Development of an active wing for flight machines using macro fiber composites

被引：0
|
作者：
Ha, Kil seong [1 ]
Huang, Ya-Wen [1 ]
Nagata, Yoshinori [1 ]
Ming, Aiguo [1 ]
机构：
[1] Univ Electrocommun, Dept Mech Engn & Intelligent Syst, 1-5-1 Chofugaoka, Chofu, Tokyo 1828585, Japan
来源：
IEEE ICMA 2006: PROCEEDING OF THE 2006 IEEE INTERNATIONAL CONFERENCE ON MECHATRONICS AND AUTOMATION, VOLS 1-3, PROCEEDINGS | 2006年
关键词：
flight machine; active wing; macro fiber composites; flapping; feathering;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Macro Fiber Composites (MFC) is a new type of piezoelectric material with softness and big displacement, developed by NASA recently. It can be used for actuating, sensing and power generating. The purpose of our work is to develop a new and intelligent flight machine by utilizing the features of the MFC. In this paper, the concept of such flight machine and the driving method of a MFC-combined structure are proposed. The feasibility of flight by using the MFC-combined structure is discussed by simulations. Based on the simulation results, an active wing capable of flapping and feathering motions has been developed. The elementary performance of the wing is investigated by an aerodynamics experiment.
引用
收藏
页码：261 / +
页数：2
相关论文
共 50 条
  • [41] Piezoelectrically strained bistable laminates with macro fiber composites
    Lee, Andrew J.
    Moosavian, Amin
    Inman, Daniel J.
    ACTIVE AND PASSIVE SMART STRUCTURES AND INTEGRATED SYSTEMS 2017, 2017, 10164
  • [42] Characterizing the pyroelectric coefficient for macro-fiber composites
    Acosta, Krystal L.
    Wilkie, William K.
    Inman, Daniel J.
    SMART MATERIALS AND STRUCTURES, 2018, 27 (11)
  • [43] Mixing Rules for the Piezoelectric Properties of Macro Fiber Composites
    Deraemaeker, A.
    Nasser, H.
    Benjeddou, A.
    Preumont, A.
    JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2009, 20 (12) : 1475 - 1482
  • [44] Active Flow Vector Flight Control Using Only SJAs for a Fixed-Wing UAV
    Li, Chunzhi
    Shen, Jianhua
    Zhai, Sheng
    Wang, Chengcai
    Yang, Jianying
    IEEE ACCESS, 2018, 6 : 76535 - 76545
  • [45] Morphing wing flexible skins with curvilinear fiber composites
    Murugan, Senthil
    Friswell, M. I.
    COMPOSITE STRUCTURES, 2013, 99 : 69 - 75
  • [46] Development of active composites using conventional structural materials
    Asanuma, H
    Haga, O
    Hakoda, G
    Ohira, J
    SMART MATERIALS, 2001, 4234 : 64 - 69
  • [47] Analytical development of single crystal Macro Fiber Composite actuators for active twist rotor blades
    Park, JS
    Kim, JH
    SMART MATERIALS & STRUCTURES, 2005, 14 (04): : 745 - 753
  • [48] Development of a Flight Dynamics Model for Fixed Wing Aircraft
    Nguyen Tien Dat
    Tran Ngoc Son
    Duong Anh Tra
    PROCEEDINGS OF THE 10TH INTERNATIONAL CONFERENCE ON COMPUTER MODELING AND SIMULATION (ICCMS 2018), 2017, : 202 - 205
  • [49] Fiber Material and Electrode Configuration Selection in Designing Piezoelectric Macro Fiber Composites
    Mallouli, Marwa
    Chouchane, Mnaouar
    DESIGN AND MODELING OF MECHANICAL SYSTEMS-VI, VOL 1, CMSM 2023, 2024, : 291 - 303
  • [50] Wind tunnel tests for a flapping wing model with a changeable camber using macro-fiber composite actuators
    Kim, Dae-Kwan
    Han, Jae-Hung
    Kwon, Ki-Jung
    SMART MATERIALS AND STRUCTURES, 2009, 18 (02)
12345