X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from smtp101.plus.mail.re2.yahoo.com ([206.190.53.26] verified) by logan.com (CommuniGate Pro SMTP 5.1c.2) with SMTP id 1315003 for flyrotary@lancaironline.net; Tue, 25 Jul 2006 07:58:21 -0400 Received-SPF: none receiver=logan.com; client-ip=206.190.53.26; envelope-from=prvt_pilot@yahoo.com Received: (qmail 24853 invoked from network); 25 Jul 2006 11:57:36 -0000 DomainKey-Signature: a=rsa-sha1; q=dns; c=nofws; s=s1024; d=yahoo.com; h=Received:From:To:Subject:Date:Message-ID:MIME-Version:Content-Type:Content-Transfer-Encoding:X-Priority:X-MSMail-Priority:X-Mailer:X-MimeOLE:Importance:In-Reply-To; b=lHFRvK1FYYAmHcvlgMBGcuO0NHgfRzHhiMaWtWxQLRkv6itINn1C47PsWF1sTyzsWnKBSOKI8UPehgBR5KdkQHfI/JoMaWJD2ThYD2pDva+r2KhiWSe4noAWAuTAHDZqndooH26On0lPKg2pW02engLxVLKd5fJFnsT9WMm3oQs= ; Received: from unknown (HELO stevehome) (prvt?pilot@71.55.75.37 with login) by smtp101.plus.mail.re2.yahoo.com with SMTP; 25 Jul 2006 11:57:35 -0000 From: "Steve Brooks" To: "Rotary motors in aircraft" Subject: RE: [FlyRotary] Re: More cooling Tests Date: Tue, 25 Jul 2006 07:57:44 -0400 Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook IMO, Build 9.0.2416 (9.0.2910.0) X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1807 Importance: Normal In-Reply-To: Bob, For your exhaust, you may want to consider ceramic coating. I had my exhaust pipe coated by a company called Jet-Hot. As I recall it only cost about $50 to do mine, but it's only about 18" long, coming from the turbo. Here is their web link: http://www.jet-hot.com/ What I got was the Jet-Hot 2000 coating, which is good to 2000 degrees. Mine has held up very well, and shows no signs of deterioration. Steve Brooks -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net]On Behalf Of Bob White Sent: Tuesday, July 25, 2006 1:30 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: More cooling Tests Thanks Dave, The fuel return to the tank is the next item on my todo list. The tank developed a leak so I have to open it up anyway. It seemed like the right time to fix it. The exhaust system is a large can with a tube thru the middle that supplies cooling air (theoretically) so the temps on the down tube should be lower than normal for a rotary. However, it's still too hot for this material, whatever it is. I hope I haven't given the impression that I'm flying yet. This is all taxi and static stuff. :( I am getting pretty close though. I hope you are doing well. I check your blog occasionally and I'm glad I don't have to deal with the temps shown in your July 13 photo. I could probably get close in Phoenix some days. Best of luck and hope the rest of your tour passes quickly. Bob W. On Tue, 25 Jul 2006 07:43:51 +0400 "David Leonard" wrote: > Hi Bob, > > I can tell from experience that even most stuff that is intended to go > directly onto exhausts will quickly desintigrate in the rotary. The stuff > that is supposed to be good up to 1400 deg will start falling apart after a > few hours. That stuff you have will be done after the first flight. > Don't forget that your exhaust temps will go above 1600! > > I did find some exhaust wrap that was good up to 2000 deg. and it is good > for about 100 hrs before becoming a little brittle and falling off. It was > worth it and made a big difference in my under cowl temps, but it was not > cheap. > > As for your fuel system.... I am sure SOMEONE has said this before (I have > not been reading the list very regularly because I am in Iraq), so let me > repeat for effect. RETURN THAT FUEL ALL THE WAY TO THE TANK! One of the > great things about this high flow fuel injection system is that it is > possible to essentially eliminate ANY chance of vapor lock. Vapor lock > HAPPENS even in certified planes. It is serious. It can be fatal. Route > that fuel back to the tank and it basically can't happen.... you have a > better system than a typicl lyc set-up. Route that fuel back to the pump > and you may even be making things worse than a lyc set up. > > Sounds like you have decided to make a change, so this is just to re-enforce > that decision and send the message to anyone else considering the easy way > out for fuel return.... > > JMHO, & congratas on getting flying by the way! cant wait to see it in > person some day.. > > Dave Leonard > > > On 7/25/06, Bob White wrote: > > > > I finished putting a layer of insulation around the exhaust system. I > > placed thermocouples in a few key locations. One inside the > > insulation, one outside, and one on the fuel rail. OAT was 80-85F. > > > > I ran the engine at 2200 rpm until the temps stabilized at 197 oil and > > water. I increased rpm's to 3100 and temps went up to 200 oil and 207 > > water. They were still increasing very slowly. I can taxi at 3100 rpm > > or less and getting a little movement should help cooling. Also, when > > I reduced power back to 2200 rpm, the temps started decreasing. So on a > > not too hot day I think the cooling will be OK for taxiing. > > > > The insulation is a layer of reflective insulation I bough at the speed > > shop that is good to 1000F. It has a metalized layer on each side and > > some kind of fibrous layer on the inside. (The stuff itches like > > fiberglass when you get it on you.) At the end of the test, the > > thermocouple on the inside layer was reading 235F and the one in the > > same place on the outside of the insulation was 167F. > > > > I still don't have the fuel return to the tank. It's going directly > > back to the fuel pump input. So the fuel rail temps were getting > > pretty high. The fuel rail was 145F and the engine was starting to run > > a little rough, presumably due to incipient vapor lock. > > > > Next step is to open the tank and install the fuel return line. I ran > > the line from the firewall to the wing root this afternoon, so the easy > > part is done. > > > > Bob W. > > > > -- > > http://www.bob-white.com > > N93BD - Rotary Powered BD-4 (first engine start 1/7/06) > > Custom Cables for your rotary installation - > > http://www.roblinphoto.com/shop/ > > > > -- > > Homepage: http://www.flyrotary.com/ > > Archive and UnSub: http://mail.lancaironline.net/lists/flyrotary/ > > > > > -- http://www.bob-white.com N93BD - Rotary Powered BD-4 (first engine start 1/7/06) Custom Cables for your rotary installation - http://www.roblinphoto.com/shop/ -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net/lists/flyrotary/