X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from [202.52.32.26] (HELO venus3.veridas.net) by logan.com (CommuniGate Pro SMTP 5.0c1) with ESMTP id 683790 for flyrotary@lancaironline.net; Sat, 27 Aug 2005 08:52:19 -0400 Received-SPF: none receiver=logan.com; client-ip=202.52.32.26; envelope-from=mburke@southernphone.com.au Received: (qmail 21279 invoked from network); 27 Aug 2005 22:51:30 +1000 Received: from dsl-202-52-51-019.nsw.veridas.net (HELO veridas) (202.52.51.19) by southernphone.com.au with SMTP; 27 Aug 2005 22:51:30 +1000 Message-ID: <000301c5ab05$e03541e0$0401010a@veridas> From: "Michael Burke" To: "Rotary motors in aircraft" Subject: Re: [FlyRotary] Re: Fire extinguishers Date: Sat, 27 Aug 2005 22:50:11 +1000 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 6.00.2800.1409 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1409 Jim. I think you missed my original post. I am not advocating sealing off the engine compartment full time. As you say there is quite a bit of heat given off by the exhaust and engine block that has to be taken away. What I am advocating is that you design the cowl so that the air supply to the engine is CONTROLLED by a inlet flap that would normally be locked open, but could be closed in the event of a fire under the cowl. I agree you would never get a 100% air seal, but (second point) combined with a halon fire suppression system one could control a fire fairly quickly. It's got to be a better system than diving towards the ground at 200mph. Michael Burke. <... isolate the engine compartment from sources of fresh air ...> Don't know how you'd do that. Radiators exhaust into the engine compartment. If there was no air circulation in the engine compartment you'd have VERY hot exhaust parts heating all that stagnant air and radiating to wherever (fuel rail? Belts & electrics? Coolant lines?) and roasting everything. Any plastic airplane (or cowl) would melt forthwith. The air leaking past even good baffling would support one hell of a fire. If there was an easy answer, it would be implemented by now ... Jim S. Dale Rogers wrote: Hans, I think you missed Michael's point. It isn't the volume of air that's at issue, but rather where that air has to go. A direct-air cooled engine needs the air to travel in intimate contact with the cylinder fins - filling the entire engine compartment. An indirect- air cooled system allows the airstream to be confined to a ductwork where there are no flamable liquids or gasses, making it far easier to isolate the engine compartment from sources of fresh air. Regards, Dale R. From: Hans Conser Date: 2005/08/26 Fri AM 10:29:50 EDT To: "Rotary motors in aircraft" Subject: [FlyRotary] Re: Fire extinguishers On Aug 26, 2005, at 12:55 AM, Michael Burke wrote: ... The point I'm making is this. The rotary is NOT air cooled, (directly anyway)therefore we can take a different approach in designing the cowl. We do not need a large volume of air blasting into the cowl, because the the radiators can be set up so that they are ducted from the outside seperately. ... Actually liquid cooled engines need a great volume of air than air cooled engines. This is because the temperature differential (Delta T) of the aircooled engine is much greater. In other words it takes less air to cool 400 degree cooling fins vs 220 degree coolant. Hans Conser