Fire extinguishing unmanned helicopter system

An unmanned helicopter and firefighting technology, which is applied to unmanned aerial vehicles, rotorcraft, motor vehicles, etc., can solve the problems of lack of technology and supporting products, insufficient flexibility, and fixed-wing drones that cannot hover. Solve the effect of slow deployment, advanced principles, and easy use of a large number of equipment

Pending Publication Date: 2018-07-06
江苏天域航空科技集团股份有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[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 difficult problem in the world. Using drones for fire fighting is an effective solution. Since fixed-wing drones cannot hover and have flexibility Not enough, only rotor UAVs can be used to develop consumer fire-fighting UAV systems
At present, there is no relevant mature technology and supporting products

Method used

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  • Fire extinguishing unmanned helicopter system

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Embodiment Construction

[0024] Such as figure 1 Shown the present invention provides a kind of unmanned helicopter system of fire-fighting and fire-fighting, comprise body structure, power system, flight control system, fire-fighting fire-extinguishing pod and fire-fighting fire-fighting bomb, described body structure is made up of main rotor 1, housing 2, The tail rotor 3 and the landing gear 4 are composed, the landing gear 4 is arranged on the bottom of the housing 2, the main rotor 1 is installed on the top of the housing 2, and the tail rotor 3 is installed on the tail of the housing 2 On the side wall of the end; the power system is the engine 5, the engine 5 is installed in the housing 2, the engine 5 is connected with the main rotor 1 and the tail rotor 3; the row control system is powered by the battery 6 , sensor system 7, integrated flight control system 8, and differential GPS system 9 together form an unmanned helicopter. The battery 6, sensor system 7 and integrated flight control syste...

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Abstract

The invention relates to a fire extinguishing unmanned helicopter system, which comprises a body structure, a power system, a flight control system, a fire extinguishing pod and a fire extinguishing bomb. The body structure comprises a main rotor, a casing, a tail rotor and a landing gear. The landing gear is disposed at the bottom of the casing, the main rotor is mounted on the top of the casing,and the tail rotor is mounted on the side wall of the rear end of the casing; the power system is an engine, the engine is mounted in a casing, the engine is coupled to the main rotor and the tail rotor; the fire extinguishing pod is mounted at the bottom of the casing, the fire extinguishing pod is located within the landing gear, and the fire extinguishing bomb is loaded inside the fire extinguishing pod; by adopting the structure, the fire extinguishing unmanned helicopter system has the advantages of low cost, high efficiency and high cost-effectiveness, and is convenient for a large number of devices.

Description

technical field [0001] The invention belongs to the technical field of unmanned helicopters, and in particular relates to an unmanned helicopter system for fire fighting. Background technique [0002] Medium and large unmanned helicopters generally use oil-powered engines as power, which have the advantages of large load, long battery life, ability to hover in the air, good stability, and easy control. UAV systems for various industrial applications based on unmanned helicopters are developing rapidly. [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 difficult problem in the world. Using drones for fire fighting is an effective solution. Since fixed-wing drones cannot hover and have flexibility Not enough, can only adopt rotor UAV to develop consumer fire extinguishing UAV system. At present, there is no relevant mature technology and supporting products. Cont...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/06B64D1/02A62C3/02
CPCA62C3/0214A62C3/025B64C27/06B64D1/02B64U50/11B64U10/10
Inventor 章晨光管建伟马玉涛葛贤坤
Owner 江苏天域航空科技集团股份有限公司
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