X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from [69.171.58.236] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 5.0.9) with HTTP id 1077644 for lml@lancaironline.net; Sun, 23 Apr 2006 12:10:39 -0400 From: "Marvin Kaye" Subject: Re: [LML] Re: CHT's To: lml X-Mailer: CommuniGate Pro WebUser v5.0.9 Date: Sun, 23 Apr 2006 12:10:39 -0400 Message-ID: In-Reply-To: <000001c6669d$f8d40160$0202a8c0@CRAIN> References: <000001c6669d$f8d40160$0202a8c0@CRAIN> X-Priority: 3 MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for "Dominic V Crain" : Walter - I think your argument is accepted by most. Picked up on it about 50 years ago. If you look at the question, it was a philosophical proposal, rather than just scientific. A statement proposing CHT's 385-400 F was mentioned. I know the Lycoming manual states keeping temps below 435 F is desirable for maximum engine life. The point is, however, what narrow temperature range is ideal. Obviously you disagree with the above statement. The drivers of the machinery we operate are heat engines. They are obviously inefficient if run too cold, equally as they are like to break down if run too hot. Therein lies an operational envelope where the heat engine is relatively efficient. According to Lycoming, quoting a temperature below which - etc., there must lie this optimum envelope. Therefore, it becomes a philosophical debate - not scientific. Kind regards Dom