X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from fed1rmmtao12.cox.net ([68.230.241.27] verified) by logan.com (CommuniGate Pro SMTP 5.1c.2) with ESMTP id 1315475 for flyrotary@lancaironline.net; Tue, 25 Jul 2006 14:17:18 -0400 Received-SPF: none receiver=logan.com; client-ip=68.230.241.27; envelope-from=steve@stevet.net Received: from [192.168.2.203] (really [68.6.58.190]) by fed1rmmtao12.cox.net (InterMail vM.6.01.06.01 201-2131-130-101-20060113) with ESMTP id <20060725181629.LDCU985.fed1rmmtao12.cox.net@[192.168.2.203]> for ; Tue, 25 Jul 2006 14:16:29 -0400 Mime-Version: 1.0 (Apple Message framework v752.2) In-Reply-To: References: Content-Type: text/plain; charset=US-ASCII; delsp=yes; format=flowed Message-Id: <31B7BDDB-EE47-4CE5-B312-B6494121220C@stevet.net> Content-Transfer-Encoding: 7bit From: Steve Thomas Subject: Re: [FlyRotary] Re: More cooling Tests Date: Tue, 25 Jul 2006 11:16:29 -0700 To: "Rotary motors in aircraft" X-Mailer: Apple Mail (2.752.2) Steve, Do you have any information on how effective the ceramic coating has been? Did you see any noticeable reduction in cowl temps as a result? Best Regards, Steve Thomas ________________________________________________________________________ On Jul 25, 2006, at 4:57 AM, Steve Brooks wrote: > 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/ > > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: http://mail.lancaironline.net/lists/flyrotary/ >