The invention provides a microminiature high-speed coaxial composite aircraft and a control method thereof. The aircraft comprises a fuselage shell, a coaxial motor rotor group, an undercarriage, a front lift augmentation stub wing, a tilting double-rotor group and a full-motion control surface. The fuselage shell adopts a streamline design, so that the air resistance during high-speed forward flight can be reduced; the coaxial motor rotor group is mounted at the top of the fuselage, the undercarriage is mounted at the bottom of a fuselage shell, the front lift-augmentation stub wing is mounted at the front part of the fuselage, the tilting double rotors are mounted at the rear part of the fuselage, the tilting motor transmission system is fixed at the rear part of a middle-layer carbon fiber plate of the fuselage, and the full-motion control surfaces are mounted on two sides of the fuselage. The microminiature high-speed coaxial composite aircraft adopts a composite structure of coaxial double rotors and tilting double rotors, so that the microminiature high-speed coaxial composite aircraft has the advantages of a rotor aircraft and a fixed-wing aircraft, and has three flight modes of a rotor mode, a transition mode and a forward flight mode, so that the aircraft can meet two task requirements of high-speed forward flight and vertical take-off and landing.
本发明提供了一种微小型高速共轴式复合飞行器及其控制方法,飞行器包括机身外壳、共轴电机旋翼组、起落架、前置增升短翼、倾转双旋翼组、全动舵面。机身外壳采用流线型设计,可降低高速前飞时的空气阻力;共轴电机旋翼组安装于机身顶部,起落架安装于机身外壳底部,前置增升短翼安装于机身前部,倾转双旋翼安装于机身后部,倾转电机传动系统固定于机身中层碳纤维板后部,全动舵面安装于机身两侧。本发明微小型高速共轴式复合飞行器采用共轴双旋翼及倾转双旋翼的复合式结构,使其具备旋翼飞行器和固定翼飞行器的优点,并具有旋翼模式、过渡模式、前飞模式三种飞行模式:使飞行器可满足大速度前飞和垂直起降两种任务要求。
Micro-miniature high-speed coaxial composite aircraft and control method thereof
微小型高速共轴式复合飞行器及其控制方法
2024-04-12
Patent
Electronic Resource
Chinese
IPC: | B64U |
Composite high-speed aircraft and control method thereof
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