Question 137Gas Turbine - Assistant Engineer70% to pass
The primary function of an axial compressor rotor blade is which of the following?
AI Explanation
The correct answer is B) To impart acceleration to the air mass, resulting in an increase in velocity.
The primary function of an axial compressor rotor blade is to accelerate the air flow, increasing the velocity of the air stream. As the air passes over the curved shape of the rotor blade, the blade imparts kinetic energy to the air, causing it to speed up. This increase in velocity is a key part of the compression process in an axial compressor.
The other answer choices are incorrect because they do not accurately describe the primary function of the rotor blade. Option A is incorrect as the rotor blades do not rely on centrifugal force to increase pressure. Option C is incorrect as the rotor blades do not act as a diffuser to increase pressure. Option D is incorrect as the primary function is to accelerate the air, not change its direction.
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#135 What type of starter is commonly used on smaller gas turbine engines? #136 Which of the following statements is true about an axial compressor disk-type rotor? #138 Why are loose-fitting blades used on the first several stages of large axial compressors? #139 What is a compressor midspan shrould? #140 What are the two common forms of axial compressor rotor blade roots?