Turbine Inlet Temperature (TIT)

Turbine Inlet Temperature (TIT)

Content control:
SKYbrary
Content source:
SKYbrary
Text

TIT (Turbine Inlet Temperature)

Description

Turbine Inlet Temperature (TIT) is the temperature of the combustion chamber exhaust gases as they enter the turbine unit. The gas temperature is measured by a number of thermocouples mounted in the exhaust stream and is presented on a flight deck gauge in either degrees Fahrenheit or degrees Celcius.

Related Articles

Categories
General, Flight Technical
The full content of this page is available to registered users only.

SKYbrary Partners:

Safety knowledge contributed by: