The invention provides an aircraft structure with wing folding and empennage swinging functions, and relates to the technical field of aircraft structures, the aircraft structure comprises two fixing blocks, and the two fixing blocks are fixedly connected to the rear end of a fuselage rod; the number of the mounting sliding grooves is two, and the two mounting sliding grooves are formed in the inner sides of the two fixing blocks correspondingly. The fixed wing is mounted at the front end of the fuselage rod; the mounting cylinder is fixedly connected to the lower end face of the fixed wing, and the mounting cylinder is slidably connected to the front end of the fuselage rod; the number of the fastening bolts is two, and the two fastening bolts are both in threaded connection with the inner side of the mounting cylinder, so that the problem that in the flying process of an existing remote control aircraft structure, when an aircraft accidentally falls to the ground due to inaccurate and appropriate control, an empennage of the aircraft is prone to being damaged or even fractured is solved; and as the empennage of the remote control aircraft is mostly fixedly mounted on the fuselage, the replacement of the empennage is troublesome, and the flight efficiency is improved.
本发明提供一种具有机翼折叠与尾翼摆动功能的飞机结构,涉及飞机结构技术领域,包括所述固定块设有两个,两个固定块均固定连接在机身杆的后端;所述安装滑槽设有两个,两个安装滑槽分别开设在两个固定块的内侧;所述固定机翼安装在机身杆的前端;所述安装筒固定连接在固定机翼的下端面,安装筒滑动连接在机身杆的前端;所述紧固螺栓设有两个,两个紧固螺栓均螺纹连接在安装筒的内侧,解决了现有的遥控飞机结构在飞行过程中,当出现因操控不够精准恰当致使飞机不慎摔落到地面时,飞机的尾翼往往很容易出现破损甚至断裂的现象,而由于遥控飞机的尾翼大多是固定安装于机身上的,想要对其进行更换就会比较麻烦的问题,提高了飞行效率。
Aircraft structure with wing folding and empennage swinging functions
一种具有机翼折叠与尾翼摆动功能的飞机结构
04.04.2025
Patent
Elektronische Ressource
Chinesisch
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