The invention provides an aircraft with split type lifting ailerons and single-duct variable-pitch rotors. The aircraft comprises an aircraft body, an undercarriage connected to the aircraft body, a left wing and a right wing which are arranged on the left side and the right side of the aircraft body correspondingly, and a power device installed on the rear portion of the aircraft body. A left split type lifting aileron is further arranged on the left wing, and a right split type lifting aileron is arranged on the right wing; the left wing is further provided with a left steering engine set, and the right wing is further provided with a right steering engine set. The power device comprises a duct, a variable-pitch mechanism, a rotor wing and a rotating motor. 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 type lifting ailerons, the duct and a rotor wing variable-pitch systems and omitting empennages.
本发明提供了一种具有分裂式升降副翼和单涵道变距旋翼的飞行器,包括机身、连接于机身上的起落架、分别设置于机身左右两侧的左机翼和右机翼、以及安装于机身后部的动力装置;所述左机翼上还设有左分裂式升降副翼,所述右机翼上设有右分裂式升降副翼;所述左机翼还设有左舵机组,所述右机翼还设有右舵机组;所述动力装置包括涵道、变距机构、旋翼以及旋转电机。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 single-duct variable-pitch rotors
一种具有分裂式升降副翼和单涵道变距旋翼的飞行器
2020-05-12
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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