Aero-engine combustion chamber, located between the compressor and turbine, provides a combustion site for fuel. When the engine is operating, fuel enters the combustion chamber, mixes with high-pressure air, and burns completely, converting the chemical energy of the fuel into thermal energy. This generates high-temperature, high-pressure gases that meet the turbine's requirements, converting work into engine thrust, thus enabling the engine to operate. The combustion chamber is one of the three core components of an aero-engine, and its quality directly affects the performance of the engine.
