首页> 外文会议>1997 ASME design engineering technical conferences (DETC'97) >SELF-EXCITED VIBRATION MODEL OF DRAGONFLY’S WING BASED ON THE CONCEPT OF BIONIC DESIGN FOR SMALL- OR MICRO-SIZED ACTUATORS
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SELF-EXCITED VIBRATION MODEL OF DRAGONFLY’S WING BASED ON THE CONCEPT OF BIONIC DESIGN FOR SMALL- OR MICRO-SIZED ACTUATORS

机译:基于仿生设计的小型或微型执行机构的德拉贡机翼自激振动模型

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This paper describes a self-excited vibration model ofrndragonfly's wing based on the concept of bionic design, which isrnexpected as a technological hint to solve the scale effectrnproblems in developing the small- or micro-sized actuators.rnFrom a morphological consideration of flight muscle ofrndragonfly, the nonlinear equation of motion for the wingrnconsidering the air drag force due to flapping of wing isrnformulated. In the model, the dry friction-type and Van der Poltyperndriving forces are employed to power the flight muscles andrnto generate the stable self-excited wing vibration. Two typicalrnJapanese dragonflies, “Anotogaster sieboldii Selys” andrn“Sympetrum frequens Selys”, are selected as examples, and thernself-excited vibration analyses for these dragonfly's wings arerndemonstrated. The linearized solutions for the nonlinearrnequation of motion are compared with the nonlinear solutions,rnand the vibration system parameters to generate the stable limitrncycle of self-excited wing vibration are determined.
机译:本文基于仿生设计的概念,描述了蜻蜓翅膀的自激振动模型,该模型有望作为解决开发小型或微型执行器时出现尺度效应问题的技术提示。rn从蜻蜓飞行肌肉的形态学考虑,考虑到由于机翼拍打而产生的空气阻力,机翼的非线性运动方程式被公式化。在模型中,干摩擦力和范德波型驱动力被用来驱动飞行肌肉并产生稳定的自激机翼振动。以两种典型的日本蜻蜓为例,分别以“ Anotogaster sieboldii Selys”和“ Sympetrum frequens Selys”为例,并对这些蜻蜓的翅膀进行了自激振动分析。将非线性运动方程的线性化解与非线性解进行比较,确定振动系统参数以产生稳定的自激机翼振动极限周期。

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