Return-Path: Received: from out010.verizon.net ([206.46.170.133] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 2775893 for flyrotary@lancaironline.net; Fri, 28 Nov 2003 09:02:37 -0500 Received: from netzero.net ([4.7.48.166]) by out010.verizon.net (InterMail vM.5.01.06.06 201-253-122-130-106-20030910) with ESMTP id <20031128140236.ENIL18505.out010.verizon.net@netzero.net> for ; Fri, 28 Nov 2003 08:02:36 -0600 Message-ID: <3FC75576.6070101@netzero.net> Date: Fri, 28 Nov 2003 09:02:30 -0500 From: Finn Lassen User-Agent: Mozilla/5.0 (Windows; U; Windows NT 5.1; en-US; rv:1.4) Gecko/20030624 Netscape/7.1 (ax; PROMO) X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: exhaust References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit X-Authentication-Info: Submitted using SMTP AUTH at out010.verizon.net from [4.7.48.166] at Fri, 28 Nov 2003 08:02:36 -0600 You don't need a cone. If you use thin (0.035) SS tubing, 1 3/4" will fit right into the port opening. You can use a mallet to pound the tubing into the exhaust opening, or squeeze the end in a vice to get the oval shape. In other words, the end of the header will protrude maybe 1/2" past the flange into the exhaust port. This will give you the smooth transition you'll want. Finn Ed Anderson wrote: >Hi John, > > My recommendation would be to use the "cone" for a smoother transistion >from the size of the exhaust ports to your 1 3/4" dia exhaust ports. Will >it work without the transition - most certainly will, but such >discontinunities in the gas flow route will imped the flow of exhaust out >the pipe to a degree. There are places such as "Burns Stainless >http://www.burnsstainless.com/ who sell just about anything you need. >Don't know if they have cones going down to 1 3/4" but you might give them a >try. > >You would not need to have 2" pipes just a 2" to 1 3/4" cone to your 1 3/4" >tubing should do it. I used schedule 40 stainless steel pipe (0.115" wall >thickness) for my 2" headers and have over 300 hours on them and they are >still in good shape. However, they are a bit on the heavy side. > >Don't know which block you are using, the turbo or NA 13B, however, be >advised the turbo block lacks the "exhaust splitters" that considerably >reduce the energy of the exhaust pulse. I can tell you from personal >experience the exhaust pulse from the turbo block without the exhaust >splitters is very powerful and has shredded stainless steel tubing that I >had squished down at the ends (see photos). This was after 15 minutes of >flight. > > >Ed > > >Ed Anderson >RV-6A N494BW Rotary Powered >Matthews, NC >eanderson@carolina.rr.com >----- Original Message ----- >From: "john" >To: "Rotary motors in aircraft" >Sent: Thursday, November 27, 2003 9:42 PM >Subject: [FlyRotary] exhaust > > > > >>I need to order the ss for the exhaust. Tracys' manual calls for 1-3/4" >>size, is this connected to the flange by a cone shape or have you used a >>hole smaller than the exhaust ports in the engine. Awhile back someone >>posted a picture of some enserts for the pipes, has anyone found some that >>havn't burned out shortly. Would the exhaust pipes need to be 2" at the >>outlet so inserts could be installed. The 13B is installed in a Tailwind >>W-10 w/ tri-gear and I don't have any room for a muffler under the cowl. >>Thanks for any and all input. JohnD in Michigan >> >> >> >> >>>> Homepage: http://www.flyrotary.com/ >>>> Archive: http://lancaironline.net/lists/flyrotary/List.html >>>> >>>>