What is the primary function of the compressor in a turbine engine?

The primary function of the compressor in a turbine engine is to increase the pressure of incoming air. This is a crucial step in the engine’s operation, as higher pressure air allows for more efficient combustion when mixed with fuel, leading to a greater energy release during the combustion process. This enhanced pressure also plays a vital role in achieving the necessary airflow through the engine, which supports the turbine and overall performance of the gas turbine propulsion system.

Increasing the pressure of the incoming air enhances the engine's thrust and efficiency, as it allows for better mixing with fuel and ensures that a more substantial amount of air can be processed through the combustion chamber. The compressor thus is integral to the engine's ability to generate power and drive the turbine, contributing to the overall functionality of the gas turbine engine system.