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  1. 学位論文
  2. 学位論文

ポリマー微細加工によって作成される羽ばたき翼微小飛行体のデザインウィンドウ探索法による開発

https://doi.org/10.18997/00009006
https://doi.org/10.18997/00009006
a4f8a71d-ef0b-4248-b988-8b44403782ab
名前 / ファイル ライセンス アクション
jou_k_369.pdf jou_k_369.pdf (8.0 MB)
アイテムタイプ 学位論文 = Thesis or Dissertation(1)
公開日 2022-11-28
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_db06
資源タイプ doctoral thesis
タイトル
タイトル Development of polymer micromachined flapping-wing nano air vehicle using iterative design window search methodology
言語 en
タイトル
タイトル ポリマー微細加工によって作成される羽ばたき翼微小飛行体のデザインウィンドウ探索法による開発
言語 ja
言語
言語 eng
著者 Rashmi Kant

× Rashmi Kant

en Rashmi Kant

Search repository
抄録
内容記述タイプ Abstract
内容記述 The specific flight mechanisms of insects like hovering and maneuverability along with their tiny size nature grasp the attention of many researchers across the globe to utilize the phenomena for the development of biomimetic flapping wing air vehicles which can be used in the wide areas like hazardous environment exploration, rescue, agriculture, pipeline inspection, and earthquake or tsunami disaster management, etc where human access is difficult. Consequently, many researchers have developed flapping wing air vehicles ranging from macro scale to the nanoscale (the largest dimension should be less than or equal to 10 cm) i.e., flapping-wing nano air vehicles (FWNAVs). The research on insect-inspired FWNAVs indicates that FWNAVs generally consist of micro transmission for getting desired flapping motion, a pair of micro wings, an actuator for the power source, and a supporting frame to support the overall structure. Recently, FWNAVs up to a size of 30 mm have been developed based on the insect’s size. However, the evolution of insects indicates that the size of ultimate small insects is about 1 mm. The further miniaturization of current FWNAVs is difficult because of the large assembly of components and complicated mechanical transmission mechanism. Though, there are mainly two difficulties to successfully developing FWNAVs at the scale of mm-size. The first is the manufacturing difficulty because of the very small structure to realize the wing’s complicated motions. The second is the design difficulty because of multisystem and involvement of coupled Multiphysics like fluid-structure interaction (FSI) design. Along with these difficulties other difficulty includes enough lift to drag ratio for hover and thrust for forwarding flight motion due to fluid mechanics at low Reynolds no (Re < 3000). These difficulties can be overcome by developing FWNAVs based on a design window search methodology where a design solution can be obtained for the design problem satisfying all the design requirements. Further fabricating the FWNAVs using advanced engineering technologies such as microelectromechanical systems (MEMS) technologies which seem to be suitable for mm-size prototypes. Computational analysis and design can be utilized for finding the design window search for FWNAVs. The finite element method (FEM) has been the standard choice as a numerical tool for performing the simulation of Multisystem, because of its capabilities to analyze the geometries of complex shapes, detailed analysis of coupled effect, boundary, and initial conditions. The purpose of this study is to develop 10 mm insect-inspired FWNAV using a 2.5-dimensional structure novel approach, iterative design window search methodology, and polymer micromachining. The proposed FWNAV consists of a micro transmission with a support frame, a micro wing, and a piezoelectric bimorph actuator. The novelty of this research includes, (1) the novel transmission mechanism using two parallel elastic hinges based on geometrically nonlinear bending deformation that produces a large rotational displacement from a small translational displacement, (2) the complete 2.5-D structure which can be fabricated using the polymer micromachining technique without any post-assembly (3) the novel design approach or iterative design window (DW) search method using the advanced computational analysis and design. The advantage of the proposed FWNAV over other FWNAVs includes the lowest energy loss due to no post assembly (friction loss is less), reducing total weight, ease in miniaturization, and enough performance without resonance mechanism. In order to develop the proposed FWNAV, firstly I have designed micro transmissions with a support frame and micro wing and later I have designed FWNAV which has been further miniaturized to design 10mm FWNAV using the iterative DW search method. I have also estimated fatigue life arising due to random cyclic stress, which is mostly ignored by the researchers. Computational flight performance of the proposed FWNAV has been evaluated using Multiphysics coupled analysis i.e., fluid-structure interaction analysis where governing equilibrium equation of motion of micro wing and surrounding airflow has been directly solved by finite element methods. The computational flight performance indicates that mean lift force is comparable to the weight of FWNAV which provides that the proposed FWNAV can lift off. The polymer micromachining has been demonstrated by fabricating the transmission which is a key and central component of FWNAV which indicates the feasibility of polymer micromachining for the development of 10 mm FWNAV. Thus, 10 mm flyable FWNAV can be developed which has enough fatigue life.
言語 en
目次
内容記述タイプ TableOfContents
内容記述 1 General Introduction||2 Proposal of 2.5-dimensional one wing transmission for flapping-wing nano air vehicle||3 Iterative design window search for polymer micromachined flapping-wing nano air vehicle||4 Computational flight performance of flapping wing nano air vehicles using fluid-structure interaction analysis||5 Development of flapping-wing nano air vehicle||6 General Conclusion
備考
内容記述タイプ Other
内容記述 九州工業大学博士学位論文 学位記番号:情工博甲第369号 学位授与年月日:令和4年9月26日
キーワード
主題Scheme Other
主題 Insect inspired design
キーワード
主題Scheme Other
主題 Microfabrication
キーワード
主題Scheme Other
主題 Design window
キーワード
主題Scheme Other
主題 Finite element analysis
キーワード
主題Scheme Other
主題 FSI analysis
キーワード
主題Scheme Other
主題 FWANV
アドバイザー
石原, 大輔
学位授与番号
学位授与番号 甲第369号
学位名
学位名 博士(情報工学)
学位授与年月日
学位授与年月日 2022-09-26
学位授与機関
学位授与機関識別子Scheme kakenhi
学位授与機関識別子 17104
学位授与機関名 九州工業大学
学位授与年度
内容記述タイプ Other
内容記述 令和4年度
出版タイプ
出版タイプ VoR
出版タイプResource http://purl.org/coar/version/c_970fb48d4fbd8a85
アクセス権
アクセス権 open access
アクセス権URI http://purl.org/coar/access_right/c_abf2
ID登録
ID登録 10.18997/00009006
ID登録タイプ JaLC
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