X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from [64.233.170.189] (HELO rn-out-0102.google.com) by logan.com (CommuniGate Pro SMTP 5.2c1) with ESMTP id 2500676 for flyrotary@lancaironline.net; Thu, 22 Nov 2007 09:05:29 -0500 Received-SPF: pass receiver=logan.com; client-ip=64.233.170.189; envelope-from=msteitle@gmail.com Received: by rn-out-0102.google.com with SMTP id e13so1840042rng for ; Thu, 22 Nov 2007 06:04:51 -0800 (PST) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=beta; h=domainkey-signature:received:received:message-id:date:from:to:subject:in-reply-to:mime-version:content-type:content-transfer-encoding:content-disposition:references; bh=HqZCUSTnZRZp5u83y6Ayjy4NdFNwKI12iUVVHsfMaXU=; b=I5ph1LBPS1jeaEntOHsRROae5MKPJTkKAx/A48Z6QAWecvOYJMokuSaNu+SZfMB4zoGd8Tz+EIiweLbRhmMepTy3SQXd42XeisvT94BqI3jHGjevvODHzCFfdWcGUNkJQbIWp1iLOr8Bc0o4aQs/kD+lDjAv11FIhN4XcZ3K8ZM= DomainKey-Signature: a=rsa-sha1; c=nofws; d=gmail.com; s=beta; h=received:message-id:date:from:to:subject:in-reply-to:mime-version:content-type:content-transfer-encoding:content-disposition:references; b=bJLEgdAXOwh98M2z+iUs18rzDLy2yhVuIEPKSRtr9NuKkZ7kRl5JHpJPysEpOxAyDi//yEu1cVulpqXQhwVaFll1zq/ecsvcagq+PuoMyZ0CIg/stB4hhWSTBpfmOJUUHsOA/e+KFpeu8nSzkSeJ2QTDr1uE0Z73GHvd8XnKglY= Received: by 10.150.92.11 with SMTP id p11mr1651158ybb.1195740291203; Thu, 22 Nov 2007 06:04:51 -0800 (PST) Received: by 10.151.10.17 with HTTP; Thu, 22 Nov 2007 06:04:51 -0800 (PST) Message-ID: <5cf132c0711220604o2a3e9befx498a187f269dbd91@mail.gmail.com> Date: Thu, 22 Nov 2007 07:04:51 -0700 From: "Mark Steitle" To: "Rotary motors in aircraft" Subject: Re: [FlyRotary] Re: Fw: [Bulk] 16x In-Reply-To: MIME-Version: 1.0 Content-Type: text/plain; charset=ISO-8859-1 Content-Transfer-Encoding: 7bit Content-Disposition: inline References: Ed, How many flight hours does your engine have on it since last rebuild? Mark On Nov 22, 2007 5:45 AM, Ed Anderson wrote: > Thanks, George, that in indeed interesting information. Long throw should > mean more torque. Be interesting to see how they have improved the sealing. > Two years more development then all the production (assuming they go forward > with it), so I should expect to see it for at least 5 years. Well, > hopefully the old 13B will hold out for that long. > > Ed > > ----- Original Message ----- > From: "George Lendich" > To: "Rotary motors in aircraft" > Sent: Thursday, November 22, 2007 1:51 AM > Subject: [FlyRotary] Fw: [Bulk] 16x > > > > > > > >> Ed, Lynn and Bill + > >> > >> This was posted to me privately and may help to clarify the > >> specifications of the 16x. Some of the info are estimations by Rolf > >> Pfeiffer ex - NSU engineer. > >> > >>> Hello George > >>> Nice to hear from you. Here is my assessment: > >> > >> Also info supplied by Don Sherman as follows:- > >> > >> I interviewed Seiji Tashima, the engineering expert for Mazda's new > >> rotary, at Tokyo on your behalf. Here are a few details he revealed: > >> Rotor width reduced by 5mm saves weight, improves apex seal performance > >> trochoid is 25mm wider, 35mm taller for more displacement and torque > >> would not reveal increase in eccentricity. New displacement is > >> 800cc/rotor. > >> > >> Aluminum end plates have plasma-sprayed wear surface direct and indirect > >> fuel injection. > >> > >> Torque gains come from longer e-dimension, more displacement, and direct > >> injection. > >> > >> He would not confirm 300 hp power goal. > >> All the gas seals are improved, with smaller flame holes adjacent to > >> spark plugs. > >> The 16x engine ran for the first time this year, full development will be > >> at least 2 more years. > >> > >> Engine weight is reduced from 125kg [275 pounds] to 100 kg [220 pounds]. > >> > >> Assessment by Rolf Pfeiffer as follows:- > >> > >>> /Now, using above dimensions we get the following: > >>> > >>> 25 mm wider means the short axis goes from 180 to 205 mm. > >>> 35 mm taller means the long axis goes from 240 to 275 mm. > >>> > >>> This results in E = 17.5 mm, and R = 120 mm. > >>> The old dimensions were E = 15 mm and R = 105 (including the radius of 3 > >>> mm for the apex seals). > >>> The ratio R/E is 6.857, down from 7.0. > >>> > >>> The ratio of stroke to piston area becomes higher which is what they > >>> want, I suppose. > >>> The RX7/8's were 0.33 S/D, above numbers would be 0.3764, a substantial > >>> 14% improvement in ratio of stroke to equivalent piston diameter. A long > >>> stroke engine, so to speak. > >>> > >>> I also had stated that: > >>> NSU also went that direction with their latest developments before > >>> folding. > >>> We are lucky that Mazda has the financial means and does carry on. > >>> > >>> The last big NSU unit EA 871 was approximately like this: (Calculating > >>> back from its displacement and width. I had already left by then, so the > >>> info is calculated.) > >>> E = 17.28, R = 120.5, width = 69 (given), displacement = 746.6 cc > >>> (given). > >>> This is very close to what Mazda seems to be doing now, if above numbers > >>> are right. > >>> NSU had great hopes in that engine. It was used in a German fan-liner. > >>> It was the high point of the Wankel development at NSU. > >>> Then the money did run out. NSU was merged with AUDI, and VW the parent, > >>> killed it all. All further development was stopped. > >>> > >>> Fan Trainer: > >>> http://www.der-wankelmotor.de/Flugzeuge/RFB/rfb.html#Fanliner > >>> > >>> Regards > >>> Rolf > >>> > >>> > >>> George Lendich wrote: > >>>> Rolf, > >>>> Could you give me your assessment of the new 16X eccentric. If I > >>>> remember correctly you gave you assessment on Paul's site. There is > >>>> discussion on another site and I would like to pass it on to interested > >>>> parties. > >>>> Also if my memory serves me right, you mentioned a manufacturer was > >>>> working on a similar size ( change in eccentric) and what company that > >>>> was. > >>>> Am I wrong to believe it was the company you were working with at the > >>>> time? > >>>> George Lendich > >> > > > > > > -- > > Homepage: http://www.flyrotary.com/ > > Archive and UnSub: > > http://mail.lancaironline.net:81/lists/flyrotary/List.html > > > > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html >