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Mechanical Engineering · Q77

Compressors, Gas Turbines And Jet Engines

Engineering and GATE · Mechanical Engineering · question 77

Q77

Work ratio of a gas turbine may be improved by

A.
Decreasing the compression work
B.
Increasing the compression work
C.
Increasing the turbine work
D.
Both (A) and (C) above
Answer

Answer: Option D

Solution

Answer: Option D
Solution:
-Increase the turbine inlet temperature provided the turbine materials can stand the temperature or one has access to replacement parts that can withstand the temperatures. -Increase the pressure ratio. There is a limit to the efficiency increase depending upon the turbine inlet temperature. One can concievably increase the pressure ratio to a point that the increased work is never recovered because the expansion across the turbine is inadequate to recover the work. - Power augmentation through steam injection. -On turbines with HP and LP turbine separated, apply reheat.