4.5 Article

Bionic microstructure on titanium alloy blade with belt grinding and its drag reduction performance

Publisher

SAGE PUBLICATIONS LTD
DOI: 10.1177/0954405420949744

Keywords

Bionic microstructure; drag reduction; belt grinding; CFD simulation; blade

Funding

  1. National Natural Science Foundation of China [U1908232]
  2. National Science and Technology Major Project [2017-VII-0002-0095]
  3. Graduate Scientific Research and Innovation Foundation of Chongqing, China [CYB20009]
  4. China Postdoctoral Science Foundation [2020M673126]

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The research delves into the drag reduction mechanism of bionic microstructure processed by belt grinding and sets up three groups of typical belt grinding bionic microstructures for CFD simulation to calculate drag reduction values. The experiment on aero-engine blade validates the airflow dynamics of drag reduction, with the results indicating that wave ribs outperform V-ribs and trapezoidal ribs in terms of drag reduction and increasing the size of bionic microstructure can improve airflow dynamic performance.
Researches show that surface with bionic structure plays an important role in improving the aerodynamic performance on aero engine parts. Belt grinding, a popular method to process titanium alloy parts such as aero-engine blade, is also found that it can be used to obtain bionic microstructure through special grinding method and parameters. In order to explore the performance of bionic microstructure processed by belt grinding and its effects on airflow dynamics, several groups of simulation and an experiment are carried out in this paper. Firstly, the mechanism of drag reduction of bionic microstructure is discussed. It shows that the effect of drag reduction of bionic microstructure is related to protrusion height, which is related to the shape and size of the bionic microstructure. Then, three groups of typical belt grinding bionic microstructure are set up. In addition, the drag reduction values are calculated in CFD simulation. The results are analyzed and discussed. Further, to verify the airflow dynamics of drag reduction of belt grinding bionic microstructure, an experiment of aero-engine blade is carried out. Finally, the effects of airflow dynamic performance of blade with belt grinding bionic microstructure are obtained in CFD simulation. In general, the shape of wave ribs, compared to V-ribs and trapezoidal ribs, has the best performance in drag reduction. To a certain extent, the improvement of airflow dynamic performance is higher with the increasing of the size of bionic microstructure, which suggests lower feed rate and higher grinding pressure for bionic structure.

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