X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from mxsf39.cluster1.charter.net ([209.225.28.166] verified) by logan.com (CommuniGate Pro SMTP 5.0c3) with ESMTP id 750542 for flyrotary@lancaironline.net; Wed, 05 Oct 2005 11:04:00 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.225.28.166; envelope-from=cardmarc@charter.net Received: from mxip27a.cluster1.charter.net (mxip27a.cluster1.charter.net [209.225.28.184]) by mxsf39.cluster1.charter.net (8.12.11/8.12.11) with ESMTP id j95F3Emu002281 for ; Wed, 5 Oct 2005 11:03:14 -0400 Received: from fep01.charter.net (HELO 209.225.8.224) ([209.225.8.81]) by mxip27a.cluster1.charter.net with SMTP; 05 Oct 2005 11:03:14 -0400 Message-Id: <4enk4p$83c8a2@mxip27a.cluster1.charter.net> X-IronPort-AV: i="3.97,178,1125892800"; d="scan'208"; a="271982914:sNHT15928974" X-Mailer: Openwave WebEngine, version 2.8.18 (webedge20-101-1108-20050216) From: To: "Rotary motors in aircraft" Subject: Re: [FlyRotary] Counterweight for engine assy, 13Brewtt Date: Wed, 5 Oct 2005 11:03:14 -0400 MIME-Version: 1.0 Content-Type: text/plain; charset=ISO-8859-1 Content-Transfer-Encoding: 7bit Here's an even better one. I have a 93/94 engine. I have two counterweights I could use for this engine. They differ by 2 oz. (one has two holes drilled on the counterweight flange, the other 2, so it WAS balanced once for a particular engine assy). Which should I use, or do I need to get a dynamic balance of the assy after I clean up the rotors? Who does that-I saw a write up of balancing the assy.....? Is there an easy way I can determine which is best? Marc Wiese > > From: David Leonard > Date: 2005/10/04 Tue PM 07:21:08 EDT > To: "Rotary motors in aircraft" > Subject: [FlyRotary] Telling rotors apart - Never trust Atkins! > > On 9/28/05, Kelly Troyer wrote: > > > > Ed Anderson has a measurement to check the depth of the combustion > > depression in the > > face of the rotor to determine the compression ratio (the deeper one is > > turbo)....... > > > How about it Ed, any info on this? Can it be used to tell the 9.4:1 86-88 > rotors from the 9.7:1 rotors? > > Bottom line check weight first then check the depth of the combustion > > depression........I have > > another way I use to determine what year my rotors are (all my engines are > > NA 86 to 91).....The > > combustion depression in the 86 to 88 is as cast in the rotor (slight > > grainy surface finish).....The > > 89-91 depression is machined and has straight machine marks....... > > > That is really interesting. My old rotors are supposed to be 1991 T2 rotors > but they have the cast appearance (However since I got them from Atkins I am > not really sure they gave me what they sold me). The rotors that Earnest > sent also have a cast appearance. But as I recall, the rotors in the engine > I rebuilt had the milling marks... hmmm.. if that is true the balance in my > current engine is all SNAFU. Are you sure that system is a valid way to do > the measuring? > So I just got back from weighing my rotors - Sure enough, the ones Atkins > sold me weighted in at 10.20 and 10.19 making them the 86-88 variety despite > the fact that I paid for a '91 engine. Worse, I have no idea what > counter-weights he decided to use. If it matched the rotors he sold me then > I have been running an unbalanced engine for the last 150 hrs. (that > explains part of why the wife won't fly in it) > Does anyone know what the correct weights of the counter weights should be > for a given year group? Or perhaps some other way of telling them apart? > BTW Ernest, the rotors you sent also weigh in at 10.18. > Dave Leonard > > Check with Ed for his method to determine compression ratio as I do not > > have it at hand......I > > am attaching the rotor weight chart from "Mazdatrix" which will help (note > > weight does not > > include any seals or springs....just the bearing.........Hope this > > helps........Any more questions > > just ask !! > > -- > > Kelly Troyer > > Dyke Delta/13B/RD1C/EC2 > > *Engine* *Year* *Compression* *Weight (Grams)* *Weight (Pounds)* *12A * > > *76-82* *9.4* *4603* *10.15* *12A * *83-85* *9.4* *4353* *9.60* *13B* * > > 74-78* *9.2* *5253* *11.58* *13B* *84-85* *9.4* *5253* *11.58* *13B N/T* * > > 86-88* *9.4* *4553* *10.04* *13B Turbo* *86-88* *8.5* *4553* *10.04* *13B > > N/T* *89-92* *9.7* *4328* *9.54* *13B Turbo* *89-92* *9.0* *4328* *9.54* *13B > > T/T* *93-95* *9.0* *4328* *9.54* > > > > *NOTE: Weights are approximate, and include rotor bearing, but do not > > include any seals or springs. * > > > > > > > -- > Dave Leonard > Turbo Rotary RV-6 N4VY > http://members.aol.com/_ht_a/rotaryroster/index.html > http://members.aol.com/_ht_a/vp4skydoc/index.html > >