Return-Path: Sender: "Marvin Kaye" To: lml@lancaironline.net Date: Mon, 03 Jan 2005 09:20:33 -0500 Message-ID: X-Original-Return-Path: Received: from mta9.adelphia.net ([68.168.78.199] verified) by logan.com (CommuniGate Pro SMTP 4.2.5) with ESMTP id 589730 for lml@lancaironline.net; Mon, 03 Jan 2005 09:17:25 -0500 Received-SPF: pass receiver=logan.com; client-ip=68.168.78.199; envelope-from=glcasey@adelphia.net Received: from worldwinds ([70.32.213.236]) by mta9.adelphia.net (InterMail vM.6.01.03.02 201-2131-111-104-20040324) with SMTP id <20050103141653.REXM14945.mta9.adelphia.net@worldwinds> for ; Mon, 3 Jan 2005 09:16:53 -0500 From: "Gary Casey" X-Original-To: "lancair list" Subject: Re: airspeed vs. power X-Original-Date: Mon, 3 Jan 2005 06:04:08 -0800 X-Original-Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="Windows-1252" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook IMO, Build 9.0.2416 (9.0.2910.0) X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 Importance: Normal I previously posted: <> Scott replied: <> I probably didn't complete the description: What I meant to say was that there is nothing in the fuel system itself that is designed to change air/fuel ratios with throttle position or air flow - they are (typically, at least) set for a constant air/fuel ratio across the air flow range for which they are designed. That is not to say the air/fuel will stay constant regardless of operating conditions. The two variables that can affect a change in air/fuel ratio are intake pulsations and reference pressure changes. The air flow pulsation characteristics can change with either throttle opening (partial throttle tends to smooth out the pulsations) or rpm, as the tuning and reverberation characteristics change with rpm. If the air flow into the servo changes its "pattern" the reference pressure could change, upsetting the calibration. In other words, it could be that the air swirls in a particular way under one conditions and then detaches from the wall or otherwise changes its flow pattern at another condition. This is especially true if the air has to make a sharp bend at the servo inlet. So what you are seeing could very well happen - the effect just isn't built into the system. As an example, my Cardinal has a very nicely designed servo inlet and the air/fuel ratio is very constant over a wide range of rpms and throttle openings. Come help me finish my ES and I'll report on that... Oh, and one more thing - the reference pressure applied to the injectors does not affect the fuel flow, but it does affect the reading of a pressure-type fuel flow indicator. The indicator is a pressure gage that is referenced to the pressure inside the cabin. The pressure drop in the injector itself is, however, referenced to the vent pressure at the injector. It is a small effect, but could change your fuel flow readings slightly. Gary Casey