The invention provides a ducted aircraft. The ducted aircraft comprises a fuselage, four transmission assemblies, a first synchronous transmission mechanism and a second synchronous transmission mechanism, wherein the first transmission assembly and the second transmission assembly are arranged on one side of the machine body, the third transmission assembly and the fourth transmission assembly are arranged on the other side of the machine body, one end of the first synchronous transmission mechanism is connected to the first transmission assembly, the other end of the first synchronous transmission mechanism is connected to the third transmission assembly, and one end of the second synchronous transmission mechanism is connected to the second transmission assembly. The other end of the second synchronous transmission mechanism is connected to the fourth transmission assembly; wherein the first transmission assembly, the second transmission assembly, the third transmission assembly and the fourth transmission assembly are the same in structure, each transmission assembly comprises a duct, an engine and a propeller, the ducts are connected to the fuselage, the propellers are arranged in the ducts, and the engines are connected to the propellers; the engine is connected to one of the first synchronous transmission mechanism and the second synchronous transmission mechanism. The ducted aircraft is large in overall load, long in endurance and stable in flight.
本发明提供了一种涵道飞行器,包括:机身、四个传动组件、第一同步传动机构和第二同步传动机构;其中,第一传动组件和第二传动组件设置在机身的一侧,第三传动组件和第四传动组件设置在机身的另一侧,第一同步传动机构的一端连接于第一传动组件,另一端连接于第三传动组件,第二同步传动机构一端连接于第二传动组件,另一端连接于第四传动组件;其中,第一传动组件、第二传动组件、第三传动组件和第四传动组件的结构相同,每个传动组件包括:涵道、发动机和螺旋桨,涵道连接于机身,螺旋桨设置在涵道内,发动机连接于螺旋桨,发动机连接于第一同步传动机构或第二同步传动机构中的一者,该涵道飞行器整机负载大、航时长且飞行稳定。
Ducted aircraft
涵道飞行器
2021-09-17
Patent
Electronic Resource
Chinese