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BASED ON THE
REYNOLDS STRESS DIFFERENTIAL MODELS SIMULATING OF TIP CLEARANCE
FLOW IN
KAPLAN TURBINE
Liao Weili Xu lianfeng Liu
Shengzhu
(Institute
of Water Resources and Hydro-Electric Engineering, Xi’an University of
Technology, Xi’an 710048)
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Abstract:
Based on the average N-S equation, adopting Reynolds stress
differential models and unstructured mesh technology, numerical
simulation is performed on the 3D turbulent flow of Kaplan turbine’s
flange clearance. The research of flow consists analyzing the velocity
distributing rules of blade surface inside Kaplan turbine flange
clearance and leakage flow of flange clearance under different
conditions. The result indicates that the leakage flow through the
clearance isn’t a single flow type but can be divided into four regions
(Ⅰ, Ⅱ, Ⅲ, Ⅳ) according to the direction of leakage flow in the flange
clearance: Ⅰregion is at leading edge of the blade’s flange, some parts
lie in pressure side which form low pressure region affected by a
fraction water leakage flowing from suction side to the pressure side,
the other lie in suction side; Ⅱ region is the middle region of blade
flange within tip clearance where the leakage flow change it’s
direction; Ⅲ region is tip leakage flow that direction of blade flange
clearance turn to suction side; Ⅳ region is trailing edge vortex region
of tip near the flange of blade. The produce and the development of
runner tip clearance flow and leakage vortex core at different operation
point and the interaction of main flow and leakage vortex and make
further study on mechanism of second flow caused by main flow and
leakage vortex, are investigated. The effect on interior flow structure
of hydraulic turbine and explain cavitations as well as cavitations
abrasion of Kaplan turbine caused by flange clearance, is revealed. The
flow rule in hydraulic turbine is improved, which provides gist for safe
operation of Kaplan turbine and designing Kaplan turbine with excellent
performance.
Key words: Kaplan turbine Reynolds stress differential models
Unstructured mesh Flange clearance flow
CLC No: TK730.2
国家自然科学基金资助项目(50379044).
Received 20040630, received in revised form 20041222
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