Return-Path: Received: from mail.tsisp.com ([65.23.108.44] verified) by logan.com (CommuniGate Pro SMTP 4.2b3) with ESMTP-TLS id 96074 for flyrotary@lancaironline.net; Sat, 29 May 2004 13:06:57 -0400 Received: from localhost by mail.tsisp.com (Technical Support Inc.) with SMTP id CQA74584 for ; Sat, 29 May 2004 13:06:26 -0400 Date: Sat, 29 May 2004 13:06:26 -0400 From: Steve Brooks To: Rotary motors in aircraft Subject: Re: [FlyRotary] Engine comparison Message-ID: X-Mailer: IceWarp Web Mail 5.2.7 X-Originating-IP: 24.136.229.128 MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit Den, Yes, mine has the lower compression rotors. Steve Brooks -----Original message----- From: "Dean Head" banana@atlantic.net Date: Sat, 29 May 2004 12:40:11 -0400 To: "Rotary motors in aircraft" flyrotary@lancaironline.net Subject: [FlyRotary] Engine comparison > Guys(John,Steve,Todd,Dave), > > It will be great to see how the different setups compare as more hours are > accumulated. Discussions on how much boost got me thinking. Steve, I believe > you told me you had a stock turbo engine so I would guess 8.5 rotors. John, > yours are 9 something if I remember. Dave/Todd I don't recall seeing in the > posts your compression ratios? This will be some great data! > > John, > > This is probably a dumb question but, did you wipe down the pipes to get any > oil off before putting the hose and clamp on? Just a thought on what could > be different in the setups. Was it the same joint that blew each time? > > Dean Head > > BKV FL > > > >