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The new Electric Cessna 172



 
 
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  #61  
Old February 1st 13, 02:54 PM posted to rec.aviation.piloting
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Posts: 2
Default The new Electric Cessna 172

On Jan 1, 1:24*pm, wrote:
wrote:

http://nextbigfuture.com/2009/12/sup...enable-electri...


--
Mark


Practical, manufacturable high temperature superconductors would enable
a whole bunch of neat things and would be as spectacular as a cure for the
common cold, lasting peace in the Middle East, and controlled fusion, and
is just as likely to happen in the near future.


I recently read up on some work being done with graphene
supercapacitors. I IRC, it was at Caltech. What was interesting is how
they performed at lower temperatures (e.g. room temp.). Also, charging
times were impressive. Still in the realm of research, so it wasn't
clear to me how well it would scale beyond smaller applications
(consumer electronics, for example.
  #62  
Old February 1st 13, 05:25 PM posted to rec.aviation.piloting
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Posts: 2,892
Default The new Electric Cessna 172

wrote:
On Jan 1, 1:24Â*pm, wrote:
wrote:

http://nextbigfuture.com/2009/12/sup...enable-electri...

--
Mark


Practical, manufacturable high temperature superconductors would enable
a whole bunch of neat things and would be as spectacular as a cure for the
common cold, lasting peace in the Middle East, and controlled fusion, and
is just as likely to happen in the near future.


I recently read up on some work being done with graphene
supercapacitors. I IRC, it was at Caltech. What was interesting is how
they performed at lower temperatures (e.g. room temp.). Also, charging
times were impressive. Still in the realm of research, so it wasn't
clear to me how well it would scale beyond smaller applications
(consumer electronics, for example.



Supercapacitors are great for things like keeping your clock from flashing
on every minor power failure, but not that great for real power application.

The basic physics of capacitors says the energy density can never be as
good as existing batteries. Graphene makes them better but it will take
yet to be invented materials to match batteries.

Capacitors are also a poor choice for running something like a motor because
of their discharge curve.

While a battery's discharge curve is basically flat until it gets close to
full discharge, then takes a big dive, a capacitor discharge curve is a
straight line between fully charged and zero.

Motors operate over a narrow voltage range. Electric motor speed control
is done by pulsing the motor voltage on and off, not by varying a constant
voltage.

Now it is possible to build a thing that will take in a lower voltage and
output some constant higher voltage to keep a motor happy.

The problem with that is it is more complexity subject to failure, not
good with airplanes, and it would require big, heavy, high current
transformers, which ups the weight a good bit.

My wild assed guess is that if electric airplanes ever become practical
without Star Trek technology, it will likely be through a fuel cell that
is yet to be invented.




  #63  
Old February 1st 13, 06:16 PM posted to rec.aviation.piloting
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Posts: 2
Default The new Electric Cessna 172

On Feb 1, 12:25*pm, wrote:
wrote:
On Jan 1, 1:24*pm, wrote:
wrote:


http://nextbigfuture.com/2009/12/sup...enable-electri....


--
Mark


Practical, manufacturable high temperature superconductors would enable
a whole bunch of neat things and would be as spectacular as a cure for the
common cold, lasting peace in the Middle East, and controlled fusion, and
is just as likely to happen in the near future.


I recently read up on some work being done with graphene
supercapacitors. I IRC, it was at Caltech. What was interesting is how
they performed at lower temperatures (e.g. room temp.). Also, charging
times were impressive. Still in the realm of research, so it wasn't
clear to me how well it would scale beyond smaller applications
(consumer electronics, for example.


Supercapacitors are great for things like keeping your clock from flashing
on every minor power failure, but not that great for real power application.

The basic physics of capacitors says the energy density can never be as
good as existing batteries. Graphene makes them better but it will take
yet to be invented materials to match batteries.

Capacitors are also a poor choice for running something like a motor because
of their discharge curve.

While a battery's discharge curve is basically flat until it gets close to
full discharge, then takes a big dive, a capacitor discharge curve is a
straight line between fully charged and zero.

Motors operate over a narrow voltage range. Electric motor speed control
is done by pulsing the motor voltage on and off, not by varying a constant
voltage.

Now it is possible to build a thing that will take in a lower voltage and
output some constant higher voltage to keep a motor happy.

The problem with that is it is more complexity subject to failure, not
good with airplanes, and it would require big, heavy, high current
transformers, which ups the weight a good bit.

My wild assed guess is that if electric airplanes ever become practical
without Star Trek technology, it will likely be through a fuel cell that
is yet to be invented.


Most of what I was reading didn't seem to indicate that the goal is to
replace, but rather to compliment existing technologies, e.g. charging
applications.

http://phys.org/news/2012-10-sponge-...ectrodes..html
- Graphene

http://phys.org/news/2011-08-energy-...-electric.html
- SMC

I'm not saying it will (ever) power an airplane. Just looked
interesting and sometimes there are great discoveries that come out of
research, often in applications that were never part of the planned
research itself.

Peace.
  #64  
Old February 1st 13, 07:01 PM posted to rec.aviation.piloting
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Posts: 2,892
Default The new Electric Cessna 172

wrote:

snip old stuff


Most of what I was reading didn't seem to indicate that the goal is to
replace, but rather to compliment existing technologies, e.g. charging
applications.

http://phys.org/news/2012-10-sponge-...lectrodes.html
- Graphene

http://phys.org/news/2011-08-energy-...-electric.html
- SMC


Lot's of little techical problems in both of those articles.

The biggest is talking about recharging in minutes.

It is a rather simple calculation to calculate the current requirments
to recharge a device (doesn't matter battery or capacitor) to the full
energy level in a few minutes.

When you do that you discover that the size of the cable required so that
it will not vaporize due to the current density is as big around as your
leg with matching connectors.

Energy sources are rated in KWh and is equivalent to 1000 x V x A x h.

A typical electric car battery is around 30 KWh and 100 volts and 6 minutes
is 0.1 hours so:

30,000 / (100 x .1) = 3,000 Amps

To put the wire required in perspective, those big heavy cables on an
arc welder are good for a current of around 100 Amps so your charging
cable would have to be about 30 times bigger than arc welder cables.

I'm not saying it will (ever) power an airplane. Just looked
interesting and sometimes there are great discoveries that come out of
research, often in applications that were never part of the planned
research itself.


Yeah, that is usually the case.


Peace.

  #67  
Old February 5th 13, 11:41 AM posted to rec.aviation.piloting
Dylan Smith[_2_]
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Posts: 53
Default The new Electric Cessna 172

On 2013-02-04, wrote:
To be precise for an interconnect of 10m, two cables of 30mm diameter
would suffice. It would give the line boy a bit of a work out but isn't
impossible. Size-wise it's a bit like two fuel hoses but *considerably*
heavier.


I think you dropped a decimal point there.

4/0 AWG wire is about 12mm in diameter and rated for about 300 A.


No decimal point dropped.

Don't forget the DC current carrying capacity is not determined by
the radius, but the cross section area of the cable. So you wouldn't need
120mm dia. cable. A 12mm dia cable has an area of 113mm^2. Multiplying
by 10 we have a cable with a 1130mm^2 cross section, or a radius of
sqrt(1130/pi), or a 38mm diameter by just making it ten times larger
than a 300A cable (and not far off my initial guesstimate of 30mm dia).

That wire has about 1.5e-5 ohm resistance per meter (or 1.5e-4 ohm
for 10 meters). Applying V=IR to find the voltage drop, we have
V=3000*0.00015, or a 0.45v drop over this cable. So we'd have to
dissipate about 1.4kW of heat over this 10 meter length during the
charge. So yes, pretty toasty but it wouldn't melt the insulation.
It's the poor line boy who gets a bit of a work out though, he'd
have to drag about 200kg of cable out to the plane. Even lifting
the last 2m up off the ground to connect to the aircraft would be lifting
40kg of copper. The health and safety police certainly would frown on
that.

Note I'm not saying it's *practical*, where I live the final distribution
circuits are only 180kW or so, which is less than the power that this
thing would need to transfer, so the FBO which probably have just a pretty
standard commercial office type electricity supply would need upgrading
to something that could power a factory (in other words, eyewateringly
expensive given that most GA FBOs are marginally profitable and live
hand-to-mouth). I also suspect that 10m of 38mm dia cable will be a bit
expensive too and a prime target for copper thieves. So even before
we get as far as thinking "will a 38mm dia cable with a suitable
protection device meet regulations?" the whole thing would be stymied
by the astronomical cost of supplying such a large amount of power to
an operation that at the best of times can just about cover the wage bill.

  #69  
Old February 5th 13, 06:05 PM posted to rec.aviation.piloting
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Posts: 2,892
Default The new Electric Cessna 172

Dylan Smith wrote:
On 2013-02-04, wrote:
To be precise for an interconnect of 10m, two cables of 30mm diameter
would suffice. It would give the line boy a bit of a work out but isn't
impossible. Size-wise it's a bit like two fuel hoses but *considerably*
heavier.


I think you dropped a decimal point there.

4/0 AWG wire is about 12mm in diameter and rated for about 300 A.


No decimal point dropped.

Don't forget the DC current carrying capacity is not determined by
the radius, but the cross section area of the cable. So you wouldn't need
120mm dia. cable. A 12mm dia cable has an area of 113mm^2. Multiplying
by 10 we have a cable with a 1130mm^2 cross section, or a radius of
sqrt(1130/pi), or a 38mm diameter by just making it ten times larger
than a 300A cable (and not far off my initial guesstimate of 30mm dia).


Sounds about right.

That wire has about 1.5e-5 ohm resistance per meter (or 1.5e-4 ohm
for 10 meters). Applying V=IR to find the voltage drop, we have
V=3000*0.00015, or a 0.45v drop over this cable. So we'd have to
dissipate about 1.4kW of heat over this 10 meter length during the
charge. So yes, pretty toasty but it wouldn't melt the insulation.
It's the poor line boy who gets a bit of a work out though, he'd
have to drag about 200kg of cable out to the plane. Even lifting
the last 2m up off the ground to connect to the aircraft would be lifting
40kg of copper. The health and safety police certainly would frown on
that.


Minor nit:

There are two wires so shouldn't that be 2.8kW and 400 kg of cable?

Note I'm not saying it's *practical*, where I live the final distribution
circuits are only 180kW or so, which is less than the power that this
thing would need to transfer, so the FBO which probably have just a pretty
standard commercial office type electricity supply would need upgrading
to something that could power a factory (in other words, eyewateringly
expensive given that most GA FBOs are marginally profitable and live
hand-to-mouth). I also suspect that 10m of 38mm dia cable will be a bit
expensive too and a prime target for copper thieves. So even before
we get as far as thinking "will a 38mm dia cable with a suitable
protection device meet regulations?" the whole thing would be stymied
by the astronomical cost of supplying such a large amount of power to
an operation that at the best of times can just about cover the wage bill.


Totally agree here.

This is why no electric vehicle of any kind is ever going to "refuel" as
quickly as a gasoline vehicle no matter what the storage device other
than a fuel cell and for most people a refuel time of hours is not
acceptable.

One would think the research money for big electrical sources would be
better spent on fuel cells (not that they don't have problems of their
own like generating a lot of heat) than on batteries and capacitors.








 




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