The invention provides a joint structure fixed wing aircraft which is characterized in that multi-section joint structure fixed wings are fixedly arranged on two sides of an aircraft body, a head wing is arranged at the head of the aircraft body, a main propeller is arranged at the tail of the aircraft body, and auxiliary propellers are arranged on the multi-section joint structure fixed wings; various flight attitudes of the aircraft are controlled by adjusting aerodynamic force changes of the wings in a segmented mode, the control area is large, the acting force is large, the large maneuvering performance of the aircraft is good, the aircraft head wing is placed at the front end of the aircraft, the control distance for a driver to control an airfoil actuating device is shortened, the control response is fast, and the manufacturing cost is low. The system can be widely applied to various airplanes, is particularly suitable for airplanes flying at low altitude, and achieves the flying travel purposes of being more energy-saving, rapid, stable and convenient to arrive.
本发明提供一种关节结构固定翼飞机,其机身的两侧固定设有多段式关节结构固定机翼,机身的头部设有头翼,机身的尾部设有主螺旋桨,多段式关节结构固定机翼上设有副螺旋桨,飞机固定翼是多段式关节结构,通过分段调整机翼的气动力变化来实现飞机的各种飞行姿态控制,控制面积大,作用力大,飞机的大机动性能好,该飞机头翼放置于飞机前端,缩短了驾驶员操控翼面作动装置的操控距离,操控响应快,制造成本低。本发明可广泛应用于各种飞机上,尤其适合于低空飞行的飞机,实现更加节能、快速、平稳、方便抵达的飞行出行目的。
Joint structure fixed wing aircraft
关节结构固定翼飞机
2024-10-22
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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European Patent Office | 2022
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