Exhaust gas temperature

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Exhaust gas temperature (EGT). The temperature of the exhaust gases as they leave the cylinders of a reciprocating engine or the turbine section of a turbine engine.

Discussion

A limiting factor in a gas turbine engine is the temperature of the turbine section. The temperature of a turbine section must be monitored closely to prevent overheating the turbine blades and other exhaust section components. This temperature varies with the ratio of fuel to air entering the cylinders and can be used as a basis for regulating the fuel/air mixture.

Some exhaust systems have an EGT probe. This probe transmits the EGT to an instrument in the flight deck, the EGT gauge. The EGT gauge measures the temperature of the gases at the exhaust manifold. The gauge is used to monitor overall engine operating conditions. The EGT gauge is highly accurate in indicating the correct mixture setting. When using the EGT to aid in leaning the fuel/air mixture, fuel consumption can be reduced. For specific procedures, refer to the manufacturer’s recommendations for leaning the mixture.

Variations of EGT systems bear different names based on the location of the temperature sensors. Common turbine temperature sensing gauges include the turbine inlet temperature (TIT) gauge, turbine outlet temperature (TOT) gauge, interstage turbine temperature (ITT) gauge, and turbine gas temperature (TGT) gauge.

References

Instruments
Turn coordinatorTurn-and-slip indicatorAirspeed IndicatorVSIInstantaneous vertical speed indicatorAttitude indicatorTachometerManifold pressure gaugeEPREGTMagnetic compassHeading indicatorHorizontal Situation IndicatorCDIRadio Magnetic IndicatorRelative bearing indicatorAttitude director indicatorFlight director indicator