Okay guys here is tonight's question:
Just exactly where is the best placement for the thermocouple looking at the exhaust gas temp? I personally think it is best placed upstream of the turbo; however the argument against that is that the thermocouple eventually burns up and ends up in the turbocharger exhaust wheel. End of turbocharger.
I have always thought that the exhaust gas loses energy as it crosses the vanes of the compressor; this is where the transfer of the energy from the exhaust gas to the compressor takes place. Necessarily there is also a temp drop as this takes place. The kicker here is what the pressure drop is across the exhaust turbine. If there is not very much pressure drop across the turbine then there should not be much temperature drop either... this from observing the behavior of high-pressure gasses as they flow across a choke on offshore production wells.
So the real question becomes how much of a pressure drop is there across the exhaust turbine... independent of the loading friction of the compressor turbine? And finally, just how much risk of trashing a turbo is there if I place my thermocouple upstream of my turbo?
I thought this would be a lively discussion forum... and I want to know what the consensus is before I install my gauges!
Just exactly where is the best placement for the thermocouple looking at the exhaust gas temp? I personally think it is best placed upstream of the turbo; however the argument against that is that the thermocouple eventually burns up and ends up in the turbocharger exhaust wheel. End of turbocharger.
I have always thought that the exhaust gas loses energy as it crosses the vanes of the compressor; this is where the transfer of the energy from the exhaust gas to the compressor takes place. Necessarily there is also a temp drop as this takes place. The kicker here is what the pressure drop is across the exhaust turbine. If there is not very much pressure drop across the turbine then there should not be much temperature drop either... this from observing the behavior of high-pressure gasses as they flow across a choke on offshore production wells.
So the real question becomes how much of a pressure drop is there across the exhaust turbine... independent of the loading friction of the compressor turbine? And finally, just how much risk of trashing a turbo is there if I place my thermocouple upstream of my turbo?
I thought this would be a lively discussion forum... and I want to know what the consensus is before I install my gauges!