CAM and Valve Springs Question
They're in EVERYTHING. Cessna, Piper, you name it. I even recall one in a Hughes 300C (helicopter-shaped object, somewhat resembling a soap bubble with a rotor and a tail) that did some work for a radio & TV station group I was an engineer for years ago. All use dual magnetos, but the failure rate is worse than any present-day electronic set-up.
If you get a reman, balancing is optional.
They're about as refined as any tractor engine from the mid 20th century. They don't run much over 2500 RPM, and you wouldn't want to as they'll shake apart much above that (see the balancing comment previous to this).
They can be brought into the present day with headers, electronic ignition and electronic fuel injection, but unless it's in an experimental plane, it's illegal to do so.
The valve springs on that engine looked the springs you'd use to check PTV and degree in the cam on an LS engine. I don't know what gauge the wire was, but it was closer to the spring on a screen door than even stock LS truck springs. Red line on that engine was 2700 rpm.
On one of the last flights I took in that Cessna involved severe pucker factor. A long trip at high altitude. You had to plan the decent to not shock cool the engine during the decent. I did everything by the book. When I got down to 1000' above ground level and added power, I found only three of my four cylinders were making power. Stuck valve. I limped it back to my farm airstrip. My passenger just about lost his mind. A more robust valve spring probably would have eliminated that. Apparently, that was pretty common on those engines. I found out after all of this fun and games that Marvel Mystery Oil would have helped. Never ran without it after that.
Unfortunately, the revenue stream for a certificated aircraft engine is no where near as large as the automobile market. As a result there isn't the investment for technology advancement that we saw with the LS1 and the subsequent LS family. The other motivation for use of an autoengine is cost. A 300 HP Lycoming IO-540 runs $120k+ new and $70k+ rebuilt. A typical IO-540 must go thru a overhaul process every 1500-1800 hours of run-time. In an autoengine that might be the equivalent of every 75,000-90,000 miles if your driving 50-60 mph all the time. The cost of an overhaul on an IO-540 is $30-$40k. For these reasons groups are popping up that do autoengine conversions for a fee in the experimental world. I know of two in the LS family and another there are others focused on the 80-150 HP range. The MooseMods facebook page has a short video clip of their production are with 7 planes undergoing stock LS3 installations with a 400-525 HP engines.
https://autopsrus.com/
http://www.moosemods.com/ https://www.facebook.com/adventureaviationwestllc/
Rick
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