一种可实现任意姿态悬停的多旋翼飞行器
By combining tetrahedral and triangular structural units with six-way connectors and motor mounting brackets, the multi-rotor aircraft can hover in any attitude, solving the hovering angle limitation problem and meeting the needs of all-round observation.
CN116039982BActive Publication Date: 2026-07-17NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
- Filing Date
- 2023-01-10
- Publication Date
- 2026-07-17
AI Technical Summary
Technical Problem
Existing multi-rotor drones have limited hovering angles, which cannot meet the needs of all-round observation in special environments.
Method used
It adopts a combination of a regular tetrahedral structural frame and a three-sided structural unit, combined with a six-way connector and a motor mounting bracket. The motor works with the propeller to generate multi-directional thrust, enabling hovering in any posture.
Benefits of technology
It enables multi-rotor aircraft to hover at any angle, meeting the needs of all-round observation in special environments and improving work efficiency and safety.
✦ Generated by Eureka AI based on patent content.
Smart Images
Figure CN116039982B_ABST
Abstract
本发明公开了一种可实现任意姿态悬停的多旋翼飞行器，属于飞行器结构设计领域，本发明飞行器整体由碳纤维管和打印件组成，相邻碳管用3D打印件进行连接和加固，以上顶点为基准点观察，中心部位为正四面体，沿四面体框架的法向延伸出三边结构单元，共延伸出六个三边结构单元与四面体框架进行组合，使整体呈中心对称，能够解决普通多旋翼无人机无法任意角度悬停的问题。
Need to check novelty before this filing date? Find Prior Art