Electric turbine duct system of aeromodelling plane

Abstract

The invention provides an electric turbine duct system of an aeromodelling plane. The system body is constituted by a lift force generation device, a framework and a lower support, wherein the framework comprises a control circuit board, a power source and a main framework body, the main framework body comprises a hollow cavity which is constituted by an upper main framework body and a lower mainframework body and a main support, the control circuit board is electrically connected with the power source, and the control circuit board and the power source are accommodated in the hollow cavity.Compared with the prior art, a main propeller structure and a subsidiary propeller structure are adopted by the electric turbine duct system of the aeromodelling plane, and can rotate in opposite directions, and thus the shortcoming that the electric turbine duct system of the aeromodelling plane cannot fly stably due to one-way force is overcome.

Description

Technical field [0001] The invention relates to an electric toy, in particular to a vertical lifting aircraft. Background technique [0002] The electric turbine ducting system of model airplanes has been loved by people since its inception. In order to meet the needs of consumers, toy manufacturers continue to develop various models of electric turbine ducts of airplane model airplanes and make continuous improvements in order to create a stable flight and An easy-to-control model airplane electric turbine duct system. At present, the electric turbine duct system of model airplanes on the market generally has the problem of unstable flight and difficult to operate. The main cause of unstable flight is that the propeller generates unidirectional force from stationary to rotating during flight, which causes ducts of electric turbine of airplane model airplanes. The system cannot maintain a balanced state during flight, which makes the flight unstable. It is not suitable for oper...

AI Technical Summary

Problems solved by technology

At present, the electric turbine duct system of aircraft model aircraft on the market generally has the problem of unstable flight and difficult operation. The main reason for the unstable flight is that the propeller generates a one-way force from static to rotating during flight, which causes the electric turbine duct of aircraft model aircraft The system cannot maintain a balanced state during flight, making the flight unstable

It is not suitable for operation because the steering mechanism of the electric turbine duct system of aircraft model aircraft on the market mostly adopts the tail steering structure, and the steering control part and the flight control part are not together, which makes the operation more difficult

[0003] In addition, the lower support of the electric turbine duct system of model airplanes on the market is mainly a tripod structure without rollers. The biggest disadvantage of this structure is that it is poor in safety.

When the model aircraft electric turbine duct system lands, there is often a large forward momentum, and because the aircraft model aircraft electric turbine duct system does not always land perpendicular to the ground, the lower bracket is easy to cause the aircraft electric motor Turbo duct system crashed

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