Aircraft Gas Turbine Engine Compressor

Aircraft gas turbine engine compressors are a crucial component of gas turbine engines used in aircraft. They are part of the supply class "Gas Turbines And Jet Engines, Aircraft, Prime Moving; And Components" in the supply group "Engines, Turbines, And Components."

The compressor is responsible for compressing the incoming air before it enters the combustion chamber. It plays a vital role in the overall performance and efficiency of the engine. The compressor consists of multiple stages, each consisting of a row of rotating blades (rotor) and a row of stationary blades (stator).

As the rotor blades rotate, they accelerate the incoming air, increasing its pressure and temperature. The stator blades then redirect the airflow and further increase its pressure. This compressed air is then mixed with fuel in the combustion chamber and ignited, producing high-temperature, high-pressure gases that drive the turbine and ultimately provide thrust for the aircraft.

The design and efficiency of the compressor are critical for the engine's performance. It needs to provide sufficient airflow and compression ratio to ensure optimal combustion and power output. Compressor efficiency directly impacts the overall efficiency and fuel consumption of the engine.

In summary, aircraft gas turbine engine compressors are essential components that compress incoming air, increasing its pressure and temperature before it enters the combustion chamber. They are part of the supply class "Gas Turbines And Jet Engines, Aircraft, Prime Moving; And Components" in the supply group "Engines, Turbines, And Components."