Return-Path: Received: from [24.25.9.100] (HELO ms-smtp-01-eri0.southeast.rr.com) by logan.com (CommuniGate Pro SMTP 4.3c3) with ESMTP id 811765 for flyrotary@lancaironline.net; Sat, 19 Mar 2005 17:28:55 -0500 Received-SPF: pass receiver=logan.com; client-ip=24.25.9.100; envelope-from=eanderson@carolina.rr.com Received: from edward2 (cpe-024-074-185-127.carolina.rr.com [24.74.185.127]) by ms-smtp-01-eri0.southeast.rr.com (8.12.10/8.12.7) with SMTP id j2JMS5Lw009618 for ; Sat, 19 Mar 2005 17:28:06 -0500 (EST) Message-ID: <000c01c52cd2$f30284b0$2402a8c0@edward2> From: "Ed Anderson" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: Engine size Date: Sat, 19 Mar 2005 17:28:17 -0500 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1106 X-MIMEOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 X-Virus-Scanned: Symantec AntiVirus Scan Engine ----- Original Message ----- From: "Charlie England" To: "Rotary motors in aircraft" Sent: Saturday, March 19, 2005 12:22 PM Subject: [FlyRotary] Re: Engine size > randy echtinaw wrote: > > > Gentlemen, > > I am building an acro rated single seat biplane that the designer > > has limited the max. engine size to IO-360. I am surmising that this > > engine limitation is based on weight and airframe maximum speed. I > > have decided to use rotary power and am slowly developing a plan as to > > what I will use. I am looking for a little more help going "vertical." > > The rotary weight (less) will be a bonus. I am not an engineer and am > > not even related to one so my question: > > Can I go to a P-port 2 rotor in the 230-240 hp range if I do not > > exceed the max. airframe speed. > > Thank you, > > Randy > > > It's like real estate, except 'prop diameter, prop diameter, prop > diameter'. I'm no aero engineer either but I do hear them talk about > stuff like 'mass flow' increases with increases in prop diameter. Vance > Jaqua, who contributed to the design of the KIS kit a/c, published a > chart several years ago showing prop efficiency for various diameters at > various speeds & it's pretty amazing what extra diameter can do, > especially if you're stuck with fixed pitch. > > I don't know if Tracy or Ed flew their 68" props on the 2.85-1 gearboxes > but if they did they could give you an idea on how much difference extra > diameter makes on the same power. I believe that both are now running > 74"-76" diameter with radical increases in climb performance. > > Relatively small increases in prop diameter result in large increases in > climb ability. Consider that 160 hp in a 2seat helicopter will lift the > a/c & 2 people straight up. > > Talk Tracy into making you a gearbox with the 3-1 ratio or talk to Ken > Welter http://homepage.mac.com/rotarycoot/ about one of his belt drive > reductions & build long gear legs for prop clearance. > > Charlie > Charlie, we could not compare the 68" prop on the 2.85 gear boxes because the 2.85 rotates opposite to the 2.17. We might upset some of our canard friends trying it. However, I can tell you the combination of the increase from 68-76 inch in prop diameter combined with the 2.85 gear ratio make a considerable improvement in take off acceleration and climb - actually added about 4-5 mph on the top end as well. I have hit 6800 rpm in WOT level flight. I would think an areo type aircraft would have to use at least the 2.85. Ed A Rv-6A N494BW Rotary Powered Matthews, NC eanderson@carolina.rr.com