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Module 15. Gas turbine engine
If a burner was down, in a multi-can system, the engine would tend to
•  hang up.
•  run up.
•  surge.

Diverdeep asking:
•  explain??


Community comments: 0
Module 15. Gas turbine engine
Turboprop engine inlet anti-ice system operates
•  cyclically independent on weather conditions.
•  cyclically dependant on weather conditions.
•  continuously.

Diverdeep asking:
•  turbine engine theoretically has 2 sections the main one operates continuously and the second one operates cyclically to avoid overload of the electric system

Community comments: 0
Module 15. Gas turbine engine
The exhaust gas temperature (E.G.T ) indicator on a gas turbine engine provides a relative indication of the
•  turbine inlet temperature.
•  temperature of the exhaust gases as they pass the exhaust cone.
•  exhaust temperature.

Diverdeep asking:
•  The exhaust gas temperature (EGT) is typically defined as the gas temperature at the exit of the turbine
https://www.researchgate.net/publication/266673900_A_Review_of_Exhaust_Gas_Temperature_Sensing_Techniques_for_Modern_Turbine_Engine_Controls#:~:text=The%20exhaust%20gas%20temperature%20%28EGT%29%20is%20typically%20defined,parameter%20for%20optimizing%20fuel%20economy%2C%20diagnosis%2C%20and%20prognosis.


Community comments: 0
Module 15. Gas turbine engine
Nozzle guide vanes give a
•  pressure increase, velocity decrease.
•  pressure increase, velocity increase.
•  pressure decrease, velocity increase.

Diverdeep asking:
•  nozzle guide vane are associated with compression section, so they're used to maximise compression performance (they're divergent) by decrease the speed & increasing pressure gain for each stage

Community comments: 0
Module 15. Gas turbine engine
Nozzle guide vanes give a
•  pressure increase, velocity decrease.
•  pressure increase, velocity increase.
•  pressure decrease, velocity increase.

Diverdeep asking:
•  nozzle guide vane are associated with compression section, so they're used to maximise compression performance (they're divergent) by decrease the speed & increasing pressure gain for each stage

Community comments: 0
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