The invention provides an aircraft with split type lifting ailerons and double-duct variable-pitch 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 a left power device (50) and a right power device (60) which are mounted at the extending ends of the left wing (30) and the right wing (40) correspondingly. The left wing (30) is further provided with a left steering engine group (71) and a left split type lifting aileron (70) driven by the left steering engine group (71), and the right wing (40) is provided with a right steering engine group (81) and a right split type lifting aileron (80) driven by the right steering engine group (81). Compared with other vertical take-off and landing fixed-wing aircrafts with double rotors, the aircraft adopts the split type lifting ailerons, the ducts and the rotor variable-pitch systems, and has the advantages of simple structure, small resistance, large thrust, high aerodynamic efficiency, high safety and the like.
本发明提供了一种具有分裂式升降副翼和双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)、以及分别安装于左机翼(30)和右机翼(40)延伸端的左动力装置(50)和右动力装置(60);所述左机翼(30)上还设有左舵机组(71)、以及通过左舵机组(71)驱动的左分裂式升降副翼(70),所述右机翼(40)上设有右舵机组(81)、以及通过右舵机组(81)驱动的右分裂式升降副翼(80)。相较于其他双旋翼的可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,具有结构简单、阻力小、推力大、气动效率高以及安全性高等优点。
Aircraft with split type lifting ailerons and double-duct variable-pitch rotors
一种具有分裂式升降副翼和双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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