The invention provides a fixed-wing aircraft rotary wing and an aircraft with the same, the fixed-wing aircraft rotary wing comprises at least one wing middle section, two wing middle section assemblies, two wing outer sections, two wing outer section assemblies and a control assembly, the wing middle section is connected with a fuselage of the aircraft, the wing middle section assemblies are installed on the wing middle section, and the wing outer section assemblies are installed on the wing middle section. The wing outer section assembly is mounted on a wing outer section, the wing outer section assembly is connected with the wing middle section assembly through a revolute pair, and the wing outer section can rotate around the wing middle section through an actuating assembly; the control assembly controls the actuating assembly to act according to the requirement of an airplane for lift force so as to adjust the angle of the wing outer section relative to the wing middle section. The requirement for the runway length during takeoff or landing of the aircraft is reduced, and the application range and application scene of the fixed-wing aircraft in a complex environment are widened.
本发明提供一种固定翼飞机旋转机翼及具有其的飞机,至少一个机翼中段、两个机翼中段组件、两个机翼外段、两个机翼外段组件和控制组件,所述的机翼中段与飞机的机身连接,所述的机翼中段组件安装在机翼中段,所述的机翼外段组件安装在机翼外段,所述的机翼外段组件与所述机翼中段组件通过转动副连接,可通过作动组件使所述的机翼外段绕所述机翼中段转动;所述控制组件根据飞机对升力的要求控制作动组件动作从而调整机翼外段相对与机翼中段的角度。本发明缩短了飞机起飞或降落时对跑道长度的要求,扩大了固定翼飞机在复杂环境下的使用范围和使用场景。
Rotary wing of fixed-wing aircraft and aircraft with rotary wing
一种固定翼飞机旋转机翼及具有其的飞机
2024-11-08
Patent
Electronic Resource
Chinese
IPC: | B64U |
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