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New alternator kit from Vans with OV

I want you to pay up!

Build9A said:
Check out these two links. While both sell for more than the old Vans re-built alternators, there's a $194 prize for the person (buyer) who can figure this one out.

http://www.plane-power.com/AL12-EI60.htm

http://www.vansaircraft.com/cgi-bin/catalog.cgi?&browse=engines&product=alternator-kit

Hint: check out the pictures.... :p
Simple Van struck a deal with plane power. Plane power has been hounding Van to stock their product. The price differnce? $569 list vs. Van's $375? Explanation= awesome. Good for us. I am guessing that Van's may have a OEM agreement that they sell only to Van customers (owner of planes or kits?). Never the less I want my $194. Email me at [email protected] for paypal or address to send check payment.

George
 
oops

George; I forgot to mention the fine print. the $194 is the savings (prize) to the buyer for buying from Vans. Sorry, I spent all my money on some aluminum, plexi glas, rivets, nuts, bolts, electrical gizmos and a little fiberglass. Put it all together and inserted $3.50+/- per gal fuel and took off. :D
 
a few things

rv72004 said:
I have Vans "rebuilt 60 amp " kit. Whats the difference with this and the new one ??

This one is new, it is internally regulated (like the old one), but has a built on overvoltage protection that trips the field breaker when the alt. puts out over a certain voltage. I believe it is also set up to rotate/spin counterclockwise like the prop/engine. There might be other differences as well.
 
Things I'll never understand

Instructions written by the IRS, Insurance policies and Alternators

This one is new, it is internally regulated (like the old one), but has a built on overvoltage protection that trips the field breaker when the alt. puts out over a certain voltage.


I thought that most ND IR alternators (including 60A rebuilt units from Van) had OV smarts :confused:

I recall some posts where the ND OV condition limits the voltage to 18 volts (still an OV condition). Does this new unit shut itself down completly? Sorry, I am still unclear what the difference is. Many thanks.
 
Looks like the mounting brackets on the new one are steel vs. the aluminum brackets that Vans supplied/fab-yourself with the old re-built one that I have.

Anybody know if the specs are different? As we now know from George, not all 60amp alternators are alike. And they are rarely rated for full-time 60amp output.

Dave
 
OK, I got good news and bad news

Davepar said:
Looks like the mounting brackets on the new one are
steel vs. the aluminum brackets that Vans supplied/fab-yourself with the
old re-built one that I have.

Anybody know if the specs are different? As we now know from George,
not all 60amp alternators are alike. And they are rarely rated for full-time
60amp output.

Dave
This new offering is from plane power.
http://www.vansaircraft.com/cgi-bin...=alternator-kit


Here are some related links of interest from Plane Power:
(keep in mind he has certified and experimental units, the EX ones are internally regulated.)
http://www.plane-power.com/Bit3.htm
http://www.plane- power.com/images/Brochure EXP 60.pdf
http://www.plane-power.com/Bit1.htm
http://www.plane-power.com/Bit2.htm

I don't work for plane power or claim to know the details of it other than
what I read above from his site.

First this new catalog item from Van's is NO LONGER a ND alternator. It
is a PLANE POWER (PP) alternator made with some ND parts. The
brushes, fan, regulator and pulley are all differnt from a stock unit. I am
going to guess the case, stator, rotor (field) and bearings are still ND or
aftermarket ND clone parts. One of the major things that PP has done is
modified or changed is the voltage regulator (VR) with an "external" OV
module bolted to the back. (You can see it in some of the pictures.)

In the past the method of ADDING OV protection by those who felt they
needed it was to add a BIG OV relay on the output of the alternator (B-
lead). That OV relay got power thru a "OV module" that would TRIP or
open the relay if voltage got to high. This was a bit of a kluge with a bunch
of extra components. However in theory it would open and disconnect the
alternator automatically in the event the alternator had a bad day. The down
side was the weight and cost. When using aeroelectrics "crow bar", nuisance
trips where common. This in turn could easily damage a good alternator if it
tripped. NEVER run and alternator disconnected from the battery. Nuff Said.

FIRST lets REVIEW: Remember your basic electromagnetism. When a
magnetic field is passed by a wire current it produced, Faraday's law. Well
an alternator has a spinning magnet (rotor) inside a wire coil (stator). The
output from the stator is controlled by varying the current into the rotor
("Field" is short for magnetic field, ie a spinning magnet). The stronger the
current, the stronger the "Field", the more current is produced in the stator.
Obviously RPM affects output as well. Current is passed to the rotor via the
brushes and slip-rings. If you want more power OUT (stator) add more
power IN to the rotor (field). The control of the field voltage (and thus
current) is thru a Voltage Regulator. The VR is a "negative feed back
control" device. If the sensed voltage is low it increases voltage to the
rotor, increasing the field and thus the voltage output of the stator. When
the set voltage is reached than the VR reduces the field. This goes back and
forth many times in a fraction of a second to give a steady state voltage.

(It should be noted that there are three different stator coils that produces
A/C current output or alternating current. The rectifier or diode bridge
turns the three A/C outputs into one DC output, but this is not critical to the
discussion for now, but should be mentioned.)

If the alternator's output is too high or you want to shut the output down
or you cut off all power to the field (rotor). Lets say the VR has failed and
field is uncontrolled and too high, to say the full voltage of the output. In
theory this could give greater and greater voltage in theory. The stock
regulator looks for this and has a secondary "CLAMP" to keep it from going
crazy, but there is a chance the "runaway" could still not be controlled. This
is highly unlikely but in theory possible. This is also where a secondary
redundant device, like what PP added on, comes in, to cover for this
unlikely event. Is this needed? The debate goes on and on and on.


So the old method of "emergency" shut down was cutting the alternators
output off, not the field. Apparently PP taps into the field and uses it to cut
the field off, which in turns cuts to output off, independent of the basic VR
control and protection. This is better, but it is hard to do with an internal VR
because you can not get to the "Field" wire easy. Much miss understood the
IGN wire on the ND alternator is NOT a field wire, it is the ON/OFF signal to
the voltage regulator, the go to sleep or wake up signal, not power to the
field or regulator. So both power to the regulator and field power are all
internal (power comes from the battery thru the big B-lead wire).

I think he modified a stock VR with a voltage sensing device and relay /
electronic switch to open the field current (ie cut it off). The relay/switch is
no doubt solid state. You can see it on the back of the PP alternator. Once
tripped is it shot? I don't know. I suspect once it is tripped, powering down
may reset it? You have to ask PP or Van's. It must be in the operation
instructions.

Again none of this is standard ND alternator. Is it needed. Well for the
price it ain't bad, and if it makes you feel better than it is worth the
premium.

What Van sold before where stock, Suzuki Samurai/ Nippondenso 55 amp
alternators (Van called it 60 amps. They are really rated by ND at 55 amp,
but do put out 60 amp at higher RPM's.) The stock alternator has stock
smaller dia steel pulley, cooling fan runs backward on our plane vs CW
rotation on cars, brushes are stock** and the VR is stock. (** PP claims
that stock brushes wear out faster due to lack of mosture at altitude, acting
as an abrasive? Not sure what new material he uses for brushes but they are
normally carbon, which is pretty slippery.)

The past problems with Van's ND alternator part # 14684 was quality
control of the rebuilds Van got. I am guessing but suspect that the quality
was not consistent, which is a known issue with rebuilds in the auto-
electric rebuild industry. I do know a little about PP and know that he is
using NEW aftermarket parts and think the consistency and quality are
going to be better REGARGLESS of the other modifications, since PP
buys from one source and has control over the product. With a standard
rebuild, the wholesalers can change re-builder without notice. Re-builder's
can can change the aftermarket parts vendor they use. Most all alternators
are rebuilt with Non Nippon Denso parts. They use aftermarket parts. These
parts are made all over the world, but many in Taiwan and mainland China. It
is reasonable to expect that not all have the same quality.

McFly said:
I thought that most ND IR alternators (including 60A
rebuilt units from Van) had OV smarts :confused:

I recall some posts where the ND OV condition limits the voltage to 18
volts (still an OV condition). Does this new unit shut itself down
completely? Sorry, I am still unclear what the difference is. Many
thanks.
Well YES and NO. A stock ND alternator will default to 18v typically, if the
main VR control fails. However there is a scenario where a part fails, shorts
out, bypassing the VR (working or not) and will cause an OV. Since the VR is
bypassed, in this case, you are semi-screwed. Good news NO one has any
proof or evidence this has ever happened. Of the 4 or 5 flaky ND alterantors I
looked into, all but one involved the pilot doing something not smart, like
turning it OFF and than back ON under load, so don't do that or worry. The
one was a mystery, but there was no evidence what happened and details
are sketchy. As long as you have a pull-able CB on the b-lead, if the warning
light comes on, pull the CB.

The advantage of the old alternator is it is replaceable with an off the shelf
unit at an auto-store in a pinch. If you have a PP alternator and it failed,
you could I suppose replace it with a stock alternator with some spicing-in
of a new connector plug in a pinch.

Bottom line the new alternator is way better for the reasons he states in his
web site. New parts with some quality control or consistency is the big
news. The hardware looks nice, the cooling fan is setup for counter CW
rotation, the pulley is aluminum and I think a little bigger dia, which slows
RPMs down. The secondary OV control unit on top of the basic control is a
nice thing. The brush wear thing is a bit of a mystery to me, but he must use
a differnt material?

The new alternator kit is better than the rebuilt product, not because the
OV module hanging off the back but because of QC. Not all aftermarket parts
are the same from my research. I think he took the time to get the better
vendors from what I heard. I would consider it and likely buy it. At $823 for
B&C, no way.

There is nothing wrong with the stock ND alternator. It is fair to say there
was no real control, knowledge about vendors and changes in parts used. If
you want the new PP unit, sell your existing unit and buy the PP unit, or keep
what you got, it is fine.

Sorry I can't predict the future. I don't have the service history on the PP
because it is new. I know the stock units work GREAT, if you install it, wire it
and operate it properly.

Cheers George
 
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thanks George

Thanks for the great explanation. I am replacing my Vans ND that I had to have rebuilt after 15 hours of use (Vans credited me the rebuild price) with the new PP now that the price is better. I'm going to keep the Vans ND as a spare, just in case. I have a total of 95 hours on the rebuilt rebuild unit.
 
Don't ask Jeeves, ask George

Yes, thanks George! Now if you could only tell me how box 14a on this 1099MISC is going to impact shedule C ... ;)
 
Build9A said:
Thanks for the great explanation. I am replacing my Vans ND that I had to have rebuilt after 15 hours of use (Vans credited me the rebuild price) with the new PP now that the price is better. I'm going to keep the Vans ND as a spare, just in case. I have a total of 95 hours on the rebuilt rebuild unit.


Let us know if the swap is "plug and play". I also have the "older" Van's ND alternator, and if it dies, would probably replace it with the newer style - just wondering if it fits in the same bracket, with the same wiring/plug?

Paul
 
I got the $244 prize

Plane Power had a booth at OSH last year and had an introductory price of $325 if you signed up for the show special. They did not have it available at the time but expected delievery in the Fall. As is often the case they did not recieve the new alternators when expected. I recieved an email December 27 notifying me that I could still get it at the OSH special price if I placed the order prior to Feb 10, which I did.

I have recieved the alternator and am impressed with the quality. I have not installed it yet so I can not report on installation or performance. I give credit to Plane Power for honering their offer, the freindly person whom I spoke to when ordering and fast delievery.
 
Just for everyone's info. I just got off the phone with Van's (upgraded my FWF kit to altenator with OV protection) and asked about the rebuilt units that are standard with the FWF kit. Gus says that these units are no longer rebuilt units. They are new units but not of the same "quality" as the New OV units. Perhaps this change had something to do with the inconsistant QA on the rebuilt units.
 
BillC said:
and asked about the rebuilt units that are standard with the FWF kit. Gus says that these units are no longer rebuilt units. They are new units but not of the same "quality" as the New OV units.

Rats! I read all this thinking my new FWF alt was going to be one of these babies. I just got the box of goodies yesterday, but haven't opened it yet. If it does happen to be one of the new ones, I'll report back, and if I get a trade-in cost from the one in the kit to the new OV unit, I'll report that as well.

Rusty (better open the box)
 
Just curious - anyone know off-hand if this is the same belt size as the old 60 amp? If I ever have a problem with my current alt, I'd consider upgrading if I don't need to pull the prop for a belt swap.

Kevin
 
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this weekend

Kevin:

I'm starting my annual this weekend and will check out the plug and play possibilities with the new PP alt. I'm hoping to be able to use the existing belt, otherwise.........pull the prop off, which I'd really rather not do. I recently had it balanced. I actually like the looks of the new brackets and may change them whether the Vans brackets and belt works or not. I'll still try to see if the new one would work with the vans bracket and belt. I'll post a messege hopefully saturday afternoon if someone else doesn't report sooner. Jack
 
High altitude Brushes, who wood-a thunk?

Talking about PP's alternator's features, special brushes where mentioned.

Apparently high altitude and low humidity can cause rapid brush wear on the
otherwise excellent unit.

I did find (googled) that there are high altitude brushes; Special blends of
materials and "adjuvants" have been developed to perform under these
conditions. Apparently the addition of barium salts to the graphite brush
compound would reduce or eliminate the high altitude brush wear.

Go figure, Learn something new everyday. Moral of the story if you fly at real
high altitudes often check and replace your brushes more often. Who would
of thought lack of humidity would affect carbon brushes.

I think there's one data point, one guy got 700 hours out of his stock
brushes. Unfortunately he discovered it on a trip, when the symptoms of
worn brushes started to show on his voltmeter, with somwhat erratic voltage
until it just quit.

I would check brushes at least every 2-3 years or 350 hours. You may want
to check more often at first to get a handle on how much it wears. Only
about 25% of my flying is above 5k-8k.

I don't know where PP gets their "high altitude" brushes to fit their ND unit,
but that's a cool deal and should slow wear for high flyer's. Good to know.

George

**Apparently low humidity conditions can exist above 5,000 feet, but for
sure above 10,000' is going to pretty dry.
 
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Just confirmed that my FWF kit alt is NOT the OV protected unit. It's a ND alt which is supposed to be new, and is internally regulated. Since I don't consider OV protection to be that necessary, I'll just use what Van's sent.

Cheers,
Rusty
 
I ordered the 60 amp Plane power alternator at OSH and received it in January. I installed on a O 320H2AD engine which required a different mounting bracket.
Plane Power worked with me to make the install seamless.
Not yet flying but it looks very good, I recommend buying direct.

Al Smith
RV 6 Finish
N495AB
KEOS
 
Good news/less good news

Ironflight said:
Let us know if the swap is "plug and play". I also have the "older" Van's ND alternator, and if it dies, would probably replace it with the newer style - just wondering if it fits in the same bracket, with the same wiring/plug?

Paul
Paul: Good news is the NEW PP alternator uses the same belt as my 0-320 D1A. So I DON'T have to remove the prop. Not so good news is that the new PP doesn't fit the old brackets. However, it's not bad news, the new brackets are rock solid and easy to install, actually easier, because the main bolt can be inserted with no problem as the bracket is longer and puts the bolt hole below the flywheel. I just installed it and really like it. Not wired yet. It comes with it's own wire plug. Just cut the old one, one wire, one splice...done. I quit to watch a basketball game UF vs UW-MIL. more info to come if you are interested. Jack
 
Can you turn it on and off safely?

I have a B&C SD-8, standby alternator to install on the vacumm pad. I want to be able to turn the main alternator on and off in flight to check the SD-8 is operational. Does anyone know if this is possible?

I asked Vans and they told me all of their alternators could be switched off in flight. I seem to recall hearing on the aeroelectric list that this was not the case.

Another option is to adjust the regulator on the SD-8 such that it puts out 0.5V more than the main alternator. That way I would not need to turn the main alternator off once energised. Does anyone know if this would work?

Thanks
Richard

(Desperately trying to avoid spending $'s on B&C externally regulated alternator)
 
That is brilliant

rwtrwtau said:
I have a B&C SD-8, standby alternator to install on the vacumm pad. I want to be able to turn the main alternator on and off in flight to check the SD-8 is operational. Does anyone know if this is possible?

I asked Vans and they told me all of their alternators could be switched off in flight. I seem to recall hearing on the aeroelectric list that this was not the case.

Another option is to adjust the regulator on the SD-8 such that it puts out 0.5V more than the main alternator. That way I would not need to turn the main alternator off once energised. Does anyone know if this would work?

Thanks
Richard

(Desperately trying to avoid spending $'s on B&C externally regulated alternator)
Let me say that (I think) this info comes from me. If you have a stock ND (nippondendso) alternator with an internal voltage regulator, I would Highly recommend you don't do it (cycle main alternator) in flight, or at all, ever. Yes the IGN wire may turn the alternator ON and OFF, as Van says while the engine is running, but it appears that grief can happen and has happened to those who tried this.

Why? No definitive reason, but it seems that when you do thus, ESPECIALLY, at high RPMs and with electrical load the alternator does not like it and can do weird things. Weird things? Yes fail or it becomes unstable and the voltage becomes erratic. How do I know this? I have made it a little mini mission to get the truth. I was reading about all these hysterical sensational stories of bad things with I-VR's a few years ago. Some where suspect at best and sounded like a sales pitch for another brand. After much research I found most stories where just that, stories, urban legend, either exaggerated, about another alternator altogether or just fiction.

HOWEVER that does not mean all is perfect. There have been many cases of low grade over voltage conditions. (Low grade, under 18 volts). Now the PUNCH LINE. Many of the problems seem tied to the pilot flicking the alternator ON and OFF while it is running under load. One guy always started the engine with the alternator off, than would flick the alternator on after start, and he would shut the alternator off before shut down. WHY? It does nothing and the alternator needs little power or HP to turn during start, because they don't come "on line" until the RPM comes up. After a while the alternator stopped responding to the IGN (ALT) switch and had unstable voltage. Another case the guy did what you say you are thinking of. Cycle the alternator in flight under load. When the pilot did this, to an alternator that was fine just before, the alternator voltage became unstable.

Keep in mind these alternators are made originally for cars. How do they work in cars? They are energized before starting the engine and are turned off when you turn the engine off (and much of the electrical load). Remember that I-VR alternators, the ND's in particular are internally powered. The "IGN" wire is only a signal to tell the alternator to rest when the car engine is not running, to save the battery. It can turn the regulator on and off under load apparently, but that is not the function it was meant for. The regulator gets its power from the B-lead (battery lead) not the IGN lead.


Long and short, there are better ways to see if the AUX alternator works. One method would be a dedicate maintenance run up. Do not turn alternator "IGN" power on and start engine. As Van said it should control the alternator. Turn AUX alternator on and apply electrical load (landing lights). Not Volts/Amps as appropriate. Shut engine down (with out powering the main alternator).

The other method is before shutting down the engine after a flight, turn all electrical power off, go to low idle and turn the main alternator off. I know I said don't turn the alternator ON/OFF while the engine is running at full speed, but I think the least risk would be to do it at idle with min electrical load. Once the main alternator is off, turn AUX on, Rev the engine, apply load and observe instruments. After test shut engine down. Do not turn alternator on.

As far as risk, the worst thing you can do is have the engine at relatively high RPM, with electrical load and turn it ON. There is more than one case where a normally operating alternators was cycled in flight, followed by immediate problems. I have no hard evidence, just that I can point to the application the alternator was designed for does not subject it to this kind of LOAD DUMP/SURGE. I could 100% wrong, but after following the few problems, in every case but one, the pilot did some variation of cycling the alternator under load; I am convince there is a correlation.

The IGN lead is not intended to "switch" large amps. It is just a go to sleep or wake up signal while the alternator is about to start turning or stop turning. Be nice to your alternator.

George

PS. I don't know if running the main and the AUX in parallel is a good idea. I think the idea of not turning the main alternator on, to do a dedicated AUX Alt ground test is best and eliminates of any worry. How often do you need to test the AUX anyway. Once a month, a year?
 
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Just to open this thread again...has anyone fitted a new Vans Altenator to an XP360 without any problems. I remember seeing some picture of slight belt miss allignment somewhere, but cant remember if it was the new or old type of altenators.

Any info appreciated.

Kind Regards
Rudi
 
Gary Bricker

The main difference is the quality. We had a couple of the RB in my area that would not work out of the box. One builder took it to a alt shop and he said it looked like a wrecking yard unit.
 
rwtrwtau said:
I have a B&C SD-8, standby alternator to install on the vacumm pad. I want to be able to turn the main alternator on and off in flight to check the SD-8 is operational. Does anyone know if this is possible?

I asked Vans and they told me all of their alternators could be switched off in flight. I seem to recall hearing on the aeroelectric list that this was not the case.

Richard

(Desperately trying to avoid spending $'s on B&C externally regulated alternator)

Richard:

I've got the same set up and had the same question. I conferred with both Bob Nuchols and the designer/manufacturer of the Plane Power alternators to discuss the point about shutting off the main alternator to test the SD-8. Both said not a problem. You will be doing this at a low power level (engine and amp draw) so it won't pose any problems.

I dumped my plan to buy a B&C alternator and LR-3C-14 regulator and went with the Plane Power 60 Amp alternator. I redrew my schematics and saved enough money to upolster my seats with the difference.

Jekyll
 
Hail RAF Warrior Richard,

rwtrwtau said:
...I want to be able to turn the main alternator on and off in flight to check the SD-8 is operational. ...

I'm not real knowledgeable on multi-sourced power systems.

However, having said the above, I'd rather LEAVE both systems ONLINE and functioning, then INTENTIONALLY shutting one OFF in-flight.

In MY opinion, the best solution is to use an ESV to monitor both outputs. If the SD-8 IS operational as backup, and you "shut down" the main system. You may also be inclined to further troubleshoot the SD-8 and "shut it down" too!

Shutting down a system, to test the backup system, seems a poor choice to me.

I'd like to KNOW if the backup was working (and the primary too!) before the primary fails.

Maybe I'm only half as smart, and twice as crazy as I think I am.
 
Richard and Sprig:

Sprig, I agree, don't be turning that charm off in flight, save it for when you're on the ground.

Shut down the main alternator on run-up to test the SD-8 before flight. Or, start you engine using the e-buss to check your SD-8. Lastly, an alterrnate method is to shut down the main after flight during your shut down sequence to test the SD-8.

Here's a tid-bit I just read from Bob Nucholls, I'll paraphrase:

"the chance of both your main alternator and your backup going bad on the same tank of gas is astronomical"

Further, the SD-8, being a permanent magenet, should have VERY high reliability.

Jekyll
 
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