AeroElectric-List Digest Archive

Sun 08/30/20


Total Messages Posted: 1



Today's Message Index:
----------------------
 
     1. 07:55 PM - Revmaster 'dual' alterantors (Robert L. Nuckolls, III)
 
 
 


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    Time: 07:55:13 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Revmaster 'dual' alterantors
    I've had a few weeks (and road trips) to apply some 'asphalt engineering' effort to a combination of threads discussing relative fragility of the Revmaster 'dual' alternators. The latest thread explored the notion that changing from SLVA to LiFePO4 was much more likely to burn an alternator winding. This is not a new topic here on the List . . . found a few other postings on the same problem. Without talking to the designers, it's difficult to KNOW the original thinking behind the design. We also cannot know what efforts the factory has applied to this issue over the years. But I think we're on pretty firm ground to assert that the current design is marginal with respect to thermal robustness. Alternator windings should be as reliable as propeller bolts. You might smoke some regulators, trash some batteries, find yourself wanting for a few more amps of output . . . but suffering destruction of the windings suggests the alternator is a weak link in the system. Based on the drawing that Dan supplied a few weeks ago it seems that the designers intended that only one of the two windings be used at the same time. I'm guessing that this is a "normal-and-spare" design philosophy. Therefore, any time a winding fails due to exceedance of thermal limits, the other winding was off line. We don't know the internal configuration of the recommended rectifier/regulator but it's almost certain to included silicon controlled rectifier and one diode in series on each conduction half- cycle. That's 3, silicon junctions in series that carry alternator output current. My current hypothesis suggests that it would be much better to use BOTH windings all the time. Reduce the current in each winding by 50% or more. It seems better to have one configuration that's bulletproof than two relatively fragile configurations that 'back each other up'. Here's the line of reasoning supporting this design goal. Recall the bits-and-pieces of design? (1) properties of materials, (2) management of energy and (3)refinement of process. In this case, our weak link seems to center on an energy management issue. Some copper windings are heating past practical operating limits. This can be either an insulation failure, wire failure or both. Properties of Materials: We know that copper has a pretty significant positive resistance coefficient for temperature. We observed this in the temperature vs. current observations in battery contactors: https://tinyurl.com/mpcgp3t https://tinyurl.com/k6bwdqo We also considered the physics of why an overloaded wire tends to burn open at the center of a free-air span. As copper heats up, resistance goes up, voltage drop goes up, dissipated energy goes up, temperature rises some more . . . and you can see where this is headed. Take this tid-bit of knowledge about copper wire and consider how many times you've observed or heard of the windings or lead wires of any system failing due to overheat. I've seen some windings burn up on alternators for reasons OTHER than poor thermal management. I've never had a winding burn on my car. I've had one short and start popping fuses . . . but I doubt that it was due to burned insulation or melted wires! The point is, ANY configuration that demonstrates repeated failure to do open wires or cooked insulation is MARGINAL at best; hazardous at worst. Okay, how to reduce the load in Revmaster alternator wires . . . hopefully without compromising ability to deliver ENERGY into the system. Here's the energy management consideration: We know that PM alternators have a checkered history of performance . . . but mostly due to stone simple regulators that DO NOT offer active current limiting. Furhter, many versions use a full wave bridge consisting of two pairs of junction diode and silicon controlled rectifiers. Alternator output current flows through two of these devices with total drop on the order of 2 volts. 2 volts out of a 14v system is a substantial proportion of energy . . . something on the order of 15 to 25 watts that needs to be managed in those cute little castings . . . but that's another story. Harking back to the earliest days of my studies in electron herding, ac rectifiers were vacuum tubes (not junctions) and ac power sources were transformers plugged into the wall (not spinning magnets). Except for the systems with very low energy requirements (table top radios), the rectifiers were dual diodes driven from either side of a center tapped transformer secondary. This configuration had some profound effects in thermal management. EACH diode carries 1/2 the total current. These devices have considerable resistance . . . watts I(squared) x R so if you reduce current by 1/2, watts goes down to 1/4. Same thing happens in the transformer secondary . . . the secondary wire size can be made smaller in a trade off between energy lost and transformer size. Refinement of process: So take a peek at the simplified proposal diagram. Hook the two Revmaster windings in series-aiding and bring out the center-tap. Connect in full wave configuration with only TWO junction rectifiers. Feed this resulting energy off to a filter capacitor size to be determined. This will give us a 'supply voltage' of some value ideally adjust to about 20VDC at cruise RPM and alternators full load design point. This voltage is going to be all over the place depending on load and engine rpm . . . but that's the nature of the PM alternator. Now, let's power condition that energy with a constant current, constant voltage, switch-mode regulator. NOW we have a BIG difference in performance: Voltage is adjustable and controlled by active electronics. Current is adjustable and limited by active electronics. I suggest this configuration offers significant improvement in Revmaster's engine driven power source. Energy being delivered to the regulator is at significantly higher than the output set point, CURRENT in from the alternator will be LOWER than current delivered by the regulator. Further, each winding works 1/2 of the time so it follows that heating effects on each winding are much reduced from the current configuration. Silicon junctions in the rectifier are significantly reduced off-setting some new losses introduced by the electronic CCCV regulator. It seems that we could craft an engine driven power system that almost never fails in exchange for one that fails too many times and for the wrong reasons. I'm tied up in some house remodeling and we've added another grandson to the population of Medicine Lodge Jr High School . . . so refinement of this idea will be slow. But I'm building an alternator drive stand, power supply and load bank out in the mess-making shop. B&C has provided me with both PM and wound-field test articles. I have a couple of those CCCV regulators that we discussed on hand right now. They may not be the right size in all respects but satisfactory for proof-of-concept experiments. I already have some LiFePO4 and SLVA batteries on hand. The pieces are coming together. Comments and considered critical review are most welcome. Bob . . .




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