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OV Protection for Three-Phase PM Alternator

 
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grnord



Joined: 23 Jan 2010
Posts: 5
Location: Council Bluffs IA

PostPosted: Mon Jan 25, 2010 5:56 pm    Post subject: OV Protection for Three-Phase PM Alternator Reply with quote

I've been considering how to use a three-phase permanent-magnet alternator instead of the single-phase units shown in the Z-figures and discussed in the AeroElectric book. I'd like to put overvoltage protection upstream of the regulator-rectifier but the three-phase output is delivered to it via three feed-wires instead of the two from a single-phase PM stator. It seems that OV disconnect relays in any two feed-lines would interrupt current from all three stator-coil sets; the two AEC 9024-20 modules operating the relays would probably be triggered at slightly different voltages due to component tolerances but an OV event in the narrow window between those two voltages seems unlikely. I have three questions:

(1) Have I overlooked something that makes the basic concept unworkable?

(2) What would be the consequences of an OV event that happened to open one relay but not the other?

(3) Is it possible to control two relays with one AEC 9024-20?

If necessary I could go with a single OV disconnect relay downstream of the regulator but that would leave that not-cheap regulator-rectifier vulnerable. Twinned OV protection is cheaper than one fried regulator...
Rick Nordgarden
Council Bluffs IA


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etienne.phillips(at)gmail
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PostPosted: Mon Jan 25, 2010 9:33 pm    Post subject: OV Protection for Three-Phase PM Alternator Reply with quote

Hi Rick

Putting an OV module upstream of the regulator when using a permanent
magnet alternator is very likely to trip incessantly, as the regulator
keeps the voltage correct by dissipating the extra energy as heat,
unlike a field-coil alternator that actively modifies the voltage
generated by the alternator.

For that reason, I wouldn't think that it's possible to have an OV
event, other than with a regulator failure, and the only way to catch
that would be to stick the OV relay and module downstream of the
regulator, after the rectification has happened, and when you're
dealing with DC.

Now on a different note, wouldn't it be a good idea to stick the OV
relay upstream of the smoothing capacitor? I've seen one of those
70,000uF caps explode due to too much juice, and it's quite
impressive! My thinking is that if your regulator goes off the hook
and supplies the cap with 40V (or whatever the permanent magnet
alternator can generate), and that thing explodes in the cockpit, the
pilot is going to need a new set of underwear...

Thoughts?

Thanks
Etienne

On 26 Jan 2010, at 3:56 AM, grnord wrote:

Quote:

>

I've been considering how to use a three-phase permanent-magnet
alternator instead of the single-phase units shown in the Z-figures
and discussed in the AeroElectric book. I'd like to put overvoltage
protection upstream of the regulator-rectifier but the three-phase
output is delivered to it via three feed-wires instead of the two
from a single-phase PM stator. It seems that OV disconnect relays
in any two feed-lines would interrupt current from all three stator-
coil sets; the two AEC 9024-20 modules operating the relays would
probably be triggered at slightly different voltages due to
component tolerances but an OV event in the narrow window between
those two voltages seems unlikely. I have three questions:

(1) Have I overlooked something that makes the basic concept
unworkable?

(2) What would be the consequences of an OV event that happened
to open one relay but not the other?

(3) Is it possible to control two relays with one AEC 9024-20?

If necessary I could go with a single OV disconnect relay downstream
of the regulator but that would leave that not-cheap regulator-
rectifier vulnerable. Twinned OV protection is cheaper than one
fried regulator...
Rick Nordgarden
Council Bluffs IA


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nuckolls.bob(at)aeroelect
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PostPosted: Tue Jan 26, 2010 12:08 pm    Post subject: OV Protection for Three-Phase PM Alternator Reply with quote

At 11:42 AM 1/26/2010, you wrote:


My recollection is that these Z diagrams have gone through changes over
time as design goals have evolved. I think I remember seeing some of the
PM diagrams without capacitors even. Some systems aren't very sensitive
to alternator noise.. Components never installed never fail.

I don't recall that. Until I did the noise studies we just
"assumed" that the single phase rectified output from the
SD-8 was going to be exemplar ordinarily noisy and adding
a capacitor was a good thing to do. Rotax and others had
been doing it for some years prior.

The surprise was that the SD-8 without a capacitor generated
no more noise than other devices qualified under mil-std-704
design goals that allow up to 1.5 v pk-pk conducted noise
in certain frequency ranges. See figure 15 in

http://www.aeroelectric.com/Reference_Docs/Mil-Specs/Mil-Std-704_excerpts.pdf
I'd guess that the vast majority of PM alternators run for the life of the
airplane so long as the components are held to reasonable temperature and
the wiring is done correctly. Similarly, the output voltage of the
unregulated PM alternator isn't _that_ high - <100V. You can pick a cap
that can stand the full output and not worry about it failing should the
regulator pack it in. I see caps rated to (and above) 100V on the digikey
site for reasonable prices.

True. However the majority of catastrophic failures I've
put my hands on were the result of hooking the capacitor
up backwards. And the SD-8 turning at 4,000 rpm on a vacuum
pump pad isn't a snarling monster either. Getting OV
protection sensed downstream of the capacitor and cutting
power upstream of the R/R seems to be the elegant solution.

Bob . . .


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