X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml Date: Tue, 08 Dec 2009 22:13:19 -0500 Message-ID: X-Original-Return-Path: Received: from mail-yw0-f197.google.com ([209.85.211.197] verified) by logan.com (CommuniGate Pro SMTP 5.3c3) with ESMTP id 4011164 for lml@lancaironline.net; Tue, 08 Dec 2009 17:07:44 -0500 Received-SPF: pass receiver=logan.com; client-ip=209.85.211.197; envelope-from=ronlaughlin@gmail.com Received: by ywh35 with SMTP id 35so1952100ywh.7 for ; Tue, 08 Dec 2009 14:07:07 -0800 (PST) DomainKey-Signature: a=rsa-sha1; c=nofws; d=gmail.com; s=gamma; h=message-id:from:to:in-reply-to:content-type :content-transfer-encoding:x-mailer:mime-version:subject:date :references; b=tlCQA3l11WAvOM5RJopzezDipknW2U15Qr5uFWrZ8j6RM+1KyYQUZq/J+J4efKUIWo 0A/j97ztlehMTOLWF6sxAvzBEnJ4OLn8LnatWBxtBIycKYFDXI4ehZXdXSuedpUcSUlB EPqr5JkP2fsXG2FYjx8uIB+n48oXnTIeJas/s= Received: by 10.101.152.38 with SMTP id e38mr7123823ano.117.1260310027291; Tue, 08 Dec 2009 14:07:07 -0800 (PST) X-Original-Return-Path: Received: from ?192.168.168.161? (adsl-65-70-125-225.dsl.okcyok.swbell.net [65.70.125.225]) by mx.google.com with ESMTPS id 6sm3206507yxg.30.2009.12.08.14.07.04 (version=TLSv1/SSLv3 cipher=RC4-MD5); Tue, 08 Dec 2009 14:07:05 -0800 (PST) X-Original-Message-Id: <3ED514E9-37AD-4631-B9F7-5B08CA7C8BEE@gmail.com> From: Ron Laughlin X-Original-To: Lancair Mailing List In-Reply-To: Content-Type: text/plain; charset=us-ascii; format=flowed; delsp=yes Content-Transfer-Encoding: 7bit X-Mailer: iPhone Mail (7D11) Mime-Version: 1.0 (iPhone Mail 7D11) Subject: Re: [LML] Super ES Cabin Heat X-Original-Date: Tue, 8 Dec 2009 16:06:57 -0600 References: Bryan, You might want to check out the system that George Braley designed for the turbo normalized SR22. He used a combination of turbo bleed air and a heat muff on the tail pipe beyond the turbo to provide adequate heat in all phases of flight. His system has the added benefit of virtually eliminating the possibility of CO poisoning. The bleed air is always at a higher relative pressure than the exhaust gasses since the muff is located on the low-pressure side of the turbo. ie, a cracked exhaust pipe will result in bleed-air leaking into the exhaust pipe rather than exhaust gasses leaking into the heating system. Ron On Dec 8, 2009, at 10:16 AM, Burr Bryan wrote: > 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 > > -- > For archives and unsub http://mail.lancaironline.net:81/lists/lml/List.html