Return-Path: Received: from relay04.roc.ny.frontiernet.net ([66.133.131.37] verified) by logan.com (CommuniGate Pro SMTP 4.2.5) with ESMTP id 541279 for flyrotary@lancaironline.net; Sun, 21 Nov 2004 22:02:30 -0500 Received-SPF: pass receiver=logan.com; client-ip=66.133.131.37; envelope-from=canarder@frontiernet.net Received: from filter02.roc.ny.frontiernet.net (filter02.roc.ny.frontiernet.net [66.133.131.177]) by relay04.roc.ny.frontiernet.net (Postfix) with ESMTP id 32DA0FED5 for ; Mon, 22 Nov 2004 03:02:00 +0000 (UTC) Received: from relay04.roc.ny.frontiernet.net ([66.133.131.37]) by filter02.roc.ny.frontiernet.net (filter02.roc.ny.frontiernet.net [66.133.131.177]) (amavisd-new, port 10024) with LMTP id 19999-31-79 for ; Mon, 22 Nov 2004 03:02:00 +0000 (UTC) Received: from JIM2004 (67-137-74-47.dsl2.cok.tn.frontiernet.net [67.137.74.47]) by relay04.roc.ny.frontiernet.net (Postfix) with ESMTP id 9932DFEC0 for ; Mon, 22 Nov 2004 03:01:59 +0000 (UTC) Message-ID: <41A1571B.8060403@frontiernet.net> Date: Sun, 21 Nov 2004 21:03:55 -0600 From: Jim Sower User-Agent: Mozilla/5.0 (Windows; U; Windows NT 5.1; en-US; rv:1.7) Gecko/20040514 X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Bubbles in fuel line from pump References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit X-Antivirus: avast! (VPS 0445-2, 11/04/2004), Outbound message X-Antivirus-Status: Clean X-Virus-Scanned: by amavisd-new-20040701 (2.0) at filter02.roc.ny.frontiernet.net Transparent lines on ALL "suction" lines (upstream of firewall) would be edifying. Watch the bubbles as they appear and if/when they increase. Might try a pump just downstream of the selector valve after you've studied the bubbles as outlined above. Finn Lassen wrote: > I'm near wit's end trying to find out why I get bubbles in the line > from my facet pump to my carburators. > > To recap my setup: > Fuselage fuel tank -> fuel selector valve -> fluel flow sensor -> G3 > automotive paper filter -> to drain point -> T-split to each fuel > pump. Separate lines from each fuel pump to carbs. Three carbs. The > two outer carbs (sharing one pump) each feed a secondary port. The > center carb, with its own pump, feeds the two primary ports. One > throttle to the outer carbs, one throttle to the center carb. When > have climbed above pattern altitude I turn off the pump to the center > carb, ready to reduce center carb throttle when all fuel has been > burned out of the bowl, and use center carb throttle to lean mixture. > Output from pumps near fuselage bottom slopes up to carbs which are > appox level with center of fuselage tank. > > Bottom of fuselage tank about 16 inches above the facet fuel pumps. > When removing the quick-drain valve, the system gravity feeds about > 17-19 GPH through the selector valve, flow sensor and filter. > > Various observations: > Idle fuel pressure on ground about 3.8 - 4 psi. > Max power fuel flow near sea level at full power only about 13.5 GPH. > 10 GPH at altitude. > Fuel pressure to outer carbs is roughly inversely proportional with > observed amount of gasses (air?) in the line from the pump to the > outer carbs. > Engine wants to quit when pressure drops to about .1 or .2 psi. (Only > happened one time after a continous full power climb to 10,000' to get > over clouds. Pressure dropped steadily to that point.) > Removed flow sensor and filter and amount of bubbles appeared to be > significantly less. > Put sensor back in, and bubbles reappeared, inconsistently. > Have mostly observed fuel pressure drop at high power climb attitude. > Seems to get worse at higher altitudes. > Have checked tank vent (used to be shared between the three tanks, but > as part of debugging now goes only to fuselage tank). Vent is pointed > forward, mounted below fuselage, center, just forward of main wing spar. > On the last test flight today, I continued to see bubbles, even after > reducing power for several minutes and levelling off. Were at 7,500'. > Pressure about 1 psi. After a dive to get down below Class B 6,000' > floor, pressure came back up to above 3 psi. > A few minutes after landing I noticed that the fuel line to outer > carbs appeared empty. Turning on the pump for a few seconds filled it > up. After turning off the pump I noticed that the line emptied out. > How can this be? By gravity feed alone, the fuel level should have > been a couple of feet up that line. I did not delect any gas leak. > Maybe 10 minutes later, the line stayed full after turning on and off > the pump (or was now full - not sure). > > This brings me to questions about vapor lock. I actually don't know > what that is. Carb bowls are vented into airbox. So how could the fuel > in the bowls be under pressure, maybe boiling, and push gasses back > down the fuel line to the pump? Unlikely? I do have a SS heat shield > between carbs and exhaust headers. Does its ability to reflect heat > lessen if it is no longer shiny? > > I guess the next step is to replace all rubber lines going to the > pumps with transparent ones so I can see what's going on the the lines > to the pumps. > > But other ideas are certainly welcome. Up till the last observation, > I've been trying to locate air leaks in lines to pumps and was ready > to replace the brand new facet pump with an old one, in case it > somehow is sucking air. > Now I'm mystified. > > Finn (please no jokes about wit). > >