The invention provides an aircraft with split type lifting ailerons and four-duct variable-pitch rotors. The aircraft comprises an aircraft body (10), an undercarriage (20), a left wing (30), a rightwing (40), a left power device (50), a right power device (55), an upper power device (60) and a lower power device (65), wherein the left wing (30) and the right wing (40) are arranged on the left side and the right side of the aircraft body (10) respectively; wherein the upper power device (60) and the lower power device (65) are arranged on the aircraft body (10). Compared with other vertical take-off and landing fixed-wing aircrafts, the aircraft has the advantages of simple structure, small resistance, long voyage, large thrust, high aerodynamic efficiency, high safety, low noise and thelike by adopting the split lifting ailerons, ducts and a rotor variable-pitch system and omitting an empennage.
本发明提供了一种具有分裂式升降副翼和四涵道变距旋翼的飞行器,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)、分别安装于左机翼(30)和右机翼(40)延伸端的左动力装置(50)和右动力装置(55)、以及设置于机身(10)上的上动力装置(60)和下动力装置(65)。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、涵道和旋翼变距系统,取消了尾翼,具有结构简单、阻力小、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-duct variable-pitch rotors
一种具有分裂式升降副翼和四涵道变距旋翼的飞行器
2020-05-12
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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