首页> 外国专利> FIRE-EXTINGUISHING BOMB ROCKET

FIRE-EXTINGUISHING BOMB ROCKET

机译:灭火炸弹火箭

摘要

An objective of the present invention is to provide a fire-extinguishing bomb rocket which is loaded in an unmanned aerial vehicle, uses propulsion of fire-extinguishing chemicals and water by compressed gas to quickly reach a fire place, and releases the fire-extinguishing chemicals in stages to efficiently suppress a fire. To this end, the fire-extinguishing bomb rocket comprises: a propulsion unit making up a rear portion of a fire-extinguishing bomb, separating and storing compressed gas and first chemicals for generation of primary propulsion and fire extinguishing, and generating first propulsion by injection of the first chemicals by the compressed gas; and a warhead unit installed on the front end of the propulsion unit as a body of the same diameter as the propulsion unit to make up a front body of the fire-extinguishing bomb, separate and store compressed gas and second chemicals for generation of secondary propulsion and fire extinguishing, and generate secondary propulsion by injection of the second chemicals by the compressed gas. The fire-extinguishing bomb rocket is separably fixed and loaded on a rocket launcher in a rocket loading compartment of an unmanned aerial vehicle, is separated and launched from the rocket launcher by the primary propulsion by injection of the first chemicals of the propulsion unit, and is accelerated by the secondary propulsion by injection of the second chemicals of the warhead unit. The injection of the first chemicals and the injection of the second chemicals of the warhead unit are carried out in stages to load the fire-extinguishing bomb rocket in the unmanned aerial vehicle. The fire-extinguishing bomb rocket can quickly reach a fire place by using propulsion of fire-extinguishing chemicals and water by compressed gas. The fire-extinguishing chemicals can be released in stages while moving to the fire place after being launched from the unmanned aerial vehicle or after reaching the fire place.;COPYRIGHT KIPO 2020
机译:本发明的目的是提供一种灭火炸弹火箭,其安装在无人飞行器中,利用灭火气体和压缩气体推动水快速到达火场,并释放灭火化学物质。分阶段有效地扑灭火灾。为此,灭火炸弹火箭包括:推进单元,其构成灭火炸弹的后部,分离并存储压缩气体和第一化学物质以产生初级推进和灭火,以及通过注射产生第一推进压缩气体中的第一种化学物质;弹头单元,其直径与推进单元的直径相同,安装在推进单元的前端,以构成灭火弹的前体,分离并储存压缩气体和第二化学物质以产生二次推进灭火,并通过压缩气体注入第二种化学物质产生二次推进。灭火弹火箭被分别固定并装载在无人飞行器的火箭装载室中的火箭发射器上,通过一次推进通过注入推进单元的第一化学物质而与火箭发射器分离并发射,并且通过注入弹头单元的第二种化学物质,通过二次推进而加速。弹头单元的第一化学药品的注入和第二化学药品的注入是分阶段进行的,以将灭火炸弹火箭装载到无人机上。通过利用压缩气体推动灭火化学物质和水,灭火弹火箭可以迅速到达火场。从无人飞行器发射后或到达火场后,灭火化学物质可分阶段释放到火场。COPYRIGHTKIPO 2020

著录项

  • 公开/公告号KR102014361B1

    专利类型

  • 公开/公告日2019-08-26

    原文格式PDF

  • 申请/专利权人 HA SANG KYUN;DRONGO CO. LTD.;

    申请/专利号KR20180046454

  • 发明设计人 HA SANG KYUNKR;

    申请日2018-04-23

  • 分类号A62C3/02;A62C19;B64C39/02;B64D1/06;

  • 国家 KR

  • 入库时间 2022-08-21 11:47:55

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