The invention discloses an electric vertical take-off and landing tandem wing aircraft with full-tilt wings, and the aircraft comprises a fuselage which is provided with a fuselage head part and a fuselage tail part; the two first wings are installed at the end, close to the aircraft head part, of the aircraft body through first tilting mechanisms correspondingly, the two first wings are symmetrically arranged on the two sides of the aircraft body, and a plurality of first rotor assemblies are arranged on each first wing at intervals; and the two second wings are arranged at the end, close to the aircraft tail part, of the aircraft body through second tilting mechanisms correspondingly, the two second wings are symmetrically arranged on the two sides of the aircraft body, and a plurality of second rotor assemblies are arranged on each second wing at intervals. According to the invention, the wings are separately driven by the tilting mechanisms, each wing is provided with a plurality of rotor assemblies, and tilting of the wings and the rotors can be realized by adopting four sets of tilting mechanisms, so that the production and manufacturing cost is reduced, and the safety redundancy is improved.
本发明公开了一种带全倾转机翼的电动垂直起降串列翼飞行器,该飞行器包括:机身,所述机身具有机头部和机尾部;两个第一机翼,分别通过第一倾转机构装设于所述机身靠近所述机头部的一端,两个所述第一机翼对称设置于所述机身的两侧,每个所述第一机翼上间隔设置有若干个第一旋翼组件;两个第二机翼,分别通过第二倾转机构装设于所述机身靠近所述机尾部的一端,两个所述第二机翼对称设置于所述机身的两侧,每个所述第二机翼上间隔设置有若干个第二旋翼组件。本发明中,机翼分别由倾转机构单独驱动,而每个机翼机翼上又设置有多个旋翼组件,采用四套倾转机构就可以实现机翼和旋翼的倾转,降低了生产制造成本,提高了安全冗余。
Electric vertical take-off and landing tandem wing aircraft with full tilt wings
一种带全倾转机翼的电动垂直起降串列翼飞行器
2024-10-15
Patent
Electronic Resource
Chinese
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