Generation of vortex lift through reduction of rotor/stator gap in turbomachinery

Lin Du, Xiaofeng Sun, Vigor Yang

研究成果: Article同行評審

11 引文 斯高帕斯(Scopus)

摘要

The axial gap between blade rowsinturbomachinery shouldbeminimizedinordertoreduce size requirements and increase efficiency; although, thereis a tradeoff between gap width and flow steadiness. The aerodynamic interaction between rotors and stators influences system performance under both steady and transient conditions. To investigate the basic physical mechanisms associated with the rotor/stator interaction, an efficient numerical scheme for solving unsteady, viscous flows on a quasi-three-dimensional coordinate system is established using an immersed boundary method. The data transfer between moving and stationary grids that slip against each other in traditional numerical methods is avoided. The effects of the axial gap between adjacent blade rows are studied by considering the flow evolution through a rotor and stator stage in different Reynolds number regimes. Results indicate that reduced blade gap leads to high lift on the rotor blade and improved stage loading. At the same time, the rotor/stator interaction increases flow unsteadiness, which may in turn increase noise and vibration. It is found that the reduced blade gap does not always improve performance, in spite of the generation of vortex lift. The present work provides guidelines for optimization of the axial gap between blade rows for turbomachinery design. Copyright

原文English
頁(從 - 到)472-485
頁數14
期刊Journal of Propulsion and Power
32
發行號2
DOIs
出版狀態Published - 2016

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Fuel Technology
  • Mechanical Engineering
  • Space and Planetary Science

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