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A New Interpretation of Hot Gas Ingress Through Turbine Rim Seals Influenced by Mainstream Annulus Swirl
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Rim seals are fitted at the periphery of the stator and rotor disks to reduce the adverse effects of hot gas ingress on highly stressed turbine components limited by temperature. Ingress is induced by rotational effects ...
Influence of Flow Coefficient on Ingress Through Turbine Rim Seals
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Rim seals are critical in terms of limiting the temperature of highly stressed engine components but function with a penalty to the power output and contribute to entropy gain stemming from mixing losses in the turbine. ...