Return-Path: Received: from smtp1.netdoor.com ([208.137.128.154] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 3111769 for flyrotary@lancaironline.net; Sun, 21 Mar 2004 17:14:54 -0500 Received: from netdoor.com (port611.jxn.netdoor.com [208.148.209.11]) by smtp1.netdoor.com (8.12.10/8.12.1) with ESMTP id i2LMEl9T026649 for ; Sun, 21 Mar 2004 16:14:47 -0600 (CST) Message-ID: <405E13D1.8070002@netdoor.com> Date: Sun, 21 Mar 2004 16:14:41 -0600 From: Charlie & Tupper England Reply-To: cengland@netdoor.com User-Agent: Mozilla/5.0 (Windows; U; Windows NT 5.1; en-US; rv:1.4) Gecko/20030624 Netscape/7.1 (ax) X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Fuel Consumption Questions References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit X-Spam-Score: 0.1 X-Scanned-By: MIMEDefang 2.31 (www . roaringpenguin . com / mimedefang) Greg Fuess wrote: >Hi Fellow Rotor heads, > >I am getting very close to starting construction of an RV-7 (much closer >than last year when I said this! - should start in 8~10 weeks) and very >interested in the potential for the Renesis engine in this application >(can't wait for Tracy to get his installed so we can read the performance >reports). I do have one question that is difficult for me to get my arms >around. What kind of fuel burn are you guys experiencing that are flying >your 13Bs? Turbocharged 13Bs? -at various power settings and altitudes? Is >there a data reference site anywhere that could provide this information? > >Ed Anderson's Rotary Power vs. 2-3-2 Cooling BTU calculation spreadsheet >indicated 12.4 to 14.9 gph at 5k to 6k rpm (all for 1,500' alt). This seems >not to compare well to the lyconosaurus published consumption rates for a >180 hp engine, though I have read elsewhere on the internet that the rotary >consumption should be similar. Am I misreading or misusing Ed's >spreadsheet, or should I get used to the higher consumption rate? Are the >Lycoming consumption rates bogus? > >I am something of a lurker here, but as I get closer to the "date", I am >getting more and more detail conscientious. Appreciate any and all >thoughts. > >Best Regards, > >Greg Fuess > Hi Greg, To add to what Ed & Tracy have already said about the rotary, here are some real world numbers on Lycs. A carburated 180 hp Lyc running at 75% power is making 135hp. The best BSFC you can expect from a stock carburated Lyc is about .45 lb per HP per hour. Av gas weighs about 6 lbs per gal. If you do the math, that's 135 X .45 / 6=10.125 gal per hour. I can tell you from personal experience that this is a realistic number for a 180hp Lyc. If you run the numbers at full power on the Lyc, it's 180 X .55 / 6 = 16.5 gal per hour. Note that the BSFC is now .55 instead of .45 (& could be worse than that; required to prevent burning exhaust valves & melting pistons in a Lyc aircooled engine). When your buddies tell you that their 180 only burns 8.5 gph (or 8.8, or whatever), ask them what rpm & manifold pressure they cruise at. If you get an 'uhhh...', walk away. If they have a fixed pitch prop, don't even bother to ask the question. :-) Most people flying Lycs tend to run them at well below 75% power thinking that they are extending engine life. Most are also afraid to properly lean, because they are afraid of burning valves & melting pistons. Put the 2 together & you will realize that most (especially with fixed pitch props) are running at down around 55% power at that 8.5 gph figure. Allowing for less than optimum leaning & running numbers again, ??hp X .5 / 6 = 8.5gph. Solving the formula yields 102hp. 102/180 is .5666. Hmmm, what a coincidence..... The Lyc factory fuel burn charts I've seen are often hard to interpret, but I think you will find that they agree fairly well with the numbers above. What does Ed's spreadsheet show for 100hp, & does it allow for improved BSFC when the engine is leaned for such a low power setting? Charlie