The invention discloses a variable sweepback wing aircraft with a movable winglet, and relates to the technical field of aircrafts. Comprising an aircraft body, a mounting groove and a winglet body, a Hall effect sensor is fixedly mounted on the front end wall of the interior of the mounting groove, and a swing device is arranged in the mounting groove; the swing device comprises a hydraulic telescopic rod, a sliding rod, a first sliding block, two connecting blocks, a limiting block, a second sliding block, a second sliding strip, a first sliding rail, a center shaft, a spherical support, a spherical stand column, a swing seat, a swing frame, a mounting seat and a second sliding rail, the number of the connecting blocks is two, and a magnet is fixedly mounted on the winglet main body. And the right side of the winglet main body is fixedly connected with a second sliding strip.
本发明公开了一种具有可动翼梢小翼的可变后掠翼飞行器,涉及飞行器技术领域;包括飞行器主体、安装槽以及翼梢小翼主体,所述安装槽的内部前端壁固定安装有霍尔效应传感器,所述安装槽的内部设置有摆动装置,所述摆动装置中包括液压伸缩杆、滑杆、第一滑块、连接块、限位块、第二滑块、第二滑条、第一滑轨、中心轴、球形支座、球形立柱、摆动座、摆动架、安装座以及第二滑轨,其中连接块为两个,所述翼梢小翼主体上固定安装有磁铁,所述翼梢小翼主体的右侧固定连接有第二滑条。
Variable sweepback wing aircraft with movable winglet
一种具有可动翼梢小翼的可变后掠翼飞行器
08.04.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Variable sweepback wing structure for aircraft and aircraft
Europäisches Patentamt | 2024
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