X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from mail08.syd.optusnet.com.au ([211.29.132.189] verified) by logan.com (CommuniGate Pro SMTP 5.1.10) with ESMTPS id 2197643 for flyrotary@lancaironline.net; Wed, 25 Jul 2007 03:17:30 -0400 Received-SPF: none receiver=logan.com; client-ip=211.29.132.189; envelope-from=lendich@optusnet.com.au Received: from george (d211-31-107-198.dsl.nsw.optusnet.com.au [211.31.107.198]) by mail08.syd.optusnet.com.au (8.13.1/8.13.1) with SMTP id l6P7Gipp029073 for ; Wed, 25 Jul 2007 17:16:45 +1000 Message-ID: <006601c7ce8b$c2a6dd40$c66b1fd3@george> From: "George Lendich" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: carbs vs efi Date: Wed, 25 Jul 2007 17:16:45 +1000 MIME-Version: 1.0 Content-Type: text/plain; format=flowed; charset="iso-8859-1"; reply-type=response Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.2180 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.2180 X-Antivirus: avast! (VPS 0657-0, 12/12/2006), Outbound message X-Antivirus-Status: Clean Bill, I bet your right, but the local engine builders tell me not as well as the Piston engines. They say it can't override restrictions to the extent a piston can, thus turning a restriction into velocity. To be on the safe side, I take that into consideration when looking at port sizing, I discount any benefits of increased velocity. George > Hey George! > The note is fine except for one thing. The rotary "sucks" or more to the > point vacuums just like a piston of similar size chambers. If it didn't it > would never start! > Bill Jepson > > > -----Original Message----- > From: George Lendich > To: Rotary motors in aircraft > Sent: Tue, 24 Jul 2007 3:10 pm > Subject: [FlyRotary] Re: carbs vs efi > > > > Jerry, > > Sounds good! > > The Street port single will give about 116hp at 7,500, but you need 1.18 > x2 sq" minimum ( 2.36 sq") = 44 Dia inlet. > > > > David McCandles has found some old info, which I will forward under > separate cover, which confirms these numbers although I haven't read it > through myself as yet. > > > > The RX8 uses smaller runners but more of them, the inlet area is massive > in total, the smaller runner maintains the velocity. However because the > Rotary doesn't suck like a piston engine ( sucking creates velocity) the > advantages of velocity over area needed, are limited. > > > > The 12A and 13B are the same size P-port 43mm, the timing/position are the > same. > > We have to start to accept that they know the advantages of sizing and > position. > > George > > George,? I just got back from Oshkosh which would have been a wasted trip > except that I got to fly a CH 701 amphib off the water.? This was a first > for ?yours truly. ? ?What a lot of fun.? The airplane handles perfectly > and is the right one for me. ? ?It is limited by the designer to 100 hp > and 200 lbs for the engine installation. So I am in the in enviable > situation of not wanting to get too much out of my p port. The plane was > powered by a 100 hp Rotax.? ?It did very well.? ? > > > > Re your analysis comparing side ports with p ports, I wonder if such an > analysis is even possible as they are quite different.? Anyway, I doubt > that a standard port can deliver 100 hp or a street port 130 hp. per > rotor, certainly not when limited to 7500 rpm.? Of course I am only > guessing.? No real knowledge or experience.?? > > > > > The only carb I saw at Oshkosh was the aero carb.? It is sized by HP and > they recommend the 38mm for? 125 to 160 hp.? This is too large for my > purposes.? I am considering going down to 35mm? (90 to 125 hp) ? ?The > problem is that I already have 38mm p ports.? Also, of interest is that > they do not recommend ram air. That simplifies the plumbing and the cowl. > ? ?The demo engine had rather long, small dia runners and an air filter > attached to the carb.? That is the "system." ((on an 80 hp v.w.))? ?If I > can get the drive figured out, ?I will build it with RB's aluminum side > plates and Atkins eccentric. ?BTW the 701 is a high wing. ?The system will > be strictly gravity. ? ?? ?Jerry > > > > > > > > > > > > > > > > On Jul 21, 2007, at 10:14 PM, George Lendich wrote: > > > > Jerry, > > I'm trying to compare the carb inlet area to port or P-port areas. > > Standard Port area 32 deg ATDC to 50 degree ABDC = 1.18 sq " each side (x2 > = 2.36sq")- using the front and back housings only. > > ? > > A street port will be 1.5sq" x 2 = 3sq" > > . > > A 44mm P-port = 2.35sq" > > A?42mm p-port = 2.14sq" > > A 40mm P-port = 1.94sq" > > A 38mm P-port = 1.75sq" > > So you see a side port on a single has more port area than a small P-port. > > Perhaps the velocity will make up for less area. > > The street port is bigger again at 3 sq" - this equates to 50mm port. > > ? > > The standard port gives about 100 hp, the street port about 130hp each > rotor. > > I wouldn't want to choke down the port areas with too? restrictive inlet > carby?area. I can't see how a 38mm will cut the mustard when your own > calculations suggest 1.6 P-port = 42mm sq". > > ? > > In reality I'm only looking for 130HPat most, if I can get that. > > ? > > I can run a 41mm ID SS tube p-port with a 42mm Carby ( and hope velocity > makes up the difference) Or I can run with two 1.5 street ported side > ports 3 sq" with two smaller carbs, perhaps 2x32mm. > > ? > > BTW street ported 13B has been dynoed to 264hp can't remember the RPM - it > might have been higher than what we run. > > More confused than ever! > > ? > > Does anyone know the IO/IC and size and HP?of the factory P-port. > > ? > > Lynn, does the timing given, calculated by the rotor uncovering and > covering the port, or the side seal uncovering/covering the port opening? > > I was thinking the RX8 rotor will be slightly different (bigger) with the > harased edges. > > George ( down under) > > ? > > ? > > ? > > ? > > ----- Original Message ----- > > > From: Jerry Hey > > To: Rotary motors in aircraft > > Sent: Sunday, July 22, 2007 9:17 AM > > Subject: [FlyRotary] Re: carbs vs efi > > > > George,? maybe I have the wrong idea, but I don't understand why you need > such a large bore carb for the single rotor.? No way you are going to > produce more than 150 hp.? I think 38mm would be enough.? This is what > Aero Carb recommends for the 0-320.? Jerry > > > > > > > On Jul 21, 2007, at 5:56 PM, George Lendich wrote: > > > > Jerry, > > Looks like Pat was wrong about Revmaster having a 44mm, the biggest they > go to is 42mm ( at the present time)?and that costs $380. If I remember > the 32mm costs $320. > > Jerry I would be interested in feed back on what you thought about the > Aero Carb, especially how it's constructed - their all a little different. > > I do like the Ellison but it's too bloody expensive. > > George ( down under) > > > George,? the web site says $326.00.? You might want to compare the aero > carb which is similar.??http://www.aeroconversions.com > I will be looking at both at Oshkosh on Tuesday and Wednesday next week.? > Jerry > > > > > > Jerry > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > On Jul 20, 2007, at 10:06 PM, George Lendich wrote: > > > > ? > > > I have been surprised at the recent flurry of carb postings.? I assumed > that everyone was doing EFI.? having experienced total electrical failure > in march on a trip to the Bahamas I was thinking a lot about that > Neanderthal carb bolted under my O320 and the magnetos, all unaware of > what was going on in the radio, GPS,?and nav lights departments.??? the > reality is that you don't want a reserve battery to get you to the ground > safely, you want to get to the Bahamas and back and THEN look into what's > wrong. > > my questions are "how much power/performance is lost with a carb, and > which carbs can do manual mixture?".? is it stupid to ask if the Lycoming > carb could run a 13B?? someone mentioned Harley carbs?having a?good > history of rough service.? what about marvel/schebler?? is this question > heresy? :-)? isn't efi a bit of overkill for an engine that basically runs > at 100% power, 75% power and idle?? scanning thru the archives I see a lot > of postings regarding mixture, mapping, abrupt failures and such.? does > this complexity buy us 5%, 20%?? the question of turbo-charging seems > to?beg similar line of questioning.??? kevin > > ? > > Kevin, > > It's probably my fault, with a number of chaps helping me out with > information. > > My Buddy Bill Jepson will tell you nothing beats EFI and when it's running > well, he's absolutely right! > > Not only that it is the best for? fuel efficiency, leaning reading fuel > flow etc. etc. > > However I'm developing a single rotor and looking at all sorts of issues > including cost effectiveness of less elaborate installations. I'm also not > keen on high pressure > > fuel under the cowl. > > Most importantly I'm not?an electronics person and seeing the problems > experienced by others has me more than a little nervous, in regard to EFI. > > Of course I know very little about carbies, so their helping me with this > as well. > > The Revmaster might be the choice for me, but I'm awaiting the sticker > shock! > > George ( down under) > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________ > AOL now offers free email to everyone. Find out more about what's free > from AOL at AOL.com. > =0 > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: > http://mail.lancaironline.net:81/lists/flyrotary/List.html >