Return-Path: Sender: (Marvin Kaye) To: flyrotary Date: Sun, 06 Oct 2002 21:34:04 -0400 Message-ID: X-Original-Return-Path: <13brv3@mchsi.com> Received: from sccmmhc02.mchsi.com ([204.127.203.184] verified) by logan.com (CommuniGate Pro SMTP 4.0b8) with ESMTP id 1798829 for flyrotary@lancaironline.net; Sun, 06 Oct 2002 10:45:07 -0400 Received: from rad ([12.218.64.232]) by sccmmhc02.mchsi.com (InterMail vM.4.01.03.27 201-229-121-127-20010626) with SMTP id <20021006144422.YDHM7903.sccmmhc02.mchsi.com@rad> for ; Sun, 6 Oct 2002 14:44:22 +0000 Reply-To: <13brv3@mchsi.com> From: <13brv3@mchsi.com> X-Original-To: "Rotary motors in aircraft" Subject: RE: [FlyRotary] Re: turbo sizing common sense..... X-Original-Date: Sun, 6 Oct 2002 09:44:21 -0500 X-Original-Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook IMO, Build 9.0.2416 (9.0.2910.0) Importance: Normal X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 In-Reply-To: Posted for "Barry Gardner" : The spreadsheet was intended to assist with turbo selection, so its main focus is on calculating pressure ratios at higher altitude. User variables are highlighted in green. ------------------------- I didn't get a spreadsheet with the message. If it won't make it through the list, can you email me a copy directly. I'd like to see it. ------------------------- Whether seven pounds of boost can normalize pressure up to some critical altitude is a matter of defining "normalize." ------------------------- Just to be picky, there really is only one definition for "normalize", which is to maintain sea level pressure at altitude. I wholeheartedly agree that the stock turbo will be inadequate for producing significant boost at altitude, but don't underestimate what you gain with a stock turbo. Say you have a 150 hp NA engine at sea level, then you add 7 psi of boost. Now you have (just making these numbers up) 200 hp. That's quite a payoff for about $400 in low mileage used parts that bolt right on. Now go to the VFR ceiling (with O2) and you still have about 150 hp. Now go to a cruise alt of say 10,000 ft, and you'll still have about 2.5 psi of boost over sea level, so maybe 165 hp. Compare these numbers to an IO-360, and you'll see that you're coming out ahead. Just food for thought. -------------------------- Additionally, if you've read any of the chatter on the RX7 auto listserves, the internal wastegate design gets easily overloaded at higher boosts, -------------------------- Boost creep does seem to be a problem, specifically with the series 4 turbo because it has a small wastegate. The S5 is much larger, but it probably isn't large enough to keep boost at 0 when it's open. The big question is- how much boost will the engine make with the wastegate wide open. I've asked the question here, and on the RX-7club forum, but no one seems to have an answer, so I guess it will be a ground run test. These wastegates can be ported, to reduce the problem, and I may just do that up front. Of course, I don't mind making a few psi of boost with the wastegate open, I just don't want to make 10 :-) --------------------- So I've resolved to bite the bullet on the added pounds and exhaust complexity of a wastegate and get a bigger turbo with a known capacity. --------------------- A reasonable approach to be sure. How long till you're going to be running, and what are you building? Cheers, Rusty Turbo 13B powered RV-3... Be Afraid :-) 1993 RX-7 R1... Stock (for now)