The invention provides an aircraft with combined folding wings, and relates to the technical field of aircrafts, the aircraft comprises: a fuselage provided with a mounting part; the folding wing mechanism comprises a pair of front wings and a pair of rear wings, and the ends, close to each other, of the front wings and the rear wings are rotationally connected with the mounting part; the folding wing mechanism comprises a first state and a second state, in the first state, the pair of front wings cling to each other and are arranged on the side, close to the front end of the fuselage, of the mounting part, and the pair of rear wings cling to each other and are arranged on the side, close to the tail end of the fuselage, of the mounting part; in the second state, the pair of front wings and the pair of rear wings are unfolded towards the two sides of the fuselage respectively, and the front wings and the rear wings located on the same side of the fuselage are tightly attached; and the driving mechanism is used for driving the front wing and the rear wing to rotate at the same time, so that the folding wing mechanism is switched between the first state and the second state. The aircraft with the combined folding wings has the advantage that the aircraft can be kept stable in the initial flight stage.
本发明提供一种带有组合折叠翼的飞行器,涉及飞行器技术领域,包括:机身,机身上设有安装部;折叠翼机构,折叠翼机构包括一对前翼和一对后翼,前翼与后翼相互靠近的一端与安装部转动连接;折叠翼机构包括第一状态和第二状态,处于第一状态时,一对前翼相互贴紧并置于安装部靠近机身前端的一侧,一对后翼相互贴紧并置于安装部靠近机身尾端的一侧;处于第二状态时,一对前翼和一对后翼分别向机身两侧展开,且位于机身同一侧的前翼和后翼贴紧;驱动机构,用于同时驱动前翼和后翼转动,以使折叠翼机构在第一状态和第二状态之间切换。本发明提供的带有组合折叠翼的飞行器具有在初始飞行阶段可保持平稳的优点。
Aircraft with combined folding wings
一种带有组合折叠翼的飞行器
2024-03-05
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
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