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Aircraft

An aircraft and main part technology, applied in the field of aviation, can solve the problem that the aircraft cannot fly safely and smoothly, and achieve the effect of improving sensitivity, ensuring safe flight, and avoiding damage

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

AI Technical Summary

Problems solved by technology

[0003] An embodiment of the present invention provides an aircraft to at least solve the technical problem that the aircraft cannot fly safely and smoothly in the above technical problems

Method used

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Embodiment Construction

[0023] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0024] It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0025] Such as figure 1 As shown, in some embodiments of the ...

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Abstract

The invention provides an aircraft. The aircraft comprises an aircraft main body provided with a first main body part with a first weight and a second main body part with a second weight and further comprises a spherical protective cover provided with a three-axis gyroscopic structure and capable of containing the aircraft main body. On the position adjacent to the geometric center of the spherical protective cover, the first main body part is supported on the three-axis gyroscopic structure; and the second main body part is mounted below the first main body part in a suspending mode, and the first weight and the second weight are designed to achieve the effect that the gravity center of the aircraft is located under the geometric center of the spherical protective cover. According to the aircraft, the effect that the aircraft horizontally rolls forwards, backwards, leftwards and rightwards in the horizontal plane and even makes upward wall-climbing movement can be achieved, the aircraft main body can keep a basic horizontal state all the time, and stability of the aircraft is ensured.

Description

technical field [0001] Embodiments of the present invention relate to the field of aviation technology, and in particular to an aircraft. Background technique [0002] With the development of science and technology, drones have been more and more widely used in all aspects of life and production, such as urban management, agriculture, geological exploration, meteorology, stores, emergency rescue, video shooting, etc. Today's drones are often easy to break, and they are helpless when encountering complex environments. They can only fall to the ground by hitting obstacles and destroying the propeller. Therefore, a protective cover is needed to protect the drone from unmanned machine damaged. In view of the above-mentioned situation, a drone with a protective cover has further appeared in the prior art, but in the existing drones with a protective cover, the drone body cannot always be kept horizontal, and is easily affected by the protective cover. influences. For example, ...

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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