Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Tue, 31 Aug 2004 18:39:58 -0400 Message-ID: X-Original-Return-Path: Received: from mta-out-1.udlp.com ([207.109.1.8] verified) by logan.com (CommuniGate Pro SMTP 4.2) with ESMTP id 387344 for lml@lancaironline.net; Tue, 31 Aug 2004 18:34:25 -0400 Received-SPF: pass receiver=logan.com; client-ip=207.109.1.8; envelope-from=Christopher.Zavatson@udlp.com Received: from asdmngwia.mpls.udlp.com (asdmngwia.mpls.udlp.com [10.1.62.22]) by mta-out-1.udlp.com (8.12.10/8.12.10) with ESMTP id i7VKkoUP011642 for ; Tue, 31 Aug 2004 15:46:50 -0500 Received: from DM-MN-06-MTA by asdmngwia.mpls.udlp.com with Novell_GroupWise; Tue, 31 Aug 2004 17:33:51 -0500 X-Original-Message-Id: X-Mailer: Novell GroupWise Internet Agent 6.0.2 X-Original-Date: Tue, 31 Aug 2004 17:33:43 -0500 From: "Christopher Zavatson" X-Original-To: Subject: [LML] Re: Engine Cooling Mime-Version: 1.0 Content-Type: text/plain; charset=US-ASCII Content-Transfer-Encoding: 7bit Content-Disposition: inline George, Electric screwdrivers are wonderful things. Obviously you can't pull the upper plugs or perform other work on the top side of the engine without removing the plenum top. The large number of screws was pre-determined by the existing hole pattern that once held all the silicone baffle material. <> Relative to my previous set-up I am about even; more difficult up top, easier on the bottom. Prior to the fully enclosed plenum, I had molded FG parts installed just inside the lower half of the inlets in an attempt to prevent the airflow from separating (was only marginally successful). These pieces had to be removed every time I wanted to remove the lower cowl. I was glad to get rid of this hassle and accept the extra screws for the plenum top. I find the extra minutes to gain full access to the engine to be well worth it, given the immense cooling improvements. I was fortunate to be able to test the system with 100+ deg F OATs and had to pinch myself when I observed the new cylinder head temperatures during take-off. Every phase of flight is improved from taxi, take-off, climb to cruise. Even the oil cooler located infront of cyl. #2 benefitted. Previously, flow separation, which the parts mentioned above attempted to correct, off the lower edge of the inlet was blanking the cooler and it would not cool while flying below 120 KIAS regardless of power setting. Now it cools all the way down to something less than flying speed. It would be nice to quantify all the positive and detrimental contributing factors in any given cooling system. Perhaps you have been able to do this and I too am interested in attending your baffle session to hear about your experience in this area. I was stuck having to make qualitative judgement calls during the design and construction of this system, but I really like the results. regards, Chris Christopher Zavatson Mobility Technologies United Defense (408)289-4329