Journal of Textile Research ›› 2022, Vol. 43 ›› Issue (08): 80-87.doi: 10.13475/j.fzxb.20210802608

• Textile Engineering • Previous Articles     Next Articles

Simulation and analysis of carbon fiber composite unmanned aerial vehicle blade

WU Xia1, YAO Juming2,3,4, WANG Yan1, RIPON Das1, JIRI Militky5, MOHANAPRIYA Venkataraman5, ZHU Guocheng1,3()   

  1. 1. College of Textile Science and Engineering, Zhejiang Sci-Tech University, Hangzhou, Zhejiang 310018, China
    2. College of Materials Science and Engineering, Zhejiang Sci-Tech University, Hangzhou, Zhejiang 310018, China
    3. Zhejiang-Czech Joint Laboratory of Advanced Fiber Materials, Zhejiang Sci-Tech University, Hangzhou, Zhejiang 310018, China
    4. College of Materials Science and Chemical Engineering, Ningbo University, Ningbo, Zhejiang 315201, China
    5. College of Textile Engineering, Technical University of Liberec, Liberec 46117, Czech Republic
  • Received:2021-08-03 Revised:2022-03-19 Online:2022-08-15 Published:2022-08-24
  • Contact: ZHU Guocheng E-mail:zgc100100@hotmail.com

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Abstract:

In order to obtain the optimal layering mode of carbon fiber in unmanned aerial vehicle(UAV) blade, the layering mode of carbon fiber composite UAV blade is designed through ACP (ANSYS Composite PrepPost) module in Workbench. The three-dimensional model of UAV blade is established by using SolidWorks three-dimensional modeling software, and HyperMesh is used to clean and mesh the blade. Ansys Workbench Fluent is used to simulate the different speeds of UAV blade, extract the pressure load on the blade surface, and simulate and analyze the carbon fiber composite UAV blades with different layers. The mechanical simulation results of carbon fiber composite UAV blades are obtained. Based on Tsai–Wu failure criterion, the failure coefficient of each layer is calculated, and the optimal carbon fiber layering mode is [0°,90°,90°,90°,0°].

Key words: carbon fiber composite, unmanned aerial vehicle blade, fluid simulation, layer design

CLC Number: 

  • O613.71

Fig.1

Schematic diagram of material direction"

Fig.2

Blade simulation model of unmanned aerial vehicle"

Fig.3

UAV blade grid. (a) Blade grid; (b) Fastener grid"

Tab.1

8 layering methods(°)"

层数 方式1 方式2 方式3 方式4 方式5 方式6 方式7 方式8
第1层 90 0 90 0 90 0 90 0
第2层 90 90 0 0 90 90 0 0
第3层 0 0 0 0 90 90 90 90
第4层 90 90 0 0 90 90 0 0
第5层 90 0 90 0 90 0 90 0

Fig.4

Fluid grid diagram"

Fig.5

Nephogram of downwash airflow velocity at different speeds"

Fig.6

Cloud chart of blade surface pressure at 1 800 r/min. (a) Face of blade; (b) Back of blade; (c) Side of blade"

Fig.7

Partial enlarged drawing of total deformation line chart of blade"

Fig.8

Three\|dimensional diagram of maximum stress of each layer under different layering modes at 1 800 r/min speed"

Fig.9

Three\|dimensional diagram of maximum failure coefficient of each layer under different layering modes at 1 800 r/min speed"

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