The invention discloses a vertical take-off and landing unmanned aerial vehicle. A platform is arranged on the support, a machine body is arranged on the platform, a first electric cylinder and a second electric cylinder are hinged to one side of the support, one end of the first electric cylinder and one end of the second electric cylinder are hinged to one side of the platform, and the first electric cylinder and the second electric cylinder are designed to be triangular. A third electric cylinder and a fourth electric cylinder are hinged to one side of the support, one end of the third electric cylinder and one end of the fourth electric cylinder are also hinged to one side of the platform, and the third electric cylinder and the fourth electric cylinder are in a triangular design; a fifth electric cylinder and a sixth electric cylinder are hinged to one side of the support, one end of the fifth electric cylinder and one end of the sixth electric cylinder are also hinged to one side of the platform, the fifth electric cylinder and the sixth electric cylinder are in triangular design, and accurate movement butt joint of the tail section is achieved through six-degree-of-freedom high-precision multi-degree-of-freedom mechanical parts.
一种垂直起降无人机,包括;支架,所述支架上设有平台,所述平台上设有机体,其中所述支架一侧铰接有第一电缸以及第二电缸,所述第一电缸以及第二电缸一端亦铰接在所述平台一侧上,所述第一电缸以及第二电缸之间呈三角形设计;所述支架一侧铰接有第三电缸以及第四电缸,所述第三电缸以及第四电缸一端亦铰接在所述平台一侧上,所述第三电缸以及第四电缸之间呈三角形设计;所述支架一侧铰接有第五电缸以及第六电缸,所述第五电缸以及第六电缸一端亦铰接在所述平台一侧上,所述第五电缸以及第六电缸之间呈三角形设计,通过六自由度这些高精度多自由度机械部件实现末段的精确运动对接。
Vertical take-off and landing unmanned aerial vehicle
一种垂直起降无人机
2025-02-11
Patent
Electronic Resource
Chinese
IPC: | B64U |