drivemusicnow
15+ Year Contributor
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- Nov 15, 2004
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Germany,
Europe
yukondoit said:I believe your on the right track, but in order to relate turbine to compressore you'll need first law equation or its varient renolds transport theorom in order to relate the shaft work supplied buy the turbine and the shaft work required for the compressor. This is were the effiecencies of both the comprosser and turnbine as it would increase the amount of work necessary.
You are, obviously, correct is saying that the work done by the compressor at full engine load needs to be provided by the turbine. This work is obviously more than the work done by the compressor at full boost/4200 rpm. As long as the turbine can provide that work at full load, you should be okay. We don't care really if it is efficient at full load, because any extra efficiency will be countered with venting off exhaust flow through the wastegate.
I don't know if I even want to start down that path at this point. I mean, we probably have some the data points we need, but since this is on a theoretical system, you don't really know changes in pressure and temperature accross the turbine/compressor. I say since the problem is theoretical, we just stick with theory, and until we have the need to actually solve the problem.
There are many examples of people running a large turbine side and a small compressor side, relative to each other, that run very quick ETs for the what the setup is. The theory is that the larger hot side gives maximum benefit, while the smallest comp wheel you can get away with will reduce inertial overhead countering the added lag from the larger hotside.
) its is much easier to go based on other people's experiences. These small compressors can be maxed out relatively easily on our motors and since you wanted a longer powerband (taken form your other thread) I suggested a hotside that was more than capable of doing so. 