Aircraft Gas Turbine Engine Compressor Component Support

Aircraft Gas Turbine Engine Compressor Component Support refers to the various components that provide support and stability to the compressor section of a gas turbine engine used in aircraft. These components are part of the supply class Gas Turbines And Jet Engines, Aircraft, Prime Moving; And Components, which falls under the supply group Engines, Turbines, And Components.

The compressor section of a gas turbine engine is responsible for compressing incoming air before it enters the combustion chamber. This compressed air is then mixed with fuel and ignited to produce the necessary thrust for aircraft propulsion. The compressor component support plays a crucial role in maintaining the structural integrity and efficient operation of the compressor section.

Some common examples of compressor component support include:

1. Compressor casing: This is the outer shell that encloses the compressor section and provides structural support. It also helps to contain the compressed air within the engine.

2. Stator vanes: These stationary blades are positioned in the compressor section to guide the airflow and ensure efficient compression. They are supported by the compressor casing and help to control the airflow direction.

3. Rotor blades: These rotating blades are attached to the compressor shaft and work in conjunction with the stator vanes to compress the incoming air. They are designed to withstand high rotational speeds and provide the necessary compression.

4. Bearings: The compressor shaft is supported by bearings, which allow for smooth rotation and reduce friction. These bearings are crucial for maintaining the stability and alignment of the compressor section.

5. Seals: Various types of seals are used in the compressor section to prevent air leakage and maintain the efficiency of the compression process. These seals help to minimize losses and ensure optimal performance.

Overall, the compressor component support plays a vital role in the operation of an aircraft gas turbine engine. It ensures the efficient compression of air, which is essential for generating the required thrust for aircraft propulsion.