Return-Path: Received: from [24.25.9.102] (HELO ms-smtp-03-eri0.southeast.rr.com) by logan.com (CommuniGate Pro SMTP 4.2.5) with ESMTP id 552318 for flyrotary@lancaironline.net; Wed, 01 Dec 2004 07:35:01 -0500 Received-SPF: none receiver=logan.com; client-ip=24.25.9.102; envelope-from=eanderson@carolina.rr.com Received: from edward2 (cpe-069-132-109-019.carolina.rr.com [69.132.109.19]) by ms-smtp-03-eri0.southeast.rr.com (8.12.10/8.12.7) with SMTP id iB1CYLkd003255 for ; Wed, 1 Dec 2004 07:34:23 -0500 (EST) Message-ID: <002201c4d7a2$1e836d60$2502a8c0@edward2> From: "Ed Anderson" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: New Muffler Design Date: Wed, 1 Dec 2004 07:34:36 -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 Yes and No, Finn My principal objective was simply to get the mechanics of the variable intake length down and working which I did. I made a number of compromises including using my first home made lower intake manifold (for convince - had it laying around) which I knew had poor flow characteristics (one of the reasons I took it off in the first place). Then to make it even easier I used an old Webber upper manifold which required I merge the primary and secondary intakes. But, I think where I really went wrong was having a tight 180 deg bend in the intake right where the throttle body was positioned. The pulses do not like sharp turns. In any case, I did vary the manifold in flight but to my surprise it did not cause the rpm to vary even 50 rpm - I would have expected some change even if due to "organ pipe" tuning effect. But, Nada! which was a little strange in itself. I then got involved in converting to the 2.85 and monster prop, so I took the variable intake off and reverted to the manifold that had proven to give me the best power. However, I will revisit the variable intake - but this time I will not merge the primary and secondary nor require the FAW to follow a tight 180 deg turn. The mechanics of running 4 tubes up and down is a bit more involved that just running two - so need to do some head scratching to come up with a lightweight and reliable mechanism. Just too many projects and not enough time/$$ to do them all {:>) Ed Anderson ----- Original Message ----- From: "Finn Lassen" To: "Rotary motors in aircraft" Sent: Tuesday, November 30, 2004 11:55 PM Subject: [FlyRotary] Re: New Muffler Design > Hi Ed, > > I just realized that you started a new project. Did you ever finish the > variable intake length testing? > > Finn > > > >> Homepage: http://www.flyrotary.com/ > >> Archive: http://lancaironline.net/lists/flyrotary/List.html >