The invention discloses a lift wing type disc type vertical take-off and landing aircraft, and relates to the field of vertical take-off and landing aircrafts, the lift wing type disc type vertical take-off and landing aircraft comprises an aircraft body, an engine, a cockpit, a mounting box and an undercarriage, the engine is arranged on the side edge of the aircraft body, the cockpit is mounted below the aircraft body, and the mounting box is arranged on the rear side of the cockpit; an undercarriage is arranged on the outer side of the cockpit, a battery box is arranged in the mounting box, conductive modules are arranged above the battery box and in the mounting box, and the left side of the mounting box is designed to be of an open structure, so that the battery box can slide out. According to the lift wing type disc type vertical take-off and landing aircraft, eight ducted propeller brushless motor engines are embedded in the edge of an upper single wing, the eight ducted engines are uniform in power distribution and high in redundancy, the aircraft has sufficient time for forced landing or homeward voyage when faults such as parking occur to the engines, the ducted engines are embedded in the wings, and therefore the aircraft has the advantages of being high in reliability, safe and reliable. Dangerous and accidents that personnel or objects are mixed into the propeller blades of the engine can be effectively avoided.
本发明公开了一种升力翼型碟式垂直起降飞行器,涉及垂直起降飞行器领域,包括机体、发动机、驾驶舱、安装箱和起落架,所述发动机设置在机体的侧边,且机体的下方安装有驾驶舱,驾驶舱的后侧设置有安装箱,并且驾驶舱的外侧设置有起落架,所述安装箱的内部设置有电池箱,电池箱的上方和安装箱的内部均设置有导电模组,且安装箱的左侧呈开口状结构设计,使电池箱能滑出。该升力翼型碟式垂直起降飞行器采用8台涵道式螺旋桨无刷电机发动机内嵌于上单翼边缘,8台涵道式发动机,动力分布均匀,冗余度高,在有发动机出现停车等故障时,飞行器有充足的时间迫降或返航,机翼内嵌涵道式发动机,能有效避免人员或物体搅入发动机螺旋桨叶的危险和事故。
Lift wing type disc-type vertical take-off and landing aircraft
一种升力翼型碟式垂直起降飞行器
2024-12-10
Patent
Electronic Resource
Chinese