Return-Path: Received: from smtp813.mail.sc5.yahoo.com ([66.163.170.83] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with SMTP id 3110942 for flyrotary@lancaironline.net; Sun, 21 Mar 2004 01:19:44 -0500 Received: from unknown (HELO HomeComputer) (gregory?fuess@68.90.40.40 with login) by smtp813.mail.sc5.yahoo.com with SMTP; 21 Mar 2004 06:19:22 -0000 From: "Greg Fuess" To: "'Rotary motors in aircraft'" Subject: Fuel Consumption Questions Date: Sun, 21 Mar 2004 00:19:23 -0600 MIME-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit X-Mailer: Microsoft Office Outlook, Build 11.0.5510 In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 Thread-Index: AcQOQP2urxhrrw7USpSvlKERENuTOQAyMJbg Message-ID: 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