X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from [207.189.223.49] (HELO email3.peakpeak.com) by logan.com (CommuniGate Pro SMTP 4.3c5) with ESMTPS id 940942 for flyrotary@lancaironline.net; Thu, 12 May 2005 03:05:07 -0400 Received-SPF: none receiver=logan.com; client-ip=207.189.223.49; envelope-from=billdube@killacycle.com Received: (qmail 9720 invoked by uid 513); 12 May 2005 07:58:38 -0000 Received: from 207.189.221.161 by email3 (envelope-from , uid 504) with qmail-scanner-1.23 (clamscan: 0.83 Clear:RC:1(207.189.221.161):. Processed in 0.565495 secs); 12 May 2005 07:58:38 -0000 Received: from 161-221-189-207.dyn.peakpeak.com (HELO tigger.killacycle.com) ([207.189.221.161]) (envelope-sender ) by email3.peakpeak.com (qmail-ldap-1.03) with SMTP for ; 12 May 2005 07:58:37 -0000 Message-Id: <4.3.1.0.20050512000541.01c79ac0@mail.chisp.net> X-Sender: billdube@mail.chisp.net X-Mailer: QUALCOMM Windows Eudora Version 4.3.1 Date: Thu, 12 May 2005 00:32:11 -0600 To: "Rotary motors in aircraft" From: "BillDube@killacycle.com" Subject: Re: [FlyRotary] Re: More about Mufflers In-Reply-To: Mime-Version: 1.0 Content-Type: text/plain; charset="us-ascii"; format=flowed At 05:19 PM 5/11/2005, you wrote: >Hey, Bill! > >Great find. Boy talk about a thorough investigation. Will take a bit to >digest even a part of it, but it looks hopeful that their may be something >I can use to quite this louder engine. They don't specifically address absorption style mufflers, but they indirectly do so when they evaluate "concentric" style resonators and vary the size and number of the connecting orifices. Looking at the charts, an absorption muffler looks like it might be a good option because of the broad band attenuation. The biggest hurdle would be to build one that is lightweight, small, robust, and can take the high exhaust temps. I think that a couple of layers Inconel screen might work for the inside "tube" of an absorption muffler. The section on varying the connection tube length on a single chamber resonator looks quite useful for designing the cross-over between rotors. I think the tube leading to an adjacent rotor will behave as a single chamber resonator with a small chamber volume. By cleverly selecting the length of the header tube before the Y, one might be able to reduce the exhaust noise at cruise significantly with no reduction in performance and no significant increase in weight. Bill Dube'