Engine Gas Turbines (Supplementary) USCG Question #228 (Set 6)

In the marine gas turbine engine shown in the illustration, the 9th stage bleed air is used for __________. Illustration GT-0017

USCG Exam Illustration GT-0017
USCG Examination Diagram: Illustration GT-0017
Official USCG Answer & Rule Citation

Correct Answer: Option D — power turbine cooling

Ninth-stage compressor bleed air is specifically routed to the power turbine section for cooling purposes. By utilizing intermediate-stage air, the system maintains the power turbine components within their metallurgical temperature limits, ensuring long-term durability and preventing thermal degradation of the turbine blades and disks during sustained high-power operations.

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