What constitutes a pressure stage in a compressor?

Study for the Aviation Maintenance Technician, Second Class (AMT2) Exam. Use flashcards and multiple choice questions, with hints and explanations provided for each question. Prepare for success!

Multiple Choice

What constitutes a pressure stage in a compressor?

Explanation:
The key idea is that a pressure stage is where the gas gets its pressure rise through both energy addition and flow turning. In an axial compressor, that happens with a rotor blade row that imparts energy to the gas, followed by a stator blade row that straightens the flow and converts that energy into additional static pressure. Together, the rotor and stator form a single stage, and stacking stages gives higher overall pressure. A single rotor blade is only part of the energy-adding process and cannot complete the stage, because without a stator to remove swirl and convert the added energy into pressure, the flow won’t achieve the desired pressure rise. Two stator blades in a row don’t add energy themselves; they merely guide and diffuse the flow. An impeller alone isn’t a complete stage in most compressor types because the diffuser or stator is needed to convert the rotor’s kinetic energy into usable static pressure. Therefore, the rotor-stator pair best defines a pressure stage.

The key idea is that a pressure stage is where the gas gets its pressure rise through both energy addition and flow turning. In an axial compressor, that happens with a rotor blade row that imparts energy to the gas, followed by a stator blade row that straightens the flow and converts that energy into additional static pressure. Together, the rotor and stator form a single stage, and stacking stages gives higher overall pressure.

A single rotor blade is only part of the energy-adding process and cannot complete the stage, because without a stator to remove swirl and convert the added energy into pressure, the flow won’t achieve the desired pressure rise. Two stator blades in a row don’t add energy themselves; they merely guide and diffuse the flow. An impeller alone isn’t a complete stage in most compressor types because the diffuser or stator is needed to convert the rotor’s kinetic energy into usable static pressure. Therefore, the rotor-stator pair best defines a pressure stage.

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