In order to study flow characteristics of tip clearance flow in turbine shroud
a cooling experimental system was designed
and the instantaneous flow field of each typical section was received by particle image velocimetry(PIV).Then the flow field characteristics of tip clearance flow were studied.The result shows:two cooling flows of the turbine shroud cavity mixing with tip leakage flow makes the flow state in shroud cavity very complex.Therefore
vortex flows with different functions and sizes are generated at different positions in shroud cavity.Meanwhile
both the two cooling airflows have blocking effect on the leakage flow
and the effect from the former hole is more obvious.
Influence of rotation on discharge coefficients of two rows of film holes in channel with rib turbulators
Cooling characteristics of pin-fin arrays with non-uniform diameters
Contact stress calculation and static strength analysis of zig-zag shrouded blade
Approach to early crack diagnosis of turbine blade based on EEMD energy entropy fusion of three-dimensional tip clearance
Rib influence on heat transfer and pressure drop in pin-fin array
Related Author
ZHANG Wei
LI Guang-chao
PENG Da-wei
WANG Cheng-jun
XIANG Song
BAI Wandong
LIANG Dong
CHEN Wei
Related Institution
Liaoning Key Laboratory of Digital Technology Simulation and Test Technique,School of Aero Dynamics and Energy Engineering,Shenyang Institute of Aeronautical Engineering
School of Power and Energy,Northwestern Polytechnical University
School of Aeronautics and Astronautics,Sichuan University