Return-Path: Sender: (Marvin Kaye) To: lml Date: Tue, 11 Mar 2003 20:42:06 -0500 Message-ID: X-Original-Return-Path: Received: from smtp03.mrf.mail.rcn.net ([207.172.4.62] verified) by logan.com (CommuniGate Pro SMTP 4.0.6) with ESMTP id 2049654 for lml@lancaironline.net; Tue, 11 Mar 2003 17:21:24 -0500 Received: from 216-164-236-12.s12.tnt3.frdb.va.dialup.rcn.com ([216.164.236.12] helo=OFFICE) by smtp03.mrf.mail.rcn.net with smtp (Exim 3.35 #4) id 18ss7f-0005wm-00; Tue, 11 Mar 2003 17:21:24 -0500 X-Original-Message-ID: <005001c2e81c$aeee3410$0ceca4d8@OFFICE> From: "Bill & Sue" X-Original-To: "Lancair Mailing List" X-Original-Cc: "Dan & Kari Olsen" References: Subject: Re: [LML] Engine cooling in 320 X-Original-Date: Tue, 11 Mar 2003 17:22:19 -0500 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2720.3000 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2600.0000 > My 320 is a couple months from flying and I am in the process of finishing the > top of the cowl. The cooling arrangement I have chosen for my stock IO-320- > D1B (160hp) is as follows: > o Standard factory baffling > o Large NACA duct on the right side of cowl for oil cooler > o "Shark gill" exit for oil cooler air on left side of cowl > o No "ramps" inside cooling air inlets > o Blast tubes for mags and fuel pump, taking air from rear baffle > Hello Dan, Here are some observations from 450 hours on our 320. 1. Standard factory baffling, well sealed. Our CHT's still run a little warm. 2. Large (2 x the cabin NACA in the manual) NACA duct on the left side of cowl for oil cooler. My oil temps ALWAYS run too cool. Behind the NACA duct I built a gradually expanding plenum that is sealed to the cooler. Every molecule that goes into the duct comes out the back side of the cooler. 3. Shark gill exit on the right side bottom NOT connected to the oil cooler. We installed this in an attempt to get more flow through the engine. This installation cooled the CHT's about 10 degrees. 4. We added ramps inside the cooling air inlets. These cooled the CHT's about 10 degrees. 5. No blast tubes. 6. We are in the process of adding little "lips", kinda like mini cowl flaps to the bottom of the cowl exit in an attempt to bring the CHT's down another 10 degrees or so. I believe that if you put in an efficient duct / plenum for the oil, you won't need a dedicated exit. I need to put in a butterfly valve to get my oil temps UP. I haven't heard of any LNC2's running too cool in the CHT's. Let the shark gill exit draw more air through the engine rather than the oil cooler (assuming your oil temp is acceptable). I believe that the ramps should probably be installed. They can't hurt and it's such a simple, easy installation. I just microed some big foam blocks to the upper cowling, shapped them with sandpaper and put a 2 bid over the whole thing. If I were starting from scratch, I'd probably go the engine plenum route like Mark Ravinski, Scott Krueger and others. This is mine, your's will surely be different. Hope that this helps. Let me know if you need any more info. Bill harrelson@erols.com N5ZQ LNC2 O-320 VA42 Fredericksburg, VA