Return-Path: Received: from mail.tsisp.com ([65.23.108.44] verified) by logan.com (CommuniGate Pro SMTP 4.2.5) with ESMTP-TLS id 485612 for flyrotary@lancaironline.net; Mon, 25 Oct 2004 10:31:26 -0400 Received-SPF: none receiver=logan.com; client-ip=65.23.108.44; envelope-from=prvt_pilot@yahoo.com Received: from stevehome by mail.tsisp.com (Technical Support Inc.) with SMTP id CQA74584 for ; Mon, 25 Oct 2004 10:30:54 -0400 Reply-To: From: "Steve Brooks" To: "'Rotary motors in aircraft'" Subject: RE: [FlyRotary] FW: Turbo failure Date: Mon, 25 Oct 2004 10:29:41 -0400 Message-ID: <009001c4ba9f$12c540e0$6400a8c0@workgroup.com> 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 CWS, Build 9.0.6604 (9.0.2911.0) X-MIMEOLE: Produced By Microsoft MimeOLE V6.00.2800.1441 In-Reply-To: Importance: Normal Buly, I'm interested to know what A/r ratio Brian thinks would be adequate for our use. Steve Brooks -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net]On Behalf Of Bulent Aliev Sent: Sunday, October 24, 2004 5:29 AM To: Rotary motors in aircraft Subject: [FlyRotary] FW: Turbo failure "Brian D. Cain" wrote: > > I've been reading this thread off and on and I'd like to give my input on > it. > > Being from the automotive arena, I've got alot of practical, in-car > experience with the > use of the two stock turbochargers (both the earlier 87-88 unit and the > 89-91 unit) and > I must say that they absolutely stink! The turbine housing is too small in > my opinion for > the breathability of the engine, even a stock engine with no modifications > done to it. It > runs far too hot. I also believe it can cause alot of backpressure past the > point of about > 8psi of positive manifold pressure. Some may disagree, but I believe this > turbo isn't > as well suited to the 13B as are some alternatives. > > One of these alternatives is the Borg Warner (Schwitzer) TO4B "replacement" > turbo > that is sold as a generic T4 turbocharger to the public. The part # is > 313102. Although > I believe it comes with a turbine housing that has too large of an A/R > ratio, I believe it > would be very well suited for you guys. It is larger than the stock unit > but not substantially. > Since it is a larger shaft unit w/ larger exhaust housing and compressor > setup, I believe it > will produce the same power you guys desire for take-off and climbing let's > say, at a > lower positive boost pressure, with far less heat. If there's one thing I > have learned about > rotaries in all of my years of working on these and blowing them up, it's > that the exhaust > system needs to be atleast 100% efficient as the intake system is. This > includes the sizing > of the turbocharger's turbine housing specifically in this case. > Comparatively to piston > engine setups, our engines demand the use of a large turbine housing to keep > exhaust > backpressure low as well as velocities high. > > This turbo is cheap (about $450 brand new) although it would probably > require a > slightly smaller A/R ratio turbine housing with the proper exhaust flange > welded on it. > This turbo also has a dry bearing housing (meaning it does not use coolant > lines). Tapped > for 1/4"NPT on the oil feed side. This is a moderately sized turbocharger > but not too > big for the application in my opinion. Definitely worth a try! > > Once I get some pictures of this 313102 TO4B unit taken here, I will post > the link. > > B > __________________ > Brian D. Cain -/- Grand Prairie, TX -/- bdc196@killspam.comcast.net > bdc@killspam.teamfc3s.org > BDC Motorsports - Performance 13B Engines, Haltech EFI tuning, Etc. > MSN bdc196@killspam.hotmail.com, Yahoo! bdc196, AOL Symajhi, ICQ# 1733105 > http://bdc.cyberosity.com -/- http://groups.yahoo.com/group/HaltechSupport-- >> Homepage: http://www.flyrotary.com/ >> Archive: http://lancaironline.net/lists/flyrotary/List.html