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You can register using your Google, Facebook, or Twitter account, just click here.Water injection is not really needed in EM/IAV engine because it would be redundant as IAV is using a modern EGR system for the same purposes. As pistonboy correctly stated water injection essentially serves the same purpose as an EGR system however pistonboy does not appear to be aware of just how far EGR systems have come as they are no longer the power robbing problems they once were. EM/IAV have already done an excellent job of explaining why they are using a modern EGR system in Tech Talk V39:
The use of this modern ECU controlled cooled EGR system along with taking advantage of modern computer modeling power to precisely model and plan the air/fuel swirling movement inside the combustion chamber all contributes to the combustion mixture remaining mixed and cooled which results in controlled high compression burn without pre-ignition or detonation. This also results in more complete combustion which reduces harmful emissions. This is how IAV can plan on safely achieving compression ratios of 12:1 on regular unleaded gasoline.![]()
The last generation of high output aero engines, such as those built for larger aircraft after WW2, successfully used water injection to help prevent detonation at high power settings, e.g. on takeoff.
If the charge temperature is lower, a higher compression ratio can be used without detonation taking place. This makes the engine more efficient. A disadvantage is that adding water to the incoming charge mix displaces some air (i.e. oxygen), so less fuel can be burnt, which reduces the power, defeating the object somewhat.
So, as an added refinement, methanol was mixed with the water. The methanol did two things. First, it prevented freezing of the water at the extremely cold outside air temperatures at high altitude. Secondly, methanol needs very little oxygen to burn, compared to gasoline (it self generates some oxygen in its chemical burning process) so it replaces that "lost" by adding water. The problem with this system was that operators of these aircraft needed to ensure that water/methanol mix was available as well as AVGAS, or the aircraft had to operate at reduced power output, or not at all.
The technology became mainly redundant with the change to gas turbine engines. One exception was the Harrier "jump jet" which used water injection for very similar reasons (to reduce turbine outlet temperature, so the engine could be safely spun to higher rpm without melting the turbine blades).
I have often thought that water/meth injection might be a better way of using sustainable alcohol fuels without the problems caused by adding it directly to the main fuel system.
I don't understand why cooling the air in the cylinder helps. Sure, I know colder air has more oxygen BUT, the air is already in the cylinder. Whatever temperature it was coming in determines the oxygen concentration. Cooling it once in there doesn't add oxygen. I must just be missing something.
I know cooler air is denser (has more oxygen to burn) but, when it enters the cylinder, it's temperature was already set... in the intake. The air gets pulled into the cylinder where it immediately begins to heat up and expand. The valves are closed at this point so no more air can get in or out (the air maintains it's amount of density at this point though as it heats up, it creates pressure). Now that I've said it like that, the pressure that is created by the air heating up slows the piston down more than if the air didn't heat up as much. If you kept the cylinder cooler, the air would slow the piston less thus increasing efficiency. I think it has more to do with the pressure created by heating up the air quickly than with the oxygen content at that point. cold air intakes are there to cool the air BEFORE it gets into the combustion chamber thus increasing the amount of oxygen available.Cooler air is "denser". IIRC (from a few years ago) The average (normally aspirated) engine has an "intake charge" efficiency around 70%. This is measured at WOT so the throttle blades aren't a restriction. Since an engine is really a glorified "air pump", It's efficiency is reliant on how well it can "suck" (vacuum) air into the cylinders. The physical act of piston "sucking" the air "stretches it" making it less dense. So, Cooling the incoming air charge ( "before" it enters the cylinder) will make it denser. It would be necessary to introduce the H2o before the key sensors (map/maf/iat) so the computer could take advantage of the denser & cooler charge.
On the other hand...it might end up being more hassle that it's worth. So, let someone else try it first.![]()
De-mineralised water is definitely required, as you suspect. otherwise the inside of the engine might eventually start to look like a furred up kettle! I'm certain that aircraft just had a simple tank for the water/meth mix, as supplied at the point of sale. Any extra on-board equipment adds unwanted weight; very bad idea on any aircraft.