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12 Volt .vs. 24 Volt

 
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bwolf1(at)tds.net
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PostPosted: Mon May 18, 2009 5:42 am    Post subject: 12 Volt .vs. 24 Volt Reply with quote

I have a feeling that this subject has been discussed before, but I
need help deciding on a voltage system for my Velocity. I intend a
robust electrical system to support a high end IFR panel. The highest
draw item will probably be an electric hydraulic pump which pulls
about 30 amps at 12 volts. I know a 24 volt will save some weight in
wiring because of the lower amperage. However, after reading Bob's
response to a Blue Mountain article

http://www.aeroelectric.com/articles/richter/response_1.pdf

the weight saved appears minimal. I don't know for sure, but I have a
feeling that the vast majority of OBAM airplanes are built around 12
volt systems. My question is, why do the likes of Cessna and Cirrus
build their single engine airplanes with 24 volt systems?

Thanks...Brooke


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Bruce(at)glasair.org
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PostPosted: Mon May 18, 2009 6:25 am    Post subject: 12 Volt .vs. 24 Volt Reply with quote

Similarity of construction.

Bruce
Glasair III (28v)
www.Glasair.org

--


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Peter Laurence



Joined: 10 Jan 2006
Posts: 50

PostPosted: Mon May 18, 2009 7:33 am    Post subject: 12 Volt .vs. 24 Volt Reply with quote

Quote:


I have a feeling that this subject has been discussed before, but I
need help deciding on a voltage system for my Velocity. I intend a
robust electrical system to support a high end IFR panel. The highest
draw item will probably be an electric hydraulic pump which pulls
about 30 amps at 12 volts. I know a 24 volt will save some weight in
wiring because of the lower amperage. However, after reading Bob's
response to a Blue Mountain article

http://www.aeroelectric.com/articles/richter/response_1.pdf

the weight saved appears minimal. I don't know for sure, but I have a
feeling that the vast majority of OBAM airplanes are built around 12
volt systems. My question is, why do the likes of Cessna and Cirrus
build their single engine airplanes with 24 volt systems?

Thanks...Brooke

I wired a Velocity XL RG for a friend as a 12v system. Dual B&C alternators
and Regulators.

No issues for over four years and five hundred hours.
Peter


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skywagon



Joined: 11 Feb 2006
Posts: 184

PostPosted: Mon May 18, 2009 8:30 am    Post subject: 12 Volt .vs. 24 Volt Reply with quote

Why 24 v. systems.... in the commercial world it is usually about costs and
profits. Less copper used, less cost.
David
---


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mrspudandcompany(at)veriz
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PostPosted: Mon May 18, 2009 9:03 am    Post subject: 12 Volt .vs. 24 Volt Reply with quote

Similarity of construction.

(Please elaborate!)
Bruce
Glasair III (28v)
www.Glasair.org
I have a feeling that this subject has been discussed before, but I
need help deciding on a voltage system for my Velocity. I intend a
robust electrical system to support a high end IFR panel. The highest
draw item will probably be an electric hydraulic pump which pulls
about 30 amps at 12 volts. I know a 24 volt will save some weight in
wiring because of the lower amperage. However, after reading Bob's
response to a Blue Mountain article

http://www.aeroelectric.com/articles/richter/response_1.pdf

the weight saved appears minimal. I don't know for sure, but I have a
feeling that the vast majority of OBAM airplanes are built around 12
volt systems. My question is, why do the likes of Cessna and Cirrus
build their single engine airplanes with 24 volt systems?

Thanks...Brooke


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nuckolls.bob(at)aeroelect
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PostPosted: Mon May 18, 2009 10:29 am    Post subject: 12 Volt .vs. 24 Volt Reply with quote

At 10:44 AM 5/18/2009, you wrote:
Quote:


Why 24 v. systems.... in the commercial world it is usually about
costs and profits. Less copper used, less cost.
David


Close. When I went to work for Cessna in '64, we had
14v airplanes (150, 172) and 28v airplanes (182, 206,
210). When you need to run high-energy electro-whizzies
you can get more WATTS of engine driven power from
essentially the same WEIGHT of system if it's 28v.
But as quantities of all airplanes sold dwindled,
it was economically more efficient to simply install
the same hardware in all aircraft. The alternators
were the same size and weight, batteries could be
sized to the task for total energy stored. Common
landing lights, nav lights, strobe kits, etc made
for fewer line items of electrical goodies in
inventory and more wider applicability of fewer
parts for field spares.

It had nothing to do with any practical level
of weight savings. We kinda like 14v stuff in the
OBAM market: unlike the uniquely aircraft
"pallet of paints" for 28V hardware, 14V automotive
hardware is stocked in thousands of varieties and
sources virtually everywhere on the planet.

The "improved performance" and "lighter weight"
canards are difficult to measure/prove without
carefully detailed studies with slice-n-dice
instrumentation. For us get-in-n-go airplane
drivers, the 14 vs. 28 volt differences are
not readily observable. So the big driver is
simply cost of ownership in terms of $acquisition$
and $time$ to maintain. 14v has it hands down.

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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BobsV35B(at)aol.com
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PostPosted: Mon May 18, 2009 10:53 am    Post subject: 12 Volt .vs. 24 Volt Reply with quote

Good Afternoon,

Definitely NOT 'Lectric Bob here!

I DO like twenty-four volt systems. I also agree that any weight saving is probably minimal on an overall basis, nevertheless, I do subscribe to the theory that ounces count.

Twenty-four volts allows us to use lighter weight starters, alternators, wires, even relays. The trouble is that most twenty-four volt units weigh as much as their twelve volt counterparts. If you want to take full advantage of a twenty-four volt system you also have to use lighter components. If thirty amps at twelve volts will handle all of your aircraft requirements, all you need is fifteen amps with a twenty-four volt system. How many fifteen amp alternators do you see available?

If you go ahead and use a thirty amp twenty-four volt alternator, you have not taken full advantage of the weight saving capabilities of the twenty-four volt regime.

Cessna went to twenty-four volts for everything from the 152 on up many years ago. It was cheaper and lighter for the whole fleet and only having to deal with twenty-four volt components made inventory control a lot easier.

Commonality of parts and all of the economies that breeds!

If you want to be able to jump start your airplane form a twelve volt car, twenty-four volts may not be for you.

Personally, If I ever have the feeling that I need a jump start for my airplane, I would also determine that I had made some sort of error in managing my flying machine.

If I leave the master on and deplete the battery, I will pull the battery, have it properly serviced, and chalk the experience up to my own stupidity. (I have, unfortunately for me, had to do that more than once.)

What I have NOT done, however, is jump start my airplane! If I need the battery at all, I want it to be fully charged and properly serviced before I fly.

Happy Skies

Old Bob
AKA
Bob Siegfried
Ancient Aviator
628 West 86th Street
Downers Grove, IL 60516
630 985-8502
Stearman N3977A
Brookeridge Air Park LL22
In a message dated 5/18/2009 12:07:06 P.M. Central Daylight Time, mrspudandcompany(at)verizon.net writes:
Quote:

Similarity of construction.

(Please elaborate!)
Bruce
Glasair III (28v)
www.Glasair.org
I have a feeling that this subject has been discussed before, but I
need help deciding on a voltage system for my Velocity. I intend a
robust electrical system to support a high end IFR panel.  The highest
draw item will probably be an electric hydraulic pump which pulls
about 30 amps at 12 volts. I know a 24 volt will save some weight in
wiring because of the lower amperage.  However, after reading Bob's
response to a Blue Mountain article

http://www.aeroelectric.com/articles/richter/response_1.pdf

the weight saved appears minimal. I don't know for sure, but I have a 
feeling that the vast majority of OBAM airplanes are built around 12
volt systems. My question is, why do the likes of Cessna and Cirrus
build their single engine airplanes with 24 volt systems?

Thanks...Brooke



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[quote][b]


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lists(at)stevet.net
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PostPosted: Mon May 18, 2009 12:44 pm    Post subject: 12 Volt .vs. 24 Volt Reply with quote

And don't forget to add that you can save much more weight in the
operation of your aircraft by going on a diet! Drop 10 to 15 pounds
off your personal frame and it will make up for many many incremental
weight saving devices in your airframe.
Steve
________________________________________________________________________

On May 18, 2009, at 11:23 AM, Robert L. Nuckolls, III wrote:

Quote:
The "improved performance" and "lighter weight"
canards are difficult to measure/prove without
carefully detailed studies with slice-n-dice
instrumentation. For us get-in-n-go airplane
drivers, the 14 vs. 28 volt differences are
not readily observable. So the big driver is
simply cost of ownership in terms of $acquisition$
and $time$ to maintain. 14v has it hands down.

Bob . . .


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Bruce(at)glasair.org
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PostPosted: Mon May 18, 2009 1:40 pm    Post subject: 12 Volt .vs. 24 Volt Reply with quote

Sorry, poor choice of words on my part. What I meant was "Commonality of
Manufacturing". It easier for the factory to use one battery, one relay,
one bulb, one starter, across the entire line than a mixed bag for each
different aircraft.

Where 28v has 14v beat is in delivery of power. I remember flying my 14v
C177RG at night with everything, including all the lights turned on.
When I reached for the gear lever and flipped it down, everything went
dim! Just about every 14v RG airplane I've flown does that. Not the 28v
ones, just the 14v. Power, when you need it, you need it!

Bruce
www.Glasair.org

--


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rtitsworth



Joined: 16 Jan 2006
Posts: 76
Location: Detroit, Mi

PostPosted: Mon May 18, 2009 5:12 pm    Post subject: 12 Volt .vs. 24 Volt Reply with quote

If you're thinking heated prop, Elec air conditioning, Elec cabin heat,
heated seals, or other high-energy goodies, then a 24V system/alternator
offers twice the "power" for roughly the same system weight as a 12v
alternator. It's not the (potential) smaller wire savings that is
significant/relevant, rather it's twice the available power from the same
weight alternator, contactors, etc (i.e. the heavy items).

This is also perhaps a consideration if you're planning on a small backup
(B&C type) alternator. The 24v version again has twice the available
"power" as the 12v (same weight/package) - i.e. more things you can drive on
the E-bus.

It used to be that 24V goodies were hard to come by. However, an evening
with an aircraft spruce (or west marine) catalog will revel that many common
items are now available 12v or 24v (14/2Cool for the same price. More over,
most modern avionics items now operate over the entire 12-28 range.

With some "shopping", perhaps the only items that needs converting down to
12v is the cigarette lighter port and Ray Allen trim tab servos.

.02
--


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bwolf1(at)tds.net
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PostPosted: Tue May 19, 2009 2:36 am    Post subject: 12 Volt .vs. 24 Volt Reply with quote

Thanks to everybody for their comments. It is much easier to make
informed decisions when armed with the insight that this group
provides. Thanks to Bob and everybody else for making this possible!

Brooke


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