Return-Path: Sender: (Marvin Kaye) To: flyrotary Date: Tue, 05 Nov 2002 19:13:55 -0500 Message-ID: X-Original-Return-Path: Received: from sunny.pacific.net.au ([203.25.148.40] verified) by logan.com (CommuniGate Pro SMTP 4.0) with ESMTP id 1853591 for flyrotary@lancaironline.net; Tue, 05 Nov 2002 16:24:30 -0500 Received: from wisma.pacific.net.au (wisma.pacific.net.au [210.23.129.72]) by sunny.pacific.net.au with ESMTP id gA5LORJi028494 for ; Wed, 6 Nov 2002 08:24:28 +1100 (EST) Received: from imanic (ppp18.dyn18.pacific.net.au [61.8.18.18]) by wisma.pacific.net.au with ESMTP id IAA15524 for ; Wed, 6 Nov 2002 08:24:24 +1100 (EST) From: peon@pacific.net.au X-Original-To: (Rotary motors in aircraft) X-Original-Date: Wed, 6 Nov 2002 08:23:36 +1100 MIME-Version: 1.0 Content-type: text/plain; charset=US-ASCII Content-transfer-encoding: 7BIT Subject: Re: [FlyRotary] 12A vs. 13B Reply-to: leon@promotorsport.com.au X-Original-Message-ID: <3DC8D188.16311.32ACF55@localhost> Priority: normal In-reply-to: X-mailer: Pegasus Mail for Win32 (v3.12c) G'day Larry, "Ain't nuthin' " wrong with 12As, especially if they are given a bit of un-natural aspiration, and the ports are given a bit of a tickle. The same porting principles apply to 12A as 13B, and similar extra power can be had, albeit at higher RPM, or higher boost. As an aside, you may notice that as a general rule, a turbocharged variant of any engine family is usually smaller in capacity, but evenso usually produce considerably more power than their bigger capacity naturally aspirated counteparts . The extra RPM/boost are not as detrimental to a 12A as they are to a `3B. Major 12A advantages are: The apex seals tend to be more durable as they are shorter. They also come stock with 3 mm apex seals, which saves the expense of re-machining apex seal grooves. 12A parts are generally much cheaper, and at this time, everything is still curently available from Mazda dealers. The overall package is somewhat lighter, as well as being 20 mm shorter in overall length. 12A bearing loads are also less due to the lighter rotor weight, and can be reduced even furher by lighteneing the rotors. I can't EVER remember seeing a 12A run a main bearing in a race motor (except of course for a very rare oil line failure), but I can sure blubber in my "Foster's Frostie" (Oz equiv to a "Bud" in the US) over 13B bearing failures, particularly on highly stressed PP race engines. (12A & 13B use the same size bearings!!) So the only real downside is that to get the same BHP, you have to rev them a bit harder, or use more boost. Interestingly, a 12A, as they came in the car, carburettored 12A engines were quoted as 125 BHP with all the emissions control gear. The carburettored 13B was quoted as 130 BHP in the same configuration, albeit with better mid-range torque characteristics (not an issue with aircraft engines). By removing the emissions gear, and fitting a set of tuned extractors, typically, the same stock 12A will make 150 + BHP @ 6,500 whereas you will get the same grunt at about 5,500 from a 13B. 6-8 PSI boost will bring the power output up to 200 BHP at the same RPM. Tickle the ports with a die grinder and an extra 25- 30 neddies can be had for a couple of hours work. I'm being conservative, and we are talking here engines without all the pollution control equipment, no cat convertoers, and both with 9.4:1 compression rotors). So no "Nit Pickers" please, this is illustrating a general principle, as there are several diffiernt types of port sizes. The best end housings to use are the Series II / III ('81- '85) type.(not 6 port - too much messing around).. So the limiting factor really boils down to PSRU ratio availability and and prop speed. The motors themselves are VERY durable.. To get the gunt without the need to rev the little sucker too hard, they respond very well to forced induction. Turbocharger wise, the 12A can get away with a smaller, lighter unit than the 13B if you don't want a lot of extra grunt.. There are some really sweet little ball beaing turbos with integral wastegates made by Garrett that sell here for about $2,300 AUD that are eminently suitable for 5-8 PSI boost on a 12A. A good starting point for someone on a budget would be to grab a turbo off a Nissan RB26 GTR. Lots of the Nissan tuning shops take the stock ones off and fit larger ones to get more grunt. I can pick them up here in OZ for the proverbial odd song or 2. In fact, the reason I mention this is that is exactly what I have planned for this summer's testing. Contrrawise, for LOTS of grunt, I have several 12A powered cars (mainly RX2s and RX3s) running around with the late model Series V turbos that produce 350 + BHP at about 18-20 pounds and I have yet to see one go "pop", even though the owners tend to subject them to ritual serial abuse! . (Local registration rules preclude 13B turbos in cars less than 1000Kg). I also still have fond memories of my BAE kit equipped Series 1 RX7 12A back in the early '80s. What a weapon!! Devestatingly quick, and a real Porsche muncher, ... and the local V8 worshiping Australopithicenes just could never cope with being wasted by a "rice burner" or "chook cooker" (as in rotisserie) as they disparragingly used to call the Cork Company's (Toyo Kogyo) little marvel!. (I confess to having been more than a little bit of a street racer back then!!) ... but I do digress. So I have been revisiting the 12A paradigm again and doing some careful sums on the 12A lately myself. Just today, I was chatting with one of the local SAAA guys who is a composites specialist, and who is in the process of finishing his prototype "White Pointer", a 2 place RV4 sized ship with LOTS of luggage space. Current powerplant is a Jabirru flat 6, but he's looking for something a LOT cheaper and with a bit more grrunt. (he is also declared himself a closet rotaryphile). 12As are especially useful where weight is a major consideration, and power output is simply a function of RPM/Boost. >From investigations so far, it would seem that for optimum performance, a PSRU ratio of about 3.1:1 , or thereabouts would be indicated. 200 BHP is easily obtained at about 8 psi boost and 7,500 RPM. This keeps the prop speed down around 2400 RPM. More grunt is available simply by revving it a bit harder, or dialing in a bit more boost. Bearing in mind that this would only be needed on takeoff and climbout, the engine could quite happily cruise @ 6,500 RPM and up to a couple of pounds boost and still make 140 - 150 BHP. (All BHP quoted are at Sea Level!). As for PSRUs, I know everybody raves about epicyclic PSRUs, but the rubber band arrangement on Ken Welter's Coot seems eminently reliable, and also give a wider range of available ratios. It also solves the problems of manifold and water pump clearances. (But then again, if you run "Plugs Up", these are no existant!!). So do some homework, talk to Ken about his PSRU arrangements, and if weight is important, then maybe a 12A turbo is the way to go. The rubber bands also seem able to take considerable abuse as Ken is know to give his engines a decent shot of "laughing gas" to make the Coot unstick from water. That also raises another viable alternative. Have a naturally aspirated 12A "on the bottle" (i.e., fitted with "Giggle Gas"). Grunt at the flick of a switch, and a lot lighter than a turbocharger/Intercooler set-up. So I hope this as given you (and others) food for thought. What I have said above is NOT definitive, but I'm certainly already investigating the feasibility of it, and in due course, after I have done some testing over the Christmas period, I'll post my findings. Cheers, Leon Promet leon@promotorsport.com.au. On 4 Nov 2002, at 19:13, Schurr, Larry wrote: > I have this opportunity to obtain an RX-7 with a 12A aboard. > All the talk, research, and apparently flying aircraft seem to be > centered around the 13B and 20B. > > What difference is there in the 12A and is it suitable for aircraft > use? Too heavy? Too wimpy? Can I turbocharge it? Or should I just > junque it? > > Larry > > >> Homepage: http://www.flyrotary.com/