Return-Path: Sender: "Marvin Kaye" To: lml@lancaironline.net Date: Mon, 14 Mar 2005 11:05:05 -0500 Message-ID: X-Original-Return-Path: Received: from mta9.adelphia.net ([68.168.78.199] verified) by logan.com (CommuniGate Pro SMTP 4.3c2) with ESMTP id 792462 for lml@lancaironline.net; Mon, 14 Mar 2005 10:08:21 -0500 Received-SPF: pass receiver=logan.com; client-ip=68.168.78.199; envelope-from=glcasey@adelphia.net Received: from worldwinds ([70.32.213.236]) by mta9.adelphia.net (InterMail vM.6.01.04.01 201-2131-118-101-20041129) with SMTP id <20050314150736.HMPM12278.mta9.adelphia.net@worldwinds> for ; Mon, 14 Mar 2005 10:07:36 -0500 From: "Gary Casey" X-Original-To: "lancair list" Subject: Re: Electronic Ignition X-Original-Date: Mon, 14 Mar 2005 07:02:21 -0800 X-Original-Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="Windows-1252" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook IMO, Build 9.0.2416 (9.0.2910.0) Importance: Normal X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 <> Thanks for all the references, Scott. Lasar seems to have some reasonable data in their website and overall, the responses I get show an improvement in BSFC at altitude of between 6 and 12 percent with between 60 and 90 percent of that available with a single advancing ignition system. Unfortunately, none of the data is for LOP operation, which I would expect to result in greater improvements. I disagree that a dyno test is no substitute for flight testing - in a dyno test all other variables can be eliminated so accurate comparisons can be made. Even Unison uses static rpm as a measure of power - not very accurate compared to a balance beam on a dyno engine. A "timing sweep" typically results in a graph that shows a single variable (BSFC or power) changing as a result of ignition advance. The fuel mixture can be held at a fixed value or can be set at LBT as the ignition timing is changed. The knowledge can be derived from an accurate and thorough dyno test may not be available from a flight test although the flight test is the end result. Gary Casey