Return-Path: Received: from secure.smtp.email.msn.com ([207.46.181.28]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Sun, 8 Oct 2000 14:18:49 -0400 Received: from vaio - 207.50.49.38 by email.msn.com with Microsoft SMTPSVC; Sun, 8 Oct 2000 11:25:01 -0700 Message-ID: <004301c03155$22807900$263132cf@tcac.net> From: "johnlasher" To: References: Subject: Re: Lancair IV-P Heating problems climbing through FL 190 Date: Sun, 8 Oct 2000 13:25:27 -0500 Return-Path: johnlasher@msn.com X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Scott Krueger wrote> > If ignition operation/timing can lead to high altitude temperature problems, > consider the followings questions in additiion to Brent's: > > 1) Klaus' specs (www.Lsecorp.com) doesn't mention an altitude range over > which his electronic ignition systems were tested. Thin air doesn't provide > the same "insulation" effect as more dense air. Any cross-fire between > components or harness? This is one of the reasons that EI is an improvement over a mag. There are no points or distributors. There is an electromagnetic pickup on the prop hub that sends pulses to a controller which intern fires two plugs simultaneously at 120 degree intervals. One of the two plugs being fired simultaneously is 24 DBTDC in the compression stroke while the other is 180 degree opposed in the exhaust stroke (a wasted spark - but then no distributor is needed). If you do the math, then all 6 cylinders are fired 24 DBTDC on the compression stroke every 720 degrees of rotation. > 2) Because of the ease which charges can jump gaps at high altitudes, > magnetos should be pressurized to eliminate timing problems. Are yours and > if so, is the pressurization working? My mag is pressurized and was overhauled and checked within the last 100 hours by Consolidated Fuel Systems. The EI doesn't require pressurization. Klaus has tested his EI systems I believe up to altitudes of 29,000 feet. I'm convinced that the EI is better than the mag and could easily exceed the TBO of the engine without maintenance except for the spark plugs. However, having only one along with a conventional mag can present possible problems in our high altitude IV-Ps as was so nicely outlined by Brent Reagan in one of his replies to my heating problems. The problem with having two, is that they are both dependent on the electrical system - requiring a backup battery system of some sort. I probably should go to two EIs. John R. Deakin has a great 4 part series of articles on "Those Fire-Breathing Turbos" on http://www.avweb.com/articles/pelperch/perchlinks.html . These articles should be read by all IV-P drivers. They are filled with factual information and graphs that will make all of us more knowledgeable and safer pilots. In the Part 2 article he writes about "The Future": "There are persistent rumors of a number of improvements in store. Chief among them is an electronic ignition system that is far superior to anything in any engine (car or aircraft) today. It will look directly at each combustion event, and modify the spark timing as needed for the succeeding event. This will produce the ideal pressure event for best power, regardless of power settings, RPM, ambient pressure/temperature, or fuel octane. There is every reason to believe this system will allow all our aircraft engines to run at full rated power on 94- to 98-octane fuel, with NO lead. That will solve the aviation fuel crisis overnight." John Lasher N411WB >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>