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The Effect of Vanes and Blades on Ingress in Gas Turbines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper presents experimental and computational results using a 1.5-stage test rig designed to investigate the effects of ingress through a double radial overlap rim-seal. The effect of the vanes and blades on ingress ...
Experimental and Computational Investigation of Flow Instabilities in Turbine Rim Seals
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: In high-pressure turbines, cool air is purged through rim seals at the periphery of wheel-spaces between the stator and rotor disks. The purge suppresses the ingress of hot gas from the annulus but superfluous use is ...
Flow Instabilities in Gas Turbine Chute Seals
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The ingress of hot annulus gas into stator–rotor cavities is an important topic to engine designers. Rim-seals reduce the pressurized purge required to protect highly stressed components. This paper describes an experimental ...