6   Artículos

 
en línea
Hui Tang, GeonHwan Cho, Mario Patinios, James A. Scobie, Carl M. Sangan, J. Michael Owen and Gary D. Lock    
Ingress is the penetration of a hot mainstream gas in a turbine annulus through the rim seal into the wheel-space between the rotating turbine disc (the rotor) and the adjacent stationary casing (the stator). Purge flow is used to prevent or reduce ingre... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
J. Michael Owen, Hui Tang and Gary D. Lock    
Increasing pressures in gas-turbine compressors, particularly in aeroengines where the pressure ratios can be above 50:1, require smaller compressor blades and an increasing focus on blade-clearance control. The blade clearance depends on the radial grow... ver más
Revista: Aerospace    Formato: Electrónico

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