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Aircraft

An aircraft and main part technology, applied in the field of aviation, can solve problems such as the influence of protective cover, potential safety hazards, and the unmanned aerial vehicle body cannot be kept level all the time, and achieve the effect of ensuring stability and reducing impact.

Inactive Publication Date: 2018-11-27
深圳创客空间科技有限公司
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  • Summary
  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

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 damage
In view of the above situation, there has been a drone with a protective cover 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
For example, once the protective cover shakes due to the influence of the wind or collides with external obstacles, the protective cover will drive the drone body to tilt or even flip, resulting in unstable flight of the drone and potential safety hazards

Method used

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Embodiment Construction

[0029] The following examples are used to illustrate the present invention, but are not intended to limit the scope of the present invention.

[0030] Such as figure 1 As shown, the aircraft of the present invention includes an aircraft body and a spherical protective cover 1 for accommodating the aircraft body, the aircraft body includes a first body part 21 and a second body part 22, and the first body part 21 has a first body part 21. a weight, the second body part 22 has a second weight, the spherical shield 1 has a three-axis gyro structure,

[0031] Wherein, at a position adjacent to the geometric center of the spherical protective cover 1, the first main body part 21 is supported on the three-axis gyro structure, and the second main body part 22 is suspended and installed on the first main body part 21, the first weight and the second weight are designed such that the center of gravity of the aircraft body is located directly below the geometric center of the spherical...

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PUM

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Abstract

The invention discloses an aircraft. The aircraft includes an aircraft body and a spherical shield which houses the aircraft body, the aircraft body includes a first body portion and a second body portion, the first body portion has a first weight, the second body portion has a second weight, the spherical shield is provided with a three-axis gyro structure, at a position adjacent to a geometric center of the spherical shield, the first body portion is supported on the three-axis gyro structure, the second body portion is suspended below the first body portion, and the first weight and the second weight are designed to make the center of gravity of the aircraft body be located directly below the geometric center of the spherical shield. The aircraft can achieve the horizontal rolling in front, back, left and right directions of the aircraft in the horizontal plane and the upward wall climbing movement, the aircraft body can always maintain a basic horizontal state, and the stability ofthe aircraft is ensured.

Description

technical field [0001] The invention relates to the field of aviation technology, 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. For example, it is used in urban management, agriculture, geological exploration, meteorology, electricity, emergency rescue and disaster relief, 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 situation, there has been a drone with a protective cover 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 . For example, once the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D45/00
CPCB64D45/00
Inventor 符晓红
Owner 深圳创客空间科技有限公司
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