Double ducted-propeller electric manned aircraft capable of taking off and landing vertically
A vertical take-off and landing, propeller technology, applied in the field of aviation equipment, can solve problems such as low energy utilization efficiency and safety hazards, and achieve the effect of highlighting substantive characteristics, saving energy and improving efficiency
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[0057] Such as Figure 1 ~ Figure 3 As shown, the double-ducted propeller vertical take-off and landing electric manned aircraft includes a flight cabin 1, a facade wing 11, a control platform 6, a ducted propeller power system 2, a self-balancing mechanism 3, a ducted rotating mechanism 4, and a battery pack 12. Among them, the side wings of the facade are located on both sides of the flight cabin and are solidly integrated with it. They are made of a common main frame 13 and skin, and are designed with a single door 14 according to its structure. The control platform 6 and the battery pack 12 that provides power for the aircraft; the number of ducted propeller power systems is two, which are respectively located at the front and rear ends of the flight cabin. The self-balancing mechanism and the ducted rotating mechanism connected to the same ducted propeller power system cooperate with each other on both sides of the ducted propeller, and the connection between the two is ...
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