Air-land amphibious four-rotor unmanned aerial vehicle

A technology of quadrotor UAV and UAV, which is applied in the field of UAV, can solve the problem that the power supply of UAV cannot meet the long-term use of UAV, and it is inconvenient, so as to achieve convenient long-term flight, convenient control, The effect of improving functionality and practicality

Inactive Publication Date: 2018-09-11
珠海诚然科技服务有限公司
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Problems solved by technology

[0003] Traditional drones are generally controlled by operating handles and large consoles, which is very i

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  • Air-land amphibious four-rotor unmanned aerial vehicle
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[0020] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0021] see Figure 1-3 , the present invention provides a technical solution: a ground-air amphibious quadrotor UAV, including a UAV body 1, a rotor device 2, a land movement device 3, a signal receiver 4, a detection device 5 and a solar power supply device 6 , the upper side of the UAV body 1 is provided with the rotor device 2 and the bottom is provided with the land movement device 3, the inner side of the land movement device 3 is provided with the signal...

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Abstract

The invention discloses an air-land amphibious four-rotor unmanned aerial vehicle. The air-land amphibious four-rotor unmanned aerial vehicle comprises an unmanned aerial vehicle body, a rotor device,a land movement device, a signal receiver, a detection device and a solar energy supply device. The upper side of the unmanned aerial vehicle body is equipped with the rotor device and the bottom ofthe unmanned aerial vehicle body is equipped with the land movement device. The inside of the land movement device is provided with the signal receiver. The detection device is located on the front side of the unmanned aerial vehicle body. The solar energy supply device is arranged on the upper side of the unmanned aerial vehicle body. The unmanned aerial vehicle performs control through a remote-control system. By arranging the detection device, an infrared detector on the lower side of a camera is used for detecting when weather is foggy or has a low poor visibility. The unmanned aerial vehicle is highly functional and practical. A signal is transmitted by a mobile phone app of the remote-control system. Then, a signal reception unit receives the signal and a controller is utilized for controlling the unmanned aerial vehicle. Therefore, the unmanned aerial vehicle is convenient to control, thereby improving convenience of operation.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a ground-air amphibious quadrotor unmanned aerial vehicle. Background technique [0002] Unmanned aircraft, referred to as "unmanned aerial vehicle", is an unmanned aircraft controlled by radio remote control equipment and self-contained program control device, or is completely or intermittently operated autonomously by the on-board computer. Compared with manned aircraft, Drones tend to be better suited for missions that are too "dull, dirty or dangerous". According to the application field, UAV can be divided into military and civilian. In terms of military use, UAVs are divided into reconnaissance aircraft and target aircraft. In terms of civilian use, drones + industry applications are the real rigid needs of drones; currently, they are used in aerial photography, agriculture, plant protection, micro selfies, express delivery, disaster relief, wildlife obse...

Claims

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Application Information

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IPC IPC(8): B60F5/02B64C27/08B64C39/02H02J7/35
CPCH02J7/35B64C27/08B64C39/024B60F5/02B64U10/10B64U2101/00B64U2201/20
Inventor 邓杰林颖邹辉龙
Owner 珠海诚然科技服务有限公司
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