The invention discloses a tandem wing type vertical take-off and landing aircraft which comprises an aircraft body, wings, lifting wings and an undercarriage, the aircraft body is a main body structure of the aircraft and is of a streamline structure, and an aircraft cockpit, an electric propulsion device cabin and a power system are arranged in the aircraft body; a main wing and a lifting wing in the wings are arranged on the two sides of the front end and the rear end of the fuselage respectively and are in tandem wing layout, the transverse extension length of the lifting wing exceeds the transverse extension length of the main wing, a plurality of groups of propellers are arranged, and an aileron is arranged on the outer side of the rear edge of a wingtip of the main wing; the aircraft can perform transverse maneuver by controlling rolling torque generated by differential deflection of the left and right ailerons; the undercarriage is located at the bottom of the fuselage, comprises a front undercarriage and a rear undercarriage and is used for supporting the aircraft when the aircraft is parked and slides on the ground; the aircraft has optimized lift force distribution and pneumatic coupling effect, lift force efficiency and stability are improved, and safety and vertical take-off and landing capability are enhanced. The aircraft is flexible in load distribution and can adapt to various task requirements.
本申请公开了一种串翼式垂直起降飞行器,飞行器包括机身、机翼、升降翼以及起落架,机身为飞行器的主体结构,采用流线型结构,机身内部设置有飞机座舱、电推进装置舱以及动力系统;机翼中主翼和升降翼分别设置于机身前端与后端两侧采用串列翼布局且升降翼横向伸展的长度超过主翼横向伸展的长度,并设置有多组螺旋桨,主翼翼梢后缘外侧设置有副翼,通过操纵左右副翼差动偏转所产生的滚转力矩可以使飞机做横向机动;起落架位于机身底部,包括前起落架和后起落架,用于在地面停放和滑行时支撑飞行器;飞行器具有优化的升力分布和气动耦合效应,提升升力效率和稳定性,并增强了安全性和垂直起降能力。飞行器的载荷分布灵活,能适应多种任务需求。
Tandem wing type vertical take-off and landing aircraft
一种串翼式垂直起降飞行器
2025-02-14
Patent
Electronic Resource
Chinese
IPC: | B64U |
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