X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from alnrmhc13.comcast.net ([204.127.225.93] verified) by logan.com (CommuniGate Pro SMTP 5.1.2) with ESMTP id 1605421 for flyrotary@lancaironline.net; Sun, 26 Nov 2006 18:59:35 -0500 Received-SPF: none receiver=logan.com; client-ip=204.127.225.93; envelope-from=rlwhite@comcast.net Received: from quail.site (c-68-35-160-229.hsd1.nm.comcast.net[68.35.160.229]) by comcast.net (alnrmhc13) with SMTP id <20061126235905b1300t9464e>; Sun, 26 Nov 2006 23:59:15 +0000 Date: Sun, 26 Nov 2006 16:59:54 -0700 From: Bob White To: "Rotary motors in aircraft" Subject: Re: [FlyRotary] N11XD - Post 1st flight inspection and second flight Message-Id: <20061126165954.c44a7001.rlwhite@comcast.net> In-Reply-To: References: X-Mailer: Sylpheed version 2.2.10 (GTK+ 2.8.10; i686-pc-linux-gnu) Mime-Version: 1.0 Content-Type: text/plain; charset=US-ASCII Content-Transfer-Encoding: 7bit Great work Jim. Glad to hear you're getting some air time. I have to echo Buly and Ed though. Get some stainless around that exhaust. I think I used 0.020 to make a plate between the exhaust and intake. I then covered that with some high temp insulation sheets I found at the speed shop. Bob W. On Sun, 26 Nov 2006 14:32:21 -0800 (PST) James Maher wrote: > Yesterday I finally got around to the post 1st flight inspection on my Delta. > Checked all the controls, skins, airframe stuff and then removed the top cowl. > Everything looked great until I got to the muffler. > The muffler was fine but the heat shield between it and the intake manifold was MELTED! > About a 4" x 4" hole directly above the center of the muffler with gobs of aluminum slag in the bottom of the cowl. > I believe that the heat shield got hot enough to droop and then contacted the muffler surface and was history after that. > It's a good thing that the plenum (also aluminum) did not melt and get sucked into the intake. > That would have ruined my day. > I fabricated another piece of alum and wrapped it up around the plenum this time to prevent it from contacting the muffler. > This is a temporary solution at best. > I have an idea for a more permanent one but did not have the material on hand at the time. > With temporary fix completed I proceeded to fly the second test flight. > The OAT was 60F, 10F degrees higher than the first flight and the engine acted accordingly. > The coolant was up to 212F and stable by the end of the runup. > Luckily the oil was only about 170F so I proceeded to takeoff. > Climbing out at 110-120MPH the coolant temp was 212F with the oil coming up. > After level off at 3000 feet the coolant eventually came back down to a more comfortable 190F with the oil about the same. > My eyes were almost glued to the EGT though, because I was concerned about another meltdown. The highest EGT that I noticed was about 1580F. > I kept the mixture a little richer than last time hoping to keep the temps down. > After circling the airport for over a half hour I decided I better land, as the I was loosing the sun again. > I turned base and final too short, so I was high and fast (flying the pattern at 120MPH takes a little getting used to), > But I did have 9000 feet of runway below me so I managed to get it down but not in the first 3000 feet like last time. > It was more like the second 3000 feet. > Any other airport it would have called for a go around. > But it wasn't a bad landing and I didn't break anything. > Didn't have time or light to look under the cowl after this flight as it was already well after 4:00PM ( I hate standard time). > Can't wait to get the airplane back to it's home airport. > An hour and a half is just too far to drive. > Jim Maher > Dyke Delta N11XD 13b (2.1 hours flown) > > -- N93BD - Rotary Powered BD-4 - http://www.bob-white.com First Flight: 11/23/2006 7:50AM - 0.4 Hours Total Time Cables for your rotary installation - http://www.roblinphoto.com/shop/