Electric aircraft

Abstract

An electric aircraft, the central space of the annular housing is equipped with upper and lower flying wing groups, the inner side of the annular housing is equipped with upper and lower annular guide rails, the outer side of the annular housing is the passenger compartment, and the upper and lower flying wing groups have There are multiple wings, and several high-speed motors are installed in each wing. The main shaft of the high-speed motor is equipped with a roller. When driving the wings to make a circular motion along the guide rail, the upper and lower flying wing groups are respectively connected to the central shaft through bearings, and the central shaft is equipped with four conductive rings, and each wing in the upper and lower flying wing groups Brushes are respectively installed at the positions; the conductive rings are respectively connected to the power lines, and the power lines are connected to the ground power supply. The electric aircraft of the invention has the advantages of simple structure, low cost, good flight stability, high safety factor, vertical take-off and landing, stable hovering in the air, no emission of harmful gas, and low flight noise.

Description

technical field [0001] The invention belongs to the technical field of aviation aircraft, in particular to a rotorcraft. Background technique [0002] Most of the existing vertically liftable aircraft such as helicopters use a single propeller (rotary wing). The disadvantage is that the stability is poor, and the tail rotor needs to be used to balance the counter torque. There are very few helicopters that use dual propellers (dual rotors), and there is no need to use the tail rotor to balance the anti-torque during flight. It is less affected by the wind and flies smoothly. But this kind of helicopter installs two sets of propellers on the same central power shaft. In order to ensure that the rotation directions of the two sets of propellers are opposite, the structure of the transmission device is very complicated. The biggest disadvantage of the above two aircraft is that the propellers rely on a single Driven by the power shaft, the safety factor is low, because if any ...

AI Technical Summary

Problems solved by technology

But this kind of helicopter installs two sets of propellers on the same central power shaft. In order to ensure that the rotation directions of the two sets of propellers are opposite, the structure of the transmission device is very complicated. The biggest disadvantage of the above two aircraft is that the propellers rely on a single Driven by the power shaft, the safety factor is low, because if any of the power shaft, drive, transmission or engine fails, the propeller will not work normally, causing the aircraft to crash

Moreover, the existing helicopters all use fuel engines, which are not only noisy, but also emit harmful exhaust gases, cause high-altitude air pollution, and destroy the ozone layer.

[0003] Above-mentioned two kinds of helicopters all can carry out long-distance horizontal movement (flight), and its structure is complicated, and cost is high, and maintenance cost is big, and the cost of each flight is high, and according to the difference of aviation use, in many occasions, we only need A fixed-point aircraft capable of carrying people and objects that can fly vertically and hover stably in the air

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