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#21
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#22
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Any aircraft engine crankcase I've been inside of has relatively small
slots below the crank where the case halves meet effectively isolating the sump from the crank in regard to "windage". Ah! The man who truly *knows* weighs in! :-) So how 'bout it, TC -- is the M20 a good thing, a bad thing, or 'bout the same thing with regards to my O-540? -- Jay Honeck Iowa City, IA Pathfinder N56993 www.AlexisParkInn.com "Your Aviation Destination" |
#23
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Mike Rapoport wrote:
But you are putting more heat in because of having the crank contact the oil more of the time. The temp will be higher. Is this true in Lycs and Contis? I don't know about the airplane engines, but car engines have the upper fill limit established to prevent this. Having the crank contact the oil will froth it pretty quickly and the oil pump can't pump aerated oil very well. This is why the dipstick always has a warning not to overfill. I'd be surprised if airplane engines permitted a fill to the point of crank contact. This is generally only done intentionally on splash lubricated engines such as those found in cheap lawnmowers. Matt |
#24
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Mike Rapoport wrote:
The case has no more area and no more airflow across its surface with more oil in the sump. No kidding, but it does have more oil contact area and thus the oil can transfer more heat to the case. Matt |
#25
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The oil level is about 1" higher and the case is highly conductive.
Mike MU-2 "Matt Whiting" wrote in message ... Mike Rapoport wrote: The case has no more area and no more airflow across its surface with more oil in the sump. No kidding, but it does have more oil contact area and thus the oil can transfer more heat to the case. Matt |
#26
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The crank in not in contact all the time but the oil is sloshing around as
the airplane moves. When the level gets down to where it isn't contacting the crank, the oil stops being blown out the breather (at least in meaningful quantities.) Mike MU-2 "Matt Whiting" wrote in message ... Mike Rapoport wrote: But you are putting more heat in because of having the crank contact the oil more of the time. The temp will be higher. Is this true in Lycs and Contis? I don't know about the airplane engines, but car engines have the upper fill limit established to prevent this. Having the crank contact the oil will froth it pretty quickly and the oil pump can't pump aerated oil very well. This is why the dipstick always has a warning not to overfill. I'd be surprised if airplane engines permitted a fill to the point of crank contact. This is generally only done intentionally on splash lubricated engines such as those found in cheap lawnmowers. Matt |
#27
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On Mon, 16 Aug 2004 02:35:58 GMT, "Jay Honeck"
wrote: Any aircraft engine crankcase I've been inside of has relatively small slots below the crank where the case halves meet effectively isolating the sump from the crank in regard to "windage". Ah! The man who truly *knows* weighs in! :-) So how 'bout it, TC -- is the M20 a good thing, a bad thing, or 'bout the same thing with regards to my O-540? I've read mixed reports about the M20, unfortunately have no personal experience. Have heard people swear by them, have heard people swear at them. Have taken care of several Bo's with the original Walker (?) air/oil sep. They were for the most part equipped with wet vac pumps as well. In those cases, there was what I would consider to be an acceptable accumulation of oil on the belly. I can't really speak with any authority on the whole "putting crud back in the crankcase" deal, but I can add that every 325-350 hp Navajo breathes through a factory-installed air/oil sep. My guess would be that these engines tend to be heavy-breathers. When they get up there in hours, the oil stripe on the bottom cowl gets heavier, in spite of the air/oil sep. Was never of the mind to bypass one to see how much difference they make. Cleaned the inside of them rather infrequently, usually at mid-time (900-1000 hrs) and at TBO. We ran the Navajo's at 11 qts after an oil change, usually keeping them between 10 and 11 in service (dump in a qt when it get down around 10). Actually, never really thought about the air/oil sep being a factor in determining that level. Only ever had one come up shy on TBO-catastrophic turbo failure w/oil contamination. Don't think I coulda blamed that one on crud from the ari/oil sep... TC |
#28
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Mike Rapoport wrote:
The oil level is about 1" higher and the case is highly conductive. So, 1" times the circumference of the case is a fair bit of area and with a highly thermally conductive Al case, that will reject additional heat to be sure. Matt |
#29
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"Mike Rapoport" wrote in message nk.net...
More oil does not improve cooling. If you think about it, it makes sense. Where would the additoinal heat go? Same oil cooler, same cooling fins, same baffles producing the same airflow. The oil will actually be hotter since the crank is going to contact the oil in the sump with 50% more oil. Thats why the top 4 qts of oil is leaving through the breather in the first place. The oil will be somewhat cleaner since the same amount of contaminates are dilluted by more oil. As a practical matter, you would probably be better off with a finer oil filter than more oil. There is an article on oil filters in Aviation Consumer this month that is worth reading. Mike MU-2 Helio Courier (arriving today!) I'm convinced Mike is right about this. Fits in the same category as the argument that auto coolant works more poorly without the thermostat 'cuz it goes thru the radiator "too fast" and doesn't cool properly. Another triumph of math & science. Bill Hale |
#30
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So let me try a theory here.
The lack of positive crankcase ventilation for these engines is really a bad feature. A friend measured the PH of the condensate water on the oil dipstick of an IO-520. PH was 2: Like nitric acid. Having that in your crankcase is bad. So why shouldn't we provide PCV by dumping the output of the wet vacuum pump directly into the crankcase? On the IO engines, I'd run it into the timing plug in the front. Then I'd have the air-oil separator on the crankcase breather. That would give several CFM of air douching the crankcase. Now the problem is: How much moisture would be condensed out of the breather air? A gallon/hour? An ounce/hour? I've wondered if the Airwolf/Walker separator could be modified so that the oil drain had about a 3/4" standpipe in it with a second drain added for water that was flush with the bottom of the device. Then the water could be drained during preflight. The oil would decant back into the crankcase. I know there are EPA considerations on this. Just a thought. I think less corrosion would lengthen the cylinder life. Bill Hale |
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