Return-Path: Received: from m9.boston.juno.com ([63.211.172.72]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Thu, 25 May 2000 17:58:10 -0400 Received: from cookie.juno.com by cookie.juno.com for <"SmYQyE9D/pZl7kicjCElWwrRLf97zpAizJ1WYwIE9d9TyOGTl9Qgog=="> Received: (from rlperry@juno.com) by m9.boston.juno.com (queuemail) id E8XTEBRK; Thu, 25 May 2000 18:03:29 EDT To: lancair.list@olsusa.com Cc: DARUS47959@aol.com Date: Thu, 25 May 2000 17:02:48 -0500 Subject: Zehrbach ceramic engine parts Message-ID: <20000525.170249.-437139.0.rlperry@juno.com> From: Richard L Perry X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> To the Lancair List: Several months ago I wrote to the list that I was extremely pleased with ny Lyc.IO-360 engine that I had Darus Zehrbach treat with all of his ceramic coatings. You may recall last year about this time My Glasair 1 retract and I landed with the wheels up. The aircraft had about 1200hrs. and since it had to be torn down anyway, I decided to have it Majored. I knew about the ceramic coatings since I had planned on one of LPE-Zehrbach V8's for my Lancair 4P. I had my overhauler, Poplar Grove Airamotive (Belvidere IL.) send the Cylinders along with the bearings, Pistons, valves etc. to Zehrbach for the ceramic and dry Lub coatings. Last fall at my first writing , I had only 5 or 6 hrs. on the new overhaul. I now have enough time on the engine to report the performance has even gotten better as the engine has broken in. I want to tell about my trip from Chicago to Sun & fun. I have never had a ground speed this high, 272kts. at 17,500 ft. Granted I had a hell of a tail wind (40 to 45kts.). I thought no one would be leave me so I took a picture of the instrument panel. (see this at www.staraviation.com) The ceramic coatings on top of the piston and in the combustion chamber tend to keep a good deal of heat from being absorbed by the engine, now it doesn't take as many BTU's to produce the same horse power. This is the reason for almost 18-20 % fuel savings. I always fly at 25 x 25 (the engine is turbo normalized). Now with less heat to deal with, some cooling drag is eliminated. I have blocked the bottom third of the oil cooler off and replaced two 4 x 6'' lovers on the bottom of the cowl with 4 x 6" al. panels. I have several pages of recorded data that I would be happy to E-mail to any one interested. Note: from this set of numbers that all my temps are lower, fuel flow is just over 10gph compared with 12gph before the overhaul. Date Alt Oat MP RPM oil tp FF IAS TAS Turbo CHT 3/11 5.5 -6 25 2500 180 10.2 185k 190k no 390F " 10.5 -8 25 2500 187 10.4 176k 202k yes 400F " 15.5 -10 25 2500 187 10.5 170k 209k yes 405F " 17.5 -13 25 2500 190 10.5 168k 215k yes 409F My engine is equipped with 4 prob EGT and 4 probe Cyl. temp. Mixtures were leaned to 50 degrees rich of peak. I am writing this as a friend of Zehrbach, and I am not receiving any compensation. Dick Perry rlperry@juno.com >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>