10C1001G05 is a precision-manufactured aerospace engine combustion chamber liner segment, designed for large commercial turbofan engines. It is a key thermal protection and combustion-participating component, forming the inner space of the combustion chamber, isolating the engine's static components from high-temperature combustion gas, which is critical for maintaining the stable combustion environment, ensuring the full combustion of fuel and air mixture, and preventing the overheating damage of surrounding engine components.
Made from high-strength, heat-resistant and oxidation-resistant nickel-based superalloy, it withstands operating temperatures up to 1500°C and continuous scouring from high-speed combustion gas. Weighing 0.4kg with an integrated cooling structure, it allows for fast installation and condition inspection during combustion chamber MRO overhauls.