Thermal Barrier Coating for Light-Duty Gas Turbine Annular Combustor Components with High-Temperature Oxidation Resistance and Thermal Fatigue Reduction

We possess professional and mature TBC (Thermal Barrier Coating) manufacturing and application capabilities for gas turbine and aero-engine hot-end components. Our team is highly experienced in coating preparation, surface treatment, precise spraying processes, and post-treatment optimization.

Our finished TBC layers feature a smooth surface, uniform thickness, flat texture, no defects, and excellent adhesion performance. The thermal barrier coating significantly isolates extreme operating temperatures, reduces component thermal fatigue, resists high-temperature oxidation and hot corrosion, and improves the thermal stability and overall reliability of high-temperature parts.

We deliver consistent, high-standard TBC coating services to meet the strict requirements of gas turbine power generation, industrial energy, and offshore power projects worldwide.

We have extensive engineering experience in thermal barrier coating for light-duty gas turbine annular combustor components, including annular combustor liners, transition segments, combustion casings, and all hot-gas-path parts.

Equipped with standardized surface cleaning, grit blasting, bond coat pretreatment, and precision spraying processes, we provide uniform thickness, smooth surface, dense structure, and flawless coating layers. Our coating perfectly adapts to the special curved and annular structure of lightweight gas turbine combustors, avoiding coating accumulation, peeling, bridging, and uneven coverage.

The advanced coating system effectively insulates extreme combustion heat, reduces thermal fatigue stress, and significantly improves high-temperature oxidation and molten salt corrosion resistance under frequent start-stop working conditions. We fully comply with OEM technical standards, providing reliable and long-lasting surface protection for various light-duty gas turbine annular combustor assemblies.

Applicable components include annular combustor liners, transition segments, combustion casings, and all hot-gas-path parts of light-duty gas turbines.