FEATURES OF GAS FLOW IN RADIAL CLEARANCES OF UNBANDERING BLADES WITH HONEYCOMB SEALS
Abstract
On the basis of experimental research of turbine stage radial clearance honeycomb seals some physical phenomena were studied when flowing blade tip areas and the design procedure of energy losses was suggested.
Keywords:
radial clearance, honeycomb seal, turbine stage, blade, flow in stage, diameter, of honeycomb cell, depth of honeycomb cell, leakageHow to Cite
T. Buglayev, V., T. Perevezentsev, V., V. Perevezentsev, S. (2001) “FEATURES OF GAS FLOW IN RADIAL CLEARANCES OF UNBANDERING BLADES WITH HONEYCOMB SEALS”, Periodica Polytechnica Transportation Engineering, 29(1-2), pp. 27–34.
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