The invention belongs to the technical field of shape design and control of aircrafts, and relates to an electric tilt-rotor aircraft. Comprising a fuselage, two wings located on the two sides of the fuselage, an empennage, a plurality of supporting rods arranged below the wings and rotors arranged at the two ends of the supporting rods. The rotor wings comprise a plurality of tilting rotor wings and a plurality of fixed rotor wings; the number of the supporting rods is even, and the supporting rods are divided into two sets with the same number and are symmetrically arranged on the two sides of the machine body. A tilting rotor wing is arranged at the front end of each supporting rod; a fixed rotor wing is arranged at the rear end of each supporting rod; the tilting rotor wings are connected with the front ends of the supporting rods through tilting mechanisms, and the tilting mechanisms are used for adjusting the orientation of the tilting rotor wings. The electric tilt rotor aircraft provided by the invention can realize the functions of vertical take-off and landing, tilt transition and cruise flight.
本发明属于飞行器外形设计与控制技术领域,涉及一种电动倾转旋翼飞行器。包括:机身、位于机身两侧的两个机翼、尾翼、设置在机翼下方的若干个撑杆、设置在撑杆两端的旋翼;所述旋翼包括若干个倾转旋翼和若干个固定旋翼;所述撑杆的数量为偶数,分成数量相同的两组对称设置在机身的两侧;在每个所述撑杆的前端设置一个倾转旋翼;在每个所述撑杆的后端设置一个固定旋翼;所述倾转旋翼通过倾转机构和所述撑杆的前端连接,所述倾转机构用于实现所述倾转旋翼的朝向的调节。本发明提供的电动倾转旋翼飞行器,可以实现垂起起降,倾转过渡与巡航飞行的功能。
Electric tilt rotor aircraft
一种电动倾转旋翼飞行器
29.04.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |