Return-Path: Received: from mxsf02.cluster1.charter.net ([209.225.28.202] verified) by logan.com (CommuniGate Pro SMTP 4.2b2) with ESMTP id 3182678 for flyrotary@lancaironline.net; Wed, 21 Apr 2004 11:27:56 -0400 Received: from [10.0.1.2] ([68.189.49.127]) by mxsf02.cluster1.charter.net (8.12.11/8.12.11) with ESMTP id i3LFLeqf093651 for ; Wed, 21 Apr 2004 11:21:41 -0400 (EDT) Mime-Version: 1.0 (Apple Message framework v613) In-Reply-To: References: Content-Type: text/plain; charset=US-ASCII; format=flowed Message-Id: <9467C584-93A7-11D8-B637-0003930BF7DE@charter.net> Content-Transfer-Encoding: 7bit From: kelseyjewett Subject: Re: [FlyRotary] 13B dynafocal mount - was dream time Date: Wed, 21 Apr 2004 08:21:36 -0700 To: "Rotary motors in aircraft" X-Mailer: Apple Mail (2.613) I like the idea of having my cg and FWF weight the same as a Lycoming o-320. I went to the web site for the Swedish rotary, and I liked the simplicity of the rear casting bolting to the standard mount. I also like Mikes comment about moving the prop flange forward two inches. My RV-7A could use a longer, sleeker forward fuselage. This could also give more room for the cooling system below the engine. KelseyJewett still dreaming On Apr 19, 2004, at 4:49 PM, Michael McGee wrote: > At 08:39 2004-04-19, you wrote: > >> > the puzzle. It seem there is a lot of re inventing >> the wheel. I >> >> >> I was thinking that, too. Then I realized that what >> is going on is parallel developement. Something you >> will probably never see in a corporate lab. Lots of >> slightly different ideas being worked on at the same >> time. >> >> What I see happening right now is that a lot of >> these ideas that have been on the workbench for >> years are coming out of developement and into long >> term testing. I think over the next year or so you >> will start to see a lot more consensus on what works >> best, as the different approaches get tested and >> we're able to see what works best in the real world. >> Then you'll start to see people willing to bet the >> farm on a business venture to create firewall >> forward packages. > > Speaking of dreaming.. > > What do you guys think of the viability of a front cover cast into the > form of a standard Lycoming dynafocal-1 mount? > > A loose collection of my thoughts so far: > > I think it would sell well enough to get the price under $500 for the > kit. I was bs-ing with the local rotary engine builder the other day > and he showed me a very nice third-gen oil pan that was cast as a > torsionally stiff replacement for the stamped steel original. The > reason behind the pan is another story but the casting work looked > great (from this engineer/ non-casting expert's perspective anyway). > He insists that he has a casting guy that is capable of making what we > need if I can get him a proto type part. > > The thought here is a Dynafocal mount would open up more of the market > to those who would convert to rotary engines (like I'm doing) if it > didn't require changing the motor mount. I realize that we can make a > decent mount without it and use something like the Schertz beam or the > bell housing that the ACRE group is working on. The Dyna-1 mount > would be an effort towards more of a standardization for aircraft use. > > I've been toying with this for the last couple of weeks and while it > needs some serious planning for water pump and alternator > accommodations, I've got a bit of it worked out. As expected it isn't > as easy as originally thought. Of course if it was it would already > be done. It would be supplied as a package with water pump system and > alternator mount. > > This does require using a remote water pump like what Paul Lamar > created and which isn't a bad idea. It gets the pump down lower for > better performance. If you use a 3rd gen water pump with its own > remote pump housing it could be mounted co-axially with the crank and > get rid of a water pump drive belt. (3rd gen pumps run opposite > direction to earlier pumps) > > It also would require using the 3rd gen crank angle sensor plate and > pickups. > > There are enough bolts on the front end plate to hold it together. > Additional reinforcements for the aerobatics crowd would be added at > the oil pan-to-front cover flange and on the top from the EGR port on > the center plate to the top of the motor mount/front cover. This > would probably be standard for the 20Bs. > > -Could be that the sealing surfaces would be a problem as a structural > interface? > -It would put the prop flange about 2 inches forward of the Lycoming > installation. However that would put the 13B c.g. about the same as > the Lyc. > > As an RV-4 owner the thought of a motor mount as compact as the > dynafocal mount is appealing. Yes, I know it has been done on an RV-4 > otherwise. I'm just looking at future possibilities and.. gee.. > ANOTHER project. > > Okay, enough for now, you guys shoot holes in this for me.... > > > Mike McGee, RV-4 N996RV, O320-E2G, Hillsboro, OR, > jmpcrftr-at-teleport.com > 13B in gestation mode, RD-1C, EC-2. > ..need to quit thinking and get some building done... > > >>> Homepage: http://www.flyrotary.com/ >>> Archive: http://lancaironline.net/lists/flyrotary/List.html >