Return-Path: Received: from postoffice.mr.net ([137.192.180.1]) by truman.olsusa.com (Post.Office MTA v3.1.2 release (PO203-101c) ID# 0-44819U2500L250S0) with ESMTP id AAA14797 for ; Sun, 29 Nov 1998 20:32:47 -0500 Received: by postoffice.mr.net (8.8.8/8.8.8) with ESMTP id TAA09090 at Sun, 29 Nov 1998 19:32:54 -0600 (CST) SMTP "HELO" = mr.net But _really_ from upp13-219.nas.mr.net [137.192.68.219] SMTP "MAIL FROM" = msmith1@mr.net SMTP "RCPT TO" = Message-ID: <3661F43F.C350B6B@mr.net> Date: Sun, 29 Nov 1998 19:26:23 -0600 From: Michael D Smith To: "lancair.list@olsusa.com" Subject: Heater X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I am thinking of alternative ways to heat my 4. I can build a muff over the crossover tube, but I was wondering how hot that tube got during various flight regimens. Is it hot only when the turbos are not boosting, i.e., below 28 inches, and as one climbs higher, less exhaust flows throughout the tube, hence chilly buns? I thought about adding an electrical heater. THere is one available from an outfit that basically looks like a 28v hairdryer, 600W max. I could pit two in, I guess, but I'd like to take advantage of the 1600 F EGT instead. I thought about a duct off the oil cooler discharge air, but that does not help my problem on the ground when the engine is cold or the oil cooler door is shut. I just don't like the thought of porting overboard turbo boost when at flight levels, as the current seems to do. Any thought you may have would be appreciated. MDS