The double-wing take-off and landing aircraft comprises an aircraft body, aircraft front wings are arranged on the left side and the right side of the front end of the aircraft body, a power unit is formed by combining 16 ducted fans and a battery, and six single ducted fans are arranged on the aircraft front wings. And 10 single ducted fans are arranged on the rear wing of the aircraft in a bilateral symmetry manner. According to the vertical take-off and landing aircraft with the ducted fans and the tilting wings, the efficiency of the fans is improved, the safety and the attractiveness are improved due to the fact that the fans are not exposed, the front wings are lower than the rear wings, the influence of downwash airflow of the front wings on the rear wings is reduced, and the redundant design of the power system ensures that power supply of the motors cannot be influenced when any battery goes wrong; the control surface and the multifunctional control surface on the rear edge of the ducted fan enable the aircraft to have good maneuvering characteristics.
本发明公开了一种配置涵道风扇的双机翼起降飞机,包括飞机机身,所述飞机机身前端的左右两侧均设置有飞机前翼,所述动力单元由16个涵道风扇以及电池组合而成,且涵道风扇其中6个单体设置在飞机前翼上,并且涵道风扇其中10个单体设置在飞机后翼上,呈左右对称布置。该涵道风扇倾转翼垂直起降飞机,增大了风扇的效率,并且没有裸露的风扇提高了安全性和美观性,前翼的高度低于后翼,减小了前翼下洗气流对后翼的影响,动力系统的冗余设计保证任一个电池出问题不会影响到电机的供电,涵道风扇后缘的舵面和多功能控制面,使飞机具有良好的机动性能。
Double-wing take-off and landing aircraft provided with ducted fans
一种配置涵道风扇的双机翼起降飞机
01.10.2024
Patent
Elektronische Ressource
Chinesisch
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