Return-Path: Received: from [65.33.160.219] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 4.2.5) with HTTP id 566608 for flyrotary@lancaironline.net; Mon, 13 Dec 2004 22:41:35 -0500 From: "Marvin Kaye" Subject: Re: [FlyRotary] Re: A First (and note to Perry) To: "Rotary motors in aircraft" X-Mailer: CommuniGate Pro WebUser Interface v.4.2.5 Date: Mon, 13 Dec 2004 22:41:35 -0500 Message-ID: In-Reply-To: References: MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit "Perry Mick" wrote: """ I've tried 4 times now to use a computerized dynamic balance system, but it won't converge on a solution. It always worked perfectly with my direct-drive fan. So it mustn't like geared engines. I'm going to trial- and-error it by moving a fender washer (weight) from one prop bolt to the next and see if the vibration level readout increases or decreases, and try to find a minimum. """ I'm curious, Perry, if a fender washer might not be overkill... last guy I saw had a prop dynamically balanced it took a short #6 screw to get the job done. Given the size of prop bolts and their associated fender washer size, aren't you concerned that will be _too much_ mass? I'd think that much weight fladdling around off-center out there at 2000+ rpm would make matters worse, not better. Like I said, just curious (and concerned).