A dyno report is a piece of evidence. Anecdotes are nothing but stories. Big difference!
I am curious about how much Lycon charges to port, polish, etc. an engine as you describe in order to obtain the promised results.
I've had long discussions with Lycoming OEM engine representatives about both the porting/polishing process Lycon offers and the legality of increasing the horsepower of their engines. It has been my experience that if you really want honest answers to your questions you can best rely upon advice from people who aren't trying to sell you their product/service.
Moreover, we all like to boast about how powerful/great our own setup is: you know, we all have an O-320 that produces 210hp and 1000 lbs. thrust at 5000' on an 850 lb. SC, not to mention we all have 12" dicks. Of course none of us have the yardsticks handy to easily measure our claims, so they're hard to prove/disprove. Really; how many of us have never exaggerated their own airplane's performance? Hyperbole is, I think, one of our common denominators, so we can't be trusted either.
Shaving weight from your aircraft will likely increase its performance far more than any pie in the sky engine tuning promise, for a lot less money. IMHO, of course.
Fact; I had an O-320 E2D built by Lycon. It came with the test run results. 10 to 1's, polished and flow balanced. 209.9 H.P. at 2700 RPMs. Unless they are faking the numbers that is what it made. I have it on the plane now and it is the smoothest, hardest pulling O-320 I've ever sat behind. I don't brag about it, I just enjoy it.
And now I need to retract that statement. With just a little Google searching I see articles that say dynos are not like rulers where an inch is always an inch. There are up to 30% variations between different dynos. That's interesting. This whole topic is interesting.
Did you advance timing on crank gear?
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Are any explanations offered for the variation, other than inaccurate torque or RPM readouts? Atmospheric conditions or fuel composition, maybe??
This is the first suggestion I have read that the timing would change. Have any of the other builders changed the timing of the crank gear when upgrading their engine ? To be honest this is the first I have ever heard of a gear on the crank dealing with timing . Lycon nor others have mentioned this before, obviously I now have to investigate . I do plan to use the P-mag when I reassemble, may or may not go with a second. I was going to use a secondary standard magneto for now see how it works out .
Yes Stewart, I'd enjoy looking at the dyno report. Dunno if you still have my email, it's gordon dot misch at gmail. Thanks for the offer.
Not a 320. Mine's an IO-400. I chose the tried and true method for producing horsepower and torque. There's no replacement for displacement.
Do your homework before putting a Catto (or any other lightweight prop) on a high compression engine. This subject was being discussed a couple years ago and some valid concerns were raised regarding the lack of flywheel in conjunction with the more pronounced impulse and deceleration cycles of the high compression engine. You might have some undesirable harmonics.
I realize that you are in Canada with different rules. I question your friends approval of that prop. If you look at the TC data sheet for that engine prop combination you will find that it is not approved with a long diameter.That said my neighbor with O-360 and the identical plane in comparison to my aircraft would be considered a poor performer. His plane is much heavier because of the engine, larger floats the large fixed pitch pawnee prop and heavier aircraft overall. I break water in half the distance and climb better, even have a slightly better useful considering his fuel burden. His aircraft is certified, he cannot deviate, He can cruise faster though , 115mph vs my 95mph.
Lots of stuff can get hurt even with a wood prop strike. If you understand the HP modifications you purpose are not cumulative, I would do them if that is what you want and leave the prop until you see how it performs with all the mods. The other issue not posted is CHT!! High compression pistons make a lot of heat. Do you have a 4 cylinder CHT/EGT? Fuel flow would also be nice. Do you really want you limit yourself to 100LL for all you flying?? I don't think P mags help HP at sea level (I could be wrong). In general high HP from small engines means shorter life. Just things to ponder, you have had great advice for others.
DENNY
I realize that you are in Canada with different rules. I question your friends approval of that prop. If you look at the TC data sheet for that engine prop combination you will find that it is not approved with a long diameter.
Also he would get better performance by reducing the weight on the nose either with a lighter prop or by the addition of ballast in the tail.
That's also why you can whoop him getting out.it's 84-52 , would account for why he cruises so fast I suppose.
That's also why you can whoop him getting out.
Your Eddie Peck wide 2000s are a big improvement on their own. I used to have a stock 172N on 2130s which was a big improvement over the 2000s. This was particularly noticeable in my 1000 foot long pond. That was a really nice airplane which in a way I wish that I still owned. I was renting it out and someone wrecked it.
Eddy's floats are actually 2250 and yes, they are a major contributor to my stellar performance. My 1967 is one of the lightest 172's made , you have a head start from the get go . I'm still making improvements, next up is my options for pistons during the current O-320 rebuild happening now ( 10:1 vs 9.5:1 or stock 8.5:1) . Then there is prop , catto 84-37 vs the Borer 1A175 82-45 I currently have . I have to make the engine piston choice today, prop can wait until later .
What c/r did you go with and what camshaft are you using?
According to LyCon's report, the 0-320-B2B they built for the cub, with everything they could throw at a certified engine, dyno'd at 187HP. Flyin at work, but will see if I cant dig up the report for ya when back home if you want.
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