Aircraft

An aircraft and frame technology, applied in the aviation field, can solve the problems of immobility, influence of flight attitude, and insufficient diversification of applications, so as to reduce the probability of crash and improve the quality.

Active Publication Date: 2017-07-18
瑞电恩吉能源技术(深圳)有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The motors of existing aircraft are installed perpendicular to the ground. The disadvantage is that if an external force is encountered in the air, it is easy to affect the flight attitude.
[0004] In addition, existing aircraft can only be used for air operations, cannot touch walls, and cannot move on the ground, resulting in insufficient diversification of applications

Method used

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Embodiment Construction

[0036] In order to make the objectives, technical solutions, and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be described clearly and completely in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of the embodiments of the present invention, not all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of the present invention.

[0037] It should be noted that the embodiments of the present invention and the features in the embodiments can be combined with each other if there is no conflict. Hereinafter, the present invention will be described in detail with reference to the drawings and in conjunction with the embodiments.

[0038] Reference Figure 1~3 As sh...

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PUM

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Abstract

The invention provides an aircraft. The aircraft comprises a main body with propellers, a first frame surrounding the main body, a second frame and a third frame, wherein the second frame and the third frame are symmetrically arranged outside the first frame. The first frame is in pivotal rotation connection with the main body through a first shaft so that the first frame can overturn relative to the main body. The second frame and the third frame are in pivotal rotation connection with the first frame through a second shaft perpendicular to the first shaft so that the second frame and the third frame can rotate in the plane perpendicular to the second shaft. The edges of the second frame and the third frame exceed the edge, in the same direction, of the first frame. The aircraft can complete actions of walking and climbing walls with the help of the frames, the crashing possibility of the aircraft can be decreased, and thus the aircraft is not limited by landforms and can rise and fall at random.

Description

Technical field [0001] The embodiment of the present invention relates to the field of aviation technology, in particular to an aircraft. Background technique [0002] With the development of multi-axis unmanned aerial vehicles, many types of multi-axis unmanned aerial vehicles have appeared on the market, but they are all based on traditional aerodynamic layout and modified structure. [0003] The motors of the existing aircraft are installed perpendicular to the ground. The disadvantage is that if an external force is encountered in the air, it will easily affect the flight attitude. [0004] In addition, the existing aircraft can only be used for aerial operations, cannot touch walls, and cannot move on the ground, resulting in insufficient diversification of applications. [0005] Therefore, it is an urgent problem to provide an aircraft with a more stable flight attitude and functions such as road operation, wall climbing, and safety protection. Summary of the invention [0006] ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/00B64C27/08
CPCB64C27/006B64C27/08B64U10/10
Inventor 白振业张术超
Owner 瑞电恩吉能源技术(深圳)有限公司
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