Zhejiang Geely Holding Group Co., Ltd

Sichuan Aerofugia Technology Development Co., Ltd

Yongxiang Sha

Liang Guo

Songbai Xue

Zhaohua Xu

Fan Xiang

Yi Tian

Junchang Luo

Qiang Tu

Shaiming Xie

A vertical take-off and landing aircraft includes a fuselage, 2N tilting rotors, and 2N fixed rotors. Wings of a fixed-wing structure are arranged on two sides of the fuselage. An empennage is arranged at a tail of the fuselage. The 2N tilting rotors are symmetrically installed on two sides of the fuselage and located on the front and rear sides of the wings respectively. The 2N fixed rotors are symmetrically installed on the wings on both sides of the fuselage, located on the front and rear sides of the wings respectively and on the outer sides of the tilting rotors. N is a natural number greater than or equal to 2. In a vertical take-off and landing configuration, projections of all the tilting rotors and all the fixed rotors on a horizontal plane are approximately centrally symmetrical about the center of gravity of the aircraft.

Vertical take-off and landing aircraft and control method of vertical take-off and landing aircraft

Aerial vehicle

Growing community of inventors

Chengdu, China

Yongxiang Sha