Return-Path: Sender: (Marvin Kaye) To: lml Date: Wed, 25 Sep 2002 10:10:46 -0400 Message-ID: X-Original-Return-Path: Received: from smtprelay2.dc3.adelphia.net ([24.50.78.5] verified) by logan.com (CommuniGate Pro SMTP 4.0b8) with ESMTP id 1790607 for lml@lancaironline.net; Wed, 25 Sep 2002 08:55:21 -0400 Received: from worldwinds ([207.175.254.66]) by smtprelay2.dc3.adelphia.net (Netscape Messaging Server 4.15) with SMTP id H2ZVW704.H03 for ; Wed, 25 Sep 2002 08:55:19 -0400 From: "Gary Casey" X-Original-To: "lancair list" Subject: V8 engines X-Original-Date: Wed, 25 Sep 2002 05:53:32 -0700 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) X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2600.0000 Importance: Normal <> I have been an "engine design hobbyist" for many years, and I have concluded that for our size aircraft the ideal piston engine configuration is the inverted direct drive turbocharged liquid-cooled V8. It has the potential for greater power/weight, more reliability and less noise than existing engines. I think the Zehrbach approach is close to the "correct" one, but not quite. I don't see the value in the dry sump or the long propshaft extension. Also, for lower-powered applications like my ES it looks like a bit of an overkill. Gary Casey