X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from [216.211.128.10] (HELO mail-in04.adhost.com) by logan.com (CommuniGate Pro SMTP 5.1c.3) with ESMTP id 1369083 for flyrotary@lancaironline.net; Fri, 08 Sep 2006 00:41:48 -0400 Received-SPF: none receiver=logan.com; client-ip=216.211.128.10; envelope-from=joeh@pilgrimtech.com Received: from Pilgrim10 (c-67-183-14-47.hsd1.wa.comcast.net [67.183.14.47]) by mail-in04.adhost.com (Postfix) with ESMTP id 3CC53E3713 for ; Thu, 7 Sep 2006 21:42:05 -0700 (PDT) (envelope-from joeh@pilgrimtech.com) From: "Joe Hull" To: "'Rotary motors in aircraft'" Subject: RE: [FlyRotary] Exhaust System - Comments? Date: Thu, 7 Sep 2006 21:40:29 -0700 Message-ID: <019e01c6d300$f37aa640$bb02a8c0@redmond.corp.microsoft.com> MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit X-Mailer: Microsoft Office Outlook 11 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.2962 In-Reply-To: Thread-Index: AcbS5i3W1v/1OHWGT7Ogz7x74LMR9wAGehWQ Looks good to me - but I would have Burns do it in the thickest piece of 321 they have (which I think is .049). Also, the slip joint at the flange is a good idea too - more like a necessary idea. Watch for places where you will have differential vibration/movement. I.e. the engine is on rubber mounts and moves independent of the fuselage - so if you support the exhaust on the engine and on the engine mount/fuselage - you've go different movement. You will need to de-couple the parts so they can move independent of one another. Joe Hull Cozy Mk-IV N31CZ (65 hrs - Rotary 13B NA) Redmond (Seattle), Washington > -----Original Message----- > From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On > Behalf Of Steve Thomas > Sent: Thursday, September 07, 2006 5:29 PM > To: Rotary motors in aircraft > Subject: [FlyRotary] Exhaust System - Comments? > > I have been lurking on this list for some time, really enjoying and > learning from all of your experiences. I'm the guy who has Mistral's > serial number 001, two rotor normally aspirated engine. > > I just finished tacking this exhaust system together and thought that > I'd ask for comments. The current material is mild steel, but my > plan is to take it to Burns Stainless (just down the road from me) > and have them duplicate it in 16 ga. 321 stainless. The collector > is from Burns, as is the muffler. If you can see the tacks, you'll > be able to see why I'm taking it elsewhere. ;-) The header pipes > are 2" and the combined pipe after the collector is 2 1/2". This was > recommended by Burns. > > After fabrication, I plan to have it coated with HPC HyperCoat > Extreme as my design goal was to get the heat out as quickly and > directly as possible and keep as much in the pipes as possible until > it exits to atmosphere. > > The oddball bends in the header were designed to keep the header > pipes the same length, which they are. Given all the difficulty some > have had with their exhaust systems, I'd thought that I'd throw it > out there for comments. > > Best Regards, > > Steve Thomas > SteveT.Net > > ________________________________________________________________________