6876865 Transition Assembly Liner

OVERVIEW

The purpose of the liner transition assembly, which is assembled on the downstream portion of the annular combustion chamber, serves to smoothly redirect the flow of high-pressure and high-temperature combustion gas into the turbine section, resulting in gas flow aligned with the direction of overall flow through the engine. The liner ensures a controlled and efficient flow of gas in the turbine section.
The liner is made of high-temperature-resistant material, which protects the underlying structure of the gas turbine. The transition liner undergoes heavy thermal stress while acting as a passage; thus, the design of the liner plays a crucial role in achieving optimal performance and efficiency in the turbine section. Part number 6876865 meets the exact design specifications and standards for easy drop-in replacements.