| Center section wing for i.e. unmanned aircraft, has fastening elements on front wall formed as wedge-shaped elements protruding from front wall by amount of electrical system connector to be greater than that of front wall | |
| 2024-10-03 | |
| 专利权人 | UNIV INNOPOLIS AUTONOMOUS NON-COMML ORG (UYIN-Non-standard) |
| 申请日期 | 2024-10-03 |
| 专利号 | RU231111-U1 |
| 成果简介 | NOVELTY - The wing (3) has a spar formed as a longitudinal box-type load-bearing element and attached to ribs forming a shape of an aerodynamic profile, where the ribs are attached to a rear wall. A skin is attached to the spar, the ribs and the rear wall. A front wall is attached to two central ribs in a forward part of a center section up to the spar, where a space is formed in the forward part of the center section between the front wall and the central ribs. An electrical system connector is attached to the front wall intended for connection with a mating electrical system connector located on a fuselage (2), where the front wall comprises fastening elements for connection to mating fastening elements on the fuselage by an insertion process. The fastening elements on the front wall are formed as wedge-shaped elements protruding from the front wall by amount of the electrical system connector to be greater than that of the front wall. USE - Center section wing for an unmanned aerial vehicle i.e. unmanned aircraft. ADVANTAGE - The wing is light in weight and simple to assemble, and provides increased stability and strength of the spar by a multilayer structure along entire length of a center section and ensures a reliable connection with main elements of an UAV structure, and has high durability. The wing increases safety performance of center section elements during transportation and assembly and design protection and design reliability and avoids need to pay increased attention to connectors and orientation of the center section. DESCRIPTION OF DRAWING(S) - The drawing shows a top perspective view of an unmanned aerial vehicle. 1UAV 2Fuselage 3Center section wing 4Center section 5, 6Consoles 7, 8Beams 9Stabilizer 10Cruise engine 11-14Electric motors 15Chassis |
| IPC 分类号 | B64C-001/26 ; 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/14960 |
| 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,RASSYPNOV M S,et al. Center section wing for i.e. unmanned aircraft, has fastening elements on front wall formed as wedge-shaped elements protruding from front wall by amount of electrical system connector to be greater than that of front wall. RU231111-U1[P]. 2024. |
| 条目包含的文件 | 条目无相关文件。 | |||||
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