| Unmanned aerial vehicle and method of its assembly has fuselage, wing attached to fuselage | |
| 2024-06-06 | |
| 专利权人 | UNIV INNOPOLIS AUTONOMOUS NON-COMML ORG (UYIN-Non-standard) |
| 申请日期 | 2024-06-06 |
| 专利号 | RU2830724-C1 |
| 成果简介 | NOVELTY - Invention relates to aircraft engineering, particularly, to collapsible unmanned aerial vehicle. Unmanned aerial vehicle comprises fuselage, wing attached to fuselage and containing centre section and cantilevers attached to it along edges, beams connected by their central part to centre section and stabilizer attached along edges to rear parts of beams. At that, upper part of fuselage and central parts of beams contain recesses repeating shape of centre section. Beams are identical and contain in the rear part the keel and under it the recess repeating the shape of the stabilizer. At that, electric motors are installed on beams in front part and in area between wing and stabilizer, and sockets for electric motors are made with possibility to change angle of electric motor fixation relative to normal in transverse plane. Group of inventions also relates to a method for assembling such an unmanned aerial vehicle. USE - Aviation. ADVANTAGE - Simplification and acceleration of assembly/disassembly and transportation of UAV, as well as increase in reliability and safety of collapsible UAV. 10 cl, 4 dwg |
| IPC 分类号 | B64C-001/00 ; B64U-020/50 |
| 国家 | 俄罗斯 |
| 专业领域 | 信息技术 |
| 语种 | 英语 |
| 成果类型 | 专利 |
| 文献类型 | 科技成果 |
| 条目标识符 | http://119.78.100.226:8889/handle/3KE4DYBR/16388 |
| 专题 | 中国科学院新疆生态与地理研究所 |
| 作者单位 | UNIV INNOPOLIS AUTONOMOUS NON-COMML ORG (UYIN-Non-standard) |
| 推荐引用方式 GB/T 7714 | DEVITT D V,BURDINOV K A,ZHITNIKOV A A,et al. Unmanned aerial vehicle and method of its assembly has fuselage, wing attached to fuselage. RU2830724-C1[P]. 2024. |
| 条目包含的文件 | 条目无相关文件。 | |||||
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