X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sat, 16 Jun 2007 11:30:15 -0400 Message-ID: X-Original-Return-Path: Received: from mta16.adelphia.net ([68.168.78.211] verified) by logan.com (CommuniGate Pro SMTP 5.1.9) with ESMTP id 2106240 for lml@lancaironline.net; Sat, 16 Jun 2007 09:17:24 -0400 Received-SPF: pass receiver=logan.com; client-ip=68.168.78.211; envelope-from=glcasey@adelphia.net Received: from [75.82.253.35] by mta16.adelphia.net (InterMail vM.6.01.05.04 201-2131-123-105-20051025) with ESMTP id <20070616131645.LPEX28396.mta16.adelphia.net@[75.82.253.35]> for ; Sat, 16 Jun 2007 09:16:45 -0400 Mime-Version: 1.0 (Apple Message framework v752.2) In-Reply-To: References: Content-Type: text/plain; charset=US-ASCII; delsp=yes; format=flowed X-Original-Message-Id: <8C192F6C-852F-4318-84BC-3323AE844492@adelphia.net> Content-Transfer-Encoding: 7bit From: Gary Casey Subject: Re: Boost switch X-Original-Date: Sat, 16 Jun 2007 06:16:43 -0700 X-Original-To: "Lancair Mailing List" X-Mailer: Apple Mail (2.752.2) I've been reading this thread with interest and finally thought I could add something - if only just my opinion: > > No. My point is that the TCM fuel system design is faulty. It has > an extraordinary sensitivity to its input fuel pressure. That > problem can be made worse by bad setup, but even with "good" setup > it is still a bad design. > I don't think I would go that far, since safety is relative, as all designs have faults and the only thing that can be done is to choose the best overall balance. The TCM fuel system is what we used to call a "speed-theta" system in that fuel flow is primarily proportional to engine speed and throttle angle. Add in various orifices to tweak the system and that's it. Very simple, few moving parts and presumably reliable and durable. An integral part of the system is the engine-driven fuel pump, which is a positive- displacement (vane) type sized to the engine flow requirements. The throttle-controlled metering valve is shaped so that the fuel flow increases roughly in proportion to the throttle area. There is nothing about the system that is related to air flow, and I think that's one reason why there is all the attention given to "set-up". Since flow is a function of all the orifices in the system the injectors themselves are part of the flow control. Automotive users of this method include the classic Hilborn used in old Indy and other race cars (that's why they had "carburetor day" at Indy, because the fuel systems had to be set up just before the race) and Magnetti Marrelli (FIAT and Harley Davidson). I think that today only H-D and Continental use this methodology. Another approach is the "speed-density" system that makes the fuel flow proportional to rpm times manifold pressure (density). This takes away the finicky throttle-controlled valve and makes the fuel flow more likely to be proportional to air flow, especially at part throttle conditions. However, there is still no connection between fuel flow and air flow. This system is used by a number of automotive manufacturers, notably Chrysler and Honda. The addition of the "aneroid" to the Continental system adds partial manifold pressure compensation to the speed-theta system. The Precision Airmotive (PAC, a.k.a. "Bendix", a.k.a. "Lycoming", although Lycoming has no connection with PAC) system is completely different and could be termed a "Mass Air Flow" (MAF) or just "Air Flow" system. Air flow is measured by creating a pressure differential in a venturi and that pressure differential is used to meter flow through a fixed metering valve. This is pretty much like in a carburetor except that the fuel remains under pressure, allowing it to be distributed to individual injectors. Fuel flow is only dependent on air flow and is totally independent of the engine. One nice byproduct of this is that the fuel system can be bench tested and just bolted on the engine - no "set-up" required other than an idle mixture adjustment. In fact, there is no mixture adjustment possible(with the mixture control full rich, of course) in the field - the metering orifice has to be changed. Of course, this doesn't mean it's perfect, but it doesn't suffer from some of the problems being discussed in this thread. Since the FLOW of the fuel is controlled in the metering system, it is completely (well, almost) insensitive to upstream pressure. It is so insensitive that the typical pump used is a diaphragm-type just as was used in cars for many years. The diaphragm pump can be oversized so much that one part number is used for most 4 and 6-cylinder engines from 150 to 400hp. Since the system measures air flow, there are only two models (the -5 an the -10) that manage all these engines. Most cars incorporate MAF systems, but non use venturis to measure air flow. The air flow measurement is sensitive to air flow pulsations, which is why the calibration of the systems is somewhat engine-specific. There are some differences in the failure modes: With the PAC system the total flow is controlled by the metering orifice, not the injectors, so if one injector plugs the flow in the others goes up, making those cylinders rich. At full throttle the Continental system can suffer almost any type of air leak - like an intake tube that falls off -without serious problem as even that cylinder will likely keep running. Even a hole in a piston or a cylinder head blowing off won't effect fuel flow unless the injector departs with the cylinder. The same failures with an air flow system will dramatically reduce the air flow through the servo, creating a lean or even no flow condition. The big difference has been thoroughly discussed here - the sensitivity to inlet pressure. With an air flow system you can turn on the boost pump any time, including at idle, and there will be no effect. The pump is a single speed and there is no worries about whether it is on or off. Without the aneroid (I think all IO-550's have them??) the fuel flow in a Continental system is completely independent of altitude, making manual mixture control very important. The PAC system compensates by the square root of air density, so it "half-compensates" for altitude. > > In previous messages, a few remedies have been offered. > The two most practical are: > 1) regulate the pressure of the fuel just upstream of the injector > servo, > 2) use a Lycosaurus IO-540 fuel injection system (or the whole > engine). I chose number 2, although I thought a lot about putting the PAC system on a Continental engine. To imply that one system is "safe" and the other is "unsafe" is unrealistic as safety is relative. In my opinion one is "more safe" than the other mainly in that it relies less on the least reliable component of the aircraft (that would be me) to keep everything working. Another related note - there has been discussion about power interruptions when switching tanks with the continental system. Since its fuel pump relies on a steady supply of fuel if that supply is interrupted for even a very short time (like a few milliseconds) it is possible that the pump will create vapor at the inlet and that vapor might cause the pump to "vapor lock", or quit pump for a few seconds. The fuel selectors shut off the fuel from the old tank before they turn on the fuel from the new tank. Is it possible that some people don't have trouble because they have a habit of moving the selector very rapidly, reducing the "off" time? Here again, the PAC system is fairly insensitive to this since there is an accumulator built into the pump, allowing it to continue delivering fuel even though the inlet is momentarily shut off. That's why I made my system so that the new tank can be turned on before the old tank is shut off. Gary Casey ES 157, N224SG