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
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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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