For better understanding of the flow characteristics of turbine blade internal cooling passage
a numerical study was conducted to investigate the influences of rib
turn and rotation on the flow characteristics in full S-shaped passage with ribs. The Reynolds number was 17000
three outlet discharge ratios were 27%
49%
24%
rotation numbers were 0
0.03
0.06
0.09. The results reveal that the fluid has stronger turbulence and lower velocity with higher blockage ratio near the leading edge of passage 1. Turn causes the flow separation and shift of mainstream downstream the turn. There is a big range of low velocity area near the bulkhead in the passage 3. Coriolis force makes the fluid shift towards the wall to which the Coriolis force points
the mainstream shifts towards suction surface and pressure surface in passage 2 and passage 3 respectively. Rotation affects the distribution of the secondary flow in passage and promotes the flow of low velocity circumfluence area downstream the turn.
Composite cooling structure on rotating turbine blade
Flow loss control of turbine based on “groove” and “dimple” technology with low Reynolds number
Influence of blowing ratio on film cooling of rotating turbine blade
Experimental research on heat transfer of "impingement/effusion" double-plate configuration in rotating state
Experimental Study of Flow Characteristics in Two-Pass Channel with Ribs and Cell Film Cooling
Related Author
朱兴丹
张靖周
谭晓茗
YANG Lin
QIAO Wei-yang
MU Zhong-qiang
LUO Hua-ling
HOU Wei-tao
Related Institution
南京航空航天大学 能源与动力学院 江苏省航空动力系统重点实验室
School of Power and Energy, Northwestern Polytechnic University
China Gas Turbine Establishment, Aviation Industry Corporation of China
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Jet Propulsion,Beijing University of Aeronautics and Astronautics
Market Department of China National Aero-Technology Import and Export Corporation