Return-Path: Received: from sire.mail.pas.earthlink.net ([207.217.120.182] verified) by logan.com (CommuniGate Pro SMTP 4.2.8) with ESMTP id 616440 for flyrotary@lancaironline.net; Fri, 21 Jan 2005 13:41:42 -0500 Received-SPF: none receiver=logan.com; client-ip=207.217.120.182; envelope-from=j-winddesigns@thegrid.net Received: from sdn-ap-010ilchicp0438.dialsprint.net ([63.189.97.184] helo=thegrid.net) by sire.mail.pas.earthlink.net with esmtp (Exim 3.33 #1) id 1Cs3iY-0004WT-00 for flyrotary@lancaironline.net; Fri, 21 Jan 2005 10:41:10 -0800 Date: Fri, 21 Jan 2005 13:41:58 -0500 Subject: Re: [FlyRotary] Re: changed to Octane Content-Type: text/plain; charset=US-ASCII; format=flowed Mime-Version: 1.0 (Apple Message framework v552) From: Jerry Hey To: "Rotary motors in aircraft" Content-Transfer-Encoding: 7bit In-Reply-To: Message-Id: <21C35554-6BDC-11D9-8ED4-0003931B0C7A@thegrid.net> X-Mailer: Apple Mail (2.552) > Lynn, I suspected the same but without the experience to back it up. > I had asked Rolf just a few minutes ago what velocity the mix would > reach in the p port runner and he calculated around 13,000 fpm for > 6000 rpm. At this speed the suction stroke is repeating every .0075 > of a second. Air/fuel mix moving through the intake at such a > velocity might even have a scrubbing effect on the runner walls as > opposed to a wetting effect. Even if this is wishful thinking on my > part, I don't see fuel building up on the inside of the bends to any > appreciable amount. By the way, I am sure you have seen various p > port intake manifolds. The one I had a chance to look at was a 90 > degree sweep with a carb mounted on top. I think it was about 12 > inches long. Does that sound right to you? It may have been shorter. > It was definitely a sweep so no problem with fuel deposition in that > case. I saw this car run through about $500 worth of rubber burning > out just because we were watching. Jerry > I cannot picture cracking motor fuel into a number of compounds in the > milisecond or two it spends in the runner. While there may be a number > of differing > velocities measurable in the runners, they will not be far enough > apart to > affect the product be burned. When the mixture is exposed to the > 375-400 degree > rotor face, and then compressed about 9 times its volume, I suggest > that it is > more likely to recombine any faulty mixture. > > I can picture wetting the outside of a turn in that runner at low > velocities, and perhaps if a very large number of other situations > exist inside that > engine, you could get it to detonate. But detonation would have to be > the goal of > the experiment, and getting it to work would be difficult. The NA > rotary does > not detonate under anything like ordinary use. > > So if the engine was highly loaded at low revs, and the gross mixture > was > reduced from near ideal to just leaner, with a very low octane fuel, > it might be > possible to get it to detonate. Detonation is charge temperature > dependant. > Nothing else. > > A long list of factors are involved in producing the high charge > temperature. > > Ignition timing, octane, RPM, plug heat range, carbon deposits and oil > fouling are just a few. > > Fuel dropping out of suspension suggests a change in velocity in a > fixed > system. > However moving from a homgenious mixture to something less just takes > the > removal of some energy from the flow, such as reducing the throttle > setting just > slightly, or inlet air temp dropping slightly. The precip of fuel > droplets > makes the mixture look leaner to the engine (any engine). Remember > pulling the > choke out on cold days? The mixture that runs fine on a warm day (rich > enough) > will not even allow a start on a cold day, because that mixture > precips into > large droplets and (due to reduced surface area) becomes too lean to > even light. > > A NA rotary can be loaded on the dyno and taken from too rich to run, > through > too lean to run, with no damage at all. > > Lynn E. Hanover > >>> Homepage: http://www.flyrotary.com/ >>> Archive: http://lancaironline.net/lists/flyrotary/List.html >