The invention discloses an aircraft with a multi-rotor arm designed into a foldable fixed wing, which comprises a multi-rotor flight system, a foldable fixed wing flight system, a cabin, a chassis and the like, and the multi-rotor arm and the foldable fixed wing are connected with the cabin; the chassis comprises a rack, a rotor wing flight system and a ground walking system. The top of the aircraft adopts an inflatable low-cost parachute, the bottom of the aircraft adopts an anti-falling safety facility, the wings are provided with anti-collision radars, and the front is provided with a miniature laser ranging radar, so that the aircraft is safe and reliable to use. The structural part is made of the carbon fiber material, so that the weight is light. The retractable folding electric vehicle has the characteristics of reasonable structure, retractable folding, small size, light weight, high controllability, low cost, safety, reliability and high intelligent degree.
本发明公开一种将多旋翼机臂设计成可折叠固定翼的飞行器,包括多旋翼飞行系统、折叠固定翼飞行系统、机舱、底盘等,与机舱连接的既是多旋翼机臂,也是折叠固定翼;底盘包括机架、旋翼飞行系统、地面行走系统。本发明机顶采用充气低成本降落伞,机底采用防坠落安全设施,机翼设有防撞雷达,前方设有微型激光测距雷达,使用安全可靠。本发明结构件采用碳纤维材料,使得重量轻。本发明具有结构合理、可收缩折叠、体积小、重量轻、操控性高、成本低、安全可靠、智能化程度高的特点。
Aircraft with multi-rotor arms designed into foldable fixed wings
一种将多旋翼机臂设计成可折叠固定翼的飞行器
2024-12-13
Patent
Electronic Resource
Chinese