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![]() Peter Dohm wrote: What diameter of prop can you turn at 4000 rpm? A Volkswagen is NOT a good direct drive aircraft engine because it produces good power at 3200 to 3800 rpm. But it's a hell of a lot easier to put a redrive on a VW than an O-200. Actually, 46 to 48" The VW 1600 was used that way with considerable success in the early KR-2 aircraft. However, that only meant 60 to 65 HP with the small displacement, and the modestly oversized cylinders which would be fitted without fairly radical case machining provided only a very modest addition of take-off power. Cruising speed was only about 115 kts within the thermal capacity of the stock heads--which has been discussed previously in this NG--so pilots who were heavier or wanted to fly faster sought more oomph. Since VW engines in race cars and hot rods (sand rails, etc) operate under continuous power at higher power settings than this (I have driven Bugs up tall mountains in 90 degree weather at 25+ inches Hg at 3000-3700 rpm for as long as the mountain lasted, which was longer than enough to heat the head all the way through) this thermal analysis theory is flawed. The 356/912 Porsche has a head not much bigger and they run for hours on the Autobahn flat out. The difference is these engines have a cooling blower, where most aircraft installations run them as free cooled engines. Free air cooling and direct drive are simple. In the old A-65 and the airframes it went into that worked okay. But the time has come to recognize that for an airplane to not be something looked on as an antique, it needs a liquid cooled engine with a flywneel, redrive, single lever power control and enough power to haul fat people and lots of crap out of high and hot fields with healthy margins to spare. |
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