The High Turbine Gas Temperature (TGT) limiting setpoint is at what temperature?

Prepare for the UH-60S Black Hawk Academic Exam 2. Test your knowledge with multiple choice questions, flashcards, and detailed explanations. Enhance your skills for the Utility Helicopter 60 Black Hawk Exam!

Multiple Choice

The High Turbine Gas Temperature (TGT) limiting setpoint is at what temperature?

Explanation:
Turbine gas temperature is a critical parameter that defines the maximum safe temperature the turbine can experience without risking damage to blades and shrouds. The engine control uses a hard limit at 1000 degrees Celsius to protect the turbine from thermal overstress and accelerated wear. When TGT approaches this limit, the FADEC reduces fuel flow to keep the temperature from exceeding it; if necessary, it will further reduce power to stay within safe margins. The other temperatures shown are lower values and do not represent the official limiting setpoint for normal operation; the 1000 C limit is the value that defines the allowable maximum.

Turbine gas temperature is a critical parameter that defines the maximum safe temperature the turbine can experience without risking damage to blades and shrouds. The engine control uses a hard limit at 1000 degrees Celsius to protect the turbine from thermal overstress and accelerated wear. When TGT approaches this limit, the FADEC reduces fuel flow to keep the temperature from exceeding it; if necessary, it will further reduce power to stay within safe margins. The other temperatures shown are lower values and do not represent the official limiting setpoint for normal operation; the 1000 C limit is the value that defines the allowable maximum.

Subscribe

Get the latest from Examzify

You can unsubscribe at any time. Read our privacy policy