What are the stationary blades located between each row of rotating blades in a turbine engine compressor called?

Prepare for the FAA Turbine Engine Test. Study with flashcards and multiple choice questions, each with hints and explanations. Get ready for your exam!

The stationary blades situated between each row of rotating blades in a turbine engine compressor are referred to as stators. These components play a crucial role in the compression process. The stators help direct airflow, maintaining efficient flow patterns and optimizing the performance of the compressor stages. They not only contribute to the aerodynamic efficiency of the engine but also assist in converting the high-speed rotational energy from the rotor blades into increased pressure for the airflow.

In contrast, the diffusers are structures that slow down the airflow to convert kinetic energy to pressure, while rotors are the moving blades responsible for compressing the air. Guides serve similar purposes to stators, directing airflow, but the specific term "stators" more accurately describes the stationary blades positioned between the rotors in the compressor section. This differentiation is important for understanding the mechanics and functions within a turbine engine.

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