klenger said:
Given your handle (jetenginedoctor), I assume that you know a lot more about turbo-charged engines than I do. I do not intend any sarcasm in that statement.
Here is my understanding of how the turbo helps at altitude: At lower atlitudes, the system is designed to produce a maximum amount of boost. Any additional airflow that the turbo generates at lower altitudes is dumped through the wastegate.
Not exactly. The wastegate bypasses exhaust around the turbine and into the downpipe to limit the compressor discharge pressure. There is no dumping of airflow (at least not in this system) anywhere. It's simply giving the exhaust gas an alternate path around rather than through the turbine.
As altitude increases, the maximum amount of airflow that the turbo can develop is reduced, but does not affect peformance until the pressure drops below the point where the wastegate is used.
Wrong. The wastegate will still function the same way, limiting compressor discharge pressure to the same GAUGE pressure. In other words, the lower the ambient pressure, the lower the boost pressure in absolute terms. The turbo has to work harder to exert the same pressure ratio at higher elevation, so the wastegate opens later, increasing drive pressure, EGT, compressor discharge pressure, firing temperature, etc. All this has a further negative impact on the power produced by the engine.
In other words, at some altitude, the wastegate does not open and performance then drops off.
But that's not how it works. The greater the elevation, the lower the density of the air at the inlet of the turbocharger. This lower density (regardless of pressure) makes the turbocharger less efficient. Trying to create the same gauge boost pressure with the lower inlet pressure and density means the turbo has to work that much harder because it must acheive an even higher pressure ratio, adding a great deal more heat to the inlet charge, further reducing charge density. The lower density of ambient air at the higher elevation means that the charge cooler (intercooler) is that much less efficient again. The hotter, less dense air (forget pressure, remember mass of air as this is what makes power) results in a smaller cylinder charge, lower cylinder pressure, higher combustion and exhaust temps, and lower power.
Below this altitude, the engine will perform much like it would at sea level.
No, it won't. Trust me.
The number I heard some time ago was 10,000 feet, but I have no idea where I heard that, and could very well be in error.
It was in error.
I'd be interested to hear what altitude other members see a reduction in boost on a stock engine.
It's not a reduction in boost! BOOST DOES NOT EQUAL POWER!!!!!
I don't have guages, so I cannot say from personal experience. In any case, a turbocharged engine will maintain it's performance at altitude much better than a non-turbocharged engine, whether it's gas, diesel, or 100 low-lead.
That may safe to say, but it absolutely DOES NOT make it immune to the effects of increased altitude.