Multi-rotor aircraft

A multi-rotor aircraft and flight status technology, applied in the field of drones, can solve the problems of aircraft damage, disassembly, lack of flexibility in installation and disassembly, etc., to reduce looseness and damage, improve stability, improve scalability and flexibility Effect

Pending Publication Date: 2018-04-27
深圳市创客火科技有限公司
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  • Abstract
  • Description
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  • Application Information

AI Technical Summary

Problems solved by technology

In addition, such an aircraft is not only inflexible in installation and disassembly, but also in the flight state, due to the connection between modules and the structural combination of building blocks, which is different from the requirements for the structure of the building block structure in the static state, it is often in the flight state due to collisions. aircraft damage and disintegration
[0004] Therefore, it is necessary to provide an unmanned aerial vehicle system to solve the problems of poor modular expansion of multi-rotor aircraft and low structural stability of multi-rotor aircraft

Method used

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Embodiment Construction

[0037] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.

[0038] In describing the present invention, it should be understood that the terms "center", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", " Orientation indicated by rear, left, right, vertical, horizontal, top, bottom, inside, outside, clockwise, counterclockwise, etc. The positional relationship is based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present invention and simplifying the description, rather than indicating ...

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Abstract

The invention discloses a multi-rotor aircraft, wherein the multi-rotor aircraft includes: a battery module, an electrical adjustment module, a flight control module and a plurality of power modules; wherein, the battery module and the electrical adjustment module are assembled with each other, and the electrical adjustment module and The flight control modules are assembled with each other; multiple power modules and the electric adjustment module are assembled with each other. The electric adjustment module is provided with a locking fastener, which is used to reinforce the multiple power modules and the electric adjustment module in the flight state. Adjust connections between modules. In the embodiment of the present invention, the multi-rotor aircraft is modularized, and the main modules are flexibly assembled by using assembly components, and expanded into various multi-axis multi-rotor aircraft, which greatly improves the scalability and flexibility of the modularization of the multi-rotor aircraft; In addition, locking fasteners are provided at key positions to strengthen the connection between modules in the flight state and improve the stability of the multi-rotor aircraft structure.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a multi-rotor aircraft. Background technique [0002] With the development of science and technology and the continuous improvement of people's living standards, the types of electronic toys are becoming more and more abundant, and the functions are becoming more and more powerful. Among these electronic toys, aircraft, as a high-end electronic toy, is deeply loved by the majority of aircraft model enthusiasts. [0003] At present, most of the aircraft are building blocks and modular combination aircraft. No matter it is a large, medium or small aircraft, they can only connect four-axis and eight-axis universally to a core platform, and also need to change the relevant electronics. The adjustment of components, the matching of battery size and other tedious configuration and installation are required to realize its functions. In addition, such an ai...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): A63H27/00A63H29/22A63H29/24
CPCA63H27/00A63H29/22A63H29/24
Inventor 严国陶
Owner 深圳市创客火科技有限公司
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