Return-Path: Received: from mail.akos.net ([209.194.60.5]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Mon, 26 Apr 1999 23:17:55 -0400 Received: from home.akos.net (root@home.akos.net [209.194.60.20]) by mail.akos.net (8.8.7/8.8.7) with ESMTP id XAA03970 for ; Mon, 26 Apr 1999 23:18:17 -0400 Received: from akos.net (ppp08.npr2.akos.net [209.194.57.73]) by home.akos.net (8.8.7/8.8.7) with ESMTP id XAA28008 for ; Mon, 26 Apr 1999 23:16:58 -0400 Message-ID: <37252C79.1029A068@akos.net> Date: Mon, 26 Apr 1999 23:18:20 -0400 From: Tom Giddings To: Lancair Mail List Subject: Cowl Flaps/Cooling X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Hi All: It has been some time since I have been compelled to respond on any subjects here.It has all been covered so well I have not felt the need for my minimal knowledge to be brought to the firing line:) Having said that I would tell that I have had some LUCK getting to my goal of cranking my 360 at full max continuous power on a hot Florida afternoon climb to altitude WITHOUT OVERHEATING(yippie)How did I do this?you ask.WELL sit down and let me continue. 1.I built a sealed plenum to insure as perfect of a seal for inlet air as possible. 2.I built inlet ramps that sealed to the plenum (approx. 10 degree angle)this allows the air to come in and slow down to do its job of cooling 3.I built a dedicated plenum for the oil cooler which uses a 5 inch NACA duct to get pressure air into the sealed plenum then direct over the oil cooler and directly out the side of cowl via a louvered vent.( it trips the air and creates a low pressure area which helps move the heated air away from the oil cooler) 4.I increased the intake inlets to 4 inch. 5.I Installed the 3.5 inch longer motor mount and the larger lower cowl splash supplied by Lancair as well as the longer cowl itself(more room behind the engine and accessories case) 6.I built a shield in front of the #1 cyl to trip the inlet air to the back of the the pressure chamber. The results are as follows; 1.Full power climb to altitude max cyl temp370(no step climbing) 2.Cruise cyl temps 75% power 322(all cyl head temps are equal) 3.8 knot increase in indicated air speed(HONEST) 4.Oil temps 180 I am not a rocket scientist.All of these things I did I learned from talking with other builders and the Factory folks(Don Goetz ect.)This list has been invaluable to me also.Thanks Marv. In conclusion(I see you yawning)I went from an airplane that climbed at 500 degrees and cruised at 435 to what I have now.An airplane that is safe and a true joy to fly. If anyone would like any particulars and whys and how's feel free to contact me Regards Tom Giddings 360TG >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html