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an intelligent drone

An unmanned aerial vehicle and intelligent technology, applied in the field of unmanned aerial vehicles, can solve the problems of no data storage, data loss, damage, etc., and achieve the effect of improving reliability, practicability and reliability

Active Publication Date: 2019-08-23
安徽七曜航空技术有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In the existing unmanned aerial vehicles, when flying and landing, due to the simple structure of the landing gear, it is easy to cause damage to the internal components of the unmanned aerial vehicle, which reduces the reliability of the unmanned aerial vehicle; During the operation, if there is a sudden power failure, the data will be lost because there is no data storage function, thus reducing the practicability of the drone

Method used

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Embodiment Construction

[0035] The present invention is described in further detail now in conjunction with accompanying drawing. These drawings are all simplified schematic diagrams, which only illustrate the basic structure of the present invention in a schematic manner, so they only show the configurations related to the present invention.

[0036] Such as Figure 1-Figure 6 As shown, an intelligent drone includes a main body 1, a central control mechanism 2, a power generation mechanism 3, a flight mechanism 4 and two landing mechanisms 6, the central control mechanism 2 is arranged on the main body 1, and the power generation mechanism 3 It is arranged above the main body 1, the flying mechanism 4 is arranged on both sides of the main body 1, two landing mechanisms 6 are arranged under the main body 1 and are respectively located at both ends of the main body 1, the power generating mechanism 3 and the flying mechanism 4 are both Electrically connected with the central control mechanism 2;

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Abstract

The invention relates to an intelligent unmanned aerial vehicle, which includes a main body, a central control mechanism, a power generation mechanism, a flight mechanism and two landing mechanisms. The landing mechanism includes a roller, a transmission shaft, a first spring, a first guide rail and two buffer mechanisms. The mechanism includes a transmission rod, a transmission gear, a second guide rail and a limit rod. The central control module includes a power-failure storage protection circuit. The power-failure storage protection circuit includes an integrated circuit, an operational amplifier, a first resistor, a second resistor, a third resistor, The fourth resistor, the fifth resistor, the sixth resistor, a capacitor and a diode. The model of the integrated circuit is LT1005. In this smart drone, the landing mechanism can perform two operations on the drone when the drone is landing. Secondary buffering, thereby improving the practicability and reliability of the UAV; not only that, through the power-down storage protection circuit, when the input power becomes low, the data can be stored first, and the UAV is improved after power-off. reliability.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to an intelligent unmanned aerial vehicle. Background technique [0002] Unmanned aircraft, referred to as "drone" for short, and "UAV" for English abbreviation, is an unmanned aircraft controlled by radio remote control equipment and its own program control device. From a technical point of view, it can be divided into: unmanned fixed-wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned parawing aircraft, etc. [0003] 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 d...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/08B64C25/62G05B19/05
CPCG05B19/054B64C25/62B64C27/08B64U10/10B64U70/60
Inventor 陈科
Owner 安徽七曜航空技术有限公司