The invention provides an aircraft with split type lifting ailerons and four-duct rotors. The aircraft comprises an aircraft body (10), an undercarriage (20), a left wing (30) and a right wing (40) which are arranged on the left side and the right side of the aircraft body (10) correspondingly, and an upper duct power device (60) and a lower duct power device (65) which are arranged on the aircraft body (10) correspondingly. The left wing (30) and the right wing (40) are consistent in structure, and the extending end of the left wing (30) and the extending end of the right wing (40) are provided with a left duct power device (50) and a right duct power device (55) respectively. And the upper duct power device (60) and the lower duct power device (65) are symmetrically arranged relative tothe machine body (10). Compared with other vertical take-off and landing fixed-wing aircrafts, the aircraft adopts the split type lifting ailerons and the ducts, and has the advantages of simple structure, long voyage, large thrust, high aerodynamic efficiency, high safety, low noise and the like.
本发明提供了一种具有分裂式升降副翼和四涵道旋翼的飞行器,包括机身(10)、起落架(20)、分别设置于机身(10)左右两侧的左机翼(30)和右机翼(40)、以及分别设于机身(10)上的上涵道动力装置(60)和下涵道动力装置(65);所述左机翼(30)与右机翼(40)的结构一致,且所述左机翼(30)与右机翼(40)的延伸端分别设有左涵道动力装置(50)和右涵道动力装置(55);所述上涵道动力装置(60)与下涵道动力装置(65)以机身(10)对称设置。相较于其他垂直起降固定翼飞行器,本发明采用了分裂式升降副翼和涵道,具有结构简单、航程远、推力大、气动效率高、安全性高以及噪声小等优点。
Aircraft with split type lifting ailerons and four ducted rotors
一种具有分裂式升降副翼和四涵道旋翼的飞行器
2020-05-12
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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