Return-Path: Received: from mail2.mx.voyager.net ([216.93.66.206] verified) by logan.com (CommuniGate Pro SMTP 4.3c1) with ESMTP id 727267 for flyrotary@lancaironline.net; Sun, 13 Feb 2005 12:27:44 -0500 Received-SPF: none receiver=logan.com; client-ip=216.93.66.206; envelope-from=dsbarno@vbe.com Received: from u036fr3za011 (d120.as0.wtma.wi.core.com [64.77.136.248]) by mail2.mx.voyager.net (8.13.2/8.10.2) with SMTP id j1DHQwlF010837 for ; Sun, 13 Feb 2005 12:26:59 -0500 (EST) Message-ID: <007e01c511f1$e5ec8240$3c40fea9@u036fr3za011> From: "Barnhart" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: Vapor Lock Date: Sun, 13 Feb 2005 11:31:48 -0600 MIME-Version: 1.0 Content-Type: text/plain; charset="Windows-1252" Content-Transfer-Encoding: 8bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1123 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1123 Al, I know what you mean about fuel being better pushed than sucked. My tech counselor/dar made it very clear that he wanted the sump at the lowest point. My low point is behind the rear seats and is a taildragger. Picked up a 1/2 inch unit from Andair and have 3 feet of head from both sides feeding it. Keeping the fuel pumps about 12 inches away. Also have a plan b.... Barny MGDQ 20bt (don't really have dial up here, more like wind up) > > > > > Al Gietzen wrote: > > > >> This issue has been worked over pretty thoroughly, but bear with me > >> through some comments and possible clarifications if this subject has > >> your interest. > >> > >> 1.) In general I don’t think it is ever a good idea to expect fuel, > >> particularly mogas, to be “sucked”. The ability to draw any liquid is > >> limited by its vapor pressure, the pressure at which it will flash to > >> vapor rather to remain as a liquid. Even water at room temp can only > >> be sucked to a head of about 30 ft (about 14 psi) beyond which it > >> will be vapor. At the boiling point, obviously it can’t be lifted or > >> drawn at all, all you get is vapor. Auto fuel at room temp can only > >> be drawn to something like a 6 ft head, less than 2 psi, or it will > >> flash to vapor. Increase its temp a bit and pretty soon you can’t > >> suck it at all; all you get is vapor. So any system in which you > >> expect to apply negative pressure to move the fuel is at risk. It may > >> work fine at normal temps, but when it warms up, look out. > >> > >> 2.) As a corollary to this, in a gravity fed system it is not a good > >> idea to have a fuel filter (or even gascolator with a fine screen) > >> upstream from the EFI pump, because it causes restriction to flow, > >> especially after it has picked up some dirt. Yes; you do not want any > >> water getting through the pump, and one good reason for having a sump > >> or header tank is the have the exit to the EFI pump above the bottom > >> so any water and dirt will be collected, and be drained with a sample > >> drain. If an upstream filter or gascolator is in the engine > >> compartment, so much the worse, because it causes a dwell time in a > >> hot place for the fuel to heat. To draw it from there to the pump, as > >> in Paul’s case, can be a setup for vapor lock. > >> > >> 3.) Normally you want the fuel to recirc through the fuel rail, with > >> the pressure regulator bypass going back to some tank upstream from > >> the EFI pump; the reasons all relate to keeping down the temp of the > >> fuel to the fuel rail. As Leon points out, it is has been the proven > >> way. Yes, you can plumb a one-way path from between the pump and the > >> regulator to the fuel rail so only fuel burned by the engine goes to > >> the engine compartment, and normally it may work fine, but the > >> residence time of the fuel in the hot environment can result in very > >> high fuel temps. It can cause variation in performance depending on > >> the temp as the density of the fuel varies. Even though the pressure > >> downstream from the EFI pump significantly reduces the likelihood of > >> vapor forming; I don’t know how hot the fuel would need to get to > >> boil at 40 psi; I can imagine the case after engine shutdown on a hot > >> day that won’t restart because the fuel in the line and rail have > >> filled with vapor; possibly bleeding back through the pump. > >> > >> 4.) The bypass fuel return from the pressure regulator can indeed be > >> under pressure if it is restricted. The regulator produces a > >> differential pressure across a restriction. If you restrict the > >> bypass flow (back pressure) the pressure in the fuel rail will > >> increase, possibly up to the limit of the pump. So in John’s case it > >> is to be expected that if the tank the return fuel is going to is > >> full, the engine will lose power because the mixture will get very rich. > >> > >> 5.) It seems to me the sump/header tank must be vented in some way to > >> allow air/vapor return to the main tank, or out. There can be > >> different circumstances for different configurations. The case that > >> Jim mentions for not having the vent in a gravity feed system is to > >> overcome a specific issue of loss of flow due to tank cap leaks which > >> caused the low pressure above the wing (strake) to offset the rather > >> small gravity pressure head. His solution of a controlled vent is a > >> good one, unless you are confident that your caps will always be > >> leaktight. > >> > >> 6.) Whether or not the Paul’s sump tank became full of vapor is not > >> known, but a vent is needed. The vent line must extend upward to a > >> level above the level of the fuel in the main tanks before going down > >> and out to avoid fuel being lost overboard. It is also important that > >> the vent lines from the main tanks and the sump tank go off the > >> highest point in the tank. If the exit is submerged, expanding fuel > >> can result in fuel going overboard. > >> > >> Ok; this got longer and maybe more boring than I had hoped, but like > >> everyone else, I’m trying to be helpful. > >> > >> Al > >> > >> Subject: [FlyRotary] Vapor Lock > >> > >> Hi, Perry....One question....Does your unburned fuel (from the fuel > >> rail) go back into your sump tank also? Or do you return the unused > >> fuel to one of your fuel tanks? If I were returning fuel to one of > >> the main tanks, I would think that venting the sump would be > >> appropriate, but since I am sending fuel undere pressure back into > >> the sump tank, I am concerned that once the sump tank is full, the > >> additional fuel pumped back into the sump tank would take the path of > >> least resistance....out the vent instead of back up the fuel line > >> into the tank? Thanks for your input. Paul Conner > >> > >> One other comment Paul: the fuel return from the fuel rail is not > >> pressurized. The pressure regulator maintains HP on the fuel rail > >> side, but the fuel return output back to the sump is not under high > >> pressure. > >> > > > > >> Homepage: http://www.flyrotary.com/ > >> Archive: http://lancaironline.net/lists/flyrotary/List.html > > > _____________________________________________________ > This message scanned for viruses by CoreComm > >