Building block component type unmanned plane and control method thereof

A drone and component technology, applied in the field of aviation models, can solve the problems of single structure and poor operability of drones, and achieve the effect of convenient splicing and strong operability

Active Publication Date: 2016-07-20
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] The purpose of the present invention is to provide a building block component type unmanned aerial vehicle, which solves the shortcomings of the current unmanned aerial vehicle with single structure and poor operability

Method used

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  • Building block component type unmanned plane and control method thereof
  • Building block component type unmanned plane and control method thereof
  • Building block component type unmanned plane and control method thereof

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Embodiment Construction

[0023] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention. Embodiments of the present invention will be described in detail b...

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Abstract

The invention relates to a building block component type unmanned plane and belongs to the technical field of model airplanes. By conducting modularization design on all units or components of the unmanned plane, the unmanned plane can topologized into a quite great number of appearance mechanisms, design concept of the unmanned plane is exploited, and operability of an unmanned plane model is improved. The components comprise a structural component, power components, a power supply component, a communication control component and a loading component, the structural component further comprises plane body units and wing units, and the power components comprise propeller units and motor units. The building block component type unmanned plane can be spliced into an unmanned aerial vehicle which can fly quickly, topologized into a quite great number of unmanned plane structures and be widely applied to the fields of child interest development, teaching demonstration, personal entertainment, simple unmanned plane application and the like.

Description

technical field [0001] The invention belongs to the technical field of aviation models, and in particular relates to a building block component type unmanned aerial vehicle and a control method thereof. Background technique [0002] Most of the existing civilian UAVs are non-detachable structures, which can be used directly, and some have the function of assembling. Although these drones provide users with more convenient use effects, they need to be assembled completely according to the established drawings, and there is no space for users to use their imagination. From the perspective of children's interest development and teaching demonstration, they appear to have single functions and poor effects; However, assembled toys have fewer functions, low technological content, and no strong operability and entertainment. Contents of the invention [0003] The purpose of the present invention is to provide a building block component type drone, which solves the shortcomings o...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): A63H27/18A63H33/04
CPCA63H27/02A63H33/04
Inventor 杨柯宛旭王宏利伊文卿王萍
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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