Question 302Steam Plants - 1st Asst/Chief

70% to pass

The astern element of a main propulsion turbine is usually designed as a/an _______________.

ACurtis stage, impulse turbine
Bsingle entry, double flow turbine
CParsons stage, reaction turbine
Dmultiple entry, helical flow turbine
AI Explanation

The correct answer is A) Curtis stage, impulse turbine. The astern element of a main propulsion turbine is usually designed as an impulse turbine, specifically a Curtis stage. This is because impulse turbines are well-suited for the astern (reverse) operation of the main propulsion turbine. The Curtis stage, which features multiple rows of impulse blading, is a common design for the astern element as it provides an efficient and effective way to generate the required reverse thrust. The other options are incorrect because: B) is a different turbine configuration not typically used for the astern element, C) is a reaction turbine which is not the standard design for the astern element, and D) is an unusual turbine configuration not commonly used for the astern element.

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