Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.4.5) with ESMTP id 770577 for rob@logan.com; Fri, 27 Apr 2001 19:55:06 -0400 Received: from ns1.abboptical.com ([208.46.5.48]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71175U5500L550S0V35) with ESMTP id com for ; Fri, 27 Apr 2001 18:54:24 -0400 Received: from progress.com (host-216-77-209-35.fll.bellsouth.net [216.77.209.35]) by ns1.abboptical.com (8.9.2/8.9.2) with ESMTP id SAA24279 for ; Fri, 27 Apr 2001 18:53:55 -0400 (EDT) Message-ID: <3AE9F8F9.60A4EAAA@progress.com> Date: Fri, 27 Apr 2001 18:55:53 -0400 From: Marcelo Pacheco Organization: PROGRESS Software Professional Services MIME-Version: 1.0 To: Lancair Mail List Subject: Re: Running lean of peak Content-Type: text/plain; charset=us-ascii Content-Transfer-Encoding: 7bit X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> > The word "new" is operative here. How many of these engines are in the > air, and how many total flying hours do they have? Yes, but GAMI has some instrumentation on a test stand that is capable of graphing a cylinder pressure through the combustion cycle with enough resolution with amazing resolution. They show there how much better running lean of peak is. It seems like you're so ingrained in the no LOP that you never even read through the LOP articles on Avweb. Look at: http://www.avweb.com/articles/pelperch/pelp0033.html The information there is VERY HOT !!! Specially the chart (here's the link just to the chart): http://www.avweb.com/articles/pelperch/graphics/pp33_rich_to_lean_lg.jpg This shows the pressure versus degrees before and after TDC (top dead center) of an IO-470 in various power settings. It will show that running an engine 100 degrees LOP is much better than running an engine 100 degrees ROP, because the pressures inside of the combustion chambers are way lower and they build far more slowly, reducing the amount of combustion energy hitting the pistons right about when they're at TDC, where most of the energy operates trying to break the crankshaft, break the pistons, instead of generating usefull crankshaft energy. Well let me stop trying to write the article to you before I get too caried away. This is due to the combustion happening in a slower, more controlled fashion (the exact oposite of detonation) > When they have half a hundred engines flying with a 1700 hours each without > burned up cylinders, we should give their technique serious > consideration. If hard measurement data is not worth a damn to you, then that's your way to go. Not mine. No offense intended please. > If they cannot substantiate it because of lesser numbers, I would not want > to be their test pilot contributing my dollars to prove their theory. John Deakin shows that he was able to lean his Turbo Normallized IO-550 engine all the way to 8GPH. If you want to have a hassle free engine management technique, don't run rich of peak by the numbers, just go 150-200 degrees lean of peak. If you descend without pulling on the power nor changing the mixture, you'll end up with an overleaned engine that eventually will stop producing power, it will not overheat, because as you descend you're leaning the engine further. All I'm trying to tell you is there's enough data out there to prove that this isn't a theory, this is FACT. If you want to be conservative, just lean to 12-13GPH, where the temps will be so low that if you should be concerned about anything, it will be that your engine is just running to cold instead of too hot. I believe that if you run your engine as rich as recommended on climb, then lean way agressively on cruise, you will get 50% more durability out of it, as the pressures and temps will be so much gentler on the engine. When you reply, please let me know if you have actually looked and understood at least the chart or better the whole article. Again, you'll be glad you did. Aproach this information with an open mind and you'll start wondering if those folks with burned engines are really running their engines LOP or just around peak. A reply to Tony's e-mail follows. Look carefully at the numbers he's showing. >My IV-P operates just fine LOP. Here are my cruise numbers, 500 hours on >TSIO-550 > >@25,000'.........2400 RPM, 29"MAP, 15GPH, 277 KTS TAS, 5PSI cabin. >EGT's 1550 CHT's 290 TIT's 1580 OIL TEMP 180 > >I get 5 hours range (1325 NM) and still land with one hour fuel. >Its a no-brainer. >I do have winglets, and cooling louvers under the cowl >Tony Durizzi Have you tried increasing MAP while leaning to maintain 15GPH ? This should give you lower yet temps. Maybe not quite full throttle but a good boost from 29-30" sea level ambient pressure. You're running a quite conservative power setting, about 58% power (15GPH * 13.7 ~ 205.5HP -> 58% power), at lop, you can find out what power setting you're running at by multiplying the fuel flow by 13.7 for 8.5:1 compression ratio engines. This is exactly my point: CHT: 290, that's very, very cold, how can this ever damage this engine. Tony have you ever performed a engine borescope to help us convince the folks which are incapable of believing in it ? Isn't the TSIO-550 recommended to be run at a minimum of 2500rpm ? Thanks for the info, Marcelo Pacheco PP-ASEL >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>