator - one Aux
alternator system.
So far, I am considering a variation of the Z-14 architecture, but
still didn't reach the "end of the line" in what regards the final
schematic, so would appreciate all suggestions.
Regards
Carlos
|
Understand. I presume your airplane will
be Lycoming powered and has a accessory
pad that will NOT be occupied with a vacuum
pump.
Correct
Do you plan to fly a significant portion of
your use under instrument flight rules, over
mountainous terrain or at night?
Not a significant portion.
But it would be nice to be able to fly IFR and at night.
Do you plan to have a gps aided wing-leveler
or better?
Better, planning an auto-pilot.
Engine electrically dependent in any way?
It is a IO-540
You need to compile a list of every currently
anticipated electro-whizzy. If you have actual
running current for each device, record that value
along. Peak currents too even if intermittent.
Already done an excel table with A consumptions
Do any of these accessories feature built in
back up batteries and/or connections brought
out for dual power sourcing?
Yes, the EFIS will be dual power sourcing.
I am using a VP-X Pro box.
How do you rate yourself for competence/confidence
that under total loss of panel instrumentation,
you could get to where you originally intended to
go with flight bag back-ups?
Well, not so sure, but I do like to fly with the old paper map over my knee…
And I suppose an iPad with electronic charts will also travel in the glove box
Since this is a 4-seated airplane, your approach
toward risk mitigation is understandably more
conservative. It's not necessary that your self-
assessments be shared with the List but do put
some thought into the skill set you plan to have
in your bag of tricks by the time you're ready
to launch with all the seats occupied.
Yeah, right
……….
If this were MY airplane, I'd be trading off
cost of ownership and practical utility of
every installed accessory while maintaining
the notion that under the worst case conditions,
I might have to dig the hand held radios out
of the flight bag. A very tiny risk to be sure
but it's your personal confidence level for making
plan-C . . . D or whatever save your buns.
I also like to have an hand-held radio in the bag of tricks
Hence the real driver for choosing how much stuff
you hang on the panel has more to do with how
well you think you can do without it. If your
confidence level is low, then a plan-b for loss
of any particular item gets elevated in priority.
THESE mental exercises will drive how many
alternators, batteries, busses and kilobux worth
of hardware will fly with you every flight whether
routinely useful or not. So mission profiles,
skill sets, FMEA and load analysis is where the
planning starts.
Ok, now what do you think?
Carlos
Quote: |
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[quote][b]
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