The invention discloses a tilt-rotor vertical take-off and landing aircraft and a vertical take-off and landing balance system.The tilt-rotor vertical take-off and landing aircraft and the vertical take-off and landing balance system.The tilt-rotor vertical take-off and landing aircraft comprises an aircraft body, wings are symmetrically arranged on the two sides of the aircraft body, wingtip small wings are arranged at the tail ends of the wings, and the wingtip small wings are arranged on the aircraft body. A pair of tilting mechanisms symmetrically arranged relative to the fuselage is arranged at the front end of the fuselage, each tilting mechanism comprises a front propeller, the front propellers are connected with the fuselage through tilting motor structures, and a micro turbojet engine is arranged at the rear end of the fuselage and connected with the fuselage through a fixing frame. The vertical take-off and landing balance system comprises a hardware part and a software part. Smooth transition between a vertical take-off and landing mode and a horizontal flight mode is achieved through optimized mode switching control logic.
本发明公开了一种倾转旋翼垂直起降飞行器及一种垂直起降平衡系统,属于飞行器领域,一种倾转旋翼垂直起降飞行器及一种垂直起降平衡系统,其中倾转旋翼飞行器包括机身,机身的两侧对称设置有机翼,机翼的末端设置有翼尖小翼,机身上前端设置有一对关于机身对称设置的倾转机构,倾转机构包括前螺旋桨,前螺旋桨通过倾转电机结构与机身连接,机身后端设置有微型涡轮喷气发动机,通过固定架与机身连接。其中垂直起降平衡系统包括硬件部分和软件部分。通过优化的模态切换控制逻辑,实现垂直起降模式和水平飞行模式之间的平滑过渡。
Tilt rotor vertical take-off and landing aircraft and vertical take-off and landing balance system
一种倾转旋翼垂直起降飞行器及一种垂直起降平衡系统
01.04.2025
Patent
Elektronische Ressource
Chinesisch
Electric vertical take-off and landing tilt rotor aircraft
Europäisches Patentamt | 2025
|Tilt-rotor vertical take-off and landing fixed-wing aircraft
Europäisches Patentamt | 2024
|Europäisches Patentamt | 2023
|Europäisches Patentamt | 2024
|Europäisches Patentamt | 2023
|