X-Virus-Scanned: clean according to Sophos on Logan.com X-SpamCatcher-Score: 50 [XX] (100%) RECEIVED: Received headers not consistent with Juno "FROM:" Return-Path: Received: from m12.lax.untd.com ([64.136.30.75] verified) by logan.com (CommuniGate Pro SMTP 5.1.6) with SMTP id 1847089 for flyrotary@lancaironline.net; Mon, 19 Feb 2007 11:24:27 -0500 Received-SPF: pass receiver=logan.com; client-ip=64.136.30.75; envelope-from=alwick@juno.com Received: from m12.lax.untd.com (localhost [127.0.0.1]) by m12.lax.untd.com with SMTP id AABC7VV2FAUD6G4S for (sender ); Mon, 19 Feb 2007 08:23:33 -0800 (PST) X-UNTD-OriginStamp: L941HVjjYzDhN3itp//mkEWPgOn1DIZGF17qzdnhllrh3Tuow5VwbA== Received: (from alwick@juno.com) by m12.lax.untd.com (jqueuemail) id MEX33K5J; Mon, 19 Feb 2007 08:22:56 PST To: flyrotary@lancaironline.net Date: Mon, 19 Feb 2007 07:51:04 -0800 Subject: Re: [FlyRotary] Re: Cowling and engine installation RV 7A Message-ID: <20070219.082200.2644.0.alwick@juno.com> X-Mailer: Juno 5.0.49 MIME-Version: 1.0 Content-Type: text/plain; charset=us-ascii Content-Transfer-Encoding: 7bit X-Juno-Line-Breaks: 4-5,11-12,20-24,26-45,47,49-50 From: al p wick X-ContentStamp: 17:8:1129695258 X-MAIL-INFO:0a24a1b5a5f99114f924ddd1ddf0b48d9514b145e195b4c181c191c44539c1ddfd6410648590e48510a05110ade080e19970ddd160d5a1f4dda434cdb9b9c5c4556d49fd84510c65fdada0a0406505e9e029748574042d89897954e1b53d3991a179b0a124593045a9a1b171696154b1a945b1d5b1b4356d1140894d792079f5549524411d953de1a5 X-UNTD-Peer-Info: 127.0.0.1|localhost|m12.lax.untd.com|alwick@juno.com I've seen dyno reports that show Hp gain at certain cam timing settings. However, I expect I'll eventually lock the timing at one ideal setting and then remove the unneeded components. It will be fun playing with it and measuring the difference. I do my best to avoid speculative decisions. If you go back thru the archives for just about any engine, it's not the OEM systems that represent our big risk items. It's the changes we make. I just got report of pilot that died recently in Canard crash. Same root cause as revealed in our recent fuel line discussions. He used materials and installation method that is sensitive to the environment. Heat and vibration sensitive. In his case, he used plastic fitting for fuel flow measure in high heat area. We don't know if the plastic fatigued first, or melted. When we analyze this, we realize he added unnecessary component to fuel system, changed the system design, and unexpectedly ended up with system sensitive to both heat and vibration. Same cause as hard plumbing fuel system. No OEM system hard plumbs these systems. Yet we innovate and increase our risk. It's difficult to appreciate the effects of vibration and stress concentrations simply because it's not something we see. -al wick On Mon, 19 Feb 2007 08:33:36 +0800 david mccandless writes: > Hi Al, > what is the point in having variable valve lift and cam timing in an > > aircraft engine? > As I understand it, these features are for low speed torque > enhancement > in cars. Not applicable in aircraft engines. > Seems to me you have extra complication and failure modes built in > . > BR, Dave McC > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: http://mail.lancaironline.net/lists/flyrotary/ > > -al wick Cozy IV powered by Turbo Subaru 3.0R with variable valve lift and cam timing. Artificial intelligence in cockpit, N9032U 240+ hours from Portland, Oregon Glass panel design, Subaru install, Prop construct, Risk assessment info: http://www.maddyhome.com/canardpages/pages/alwick/index.html