X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from mx2.netapp.com ([216.240.18.37] verified) by logan.com (CommuniGate Pro SMTP 5.3.2) with ESMTPS id 4120959 for flyrotary@lancaironline.net; Thu, 11 Feb 2010 10:30:31 -0500 Received-SPF: softfail receiver=logan.com; client-ip=216.240.18.37; envelope-from=echristley@nc.rr.com X-IronPort-AV: E=Sophos;i="4.49,453,1262592000"; d="scan'208";a="314895245" Received: from smtp1.corp.netapp.com ([10.57.156.124]) by mx2-out.netapp.com with ESMTP; 11 Feb 2010 07:29:54 -0800 Received: from [10.62.16.80] ([10.62.16.80]) by smtp1.corp.netapp.com (8.13.1/8.13.1/NTAP-1.6) with ESMTP id o1BFTrS0015089 for ; Thu, 11 Feb 2010 07:29:54 -0800 (PST) Message-ID: <4B742270.4060809@nc.rr.com> Date: Thu, 11 Feb 2010 10:29:52 -0500 From: Ernest Christley Reply-To: echristley@nc.rr.com User-Agent: Thunderbird 2.0.0.23 (X11/20090817) MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Flywheel turbo References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit Al Gietzen wrote: > I'm taking the intake air from around the side of the gearbox, through > its mounting plate. The flywheel will have an impeller attached to it. > I built a fiberglass shroud to enclose the area between the gearbox > mounting plate and the engine. Intake air is taken from this > centrifugal pump. > > I admire the creativity and effort, but I see big question marks. My only > point of reference is a large furnace type centrifugal blower which > generates maybe 1/2" HG pressure. And how is this approach going come > close to the efficiency of a well designed supercharger. > > I've been wrong before; so go ahead - shoot me. > > Al > > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html > > I ain't claiming to be right until my engine runs, but... The research I've done leads me to believe that a centrifugal pump can give you pressure or volume. The 1/2" HG may be all that was needed to get the volume of airflow the designers wanted? I'm trying to remember the numbers off the top of my head, so please forgive me if I'm way off, but with the approximately 11" diameter of the flywheel spinning between 6000 and 6500RPM, the equations said I would get 2lbs of pressure increase. 2lbs of pressure translates into somewhere around 20Hp. I tested the static pressure of my electric leaf blower. Labeled to spin at 9000RPM with a 6" impeller. I got over 9" of static pressure. That was enough incentive for me to give it the old college try. If you look at the numbers for "high efficiency" vs a round plate with perpendicular vanes bolted to it, the efficiency drops from the mid-90s to the mid-80s. Quite a lot of specialized engineering goes into squeezing out that last 10 points. I don't yet have the environmental data or skills to design or manufacture what would be needed to get that last 10 points. Sooo .... I'll see what I can get with what I can do, and then decide if I should expand on what I can do. I've attached a OpenOffice document dealing with the design of centrifugal compressors for your reading pleasure. (EDIT: My mail bounced because the document was to big. If you want it, I'll email it to you directly.) My engine has not run yet. This may be a complete waste of time. YMMV. Not applicable outside of the continental United States. Franchisees are individual owners and may not participate in this promotion. etc.... Lynn, I gave some consideration to the multiple stage idea. The leading scenario would be to have a two piece shroud. An impeller would be attached to the engine shaft, then the first shroud would be bolted to the engine. Then the flywheel mounted, followed by the front impeller, followed by the second shroud. The two big problems were the complexity of all the clearances needed, and, more importantly, the counterweight. There simply wasn't enough room to get enough flow. You need significantly more pump volume than needed for the intake in order to develop rated pressure.