Engine Gas Turbines (Supplementary) USCG Question #141 (Set 5)

To prevent overheating of the illustrated turbine blade, which of the following fluids is circulated through it via the shaped internal passages? See Illustration GT-0035 Illustration GT-0035: the U.S. Coast Guard has not released this illustration.

Official USCG Answer & Rule Citation

Correct Answer: Option D — Bleed air.

High-pressure bleed air, extracted from the compressor section, is directed through internal cooling passages in turbine blades. This film cooling technique creates a protective boundary layer, preventing the metal from exceeding its metallurgical temperature limits when exposed to the extreme heat of the combustion gas path.

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