Fahrenheit 3,600

摘要

One of the basic rules of gas turbines is that the hotter the gas that enters the work-producing turbine from the combustor, the greater the thermal efficiency and output. Still, there are limits. Turbine inlet temperatures in the gas path of modern high-performance jet engines usually don't exceed 3,000℉, while non-aviation gas turbines operate at 2,700℉ or lower.