Once when I was sitting on the flight deck of a 747 and looking at the flight engineer's panel I seem to recall the total in-flight electrical load was surprisingly large, like 100's of kW or perhaps megawatts. This would have been for hydraulic pumps, HVAC systems, lighting, electronics, galley systems, avionics, fuel pumps and all sorts of things I can't recall. It surprises me that generation at 240 VAC or 400 VAC would be sufficient to handle this. I can't recall what the voltages on the the 747 were, but surely higher voltages would lead to thinner wires and lighter weight, or does that have to be offset with the additional weight of transformers?