X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from dewhirst.ca ([64.26.156.111] verified) by logan.com (CommuniGate Pro SMTP 4.3.4) with ESMTP id 1001962 for flyrotary@lancaironline.net; Tue, 14 Jun 2005 16:00:17 -0400 Received-SPF: none receiver=logan.com; client-ip=64.26.156.111; envelope-from=idewhirst@dewhirst.ca Received: from spatoday.com (www.dewhirst.ca [192.168.1.10]) (authenticated using Trusted-IP) by dewhirst.ca (ISMail v1.8.0) with SMTP; Tue, 14 Jun 2005 16:06:58 -0400 Received: from 205.194.127.36 (proxying for unknown) (SquirrelMail authenticated user idewhirst) by www.dewhirst.ca with HTTP; Tue, 14 Jun 2005 16:06:58 -0400 (Eastern Daylight Time) Message-ID: <26715.205.194.127.36.1118779618.squirrel@www.dewhirst.ca> Date: Tue, 14 Jun 2005 16:06:58 -0400 (Eastern Daylight Time) Subject: Re: Failure to compute From: "Ian Dewhirst" To: flyrotary@lancaironline.net Reply-To: idewhirst@dewhirst.ca User-Agent: SquirrelMail/1.4.2 MIME-Version: 1.0 Content-Type: text/plain;charset=iso-8859-1 Content-Transfer-Encoding: 8bit X-Priority: 3 Importance: Normal Tracy wrote "It could be argued that the exhaust energy was free anyway so it doesn’t matter. I don't have enough real world data to back it up but I don't think this is true." Back pressure rises with turbine load so you are quite right Tracy, the energy is not free. One of the problems that I see with venting the compressor output is that it won't work. Compressor maps assume that you have more then enough power to drive the compressor. If your compressor is stalling at WOT you don't. Dave, I understand your concern - you do not want to run the turbo at 150,000 rpm. You solved that problem by putting a P trim wheel that was designed to require a lot more exhaust gas and a bigger hot side housing to generate shaft power. You also improved the waste gate. If you put a smaller compressor up front again (not too much smaller but smaller) it will work as desired and run at a reduced RPM. Now if you want to try the hole in the manifold workaround, this “might” work, I think that it has a better chance then venting to the atmosphere. Vent part of the compressor output back into the compressor inlet. This will force the turbo to operate at a higher rpm where it is likely a bit more efficient. Start with a 1/2” bypass and work up, remeber that a no load compressor has the potential for very high rpm. A different compressor would still be a much better solution. Porting the engine and building a better intake manifold could potentially be enough to get the job done, here is a another way to do it: In the mid 90’s I visited a fiend of mine who was the project manager on a project yacht called Global One, it was being built to challenge the QE2 transatlantic record. This yacht that had 2 16V92 Detroit Diesel engines -1800HP each. Each engine had 4 turbochargers that fed into a BIG supercharger which blew through a HUGE air / water intercooler. The supercharger was needed to help the engine create sufficient exhaust energy for the turbochargers, once the turbochargers were online and pressurizing the intake the the supercharger was largely bypassed, the engines where able to make more power, more boost, more rpm, the boat (90' Aluminum) came up on plane and off you went with a 300' rooster tail trailing along behind you. Good Luck -- Ian (The partial pressure experiment worked exactly as you said it would and I hate to see you flogging this horse…)