Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.5.4) with ESMTP id 1040823 for rob@logan.com; Tue, 05 Feb 2002 05:42:35 -0500 Received: from harrier.prod.itd.earthlink.net ([207.217.120.12]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71866U8000L800S0V35) with ESMTP id com for ; Mon, 4 Feb 2002 22:16:24 -0500 Received: from user-38ldaih.dialup.mindspring.com ([209.86.170.81] helo=earthlink.net) by harrier.prod.itd.earthlink.net with esmtp (Exim 3.33 #1) id 16Xw7m-0001NM-00 for lancair.list@olsusa.com; Mon, 04 Feb 2002 19:18:26 -0800 Message-ID: <3C5F504A.954F864B@earthlink.net> Date: Mon, 04 Feb 2002 22:23:54 -0500 From: Marcelo Pacheco MIME-Version: 1.0 To: lancair.list@olsusa.com Subject: Re: Engine dynamics 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 leaky exhaust valve issue isn't caused by proper LOP operation. It's caused by running the engine very close to peak temps. Typically, single engine EGT gauges are installed on the cylinder known to be the leanest. So on such system, when you think you're running all cyls at 50 degrees LOP, you're probably running some cyls rich of peak, some very close to peak, and hopefully at least one lean of peak. The ones at or just rich of peak are the troublesome ones. If you have proper (even) fuel and air distribution to all cylinders, then there should be no problems from running the engine 50 or more degrees lean of peak. The only way you can be sure this is happening is if you have an all cylinders engine monitoring package, and depending on the engine, you'll need GAMIjectors to achieve that good fuel distribution. For example, IO-320 or 360 are known not to have good fuel distribution with stock injectors. By the way, I'm just someone who pretends to understand this stuff. The people that really understand are the engine professionals. I'm just a computer geek with some aviation experience that likes to read about engines and have physics knowledge you get out of a computer engineering degree. I read all John Deakin articles from beginning to end and I think I understood them completely (you never do, but I still think). Now, if you're running a non-turbo charged engine at a high enough altitude where your power output will be about or lower than 65%, then running the engine just lean of peak is a better idea, as available power goes down from there. For example, above 10k, I would run any non-turbo charged engine at max MP, 24-2500 rpm and just lean of peak mixture to get maximum power. I would climb full rich until less than 25" MP is available, where I would start a little leaning to get some more power. Below 10K, I would run them at full throttle, 2400-2500rpm, leaning to obtain a fixed fuel flow which gives me the power output I want, let's say 70% power. If the MP is higher than the MP setting where that fuel flow results in peak temps, then you'll be lean of peak by definition. My personal theory about why some engine manufacturers say their engines aren't to be run LOP is they want to assume all their customers are dumb and can't lean properly, while also being incapable or don't think there's financial return in competing with GAMI. But that's just one of my many conspiracy theories. No, I'm not financially associated with any airplane/engine/accessory company. Marcelo Pacheco PP-ASEL IFR 220 hrs >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://members.olsusa.com/mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please remember that purchases from the Builders' Bookstore assist with the management of the LML. Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>