Except that the G1000 Cessna 172 and 182 did not use larger alternators.
Moreover, at a given RPM, it takes a specific field current to produce a specific output current. There is nothing free here. A larger alternator has heavier windings and can carry more field and output currents.
Have you ever measured the pulley sizes on crankshaft and alternator pulleys? I have, and the alternator is driven at a ratio to keep it within its design RPM. Yes, newer, smaller alternators on cars have higher redlines, but now we're comparing apples and oranges. They also have slip rings of a much smaller diameter than the lower-RPM alternators usually found in aircraft, which reduces the feet-per-second speed against the brushes.
I inspected a lot of alternators as a mechanic, and my experience showed that one could not expect more than maybe 1200 or 1400 hours before the brushes failed and their spring arced against the slip rings and trashed them. On POA we regularly hear of failed alternators, and in most cases it's worn-out brushes. People keep thinking that their car's alternator has 200,000 miles on it, so the one in their airplane must be just fine. But cars are not airplanes, and never will be, Their operating parameters are vastly different, and the risks arising out of failures are much worse.
What are your qualifications and experience in aviation maintenance?
Let's look at an excerpt from a Cessna inspection checklist found in their service manuals:
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See that "7" under special inspection item?
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Plane Power sells a lot of alternators. Some folks think that they're better because they're newer designs and should last a very long time. But if we start checking their service manuals we see stuff like this that isn't in their ads in magazines or aviation websites:
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Then we encounter this:
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