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Novel unmanned plane

A new type of unmanned aerial vehicle technology, applied in the field of unmanned helicopter equipment, can solve the problems of increased control difficulty, aerodynamic performance damage, and overall structural imbalance, and achieve weight reduction, installation difficulty, and good aerodynamic performance. Effect

Inactive Publication Date: 2013-06-26
XIAMEN RUIHANG PRECISION TECH CO LTD
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AI Technical Summary

Problems solved by technology

The disadvantage of this structure is that the aerodynamic performance is damaged due to the extra structure of the camera, which causes the overall structure to be unbalanced and increases the difficulty of manipulation

Method used

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  • Novel unmanned plane

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Embodiment Construction

[0020] Such as figure 1 Embodiments of the invention shown:

[0021] The present invention is an unmanned aerial vehicle in the form of a helicopter. Its main body 1 is in the form of an elongated cylindrical hollow shell symmetrical along the central axis. The main body 1 is provided with 6 rotor struts 2. The rods 2 are distributed symmetrically with respect to the main body, that is, there are three rotor struts 2 on both sides of the central axis of the main body 1, and the rotor struts 2 on both sides are arranged symmetrically. In other embodiments, different numbers of rotor struts can be designed according to needs.

[0022] In this embodiment, two support feet 5 symmetrical to the central axis plane of the main body 1 are provided under the main body 1 .

[0023] The main body 1 in this embodiment, the six rotor struts 2 and the legs 5 are an integrated hollow shell made of composite materials according to the molding process. The main body 1 is a streamlined cylind...

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Abstract

The invention provides a novel unmanned plane which is characterized by being provided with a barrel-shaped hollow main unit body, wherein a plurality of rotor wing supporting rods are arranged on the main unit body and are symmetrically arranged relative to the main unit body; rotor wings are arranged at the ends of the rotor wing supporting rods; power sources connected with and driving the rotor wings are arranged in the main unit body or the rotor wing supporting rods; a camera hole covered by a transparent material is formed in the lower surface of the main unit body; a camera assembly is arranged in the main unit body and corresponds to the camera hole; and a controller connected with and used for controlling the power sources and the camera assembly is arranged in the main unit body. The main unit body and the rotor wing supporting rods form a shell with an integrated structure. According to the novel unmanned plane, the camera assembly is arranged in the main unit body, and the main unit body and the rotor wing supporting rods are integrated, so that the streamline-type shell is high in aerodynamic performance.

Description

technical field [0001] The invention belongs to a flying device, in particular to an unmanned helicopter device. Background technique [0002] Unmanned helicopter is a kind of flying equipment that is gradually becoming practical at present. Cameras are mounted on unmanned helicopters, which are used in firefighting, military, and police fields to achieve cruising photography or designated monitoring of required areas. The unmanned helicopter has many advantages such as small footprint, flexible take-off and landing, hovering, and easy manipulation. [0003] At present, the most common type of unmanned helicopter is a single-axis single-propeller or a single-axis common-propeller form. Above a mechanical frame containing a drive motor (electric motor or internal combustion engine) is a rotor, and a camera is hoisted below the mechanical frame. The disadvantage of this structure is that the aerodynamic performance is damaged due to the extra structure of the camera, which ca...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/02B64C1/00B64D47/08
Inventor 王麒麟
Owner XIAMEN RUIHANG PRECISION TECH CO LTD
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