The invention provides an aircraft with split type lifting ailerons and single ducted rotors. The aircraft comprises an aircraft body (10), undercarriages (20), a left wing (30), a right wing (40) anda ducted power device (50), 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, and the ducted power device (50) is installed behind the aircraft body. More than two undercarriages (20) are respectively arranged on the aircraft body (10), the left wing (30) and the right wing (40); the left wing (30) and the right wing (40) are symmetrically arranged relative to the aircraft body (10); and the duct power device (50) is connected with the undercarriage (20) arranged on the aircraft body (10). Compared withother 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, highaerodynamic 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单涵道旋翼的飞行器,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)、以及安装于机身(10)后部的涵道动力装置(50);所述起落架(20)设有两件以上,且分别设于机身(10)、左机翼(30)以及右机翼(40)上;所述左机翼(30)与右机翼(40)以机身(10)对称设置;所述涵道动力装置(50)与设置在机身(10)上的起落架(20)相连。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 single ducted rotors
一种具有分裂式升降副翼和单涵道旋翼的飞行器
2020-05-12
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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