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1. (WO2018145355) VERTICAL TAKE-OFF AND LANDING AIRCRAFT HAVING FIXED WINGS

Pub. No.:    WO/2018/145355    International Application No.:    PCT/CN2017/079204
Publication Date: Fri Aug 17 01:59:59 CEST 2018 International Filing Date: Sun Apr 02 01:59:59 CEST 2017
IPC: B64C 27/26
B64C 29/00
Applicants: SHENZHEN LONGING INNOVATIVE AVIATION TECHNOLOGY CO., LTD.
深圳市龙云创新航空科技有限公司
Inventors: BAO, Jingyun
鲍静云
LIU, Shuang
刘双
FAN, Jinhong
范晋红
YIN, Lanlan
殷兰兰
Title: VERTICAL TAKE-OFF AND LANDING AIRCRAFT HAVING FIXED WINGS
Abstract:
A vertical take-off and landing aircraft having fixed wings, comprising a fuselage (100), wings (210) symmetrically distributed relative to the fuselage (100), and vertical tails (310) vertically connected to the wings (210) and symmetrically distributed relative to the fuselage (100). Rotors (410) are arranged on the wings (210) and the vertical tails (310), and at least the rotors (410) on the vertical tails (310) rotate independently. The aircraft has the advantages of both an aircraft having fixed wings and a helicopter, and may carry out vertical take-off and landing, thus reducing the requirements for a site, and at the same time, the speed, journey and load capacity thereof are greatly improved. In addition, the flight mode is switched by means of the inclination of the whole fuselage (100), so that the aircraft has a low level of technical difficulty, a simple structure, good stability and is simple to operate in comparison to an aircraft having revolving wings.