某高速无人机机翼结构设计与气动弹性分析  

Structural Design and Aerodynamic Analysis of Wing for High Speed UAVs

作　　者：冯正建 胡琦 李欣 刘其琛 刘张君 王昆 FENG Zhengjian;HU Qi;LI Xin;LIU Qichen;LIU Zhangjun;WANG Kun(Aerospace Times Feihong Technology Company Limited,Beijing 100094,China)

机构地区：[1]航天时代飞鸿技术有限公司,北京100094

出　　处：《机械制造与自动化》2025年第1期192-196,共5页Machine Building & Automation

摘　　要：针对某型高速无人机的结构设计要求,设计一种相对厚度小、承载能力强的双梁式复合材料机翼。在Hyperworks中建立机翼的有限元模型,采用最大应变准则和Von-Mises准则对机翼的复合材料结构和金属结构进行强度校核,结果表明位移与应变均在允许范围之内。对机翼进行气动弹性分析表明机翼结构满足气动弹性的要求。通过静力试验结果表明机翼结构满足强度和刚度的要求。In order to meet the structural design requirements of a high-speed UAV,a double-beam composite wing with relatively small thickness and high-bearing composite wing is designed.The finite element model of the designed wing is established in Hyperworks software.The strength analysis of metal and composite structure is carried out using Von-Mises criterion and Maximum strain criterion.The results indicate that the displacement and strain are within the allowable range.The aerodynamic analysis of the wing shows that the structure of the wing meets the requirements of aeroelasticity.And the static test verifies that the structure of the wing meets the strength and stiffess as required.

关 键 词：无人机 复合材料 机翼 结构设计 气动弹性 

分 类 号：V214.1[航空宇航科学与技术—航空宇航推进理论与工程]