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Bret Ludwig wrote:
J.Kahn wrote: snip Exactly right Clare. The soob has a bulletproof interior but the use of liquid cooling plus a drive system adds two complete failure modes that aren't there at all with the Corvair. With the Corvair if you take care of the systems design aspect, basically by using sound aircraft design practices for carburation and ignition, I question whether LyCon practice, which is actually derived from small flathead gasoline burning farm tractors- a big single barrel updraft carb and two farm tractor magnetos- is intrinsically "Sound design practice". Remember when the Continental, Lycoming and Franklin engines were introduced they were not considered sound aircraft design! Real airplanes used P&W or Wright radials or Allison or Curtiss liquid cooled inlines-the E-2/J-2 Cub and similar planes were considered the ultralights of their day, and before WWII one could fly an airplane without a license if it wasn't registered and flown only within one state (until the states, except Oregon, outlawed it-which is why the early homebuilders often moved there.) Nothing smaller than a Waco was considered a real airplane. Simple, light, reliable is the Prime Directive, regardless of how old the technology is. When it comes to airplanes, that is sound design practice, when considering ass pucker levels while in climbout over a builtup area or over a tree line. I don't care if it's made of rocks. If it's simple, light and reliable, the fact that it's derived from tractors is irrelevant. The big radials of the old days, when you look at it, were also very simple, light reliable designs in relative to the alternatives in view of the power requirements. You will note that the "more sophisticated" liquid cooled aircraft engines never survived in a significant way past WWII in commercial service, with one unusual exception, the Canadair North Star airliner, which used Merlins. Everything else was radials because relatively speaking they were the simplest and lightest and most reliable solutions before jet engines, even if their air cooling and pressure carbs were "crude". This is the point. If you want to take advantage of technology like electronic control, you have to design for complete redundancy if your control system has a sudden potential failure mode. Not practical for the homebuilder. The farm tractor technology engine can have its components built with sufficient inherent robustness, or have a very gradual failure mode, to provide the required safety without needing duplicate systems, (like a crude but simple carb) or at least a minimal level of redundancy. I am a fan of auto conversions, but believe that those conversions to be viable must be as close as possible to a traditional aircraft engine from the standpoint of simplicity and overall design, and the Corvair using a Stromberg aircraft carb and a dual primary points ignition comes closest to fitting the bill of any conversion I have seen besides a Great Plains VW. Now that the crankshaft strength issues are known and a way forward is clear, the Corvair engine's potential is even better than before as a conversion IMHO. Cheers John Kahn Montreal |
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![]() "Lou" wrote in message oups.com... But would you have to replace the engine? Maybe just a crank overhaul every 4-500 hours, in the middle of winter, after a good snow storm, nothing else to do. Good point what would a like new, best for the engine, crankshaft cost? |
#3
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$50-76 on ebay,
$600 to have Bill Wynne modify it. |
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![]() "Lou" wrote in message ups.com... $50-76 on ebay, $600 to have Bill Wynne modify it. Replace it every year or two at annual it's still a great deal. |
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