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一类扑翼机的设计及静动态性能分析

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本文指出仿生扑翼机具有独特的仿生学原理和出众的机动性,一直是飞行器领域的研究热点.为了研究仿生扑翼飞行器机构之间的配合关系,提高飞行器的稳定性,本文在传统曲柄摇杆机构的基础上,研究并制作了一种以空间RSSR机构为驱动机构的仿鸟型扑翼机.对传动机构和扑翼机构的配合情况进行了分析对比;基于翼展的静力学特性分析,验证了机构间配合状况良好且扑翼所选材料满足强度条件.对整体模型进行了模态仿真分析,研究传动机构对扑翼机构运动特性的影响;通过流体仿真分析,得到了两种扑动模式下的气动力特性,验证了该扑翼飞行器的可行性.
Design and Static-Dynamic Performance Analysis of a Type of Flapping-wing Aircraft
This paper points out that the biomimetic flapping-wing aircraft,with its unique biomimetic principles and outstanding maneuverability,has always been a research hotspot in the field of aircraft.In order to study the coordination between the mechanisms of biomimetic flapping-wing aircraft and improve the stability of the aircraft,based on the traditional crank-rocker mechanism,this paper studies and develops a bird-like flapping-wing aircraft driven by a spatial RSSR mechanism.The coordination between the transmission mechanism and the flapping mechanism is analyzed and compared;based on the aerodynamic characteristics of the wingspan,the good coordination between the mechanisms and the strength conditions of the selected flapping materials are verified.Modal simulation analysis of the overall model is conducted to study the influence of the transmission mechanism on the motion characteristics of the flapping mechanism;through fluid simulation analysis,the aerodynamic characteristics of the two flapping modes are obtained,verifying the feasibility of the flapping-wing aircraft.

flapping-wing aircraftmechanical designmodal analysisfluid simulation

孟宪飞、冯晶晶、闫天府、程欣宇、王娟、李国民

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天津理工大学天津市先进机电系统设计与智能控制重点实验室,天津 300384

天津理工大学机电工程国家级实验教学示范中心,天津 300384

扑翼飞行器 机械设计 模态分析 流体仿真

2024

科技创新与生产力
太原科技战略研究院

科技创新与生产力

影响因子:0.271
ISSN:1674-9146
年,卷(期):2024.45(12)