[1]吴 斌,荣海春,王呈顺,等.某无人机载雷达挂架结构设计[J].机械与电子,2019,(12):26-29.
 ,,et al.Structure Design of the Bracket Used in an Unmanned Aerial Vehicle Carried Radar[J].Machinery & Electronics,2019,(12):26-29.
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某无人机载雷达挂架结构设计()
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机械与电子[ISSN:1001-2257/CN:52-1052/TH]

卷:
期数:
2019年12期
页码:
26-29
栏目:
设计与研究
出版日期:
2019-12-24

文章信息/Info

Title:
Structure Design of the Bracket Used in an Unmanned Aerial Vehicle Carried Radar
文章编号:
1001- 2257(2019)12- 0026- 04
作者:
吴 斌荣海春王呈顺许 军
中国电子科技集团公司第三十八研究所,安徽 合肥 230088
Author(s):
WUBinRONGHaichunWANGChengshunXUJun
No.38ResearchInstituteofCETC,Hefei230088,China
关键词:
无人机挂架仿真分析
Keywords:
unmannedaerialvehiclebracketsimulationanalysis
分类号:
TN957.8
文献标志码:
A
摘要:
针对某无人机载雷达挂架结构的技术特点,开展了结构技术研究和实践工作,包括该挂架的结 构形式、材料选择、工艺设计、表面处理和仿真分析等。为验证挂架的承载能力是否满足机载雷达的技术指标要求,基于有限元软件对其结构进行了有限元分析,计算了系统平飞状态和降落状态时挂架的刚强度以及机载雷达的倾斜角度。计算结果显示刚度和强度均满足使用要求。此外,实际应用显示,该挂架的使用稳定可靠,安装工艺简单、运输方便,达到了设计目标。
Abstract:
In view of the technical characteristics of the bracket of unmanned aerial vehicle radar, systematic research and practice were carried out, including structural style and material selection, process design, surface treatment, simulation analysis. To test the carrying capacity of the bracket, the finite element model was established based on FEM software. The corresponding mechanical response date of deformation and stress, the angle of inclination of radar, were obtained, which is in level flight state or landing state. The results show that the structure design of this bracket satisfies the requirements. Besides,the feedback from experimenters and users shows that the bracket runs steadily and reliably, and is easy embedded with high carrying performance.

参考文献/References:

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备注/Memo

备注/Memo:
收稿日期:2019- 08- 14
作者简介:吴 斌 (1983-),男,安徽亳州人,高级工程师,主要从事传感器飞行器结构设计工作。
更新日期/Last Update: 2019-12-23