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Multi-rotor fire extinguishing unmanned aerial vehicle (UAV) system

A fire-fighting unmanned aerial vehicle and multi-rotor technology, applied to rotorcraft, unmanned aircraft, motor vehicles, etc., to achieve high cost-effectiveness, advanced principles, and high hit accuracy

Pending Publication Date: 2018-08-24
南京壹诺为航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, there are no related products in China

Method used

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  • Multi-rotor fire extinguishing unmanned aerial vehicle (UAV) system
  • Multi-rotor fire extinguishing unmanned aerial vehicle (UAV) system

Examples

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Embodiment Construction

[0032] Such as figure 1 and figure 2 A multi-rotor fire-fighting unmanned aerial vehicle system is shown, including frame 1, machine arm 2, landing gear 3, motor base 4, motor 5, quick-release paddle base 6, paddle 7, flight control system 9, battery pack 10 and a fire fighting pod 11, the machine arm 2 is installed around the frame through the arm folding connector, the landing gear 3 is installed under the main frame through the connector, and the motor base 4 is installed on The arm terminal, the motor 5 is installed on the motor base 4, the electric regulator 8 is also installed on the motor base 4, the quick release paddle base 6 is installed on the motor, and the paddle 7 is installed on the quick On the propeller removal seat, the flight control system 9 is installed at the center of the top of the frame 1, the battery pack 10 is installed on the top of the frame 1, and the fire fighting pod 11 is installed below the frame 1 , the fire extinguishing pod 11 is filled ...

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PUM

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Abstract

The invention relates to a multi-rotor fire extinguishing unmanned aerial vehicle (UAV) system, comprising a chassis, engine arms, an undercarriage, motor bases, motors, quick release propeller seats,propellers, a flight control system, a battery pack and a fire extinguishing pod, wherein the engine arms are installed at the periphery of the undercarriage by means of engine arm folding connectionpieces; the undercarriage is installed under a main body of the chassis by means of a connection piece; the motor bases are respectively installed at terminals of the engine arms; the motors are installed on the motor bases; an electronic speed controller is also installed on each motor base; the quick release propeller seats are respectively installed on the motors; the propellers are installedon the quick release propeller seats; the flight control system is installed at the central position of the top of the chassis; the battery pack is installed on the top of the chassis; the fire extinguishing pod is installed under the chassis and is internally filled with fire extinguishing bullets. The multi-rotor fire extinguishing UAV system has the advantages of being simple in structure, easyto manufacture, practical and efficient.

Description

technical field [0001] The invention belongs to the technical field of multi-rotor UAVs, and in particular relates to a multi-rotor UAV system for fire fighting. Background technique [0002] Multi-rotor drones use lithium batteries as power, and have the advantages of simple structure, stable flight, and easy control. UAV systems based on multi-rotor drones for land surveying, agricultural plant protection, and anti-terrorism have been widely used. [0003] Due to the increasing number of high-rise and super high-rise buildings in major and medium-sized cities, the problem of fire fighting has always been a problem in the world. Using drones for fire fighting is an effective solution. Multi-rotor drones have good safety performance and are suitable for use in For internal use in cities, it is an effective solution to use multi-rotor UAVs to carry fire extinguishing devices for fire fighting activities in urban high-rise buildings. At present, there is no related product co...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64C27/08B64D1/06B64C27/14A62C3/02
CPCA62C3/025B64C27/08B64C27/14B64C39/024B64D1/06B64U50/19B64U10/10B64U2101/00
Inventor 葛贤坤乔治军张先锋马宏伟诸庆生
Owner 南京壹诺为航空科技有限公司
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