Return-Path: Sender: (Marvin Kaye) To: flyrotary Date: Thu, 01 May 2003 22:57:00 -0400 Message-ID: X-Original-Return-Path: Received: from ms-smtp-03.southeast.rr.com ([24.93.67.84] verified) by logan.com (CommuniGate Pro SMTP 4.1b4) with ESMTP id 2330335 for flyrotary@lancaironline.net; Thu, 01 May 2003 22:29:13 -0400 Received: from mail5.carolina.rr.com (fe5 [24.93.67.52]) by ms-smtp-03.southeast.rr.com (8.12.5/8.12.2) with ESMTP id h422RLN2004397 for ; Thu, 1 May 2003 22:27:34 -0400 (EDT) Received: from o7y6b5 ([24.93.78.62]) by mail5.carolina.rr.com with Microsoft SMTPSVC(5.5.1877.757.75); Thu, 1 May 2003 22:25:48 -0400 X-Original-Message-ID: <001801c31052$ffa56d20$1702a8c0@WorkGroup> From: "Ed Anderson" X-Original-To: "Rotary motors in aircraft" References: Subject: Are Blowoff valves where its at? X-Original-Date: Thu, 1 May 2003 22:31:55 -0400 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 6.00.2800.1106 X-MIMEOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 > Posted for "Tracy Crook" : > > Not having any turbo experience I hesitate to give an opinion on this but > here's my take on it. > > This is not meant to discourage anyone from using a turbo but it is > imperative that you develop a good mental model of how it works prior to > leaving the ground. This is not hard to do. Just a basic understanding and > few good ground rules about wastegate operation is all it should take. > > Tracy Crook I would like to join Tracy regarding turbo. While I have not turbocharged my 13B, I have built my own turbocharger installations for two automobiles back in the mid 70s. While I finally got the bugs worked out (after shatter pistons and bent piston rods) and experienced the rush of beating anemic corvettes from 0- 60, it was worth it - however, it certainly was not without challenges. A few which left me blowing oil out the valve cover and over the windshield, shearing piston ring lands off pistons, etc. Therefore, I sort of cringe when I hear people talking about controlling their boost with manually operated boost controllers. My experience was that when the boost came on, it would very quickly head out of limits very fast. Taking your foot off the accelerator would quickly reduce the boost if you caught it soon enough, but it builds exponential and with the free breathing rotary I would think the problem would be even worst. Perhaps other folks have quicker reaction times that I do, but I would want to ensure that: 1. If not using a waste gate, ensure that the maximum boost achievable is within your set limits. In other words the size A/R of the turbine and/or combination with exhaust restrictions ensures that your max boost limit is not exceedable. You need to be careful with this approach for while it would be perfect operating at one altitude - it could lead to compressor surge at higher altitudes. 2. If using a waste gate, ensure that you have some means of cockpit control. The reason is that as you increase in altitude and keep a steady boost the boost ratio over ambient pressure continues to increase to the point you could enter the surge zone of the compressor. There may also be some reason you might want to pull more power without the resulting boost. 3. A blow off valve is certainly better than no safety net, but not as good as a wastegate or properly selected A/R for the turbine in my opinion. The reason is that the operation of the blow off valve itself can push a compressor into surge mode or more likely result in overspeed of the compressor (less resistance to the compressor, turbine spins compressor faster and faster - at least until the effect of less boost takes hold) 4. If everything is done conservatively then you may get away with some less that sterling design decisions, I certainly am not trying to discourage anyone from the turbocharging route - I intend to dive into that challenge in the next year or two myself. Read some of the available reference material on turbochargers and while there is not much out there on turbocharging aircraft, some of the references to turbocharging Pikes-Peak Mountain race automobiles addresses the effects of changing altitude. The 1971 printing of Hugh MacInnes "How to Select and Install TURBOCHARGERS" has a chapter on High-Altitude Turbocharging that is well worth reading. Chapter 14, page 107. One comment worth nothing "If the engine is to be operated at several different altitudes (I wonder who fly at only one altitude?) then an aneroid type control should be used to prevent overboosting at lower altitudes" and there are a number of other cautions and suggestions. Well, worth reading if you can find a copy. There are undoubtedly other considerations that could be made, but once boost starts climbing things happen awfully fast. FWIW Ed Anderson