X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from mail-ig0-f174.google.com ([209.85.213.174] verified) by logan.com (CommuniGate Pro SMTP 6.0.9e) with ESMTPS id 6824394 for flyrotary@lancaironline.net; Fri, 11 Apr 2014 18:14:43 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.85.213.174; envelope-from=msteitle@gmail.com Received: by mail-ig0-f174.google.com with SMTP id h18so1371724igc.1 for ; Fri, 11 Apr 2014 15:14:10 -0700 (PDT) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=20120113; h=subject:references:from:content-type:in-reply-to:message-id:date:to :content-transfer-encoding:mime-version; bh=4qLyhZ3P/vRkhqk1AuGdFpArVNJ4lyvH0uYBnBZh9H0=; b=V2MJpkvRnmA0WWpYoaju5GoYdcizaawOGC/ICfuc/QU5Qw1HKw8W0soV/lQhTPLDr1 iTTOF7/HZzxNSLUuRbiJLl5b/+tFwvgcuF5zlW/MGoFKwnXM+vCMiLUTS19HLyLURRvu gXLg1De0wjqG4lMxerdTLUugdHZdL55zTB1KyPrebPbNRKZc+IIzkHJxdqUx4W/ts8PT DNvQGAj6Bx04QUfMYTpBq0YbJr/UE6twobU0VhFQ4Lu0vyzHlyHyOuW79iaDBPT1z3Fy cBa+Nxg7UxJvf/C5/KHsvP1MMcAwhochtBVwUVMsLTfXTAfWDudPzZelLIbs4aExPRDl YOqw== X-Received: by 10.50.25.7 with SMTP id y7mr193830igf.17.1397254450441; Fri, 11 Apr 2014 15:14:10 -0700 (PDT) Return-Path: Received: from [192.168.1.102] (104-7-220-110.lightspeed.austtx.sbcglobal.net. [104.7.220.110]) by mx.google.com with ESMTPSA id r4sm8770816igh.1.2014.04.11.15.14.09 for (version=TLSv1 cipher=ECDHE-RSA-RC4-SHA bits=128/128); Fri, 11 Apr 2014 15:14:09 -0700 (PDT) Subject: Re: [FlyRotary] Switcheroo from turbo to not References: From: Mark Steitle Content-Type: multipart/alternative; boundary=Apple-Mail-C68E5B1E-3B4A-404A-945C-BA72313BEC11 X-Mailer: iPad Mail (11D167) In-Reply-To: Message-Id: Date: Fri, 11 Apr 2014 17:14:09 -0500 To: Rotary motors in aircraft Content-Transfer-Encoding: 7bit Mime-Version: 1.0 (1.0) --Apple-Mail-C68E5B1E-3B4A-404A-945C-BA72313BEC11 Content-Type: text/plain; charset=us-ascii Content-Transfer-Encoding: quoted-printable Sounds like a prudent plan to me. Sent from my iPad > On Apr 11, 2014, at 4:51 PM, shipchief@aol.com wrote: >=20 > I went out to the Hangar last Tuesday to start installing the intercooler.= Well, at least to fit a few tubes and hoses, then hold up some parts and ma= ke plans. > As I took the air discharge tube off the compressor, I noticed the whole t= urbo compressor & bearing assembly wiggling around on the turbine housing! > I checked all the mounting bolts and clips, everything was tight. > So I took the turbo off the engine, and realized that I probably cooked th= e turbine housing. I did see EGT excursions to 1800F. What's worse, I had a n= ew turbo blanket. I think a heat shield would have been better, so some cool= ing air could pass over the housing, but still block radiant heat. > Bummer. > So I decided to go with Plan B: I ordered the bits and tube bends to switc= h to naturally aspirated operation. I'm keeping the exhaust header that the t= urbo sat upon, and replacing everything else past the bottom of the firewall= , to the new pipe & muffler I recently added. > I'm retaining the ability to 'Go Turbo' later, but I've become curious abo= ut what the turbo must boost to equal full throttle of 'Naturally Aspirated'= . > I did build and have been running a tuned intake manifold. The exhaust won= 't be a tuned header, but it is pretty good, possibly better than the stock e= xhaust reactor and a whole lot lighter. It has port discharge nozzles (rever= sion cones) EGT probes and a gentle sweeping shape. Plus it's proven strong w= hile carrying the weight of the turbo beyond 1800F, and it passed inspection= . I trust it. > So I hope to run it, find the performance satisfactory, the fuel consumpti= on significantly reduced, and use 87 octane ethanol free mogas instead of 92= . (low compression rotors) > Also, I can advance the timing to the NA spec. =20 > Anyone see a problem or have advise? --Apple-Mail-C68E5B1E-3B4A-404A-945C-BA72313BEC11 Content-Type: text/html; charset=utf-8 Content-Transfer-Encoding: 7bit
Sounds like a prudent plan to me.

Sent from my iPad

On Apr 11, 2014, at 4:51 PM, shipchief@aol.com wrote:

I went out to the Hangar last Tuesday to start installing the intercooler. Well, at least to fit a few tubes and hoses, then hold up some parts and make plans.
As I took the air discharge tube off the compressor, I noticed the whole turbo compressor & bearing assembly wiggling around on the turbine housing!
I checked all the mounting bolts and clips, everything was tight.
So I took the turbo off the engine, and realized that I probably cooked the turbine housing. I did see EGT excursions to 1800F. What's worse, I had a new turbo blanket. I think a heat shield would have been better, so some cooling air could pass over the housing, but still block radiant heat.
Bummer.
So I decided to go with Plan B: I ordered the bits and tube bends to switch to naturally aspirated operation. I'm keeping the exhaust header that the turbo sat upon, and replacing everything else past the bottom of the firewall, to the new pipe & muffler I recently added.
I'm retaining the ability to 'Go Turbo' later, but I've become curious about what the turbo must boost to equal full throttle of 'Naturally Aspirated'.
I did build and have been running a tuned intake manifold. The exhaust won't be a tuned header, but it is pretty good, possibly better than the stock exhaust reactor and a whole lot lighter. It has port discharge nozzles (reversion cones) EGT probes and a gentle sweeping shape. Plus it's proven strong while carrying the weight of the turbo beyond 1800F, and it passed inspection. I trust it.
So I hope to run it, find the performance satisfactory, the fuel consumption significantly reduced, and use 87 octane ethanol free mogas instead of 92. (low compression rotors)
Also, I can advance the timing to the NA spec.  
Anyone see a problem or have advise?
--Apple-Mail-C68E5B1E-3B4A-404A-945C-BA72313BEC11--