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.
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