Embodiments provide an electric aircraft having a plurality of lift fan assemblies configured to provide vertical lift, and one or more propulsion propellers configured to provide forward thrust. The lift fan assembly may be coupled to a wing of the aircraft via one or more support structures, and the wing may be coupled to an upper region of the fuselage. The propulsion propeller (s) may be coupled to the aft end of the fuselage. The lift fan assembly and the propulsion propeller (s) may provide thrust and movement in directions orthogonal to each other. A control system coupled to the aircraft may control the lift fan assembly and the one or more propulsion propellers to activate, increase in power, and decrease in power. The lift fan assembly and the one or more propulsion propellers may be operated separately and may be active at different times.
实施例提供一种电动飞行器,其具有构造成提供垂直升力的多个升力风扇组件,和构造成提供向前推力的一个或多个推进式螺旋桨。升力风扇组件可经由一个或多个支撑结构联接到飞行器的机翼,并且机翼可联接到机身的上部区域。(一个或多个)推进式螺旋桨可联接到机身的尾端。升力风扇组件和(一个或多个)推进式螺旋桨可在正交于彼此的方向上提供推力和移动。联接到飞行器的控制系统可控制升力风扇组件和一个或多个推进式螺旋桨以激活,在功率方面增加和在功率方面减小。升力风扇组件和一个或多个推进式螺旋桨可被单独地操作,并且可在不同的时间是起作用的。
Aircraft with propulsion propellers
具有推进式螺旋桨的飞行器
2022-11-04
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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