This stationary compressor vane is designed to direct airflow effectively between stages, enhancing turbine performance. It reduces airflow velocity while increasing pressure and minimizes boundary layer thickness to decrease drag. Manufactured from durable super alloys, part number K465P03 meets precise specifications for straightforward replacement in demanding turbine enviro
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Overview
Stage 5 stationary compressor vane that helps direct and guide the airflow from its previous stages. Vanes ensure the flow of gas in the desired direction for the optimum efficiency of the turbine. Vanes contribute to the compressor by decreasing the velocity of airflow, thus increasing the pressure. The vanes of a compressor play a crucial role in minimizing the thickness of the boundary layer of air and reducing drag. Part number K465P03 is manufactured from super alloys that withstand the demanding conditions in a turbine and meet the exact design specification for easy replacement.
Technical Information
ATA Number
72
ATA Chapter
Engine Turbine / Turbo Prop Ducted Fan / Unducted Fan
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