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毫米级静电微扑翼驱动器的结构设计、工艺与测试 被引量:2

Structure design,fabrication and testing of millimeter-scale electrostatic micro flapping-wing actuator
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摘要 针对仿昆虫扑翼飞行器核心动力装置——微驱动器的结构特点和研究难点,设计了一种基于静电驱动原理的毫米(mm)级微扑翼驱动器,并针对各个部件研究了整套加工工艺与测试方法。运动优化与升力测试结果表明:微扑翼驱动器(翼展9 mm,重量3 mg)以91 Hz的频率实现了±40°的拍动和±25°的扭转运动,输出1.5 mg的升力,升重较以往静电微扑翼驱动器有大幅提升。研究成果为实现仿昆虫微型飞行器的自主飞行提供了新的方向,并奠定了理论与试验基础。 Insect-inspired flapping-wing micro air vehicles(FMAV) are small in size and with high maneuver.Aiming at problems of structure characteristic and research difficulties of micro actuator,core power device of FMAV,a millimeter-scale electrostatic micro flapping-wing actuator based on electrostatic-actuated principle is designed. Moreover,a series of fabrication and testing methods are also developed. The result of testing shows that the 9 mm in wing span and 3 mg in weight stroke frequency of actuator is 91 Hz,flapping angle is ± 40°,rotating angle is ± 25°and lift force is 1. 5 mg. Lift-to-weight ratio is highly increased compared to previous results. These achievements lead to a new way to realize liftoff of FMAV and lay the foundation for theory and experiment.
作者 杨艺 车云龙
出处 《传感器与微系统》 CSCD 2018年第1期91-95,共5页 Transducer and Microsystem Technologies
基金 国家自然科学基金资助项目(11602010)
关键词 微型飞行器 微机电系统 微驱动器 静电驱动 micro air vehicle (MAV) micro-electro-mechanical systems (MEMS) micro actuator electrostaticactuator
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  • 1James M M, Michael S F. Micro air vehicles-toward a new dimension in flight[ R]. US DARPA/TTO Report,1997.
  • 2Ashley S. Palm-size spy planes[J]. ASME J Mech Eng,1998(120) : 74-78.
  • 3Wilson J R. Mini technologies for major impact[ J]. Aerospace America, 1998 (36) :36.
  • 4Grasmeyer J M, Keennon M T. Development of the black widow micro air vehicle[ R]. AIAA Paper,2001.
  • 5Wilson T J. MicroSAR meets MAV [ J]. Aerospace America, 1999 (38) :32 -35.
  • 6Morris S J, Holden M. Design of micro air vehicles and flight test validation[ C ]//Proceedings of the Conference: Fixed, Flapping and Rotary Wing Vehicles at Very low Reynolds Numbers. University of Notre Dame,2000:53-176.
  • 7Bret S, Mujahid A. Design and optimization of morphing mechanisms for highly flexible micro air vehicles [ R ]. AIAA Paper, 2006.
  • 8Hewish M. A bird in the hand-miniature and micro air vehicles challenges conventional thinking [ J ]. Jane ' s International Defense Review, 1999,32 ( 11 ) :22-25
  • 9Miki N, Shimoyama I. A micro-flight mechanism with rotational wings [ C ]//Proceedings of the IEEE MEMS,2000 : 155 - 163.
  • 10George R H. Multidisciplinary design and prototype development of a micro air vehicle[ J]. J of Aircraft,1999,36( 1 ) :227 -234.

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