Return-Path: Received: from smtpauth08.mail.atl.earthlink.net ([209.86.89.68] verified) by logan.com (CommuniGate Pro SMTP 4.2.5) with ESMTP id 576031 for flyrotary@lancaironline.net; Tue, 21 Dec 2004 19:56:32 -0500 Received-SPF: pass receiver=logan.com; client-ip=209.86.89.68; envelope-from=Dastaten@earthlink.net Received: from [24.238.206.157] (helo=earthlink.net) by smtpauth08.mail.atl.earthlink.net with asmtp (Exim 4.34) id 1CgunL-0001KQ-B2 for flyrotary@lancaironline.net; Tue, 21 Dec 2004 19:56:04 -0500 DomainKey-Signature: a=rsa-sha1; q=dns; c=simple; s=test1; d=earthlink.net; h=Message-ID:Date:From:Reply-To:User-Agent:X-Accept-Language:MIME-Version:To:Subject:References:In-Reply-To:Content-Type:Content-Transfer-Encoding; b=Wvq+Kb3hQag4TLnHoMi6l4ZBJ7fg60l2cW0o6z/eCEukPXI+nMZwmTX7yJjyeyDq; Message-ID: <41C8C559.6060000@earthlink.net> Date: Tue, 21 Dec 2004 18:52:41 -0600 From: David Staten Reply-To: Dastaten@earthlink.net User-Agent: Mozilla/5.0 (Windows; U; Windows NT 5.1; en-US; rv:1.4) Gecko/20030624 Netscape/7.1 (ax) X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: front cover oil fitting thread? References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit X-ELNK-Trace: 9a30bff84e6cb88f95c85d38d22416599ef193a6bfc3dd486397e1b15554a9601bdbfb2a389a0b85666fa475841a1c7a350badd9bab72f9c350badd9bab72f9c X-Originating-IP: 24.238.206.157 I think if you actually look at the oil system schematic, you will discover that the oil return portion is not under "suction" whatsoever but still positively pressurized. I'm not commenting on the diameters of the hoses. I'm simply saying the rationale you give doesnt make sense to me. Dave Marvin Kaye wrote: > "Russell Duffy" <13brv3@bellsouth.net>: > > """ > My current oil system started out as AN12 all the way, but I ended up > having > to use an AN10 fitting at the engine, so the lines change from AN12 > to AN10 > along the way. > ...snip.... > Rusty (I know bigger is better, but AN10 is going to have to do) > """ > > Here's a data point for you, Rusty. On the Eagle we use AN8 for the > oil presssure lines (between engine and oil coolers) and AN10 for the > returns. The pressure side can typically be smaller than the return, > something about flow under pressure vs flow under suction. Ditto for > the coolant lines... 1.25ID for pressure, 1.50ID for suction. I > thought you'd be interested. > > > > >>> Homepage: http://www.flyrotary.com/ >>> Archive: http://lancaironline.net/lists/flyrotary/List.html >> >