Aircraft Gas Turbine Engine Compressor Vane

Aircraft Gas Turbine Engine Compressor Vanes are components used in gas turbine engines to help compress the incoming air before it enters the combustion chamber. These vanes are typically made of high-strength materials such as titanium or nickel-based alloys to withstand the high temperatures and pressures within the engine.

The compressor vanes are located in the compressor section of the engine, which is responsible for increasing the pressure of the incoming air. They are positioned between the compressor blades and help to direct the airflow and maintain the efficiency of the compressor.

The vanes are designed with aerodynamic profiles to optimize the airflow and minimize losses due to turbulence. They play a crucial role in ensuring the proper functioning of the engine by providing efficient compression of the air, which is essential for combustion and overall engine performance.

In the supply class Gas Turbines And Jet Engines, Aircraft, Prime Moving; And Components, the Aircraft Gas Turbine Engine Compressor Vanes are categorized as components specifically used in gas turbine engines for aircraft propulsion. They are part of the broader supply group Engines, Turbines, And Components, which includes various components and systems related to engines and turbines used in aviation.

These compressor vanes are critical components in aircraft gas turbine engines, as they contribute to the overall efficiency, performance, and reliability of the engine.