Turbine Inlet Temperature

Views Updated: Dec 15, 2025

Key Facts

Abbreviation
TIT
Pronunciation
/ˈtərbaɪn ˈɪnˌlɛt ˈtɛmpərəʧər/
Category
Miscellaneous
Related Field
Aircraft & Aviation

Examples in Context

  1. The fuel utilization and fuel flowrate to combustor were chosen to control the turbine inlet temperature.
  2. Now improvement of gas turbine performance depends on cycle innovation and turbine inlet temperature elevation.
  3. This paper introduces the parameter estimation research for the turbine inlet temperature and compressor exit pressure by using the engine variables measured under the different flight conditions.
  4. Finally, we also analyse the influences of environment temperature, turbine inlet temperature, the efficiency of assemblies, drag in flow and regenerator effectiveness on the specific output and thermal efficiency of simple cycle and regenerative cycle.
  5. In order to improve efficiency of gas turbine, The turbine inlet temperature is increasing continuously.

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