X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from mail03.syd.optusnet.com.au ([211.29.132.184] verified) by logan.com (CommuniGate Pro SMTP 5.2.7) with ESMTPS id 3116770 for flyrotary@lancaironline.net; Sat, 06 Sep 2008 01:26:23 -0400 Received-SPF: pass receiver=logan.com; client-ip=211.29.132.184; envelope-from=lendich@optusnet.com.au Received: from george (d211-31-70-177.dsl.nsw.optusnet.com.au [211.31.70.177]) by mail03.syd.optusnet.com.au (8.13.1/8.13.1) with SMTP id m865PfFI025183 for ; Sat, 6 Sep 2008 15:25:43 +1000 Message-ID: <001f01c90fe1$04fcbba0$6400a8c0@george> From: "George Lendich" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: New rotary engine-mazda points on design Date: Sat, 6 Sep 2008 15:25:46 +1000 MIME-Version: 1.0 Content-Type: text/plain; format=flowed; charset="iso-8859-1"; reply-type=original Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.3138 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.3350 X-Antivirus: avast! (VPS 080905-0, 05/09/2008), Outbound message X-Antivirus-Status: Clean Ed, Of course I'm playing the devils advocate, when I mention these things as I'm as hopeful as anyone that it's exceptional, however I didn't know they were using ceramic coating on the aluminum -I would be concerned about ceramic coatings! George ( down under) >I understand your points and concern, George. But, just think about what > folks must have thought when the first rotary engine came out {:>). I > agree > with Ernest, the technology has come a long ways on ways to protect the > aluminum housings. > > I think most of the HP increase is as Ernest points out from combustion > volume increase (and a bit from less cooling of the combustion by the > walls) > so more heat to push the rotor. So I don't expect anything as exotic as > the > current Renesis engine in the intake department - they simply don't need > it > and the complexity and the cost it entails. But, of course, this all > remains to be seen. > > I'll take the chance on being one of the early ones to try the 16B - > getting > a bit tired of the 13B and haven't done anything to the aircraft in over a > year - its just starts up and takes me where I want to go. I guess the > honeymoon is over {:>) > > Still don't have any good feel on how soon we might see this engine - I > doubt it will be in the 2009 model year (probably out now). I hope to > heck > that FORD doesn't try to kill it which is a constant concern. > > Ah, well - back to programming. > > > > Ed Anderson > > Rv-6A N494BW Rotary Powered > > Matthews, NC > > eanderson@carolina.rr.com > > http://www.andersonee.com > > http://members.cox.net/rogersda/rotary/configs.htm#N494BW > > http://www.dmack.net/mazda/index.html > > -----Original Message----- > From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On > Behalf Of Ernest Christley > Sent: Friday, September 05, 2008 6:51 PM > To: Rotary motors in aircraft > Subject: [FlyRotary] Re: New rotary engine-mazda points on design > > George Lendich wrote: >> Ed, >> I was wondering about all that and hope any gains aren't negated by >> the removal of some highly tuned and complicated intake manifold, that >> won't fit into a cowl- like the Renesis manifold. >> > The gains are coming from increased volume. When it comes to power, > there is NO substitute for volume. We may not be able to get rated > power with an unoptimized, NA intake, but we WILL get more power. >> There is also the concern of how good the surface treatment of the >> aluminium side housing are going to be. I guess only time will tell. I >> hate the first release of anything like this, it invariably has problems. >> > That is a valid concern, but ceramic surface coatings have come a LONG > way in the past 20 years and are well understood by the people that need > to understand them. There isn't anything really cutting edge about what > they're doing. I plan to treat the engine I'm almost ready to start as > a 500hr engine. I'd treat the 16B the same way, just because they're so > cheap to replace. >> Then there's the complexity of injection and the very high pressure of >> direct injection, as well as the associated hardware and much needed >> software to make it all work. > From the animations, the injection timing will have the injectors > blowing fuel into a chamber that is below atmospheric, unless there is a > turbo pumping up the working chamber. Remember, the rotor is pulling > air into the chamber so you'll have less than 100% VE. Neither the > hardware nor the software are anything new. The only thing different is > when the software tells the hardware to blow fuel. Just a little > tweaking of some software parameters. No new territory is being > discovered. Again, nothing cutting edge. > > -- > > http://www.ernest.isa-geek.org > > > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: > http://mail.lancaironline.net:81/lists/flyrotary/List.html > > __________ Information from ESET NOD32 Antivirus, version of virus > signature > database 3267 (20080714) __________ > > The message was checked by ESET NOD32 Antivirus. > > http://www.eset.com > > > > __________ Information from ESET NOD32 Antivirus, version of virus > signature > database 3267 (20080714) __________ > > The message was checked by ESET NOD32 Antivirus. > > http://www.eset.com > > > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: > http://mail.lancaironline.net:81/lists/flyrotary/List.html