Artificial intelligence low-altitude aircraft

一种低空飞行器、人工智能的技术,应用在飞行器、无人驾驶的飞行器、飞机零件等方向,能够解决降落缓冲防护力度不够、测控摄像头不便调节等问题,达到避免下降力度过大、加大力度、保护力度的效果

Inactive Publication Date: 2021-06-29
LINGJING (HUBEI) TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In view of the deficiencies in the prior art, the present invention provides an artificial intelligence low-altitude aircraft, which has the advantages of improving the landing protection of the aircraft and conveniently adjusting the angle of the measurement and control camera. The problem of inconvenient adjustment of the camera

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0027] Present embodiment is the embodiment of artificial intelligence low-altitude aircraft.

[0028] see Figure 1-4 , an artificial intelligence low-altitude aircraft, including an aircraft 1, the bottom of the aircraft 1 is provided with a landing protection mechanism 2, and the top of the aircraft 1 is provided with a measurement, control and adjustment mechanism 3;

[0029] The landing protection mechanism 2 includes a landing rod 21 that is rotatably connected to the bottom of the aircraft 1, and the outer surface of the landing rod 21 is fixedly connected with a buffer limit rod 22, and the top of the landing rod 21 is slidably connected with a buffer rod 23, and the top of the buffer rod 23 A buffer cylinder 24 is movably connected, and a connecting rod 25 is fixedly connected to the inner side of the drop rod 21, and the side of the connecting rod 25 away from the drop rod 21 is slidably connected with a buffer protection plate 26;

[0030] Through the above-mention...

Embodiment 2

[0045] This embodiment is the embodiment of the landing protection mechanism of the artificial intelligence low-altitude aircraft.

[0046] The landing protection mechanism 2 of the artificial intelligence low-altitude aircraft includes a landing rod 21 that is rotatably connected to the bottom of the aircraft 1, and the outer surface of the landing rod 21 is fixedly connected with a buffer limit rod 22, and the top of the landing rod 21 is slidably connected with a buffer rod 23 The top of the buffer rod 23 is movably connected with a buffer cylinder 24, the inner side of the drop rod 21 is fixedly connected with a connecting rod 25, and the side of the connecting rod 25 away from the drop rod 21 is slidably connected with a buffer protection plate 26.

[0047] Through the above-mentioned embodiment, the top of the landing rod 21 can buffer the impact of the buffer rod 23 by the gas in the buffer cylinder 24 when the aircraft 1 lands through the buffer rod 23, and at the same ...

Embodiment 3

[0049] This embodiment is the embodiment of the measurement, control and adjustment mechanism of the artificial intelligence low-altitude aircraft.

[0050] The measurement and control adjustment mechanism 3 of the artificial intelligence low-altitude aircraft includes a measurement and control camera 31 that is movably connected to the top of the aircraft 1, and the outer surface of the measurement and control camera 31 is slidingly connected with a measurement and control fixed protective gear 32, and the internal sliding connection of the measurement and control fixed protective gear 32 has a direction The fixed block 33 and the bottom of the measurement and control camera 31 are fixedly connected with a counterweight 34 , and the outer side of the direction fixed block 33 is movably connected with a telescopic control motor 35 .

[0051] Through the above-mentioned embodiment, the inner wall of the measurement and control fixed protective device 32 is slidingly connected wi...

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PUM

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Abstract

The invention relates to the technical field of artificial intelligence, and discloses an artificial intelligence low-altitude aircraft which comprises an aircraft body, a landing protection mechanism is arranged at the bottom of the aircraft body, a measurement and control adjusting mechanism is arranged at the top of the aircraft body, and the landing protection mechanism comprises a landing rod rotationally connected to the bottom of the aircraft body. The outer surface of the falling rod is fixedly connected with a buffering limiting rod, the top of the falling rod is slidably connected with a buffering rod, and the top of the buffering rod is movably connected with a buffering air cylinder. According to the artificial intelligent low-altitude aircraft, buffering is performed through gas in a buffering air cylinder, the situation that the descending force is too large is avoided, an auxiliary buffering rod protects the aircraft body, and meanwhile when the aircraft lands, the aircraft slides out of a buffering protection plate through a connecting rod; and a buffer spring fixedly connected to the top of the buffer protection plate further buffers the aircraft, so that landing of the aircraft is protected through multiple buffering, and the effect of increasing the aircraft protection force is achieved.

Description

technical field [0001] The invention relates to the technical field of low-altitude aircraft, in particular to artificial intelligence low-altitude aircraft. Background technique [0002] Low-altitude aircraft is any flying object that is manufactured by humans, can fly off the ground, fly in space and be controlled by humans for personal use; with the popularity of aircraft, personal aircraft must be the future development direction; lightweight, flexible low-altitude, low-speed Aircraft will be the development direction of personal aircraft; at the same time, with the popularity of aircraft, the requirements for intelligent control of aircraft will become more and more stringent. [0003] At present, artificial intelligence low-altitude aircraft on the market can only control the flight direction of the aircraft. However, when the aircraft flies to high altitude, there is an error in the distance from the human eye, so it is necessary to check the distance between the airc...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/08B64C25/58B64C25/62
CPCB64D47/08B64C25/58B64C25/62B64U10/13B64U2101/30
Inventor 屈松
Owner LINGJING (HUBEI) TECH CO LTD
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