The invention discloses an electric wing unit, a wing and an aircraft, and the electric wing unit comprises a duct which is respectively provided with a front port and a rear port along two axial ends; the supporting part is arranged in the duct; the driving part is arranged on the supporting part; the fan is connected with the driving part, and the driving part is used for driving the fan to rotate; the fixed wing is fixedly arranged at the position of the rear end opening, and the length direction of the fixed wing is perpendicular to the axial direction of the duct; the rudder body is rotatably arranged at the end, away from the duct, of the fixed wing, and a rotating shaft of the rudder body is perpendicular to the axial direction of the duct. Through application of the electric wing unit, the electric wing unit is high in integration degree, especially suitable for wings of aircrafts, beneficial to unitized design, high in working reliability, high in safety, low in noise and wide in application range.
本发明公开了一种电动机翼单元、机翼以及飞行器,其中,电动机翼单元,包括:涵道,所述涵道沿轴向的两端分别形成有一前端口和一后端口;支撑部,所述支撑部设置于所述涵道内;驱动部,所述驱动部设置于所述支撑部上;风扇,所述风扇与所述驱动部连接,所述驱动部用于驱动所述风扇的转动;固定翼,所述固定翼固定地设置于所述后端口处,所述固定翼的长度方向与所述涵道的轴向垂直设置;舵体,所述舵体可转动地设置于所述固定翼远离所述涵道的一端,所述舵体的转动轴与所述涵道的轴向垂直设置。通过对本发明的应用,提供了一种集成程度较高的电动机翼单元,尤其适用于飞行器的机翼,有利于单元化设计,且工作可靠性较高,安全性较高,同时噪音较低,适用范围较广。
Electric wing unit, wing and aircraft
一种电动机翼单元、机翼以及飞行器
03.12.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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