X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from sj-iport-2.cisco.com ([171.71.176.71] verified) by logan.com (CommuniGate Pro SMTP 5.0c5) with ESMTP id 771139 for flyrotary@lancaironline.net; Mon, 17 Oct 2005 15:54:04 -0400 Received-SPF: softfail receiver=logan.com; client-ip=171.71.176.71; envelope-from=echristley@nc.rr.com Received: from sj-core-1.cisco.com ([171.71.177.237]) by sj-iport-2.cisco.com with ESMTP; 17 Oct 2005 12:53:21 -0700 Received: from xbh-rtp-211.amer.cisco.com (xbh-rtp-211.cisco.com [64.102.31.102]) by sj-core-1.cisco.com (8.12.10/8.12.6) with ESMTP id j9HJq9vF002474 for ; Mon, 17 Oct 2005 12:53:18 -0700 (PDT) Received: from xfe-rtp-202.amer.cisco.com ([64.102.31.21]) by xbh-rtp-211.amer.cisco.com with Microsoft SMTPSVC(6.0.3790.211); Mon, 17 Oct 2005 15:52:49 -0400 Received: from [64.102.45.251] ([64.102.45.251]) by xfe-rtp-202.amer.cisco.com with Microsoft SMTPSVC(6.0.3790.211); Mon, 17 Oct 2005 15:52:49 -0400 Message-ID: <43540111.7080502@nc.rr.com> Date: Mon, 17 Oct 2005 15:52:49 -0400 From: Ernest Christley Reply-To: echristley@nc.rr.com User-Agent: Mozilla Thunderbird 1.0.2 (X11/20050317) X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: Displacement - Again? Timing of the Work References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit X-OriginalArrivalTime: 17 Oct 2005 19:52:49.0420 (UTC) FILETIME=[5A3714C0:01C5D354] Bob White wrote: >Let me re-emphasize this: Every detail of Ed's analysis looks exactly >correct to me. The Mazda 13B produces power and breathes about the same >way a 4 cylinder 2.6L 4 cycle piston engine does, or about the same as a >2 cylinder 1.3L 2 cycle piston engine. > > > Yeah, but what if the eShaft had an integrated reduction drive that dropped the ouput to 1/3, so that the eShaft output and the rotors had the same speed. Would it then breathe like a 3.9L 2 cycle, or a 5.2L 4 cycle? 8*) >I also think it sound better to think of the rotary as a 3.9L engine >turning 3000 rpm (rotor speed) rather than a 1.3L engine turning 9000 >rpm (output shaft speed). It's too bad we can't easily couple the >propeller directly to the rotors and eliminate the PSRU. Now that >would be a setup. > >Bob W. > > We could do that; especially easy on a single rotor. Press in a propeller adapter in place of the rotor bearing. Then the wobble of the propeller would almost be enough to make you think your were flying behind a Lycoming again! The certified crowd would feel right at home!! (The peanut gallery hath spoken 8*) -- ,|"|"|, | ----===<{{(oQo)}}>===---- Dyke Delta | o| d |o www.ernest.isa-geek.org |