Air transportation aircraft with automatic balancing function

An air transportation and automatic balancing technology, which is applied in the field of air transportation aircraft and aircraft, can solve the problems of not effectively solving the balancing effect of the aircraft, unable to fully realize the function, and the interference of the balancing device.

Inactive Publication Date: 2017-05-31
JIANGSU JINGWEI TECH INNOVATION CONSULTING CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0008] The above three related technologies have not effectively solved the balance function that the aircraft should have when carrying cargo or emergency landing, and the general balance device is also easily disturbed by external environmental factors
Can't fully realize its function

Method used

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  • Air transportation aircraft with automatic balancing function

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Embodiment Construction

[0021] The preferred technical solutions of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0022] Such as figure 1 As shown, a kind of air transport aircraft with automatic balancing function of the present invention includes an aircraft body 1 of the aircraft, a pipeline 2 is arranged on the aircraft body 1, and a gravity groove 3 is arranged near the bottom of the aircraft body 1, so One end of the pipeline 2 communicates with the gravity groove 3, and several accommodation grooves 4 are sequentially arranged in the pipeline 2 along the length direction, and each accommodation groove 4 is provided with a perforated plate 5 along the side of the pipeline 2 towards the gravity groove 3, and the accommodation grooves 4 is provided with a water storage bubble 6, the gravity tank 3 is filled with water-absorbing material 7, the outside of the pipeline 2 is provided with a pressure bar 8, and the pressure bar 8 is provided ...

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PUM

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Abstract

The invention discloses an air transportation aircraft with an automatic balancing function. The air transportation aircraft with the automatic balancing function comprises a pipeline arranged on an aircraft main body; a gravity groove is formed in the aircraft main body; a plurality of accommodating grooves are formed in the pipeline; water storage vacuoles are arranged in the accommodating grooves; a pressure strip is arranged outside the pipeline; and a plurality of nail cones are arranged on the pressure strip. Compared with the prior art, the air transportation aircraft with the automatic balancing function is advantaged in that the water storage vacuoles can be punctured by using the nail cones when the aircraft is out of control in the air; therefore, water flows into the gravity groove to control the aircraft main body to be not inclined in case that the gravity is concentrated upon the lower part of the aircraft; and the loaded cargoes are prevented from directly touching the ground to be damaged when the aircraft main body lands.

Description

technical field [0001] The invention relates to an aircraft, in particular to an air transport aircraft with an automatic balancing function, and belongs to the field of logistics transportation. Background technique [0002] At present, the development of multi-rotor drones is very rapid. In order to ensure flight safety, most of them adopt various obstacle avoidance technologies, that is, to prevent the aircraft from contacting obstacles. [0003] In the anti-collision protection of the aircraft, the most common one is to add a protective ring around the blades. This method can only protect the blades to a certain extent, but cannot protect other parts of the aircraft, let alone effectively guarantee Efficient flight of aircraft after collision. [0004] Another relatively good anti-collision structure, such as the Chinese patent application with application number 201480024468.2, discloses a vertical take-off and landing aircraft, including an inner frame, a gimbal syste...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C17/02
CPCB64C17/02
Inventor 汪屹
Owner JIANGSU JINGWEI TECH INNOVATION CONSULTING CO LTD
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