English  |  正體中文  |  简体中文  |  全文筆數/總筆數 : 58323/91876 (63%)
造訪人次 : 14061696      線上人數 : 53
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library & TKU Library IR team.
搜尋範圍 查詢小技巧:
  • 您可在西文檢索詞彙前後加上"雙引號",以獲取較精準的檢索結果
  • 若欲以作者姓名搜尋,建議至進階搜尋限定作者欄位,可獲得較完整資料
  • 進階搜尋
    請使用永久網址來引用或連結此文件: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/116756

    題名: Fabrication of flapping wing mechanism using fused deposition modeling and measurement of aerodynamic forces
    作者: Saravana Kompala;Balasubramanian Esakki;Lung-Jieh Yang;Wei-Chen Wang;Reshmi Waikhom;Chin-Yu Jen
    關鍵詞: flapping wing micro aerial vehicle;fused deposition modeling;injection moulding;wind tunnel;finite element analysis
    日期: 2019-03
    上傳時間: 2019-05-23 12:10:36 (UTC+8)
    出版者: 中華民國航太學會
    摘要: Flapping wing micro aerial vehicles (FWMAVs) are anticipated to play a significant role in futuristic defense and civilian applications. Mechanism design and fabrication of micro mechanisms linkages imposes several challenges for sustainability to withstand cyclic loading conditions. Existing manufacturing methods such as electrical discharge wire cutting (EDWC) and injection moulding (IM) requires much human effort and involve cost penalty. The present work focused on fabrication of micro mechanism linkages using fused deposition modeling (FDM) to obtain functional parts swiftly. Design modifications are performed to improve the strength of Evans mechanism linkages and finite element analysis (FEA) is carried out for static as well as cyclic loading conditions. FEA results suggested that 50% of reduction in stress as compared to IM process. Fabricated parts are assembled and tested for its functionality. Further, the assembled Evans mechanism are parylene coated to reduce the friction among moving parts. Wind tunnel experiments are conducted to determine the lift and thrust forces of 3D printed mechanism. Comparative evaluation between IM and 3D printed mechanism suggested that, the aerodynamic performance is properly maintained due to the improved strength of mechanism by FDM and parylene coating herein. Hence, 3D printing is justified for fabrication of micro mechanism parts with less cost and minimal efforts in comparison to conventional manufacturing processes.
    關聯: Journal of Aeronautics, Astronautics and Aviation 51(1), p.131-140
    DOI: 10.6125/JoAAA.201903_51(1).09
    顯示於類別:[機械與機電工程學系暨研究所] 期刊論文


    檔案 描述 大小格式瀏覽次數
    Fabrication of Flapping Wing Mechanism Using Fused Deposition Modeling and Measurement of Aerodynamic Forces.pdf680KbAdobe PDF0檢視/開啟



    DSpace Software Copyright © 2002-2004  MIT &  Hewlett-Packard  /   Enhanced by   NTU Library & TKU Library IR teams. Copyright ©   - 回饋