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#11
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Oh those CERTIFIED plane engines !!!!!!!!!!!!!!!!!
"Richard Lamb" wrote in message ink.net... RapidRonnie wrote: Bottom line is that if you use an auto engine made in the millions you can research the failure rate, particularly if you pick an engine used in motorsports run to destruction you can see where they fail first. I would pay a premium, a big premium, to be able to fly a small block Chevy in terms of a bigger airframe than you otherwise would, just for that huge knowledge base. Gently disagree, Ron. The reason is that the prop loads are far different from anything you'll see on the race track. Apples and oranges again... Richard Perhaps, but it is entirely possible to use a Geschwender chain drive or one of several belt drives that have all been around for 30 years themselves. Their job is to match the prop to the crank. The loads on the crank can be reduced to nothing but torque, and the torsional vibration issues dealt with. The engineering has been done, and it works. The NorthWest Aero belt drive http://www.northwest-aero.com/ as an example, was derived (I think) from the Blanton PSRU that has been around since the 1960's. Many Ford 3.8 and GM 4.3l V6's and 350 V8's have been run many thousands of hours. Improvements have been made over the years (better belts, different bearings, easier adjustments. If there has been a failure of a properly maintained one in the last few years, I'd love to hear about it. Failures of auto conversions tend to be stupid stuff anyway. This guy http://www.epi-eng.com/Prop-SudnStop.htm somehow left one of those blue paper towels inside his cowling. It got sucked through the turbocharger, shredded, and completely clogged the air filter. Bad...but not the fault of the fact that it was an auto engine. |
#12
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Oh those CERTIFIED plane engines !!!!!!!!!!!!!!!!!
The vast majority of auto conversions use a PSRU to transmit the power
from the motor to the prop. Ron has pointed that out nicely. You can see mine up close by going to my website and clicking on pics. Quick, simple and a picture is worth a thousand words. Ben www.haaspowerair.com |
#13
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Oh those CERTIFIED plane engines !!!!!!!!!!!!!!!!!
Just guessing here, but aren't the O-235 adn O-320 cranks solid rather than
hollow (for constant speed props)? They are hollow, and some models of the engines have provision for a governor. That hollow crank has been the subject of an AD; the front end of the crank gets cold in flight due to the prop's heat loss and the hollow bore, open to the case, gets condensation and oil in it. Those mix and form sludge and acids that eat away at the inside of the bore and weaken the crank. See: http://www.airweb.faa.gov/Regulatory...5?OpenDocument Hollow shafts are stiffer than solid shafts. The stresses are all concentrated in the outside wall, with no central material to act as a fulcrum to stretch the outside on bends. Try bending a piece of 5/8" bar and one of 5/8" tube sometime (same material, of course) and see the difference. The bar will bend, but the tube will resist bending until it suddenly kinks. Cranks need to be stiff, especially where they are loaded with gyroscopic forces, and need to be light, so they're mostly hollow. Dan |
#14
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Oh those CERTIFIED plane engines !!!!!!!!!!!!!!!!!
The motor is actually a 347 cu in displacement, that was obtained by using a stroker crank and .030 overbore. Yea, that's a very common thing to do. All the parts available. Right now there are probably 100 or so of those cranks on ebay. The whole thing is not really that inexpensive to create because the bare Ford aluminum block by itself is 4400.00 dollars. That's why I went with a Ford SOHC 4.6l instead, for my personal project. I found a short block - new - aluminum block and forged internals for $400 on EBay. Another $1K for heads and all the other stuff, and the motor was running. I didn't realize how much bigger physically the 4.6l is than the 5.0l pushrod motor. It's on an (modified Adventurer) Amphibian, with a pusher configuration and mounted right at the CG. With a pusher, you want the prop traveling through air that is uniform all the way around, and disturbed as little as possible. My cowl will be a big cylinder, uniform all the way around centered on the prop flange so the size is not really a problem for me, but it'd not be the best choice for a normal tractor aircraft. Weight is not much over 450#, but the footprint is huge in comparison. Like I said - your choice is much better! But I'm having fun anyway... |
#15
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Oh those CERTIFIED plane engines !!!!!!!!!!!!!!!!!
Ron wrote;
My cowl will be a big cylinder, uniform all the way around centered on the prop flange so the size is not really a problem for me, but it'd not be the best choice for a normal tractor aircraft. Weight is not much over 450#, but the footprint is huge in comparison. Like I said - your choice is much better! But I'm having fun anyway... /////////////////////////////////////////////////////////////////////////////////////////////////////////// If ya got a digital cam I would love to see some pics of the project your building. Send it to stol83001 at yahoo dot com. Ben |
#16
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Oh those CERTIFIED plane engines !!!!!!!!!!!!!!!!!
"stol" wrote:
My same package is at 434 lbs and can be configured to put out from 120 hp all the way to 600+. The 600 number is for takeoff and five minutes, then you have to throttle it back to the the low 5's to get it to live. Getting an honest 600 horsepower from a 347 cubic inch engine would require doing things to it that would seem to be quite incompatible with service in an aircraft. Approaching 2 horsepower per cubic inch requires either significant turbo/supercharger boost and/or turning the engine at VERY high rpms. Have you actually dyno'd the engine to check the realistic horsepower? 400 would probably be enough to do VTOL on a CH801... ;-) Mark Hickey |
#17
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Oh those CERTIFIED plane engines !!!!!!!!!!!!!!!!!
Mark Hickey wrote:
"stol" wrote: My same package is at 434 lbs and can be configured to put out from 120 hp all the way to 600+. The 600 number is for takeoff and five minutes, then you have to throttle it back to the the low 5's to get it to live. Getting an honest 600 horsepower from a 347 cubic inch engine would require doing things to it that would seem to be quite incompatible with service in an aircraft. Approaching 2 horsepower per cubic inch requires either significant turbo/supercharger boost and/or turning the engine at VERY high rpms. Have you actually dyno'd the engine to check the realistic horsepower? 400 would probably be enough to do VTOL on a CH801... ;-) Mark Hickey I'm kind of curious about how Chris Heintz feels about hanging such a monster motor on his airplane. His web site says 150 to 240 bhp with max installed weight of 440 lbs. http://www.zenithair.com/stolch801/performance.html |
#18
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Oh those CERTIFIED plane engines !!!!!!!!!!!!!!!!!
Richard said:
I'm kind of curious about how Chris Heintz feels about hanging such a monster motor on his airplane. His web site says 150 to 240 bhp with max installed weight of 440 lbs. ///////////////////////////////////////////////////////////////////////// I am under the 440 lbs as he spec'd out. Altho that is a old number, even since the 801 disintagrated over Calif a few years back .Zenith reduced it to 400 lbs if I remember correctly. I do check my airframe very closely often and it shows no signs of deforming anywhere, I am based at 6500 msl so the 330 sea level nuumbers are reduced by about 25-30%, that puts my set up in the 250-260 range. I will need to be careful when I get my toy down to sea level where thick air lives though. I should add the Calif crash was not caused by the plane though, "we hope". The NTSB found a high level of drugs in the pilot and passengers blood which apparently lead to them to believe they invincable while doing areobatics. They won't do that again. Ben N801BH |
#19
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Oh those CERTIFIED plane engines !!!!!!!!!!!!!!!!!
"stol" wrote:
Seeing how this same engine design and componants are used in the Nascar truck series week after week with some teams going several race weekends without freshening up the motor pretty much explains how bulletproof the package is. Also keep in mind they are putting out closer to 750 hp @ 8800 rpms or so this year. A couple thoughts there - turning an American V8 at 8800 rpm on an airplane wouldn't be something I'd be tempted to do - even once, and I'm demonstrably more stupid than most people. And those Craftsman Series trucks aren't running WOT all day long. "Several race weekends" involves only a few hours (maximum) at full power, and even then it's not at all unusual to see them leave their motors on the ground in pieces down the back straight. Keep in mind too they are flat tappet motors too. Mine is a full roller set up which adds alot of available HP due to much less friction in the motor. There's a difference, but it's not that big. Remember that any difference would be converted to heat, and if you were losing any meaningful percentage of the power by heating the cam and lifters, the top of the motor would melt in VERY short order (since the oil would stop working). The other issue you'd have to face is that if your PSRU is optimized for cruise speed (to give you reasonable cruise at the "low" RPM you run it at cruise), you're gonna be spinning that prop WAY past its design limits at 8800 rpm. Mark Hickey |
#20
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Oh those CERTIFIED plane engines !!!!!!!!!!!!!!!!!
A couple thoughts there - turning an American V8 at 8800 rpm on an airplane wouldn't be something I'd be tempted to do - even once, and I'm demonstrably more stupid than most people. And those Craftsman Series trucks aren't running WOT all day long. "Several race weekends" involves only a few hours (maximum) at full power, and even then it's not at all unusual to see them leave their motors on the ground in pieces down the back straight. Keep in mind too they are flat tappet motors too. Mine is a full roller set up which adds alot of available HP due to much less friction in the motor. There's a difference, but it's not that big. Remember that any difference would be converted to heat, and if you were losing any meaningful percentage of the power by heating the cam and lifters, the top of the motor would melt in VERY short order (since the oil would stop working). The other issue you'd have to face is that if your PSRU is optimized for cruise speed (to give you reasonable cruise at the "low" RPM you run it at cruise), you're gonna be spinning that prop WAY past its design limits at 8800 rpm. Mark Hickey /////////////////////////////////////////////////////////////////////////////////////////////////// No need wasting any more of my time on you. This is America and we all have our own opinions. You clearly didn't read my previous post or my explainations of using a percentage of power. This afternoon I will be flying in an auto engine powered plane while you sit there and fly your keyboard.... Have fun and type safely...... Ben |
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