X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from m12.lax.untd.com ([64.136.30.75] verified) by logan.com (CommuniGate Pro SMTP 5.0.3) with SMTP id 866056 for flyrotary@lancaironline.net; Tue, 06 Dec 2005 18:34:04 -0500 Received-SPF: pass receiver=logan.com; client-ip=64.136.30.75; envelope-from=alwick@juno.com Received: from m12.lax.untd.com (localhost [127.0.0.1]) by m12.lax.untd.com with SMTP id AABB3NH65AFMDK82 for (sender ); Tue, 6 Dec 2005 15:32:43 -0800 (PST) Received: (from alwick@juno.com) by m12.lax.untd.com (jqueuemail) id LBKVQCWZ; Tue, 06 Dec 2005 15:31:39 PST To: flyrotary@lancaironline.net Date: Tue, 6 Dec 2005 15:31:08 -0800 Subject: Re: [FlyRotary] fuel system issues Message-ID: <20051206.153116.3888.9.alwick@juno.com> X-Mailer: Juno 5.0.33 MIME-Version: 1.0 Content-Type: text/plain; charset=iso-8859-1 Content-Transfer-Encoding: 8bit X-Juno-Line-Breaks: 0-12,14-17,25-32,34-47,49-55 From: al p wick X-ContentStamp: 17:8:3480138192 X-MAIL-INFO:1597973aabdb9adeda4ab73acab7cbbf7e9fbeb737fbba83ab37be9f37ea375ef70bbb7797073a2a3a13abd3cb7a8ad3dedb6a X-UNTD-OriginStamp: L941HVjjYzDhN3itp//mkGNDRwbErfuOaTI2Flmkspq/uGDd6c+yTA== X-UNTD-Peer-Info: 127.0.0.1|localhost|m12.lax.untd.com|alwick@juno.com On Tue, 6 Dec 2005 16:09:43 -0700 "sboese" writes: As a separate test, I connected a fuel pressure > regulator to the > RX7 donor car’s fuel tank which was filled with fuel and had the > original > submerged fuel pump in it with a clean inlet sock. Running the pump > in this > setup gave the same results: bubbles in the return line, but > nowhere else. So cool that you are doing the real world tests! Keep it up! > I don’t think there is a problem when the fuel is returned to the large wing > tank where it would be unlikely for the bubbles to get into the line > supplying the pump. I certainly agree. It seems reasonable to assume that the return line always deposits bubbles into the tank. I'm told sock is effective at removing them, obviously returning fuel some distance from inlet is valuable. I have 2 gallon header, vented. Unable to get it close to vapor lock. Only exception was brief moment on restart of overheated engine (during my test phase years ago). That was only after 5 minute heat soak. Pretty clear that was due to the 6" of tubing in engine compartment getting too hot. It could be an issue, however, if the fuel is > returned > to a smaller header tank depending on how the header tank is > constructed and > vented. I suspect you want it vented. Unvented opens you to new problems. Like fuel sys that won't self prime. > > If the fuel is recirculated long enough, and if the bubbles are > really air; > the dissolved air should be eventually nearly eliminated from the > system, > but I didn't run the pump long enough to see if this is true. I > haven’t > tried the tests with avgas, either. > > My apologies to the list if this is common knowledge. Don't apologize. This is valuable info that deals with one of the biggest risk items our conversion have. Thanks for providing some science. -al wick Artificial intelligence in cockpit, Cozy IV powered by stock Subaru 2.5 N9032U 200+ hours on engine/airframe from Portland, Oregon Prop construct, Subaru install, Risk assessment, Glass panel design info: http://www.maddyhome.com/canardpages/pages/alwick/index.html