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Solar charging question



 
 
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  #1  
Old January 17th 11, 08:42 PM posted to rec.aviation.soaring
Ed
external usenet poster
 
Posts: 6
Default Solar charging question

On Jan 17, 10:35*am, Eric Greenwell wrote:
On 1/16/2011 8:55 PM, Ed wrote:

Thank you, Eric, this is a good start knowing that I have to upgrade a
bit.


The complicating factor is that the glider is tied down on the flight
line in the summer, far from the trailer. Whatever I come up with has
to be a self-contained, compact and secure solution which will either
fit in the glider or is weatherproof and resistant to wind. Most 20 W
panels make excellent weathervanes, and the only securing mechanism I
have is the tie down cable and eyes. Since I live an hour from the
airport I need a "set it and forget it" solution that charges while
I'm away. I don't often fly on back to back days, and I do get some
recharge from the alternator on launch as well, so I probably need to
make up only about 6-8 Ah.


For the typical soaring season, laying the panel flat on the ground
works well. It does require a bigger panel, compared to one that's
optimally aimed at the sun, but it's easier to secure. If you aren't
flying consecutive days, a 20 watt panel would probably suffice, but a
30 watt is much more expensive.



You've given me an interesting idea. I wonder if I could construct a
small aux battery box with a LN5014 DC/DC converter which I leave in
the glider to top off the battery after I leave. On return to the
airport I could remove the unit and charge it on the AC charger in the
hangar while I'm flying. If that few hours of recharge cycle time were
not enough it would be easy just to buy a second battery and swap them
out so that a fully charged one is always ready when I leave the
airport.


That plan would work fine. You do need a way to automatically disconnect
the LN5014 from the battery after 10-12 hours: while it will
automatically stop charging the glider battery when it's full, the
LN5014 continues to draw about 50 ma from the battery that powers it. A
12 hour mechanical timer (like you see on bathroom fans or heating
lamps, for example) between the LN5014 and the battery powering it would
do the trick.

So this leads to two more questions....


Is the LN5014 ok to leave attached for that long (ie., is it like a
charge controller which will shut the current off when the main
battery is recharged)? *If so, is it possible to do what you do with
respect to connecting my existing 300 mA solar panel and Morningstar
controller in parallel?


Yes, you could use them in parallel. You still need the timer switch to
disconnect the LN5014 from it's battery, or the battery will discharge
too far.

--
Eric Greenwell - Washington State, USA (change ".netto" to ".us" to
email me)


Again, thank you Eric for your thoughtful replies. I think I may have
found just what I need. I'll post the details in case someone else
might benefit.

If you go to http://www.powerstream.com/DC-input-chargers.htm and
click on the PST-BC1212-15DCDC Charger you can see this option. It
costs about twice as much as the LN5014, but I spoke with the engineer
who built it and he seems to think it will work well. We devised a
system where I can keep a source battery on the floor of the aircraft
which becomes the input of this converter. It needs to be about 1.5
times the Ah deficit that needs to be replaced (so for a 10 Ah boost
it needs to be at least 15 Ah). It doesn't run hot, so I can keep it
in the aircraft and not worry about weatherproofing. Interestingly,
this setup, run in reverse, allows me to take the source battery and
leave it in my car while I am flying, charging the source battery from
my car battery. The advantage I see to this product is that is it a
smart controller which will keep topping off the main aircraft battery
as needed and then stay in the background until the main battery needs
topping off again. If the source battery is large enough, even if I
don't get a complete recharge from my car I can always take it back to
the the hangar and bring it all the way back up with an AC charger. I
think I'm going to go in this direction since it was specifically
designed to do the very thing I am trying to accomplish. It does not
need to be attended while charging, so it looks as though it is the
'set it and forget it' solution I was looking for.

Andy, thanks for your post as well. Yes, the ultimate solution is
battery removal if all else fails, but the designer of this aircraft
made that difficult to do. It isn't just popping open a small battery
box -- it requires some disassembly of the front instrument panel and
the removeal of some tight clearance attachment hardware for the
terminals. I've done it enough times to know that it will be my
desperation solution if all else fails.
  #2  
Old January 17th 11, 09:32 PM posted to rec.aviation.soaring
Eric Greenwell[_4_]
external usenet poster
 
Posts: 1,939
Default Solar charging question

On 1/17/2011 12:42 PM, Ed wrote:
Again, thank you Eric for your thoughtful replies. I think I may have
found just what I need. I'll post the details in case someone else
might benefit.

If you go tohttp://www.powerstream.com/DC-input-chargers.htm and
click on the PST-BC1212-15DCDC Charger you can see this option.


It looks like a good choice for your situation. Did they say how much
current it drew from the source battery when it wasn't charging the
glider battery?

--
Eric Greenwell - Washington State, USA (change ".netto" to ".us" to
email me)
  #3  
Old January 17th 11, 11:30 PM posted to rec.aviation.soaring
Ed
external usenet poster
 
Posts: 6
Default Solar charging question

On Jan 17, 1:32*pm, Eric Greenwell wrote:

It looks like a good choice for your situation. Did they say how much
current it drew from the source battery when it wasn't charging the
glider battery?

--
Eric Greenwell - Washington State, USA (change ".netto" to ".us" to
email me)


I didn't ask, and it doesn't seem to be available on the website.
Since it's generating a constant float I imagine that it is not
inconsequential. I'll find out when it arrives. I'm not an electrical
engineer, but my guess is that the converter will shut down at some
low voltage like 11.9 v and drop the source battery out of the
picture. That's why I wonder if I need to keep the solar charger in
the mix. The question then becomes should I have the 5W solar panel in
parallel with the main aircraft battery to take over the topping of
the battery (output side of the converter), or should I try to keep
the source battery above the lower limit using the solar. The unit is
also flexible enough that if the source power is interrupted it will
figure out where things stand and pick up the charge at the right
place. There's an interesting charge state digram on the website that
shows this. I may need to think about a timer that only allows the
source battery to be available for a certain amount each day so that
it lasts longer.
  #4  
Old January 18th 11, 02:54 AM posted to rec.aviation.soaring
Eric Greenwell[_4_]
external usenet poster
 
Posts: 1,939
Default Solar charging question

On 1/17/2011 3:30 PM, Ed wrote:
On Jan 17, 1:32 pm, Eric wrote:

It looks like a good choice for your situation. Did they say how much
current it drew from the source battery when it wasn't charging the
glider battery?



I didn't ask, and it doesn't seem to be available on the website.
Since it's generating a constant float I imagine that it is not
inconsequential. I'll find out when it arrives. I'm not an electrical
engineer, but my guess is that the converter will shut down at some
low voltage like 11.9 v and drop the source battery out of the
picture. That's why I wonder if I need to keep the solar charger in
the mix. The question then becomes should I have the 5W solar panel in
parallel with the main aircraft battery to take over the topping of
the battery (output side of the converter), or should I try to keep
the source battery above the lower limit using the solar. The unit is
also flexible enough that if the source power is interrupted it will
figure out where things stand and pick up the charge at the right
place. There's an interesting charge state digram on the website that
shows this. I may need to think about a timer that only allows the
source battery to be available for a certain amount each day so that
it lasts longer.


The self-discharge rate on the typical SLA is low enough, you could
forget about more charging for a month, once it was fully charged.
Unless, of course, your temperatures average over 90-100 F. But,
putting that little 0.3A panel on would keep it topped off.

--
Eric Greenwell - Washington State, USA (change ".netto" to ".us" to
email me)
  #5  
Old January 18th 11, 05:06 PM posted to rec.aviation.soaring
Darryl Ramm
external usenet poster
 
Posts: 2,403
Default Solar charging question

On Jan 17, 3:30*pm, Ed wrote:
On Jan 17, 1:32*pm, Eric Greenwell wrote:

It looks like a good choice for your situation. Did they say how much
current it drew from the source battery when it wasn't charging the
glider battery?


--
Eric Greenwell - Washington State, USA (change ".netto" to ".us" to
email me)


I didn't ask, and it doesn't seem to be available on the website.
Since it's generating a constant float I imagine that it is not
inconsequential. I'll find out when it arrives. I'm not an electrical
engineer, but my guess is that the converter will shut down at some
low voltage like 11.9 v and drop the source battery out of the
picture. That's why I wonder if I need to keep the solar charger in
the mix. The question then becomes should I have the 5W solar panel in
parallel with the main aircraft battery to take over the topping of
the battery (output side of the converter), or should I try to keep
the source battery above the lower limit using the solar. The unit is
also flexible enough that if the source power is interrupted it will
figure out where things stand and pick up the charge at the right
place. There's an interesting charge state digram on the website that
shows this. I may need to think about a timer that only allows the
source battery to be available for a certain amount each day so that
it lasts longer.


These devices are really designed to charge a 12V wheelchair from a
car electrical system - typically including while the car is running
and as such often have a low voltage disconnect (LVD) to prevent the
car battery becoming so flat that it can't crank the starter to start
the car again and that may mean you can't get a full charge out of the
"donor" battery. It all depends on the LVD set point and I have no
idea what Powerstream do in this case - although they talk about a 10V
low voltage alarm, it that is also the LVD set point then that seems
great for this application. I've seen some attempts to do this with
similar systems and undersizing of the donor battery has caused some
problems even with a low LVD set pount. I'd personally be thinking of
a larger VRLA battery (2-3X the glider battery capacity) - maybe on a
small hand cart.

I would not run the small solar panel in parallel with this charger or
on the donor battery. Just let the the charger just see the VRLA
battery it is charging. Such a small solar panel is pretty useless as
you have already found out, may interfere with the other charger if
used on the recipient battery (depending if it has isolation diodes
etc.) and is just overall more unecessary complexity to deal with. As
Eric points out self discharge of a VRLA battery is usually extremely
low.

Darryl



  #6  
Old January 19th 11, 03:08 PM posted to rec.aviation.soaring
Ed
external usenet poster
 
Posts: 6
Default Solar charging question

On Jan 18, 9:06*am, Darryl Ramm wrote:
On Jan 17, 3:30*pm, Ed wrote:





On Jan 17, 1:32*pm, Eric Greenwell wrote:


It looks like a good choice for your situation. Did they say how much
current it drew from the source battery when it wasn't charging the
glider battery?


--
Eric Greenwell - Washington State, USA (change ".netto" to ".us" to
email me)


I didn't ask, and it doesn't seem to be available on the website.
Since it's generating a constant float I imagine that it is not
inconsequential. I'll find out when it arrives. I'm not an electrical
engineer, but my guess is that the converter will shut down at some
low voltage like 11.9 v and drop the source battery out of the
picture. That's why I wonder if I need to keep the solar charger in
the mix. The question then becomes should I have the 5W solar panel in
parallel with the main aircraft battery to take over the topping of
the battery (output side of the converter), or should I try to keep
the source battery above the lower limit using the solar. The unit is
also flexible enough that if the source power is interrupted it will
figure out where things stand and pick up the charge at the right
place. There's an interesting charge state digram on the website that
shows this. I may need to think about a timer that only allows the
source battery to be available for a certain amount each day so that
it lasts longer.


These devices are really designed to charge a 12V wheelchair from a
car electrical system - typically including while the car is running
and as such often have a low voltage disconnect (LVD) to prevent the
car battery becoming so flat that it can't crank the starter to start
the car again and that may mean you can't get a full charge out of the
"donor" battery. It all depends on the LVD set point and I have no
idea what Powerstream do in this case - although they talk about a 10V
low voltage alarm, it that is also the LVD set point then that seems
great for this application. I've seen some attempts to do this with
similar systems and undersizing of the donor battery has caused some
problems even with a low LVD set pount. I'd personally be thinking of
a *larger VRLA battery (2-3X the glider battery capacity) - maybe on a
small hand cart.

I would not run the small solar panel in parallel with this charger or
on the donor battery. Just let the the charger just see the VRLA
battery it is charging. Such a small solar panel is pretty useless as
you have already found out, may interfere with the other charger if
used on the recipient battery (depending if it has isolation diodes
etc.) and is just overall more unecessary complexity to deal with. As
Eric points out self discharge of a VRLA battery is usually extremely
low.

Darryl- Hide quoted text -

- Show quoted text -


Darryl -

Thank you, this additional perspective is very helpful. The idea of
additonally having an input to charge from the car is a great idea.
Whatever it takes to get flying!!
 




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