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#151
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A perfectly reasonable statement if and only if you are comparing identical intake conditions. |
#152
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He's not saying that EGT and CHT are equal, he's saying that across the cylinders CHT won't vary much, and neither will EGT.
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#153
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#154
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What I am saying is obvious for anyone who has flown a piston engine aircraft with individual CHT/EGT. You can see the power robbing temperature differences of introducing fuel anywhere in the intake system. Only by metering fuel with a direct injection system will the cylinders have equal EGT's and CHT's across the engine. Quote:
Last edited by Crumpp; 06-28-2011 at 09:13 PM. |
#155
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Of course EGT is not going to equal CHT in an individual cylinder, that is a silly concept. Only in direct injection will the EGT and CHT be equal across the cylinders of your engine. Fuel introduced in the intake will cause the cylinders to draw different mixture ratios as the firing order is cycled. The different fuel mixture ratio will cause each cylinder to have a different CHT and EGT from the other cylinders in the engine. This is a very common known fact for pilots as you see it every time you fly so you don't get worried when one cylinder has a temperature 100 degrees lower than another cylinder. That is just a by product of introducing fuel into the intake system instead of directly injecting it in the cylinders so the mixture can precisely metered. Last edited by Crumpp; 06-28-2011 at 09:20 PM. |
#156
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In many ways it's tougher because the pressures are higher. However, the alternatives are worse, so injection becomes the route of least resistance sooner.
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#157
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You don't have to worry about getting fuel and spark to the chamber at the right time, just the fuel. Last edited by Crumpp; 06-29-2011 at 11:44 AM. |
#158
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Sure the fuel cools the charge but the airflow volume is restricted by the fuel metering device. Carburetors, whether float, SU, or TBI restrict the airflow volume. With Direct Injection, the intake can be designed free from the volume and flow obstruction of a fuel metering system component. |
#159
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It was not solved in the "Spitfire II" the problem of negative G?
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#160
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Oh, i see. Thanks for the clarification cheesehawk!
Regards |
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