Intelligent multipurpose rescue unmanned aircraft

An unmanned aerial vehicle, multi-purpose technology, applied in the field of rescue unmanned aerial vehicle, can solve the problems of poor environmental protection, the flying distance of the aircraft body is not far, the power is insufficient, etc., and achieve the effect of good environmental protection

Active Publication Date: 2015-05-13
NINGBO CITY HIGH TECH ZONE YONGJING MICROELECTRONICS
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, the energy used in the energy supply system is mainly gasoline, which leads to the following problems for rescue unmanned aerial vehicles: 1. Pollution to the environment, poor environmental protection; 2. The available power of the power drive system is insufficient, so only four One or even t

Method used

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  • Intelligent multipurpose rescue unmanned aircraft

Examples

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Example Embodiment

[0016] Embodiment: As shown in the figure, an intelligent multi-purpose rescue unmanned aerial vehicle includes an aircraft body, a main control system, a power drive system, and an energy supply system. The aircraft body includes a base 1 and a top cover 2 arranged on the base 1. The base 1 and the top cover 2 are made of hydrogen storage metal materials. A sealed compartment 3 is formed between the base 1 and the top cover 2. The energy supply system includes a solar panel 4, an organic fuel cell, and a lithium battery arranged above the top cover 2. The solar panel 4 and the organic fuel cell are connected to the lithium battery, the lithium battery is connected to the super capacitor, and the super capacitor is connected to the main control system and the power drive system. The bottom of the base 1 is provided with a first interlayer 5, the solar panel A second interlayer 6 is arranged between the top cover 4 and the top cover 2. A plurality of airbags for accommodating hyd...

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Abstract

The invention discloses an intelligent multipurpose rescue unmanned aircraft, including an aircraft body, a main control system, a power drive system and an energy supply system, the aircraft body comprises a base and a top cover arranged on the base, the base and the top cover materials are hydrogen storage metal materials, a sealed chamber is formed between the base and the top cover, the energy supply system includes a solar panel, an organic fuel cell, a lithium cell and a super capacitor which are arranged above the top cover, the solar panel and the organic fuel cell are respectively connected with the lithium cell, the lithium cell is connected with the super capacitor, the super capacitor is respectively connected with the main control system and the power drive system, a first interlayer is arranged on the bottom of the base, a second interlayer is arranged between the solar panel and the top cover, the first interlayer and the second interlayer are respectively provided with a plurality of hydrogen accommodating airbags, the plurality of hydrogen accommodating airbags are connected with the organic fuel cell by pipes, and the intelligent multipurpose rescue unmanned aircraft has the advantages of better environmental protection property, and sufficient available power of the power drive system.

Description

technical field [0001] The invention relates to a rescue unmanned aerial vehicle, in particular to an intelligent multi-purpose rescue unmanned aerial vehicle. Background technique [0002] An unmanned aerial vehicle refers to a flying device that does not require direct driving and control by a human being. Generally speaking, it is an unmanned aircraft. At present, various types of unmanned aerial vehicles are spread across various fields. Among them, the rescue UAV is mainly used in the rescue field for information transmission and material delivery. [0003] The traditional rescue unmanned aerial vehicle mainly includes the main control system, the aircraft body, the power drive system and the energy supply system. The energy supply system provides the power required for the work of the main control system and the power drive system, and the power drive system drives the aircraft body to fly according to the control commands of the main control system. At present, the...

Claims

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Application Information

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IPC IPC(8): B64C1/00B64C27/08B64D27/02B64D27/24
CPCY02T90/40
Inventor 张承彬张国鹏
Owner NINGBO CITY HIGH TECH ZONE YONGJING MICROELECTRONICS
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