| 摘要 |
The invention relates to a method for determining an exhaust gas temperature downstream of a turbocompessor turbine for a turbocharged engine consists in determining a temperature upstream of the turbocompessor turbine, calculating a correction term on the basis of the engine operating parameters and in determining a temperature downstream of said turbocompessor turbine by subtracting the correction term of the temperature upstream of the turbocompessor turbine.
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