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#41
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Morgans wrote:
"Matt Whiting" wrote How so? Whem I was much younger, an all cars had points and condensers, I would do my own tune-ups. Sometimes the timing would need to be adjusted. How to do it, if you did not have a timing light handy? I would loosen the distributor bolt, until it was tight enough to move by hand, but not so loose that it would not vibrate around. After that, I would get the engine warmed up, and take it out on the road, and punch it. It was not so obvious if the timing was retarded a bit, until it was really retarded. It was _quite_ obvious when it was too far advanced, as would not have much power, and would knock like crazy. That a good enough answer? Maybe to another question. You didn't address why having the timing advanced too far would cause a greater power loss with mogas than with avgas. And noise from igniting the mixture too soon and detonation are two different phenomenon. Matt |
#42
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![]() "Matt Whiting" wrote Maybe to another question. You didn't address why having the timing advanced too far would cause a greater power loss with mogas than with avgas. And noise from igniting the mixture too soon and detonation are two different phenomenon. Sorry, I'll try again. The higher octane of 100LL will allow more advanced spark settings without knock and detonation, than will the lower octane mogas. End result would be that the mogas could show a loss of power, when avgas is still allowing the engine to function normally. I don't disagree with the fact that in normal conditions, and a normal engine, the power of an engine running 100LL or mogas should be virtually the same. -- Jim in NC |
#43
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Morgans wrote:
"Matt Whiting" wrote Maybe to another question. You didn't address why having the timing advanced too far would cause a greater power loss with mogas than with avgas. And noise from igniting the mixture too soon and detonation are two different phenomenon. Sorry, I'll try again. The higher octane of 100LL will allow more advanced spark settings without knock and detonation, than will the lower octane mogas. End result would be that the mogas could show a loss of power, when avgas is still allowing the engine to function normally. This is only true for engines that have very advanced ignition timing, which isn't true for most GA piston engines, or engines with very high compression ratios, again, not true for most GA piston engines. Keep in mind that most were designed to run on 80 octane avgas... I don't disagree with the fact that in normal conditions, and a normal engine, the power of an engine running 100LL or mogas should be virtually the same. Yes, I can't imagine many GA piston engines where this wouldn't be the case. Maybe a turbocharged engine running very hot. Matt |
#44
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Jay Honeck wrote:
All good ideas. I, too, have often wondered why I have all the data in the world on my JPI engine analyzer, but no "under-the-cowl" temperature readings. Jay, there's no reason you couldn't take one of the unused channels and put a thermocouple on it. Hmm, maybe not. If you put it on the IAT, I think that will change the carb temp to TIT. That's assuming you have the oil temp, OAT, and carb temp probes like I do. |
#45
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Matt Whiting wrote:
This is only true for engines that have very advanced ignition timing, which isn't true for most GA piston engines, or engines with very high compression ratios, again, not true for most GA piston engines. Keep in mind that most were designed to run on 80 octane avgas... I don't disagree with the fact that in normal conditions, and a normal engine, the power of an engine running 100LL or mogas should be virtually the same. Yes, I can't imagine many GA piston engines where this wouldn't be the case. Maybe a turbocharged engine running very hot. Matt There are plenty of high compression GA piston engines that can't use mogas because the octane requirement is too high. The majority of GA engines are lower octane (something like 78% of the engines IIRC). The majority of the hours flown in piston aircraft however is done by the 21% of aircraft that have higher octane requirements than mogas can offer, my 260 HP O-540-E4B5 included. It is a normally aspirated 6 cylinder engine, but with high enough compression that there is not sufficient detonation margin with less than 96 octane fuel. |
#46
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Ray Andraka wrote:
Matt Whiting wrote: This is only true for engines that have very advanced ignition timing, which isn't true for most GA piston engines, or engines with very high compression ratios, again, not true for most GA piston engines. Keep in mind that most were designed to run on 80 octane avgas... I don't disagree with the fact that in normal conditions, and a normal engine, the power of an engine running 100LL or mogas should be virtually the same. Yes, I can't imagine many GA piston engines where this wouldn't be the case. Maybe a turbocharged engine running very hot. Matt There are plenty of high compression GA piston engines that can't use mogas because the octane requirement is too high. The majority of GA engines are lower octane (something like 78% of the engines IIRC). The majority of the hours flown in piston aircraft however is done by the 21% of aircraft that have higher octane requirements than mogas can offer, my 260 HP O-540-E4B5 included. It is a normally aspirated 6 cylinder engine, but with high enough compression that there is not sufficient detonation margin with less than 96 octane fuel. I'd like to see your source of these statistics. Matt |
#47
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Matt Whiting wrote:
Ray Andraka wrote: Matt Whiting wrote: This is only true for engines that have very advanced ignition timing, which isn't true for most GA piston engines, or engines with very high compression ratios, again, not true for most GA piston engines. Keep in mind that most were designed to run on 80 octane avgas... I don't disagree with the fact that in normal conditions, and a normal engine, the power of an engine running 100LL or mogas should be virtually the same. Yes, I can't imagine many GA piston engines where this wouldn't be the case. Maybe a turbocharged engine running very hot. Matt There are plenty of high compression GA piston engines that can't use mogas because the octane requirement is too high. The majority of GA engines are lower octane (something like 78% of the engines IIRC). The majority of the hours flown in piston aircraft however is done by the 21% of aircraft that have higher octane requirements than mogas can offer, my 260 HP O-540-E4B5 included. It is a normally aspirated 6 cylinder engine, but with high enough compression that there is not sufficient detonation margin with less than 96 octane fuel. I'd like to see your source of these statistics. Matt I believe the numbers were from AOPA. I'd have to do some digging to find them now. Those are the approximate numbers they were throwing around about a year ago. |
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