Electric aircraft

Abstract

The electric aircraft has ring casing, upper layer and lower layer of flying wing assembly inside the casing, upper layer and lower layer of ring guide tracks on the inside of the ring casing, and manned modules on the outside of the ring casing. In each of the upper layer and lower layer of flying wing assembly, there are several wings with several high speed motors, and the main shaft of each high speed motors has roller mounted to move along the guide track to drive the wings. The upper layer and the lower layer of flying wing assemblies are connected to the central shaft via bearings, the central shaft has four conducting rings corresponding to the electric brushes in the wings, the conducting rings are connected to power supply on the ground wire power cable. The electric aircraft has simple structure, low cost, high flying performance, high safety coefficient, capacity of vertically launching and landing, capacity of air suspension, no exhaust of harmful gas and low noise.

Description

technical field [0001] The invention belongs to the technical field of aeronautical aircraft, and particularly relates to a rotary-wing helicopter. Background technique [0002] Most of the existing vertically liftable aircraft such as helicopters use a single propeller (rotary wing), which has the disadvantage of poor stability and needs to use a tail rotor to balance the counter torque. There are very few helicopters that use dual propellers (dual rotors), which do not need to use tail rotors to balance the counter torque during flight, and are less affected by wind and fly smoothly. However, in this helicopter, two sets of propellers are installed on the same central power shaft. In order to ensure that the two sets of propellers rotate in opposite directions, the structure of the transmission device is very complicated. The biggest disadvantage of the above two types of aircraft is that the propellers rely on a single The power shaft drive has a low safety factor, becau...

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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