X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml Date: Tue, 08 Dec 2009 11:16:31 -0500 Message-ID: X-Original-Return-Path: Received: from bosmailout20.eigbox.net ([66.96.185.20] verified) by logan.com (CommuniGate Pro SMTP 5.3c3) with ESMTP id 4010670 for lml@lancaironline.net; Tue, 08 Dec 2009 11:06:12 -0500 Received-SPF: pass receiver=logan.com; client-ip=66.96.185.20; envelope-from=SRS0=m+EfUc=H2=mwheli.com=bjburr@eigbox.net Received: from bosmailscan20.eigbox.net ([10.20.15.20]) by bosmailout20.eigbox.net with esmtp (Exim) id 1NI2ZE-0006AD-E7 for lml@lancaironline.net; Tue, 08 Dec 2009 11:05:36 -0500 Received: from bosimpout02.eigbox.net ([10.20.55.2]) by bosmailscan20.eigbox.net with esmtp (Exim) id 1NI2ZE-0006Nv-8y; Tue, 08 Dec 2009 11:05:36 -0500 Received: from bosauthsmtp16.eigbox.net ([10.20.18.16]) by bosimpout02.eigbox.net with NO UCE id Eg5A1d0080LoEWa01g5A9L; Tue, 08 Dec 2009 11:05:10 -0500 X-EN-OrigOutIP: 10.20.18.16 X-EN-IMPSID: Eg5A1d0080LoEWa01g5A9L Received: from c-76-27-82-124.hsd1.ut.comcast.net ([76.27.82.124] helo=[192.168.0.7]) by bosauthsmtp16.eigbox.net with esmtpa (Exim) id 1NI2ZA-0000Na-TT; Tue, 08 Dec 2009 11:05:36 -0500 X-Original-Message-Id: <5921DBA9-5E11-4A75-BD8B-48C6A7B00ABF@mwheli.com> From: Burr Bryan X-Original-To: List Lancair Content-Type: text/plain; charset=US-ASCII; format=flowed; delsp=yes Content-Transfer-Encoding: 7bit Mime-Version: 1.0 (Apple Message framework v936) Subject: Super ES Cabin Heat X-Original-Date: Tue, 8 Dec 2009 09:05:29 -0700 X-Original-Cc: "Lancair_ES@yahoogroups. Com" X-Mailer: Apple Mail (2.936) X-EN-UserInfo: afb066d8b4230608b04b264cad72a5d8:59efd05c4346593dae8a30875e4d072b X-EN-AuthUser: bjburr@mwheli.com X-Original-Sender: Burr Bryan X-EN-OrigIP: 76.27.82.124 X-EN-OrigHost: c-76-27-82-124.hsd1.ut.comcast.net The Lancair Super ES (TSIO 550E) normally takes the cabin heat from the sonic venturi ports on the induction air system. This does not provide very much heat, it is extremely noisy, and what heat is provided is lost in decent when power is reduced and the turbochargers are not in demand. In pressurized airplanes ie. LIVP and Piper Mirage, the heat is provided through the pressurization system and these problems are eliminated. I have contacted Aerospace Welding Minneapolis, manufactures of several exhaust systems for many different GA aircraft, about making a heat muff system for this engine. They are willing to look at manufacturing a heat muff shroud that would wrap around the R/H exhaust pipe. We looked at the turbo crossover tube but there is not much clearance between the tube and the firewall. Is anyone interested in this type of system for their TSIO550 powered ES? I am trying to get an idea of how many systems could be produced at one time if a group order were placed. Also, would anyone be willing to part with their r/h exhaust pipe for evaluation purposes? Thanks, Bryan Burr N132BB Lancair Super ES