KR20070101675A - Fire extinguishing rocket fire for long distance fire extinguishing - Google Patents

Fire extinguishing rocket fire for long distance fire extinguishing Download PDF

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KR20070101675A
KR20070101675A KR1020060033047A KR20060033047A KR20070101675A KR 20070101675 A KR20070101675 A KR 20070101675A KR 1020060033047 A KR1020060033047 A KR 1020060033047A KR 20060033047 A KR20060033047 A KR 20060033047A KR 20070101675 A KR20070101675 A KR 20070101675A
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fire
rocket
warhead
timer
extinguishing agent
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이웅부
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이웅부
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    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62C—FIRE-FIGHTING
    • A62C19/00—Hand fire-extinguishers in which the extinguishing substance is expelled by an explosion; Exploding containers thrown into the fire
    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62C—FIRE-FIGHTING
    • A62C3/00—Fire prevention, containment or extinguishing specially adapted for particular objects or places
    • A62C3/02—Fire prevention, containment or extinguishing specially adapted for particular objects or places for area conflagrations, e.g. forest fires, subterranean fires
    • A62C3/0228—Fire prevention, containment or extinguishing specially adapted for particular objects or places for area conflagrations, e.g. forest fires, subterranean fires with delivery of fire extinguishing material by air or aircraft
    • A62C3/025—Fire extinguishing bombs; Projectiles and launchers therefor

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  • Health & Medical Sciences (AREA)
  • Public Health (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)

Abstract

본 발명은 로켓형으로 발사되는 소화로켓탄을 구성하여 발사장치에 의해 발사되면 먼 거리에 있는 화재장소까지 비행한 후 화재장소의 상공 일정 높이에서 폭파되어 소화약제를 살포토록 하는 것을 특징으로 하는 것이다.The present invention is characterized by constituting a fire rocket fired in a rocket type, when fired by the launching device to fly to a fire place in the distance and then blasted at a predetermined height above the fire place to examine the extinguishing agent.

구성의 요지로는 탄두(10)가 일반적인 군사용 포탄과 유사하게 유선형을 가지면서 수개의 날개(11)를 갖고, 표면에는 절개홈(12)을 다수 형성하며, 탄두(10)의 앞쪽에는 제어장치를 설치할 장치공간(16)을 마련한 후, 소화로켓탄(1)의 발사를 위한 점화장치(21)의 점화와 동시에 작동을 시작하는 타이머(13)를 설치하고, 그 나머지 탄두(10)의 내부에는 액체 또는 분말 형태의 소화약제(17)를 압축된 상태로 충진하고, 소화약제(17)의 중앙에 폭약(18)을 장착하고 상기 타이머(13)와 연결되어 타이머(13)의 작동완료 신호를 받아 점화하는 전자뇌관(19)을 폭약(18)에 장착하며, 탄두(10)의 후단에는 장거리 추진을 위해 추진용 연료가 충진되는 로켓추진체(20)를 형성하며, 탄두(10)의 후단 내부에는 로켓추진체(20)에서 발생하는 열을 차단하기 위한 단열성능이 뛰어나고 내열성이 뛰어난 비금속 재질로 된 차열판(30)을 구성함을 특징으로 한다. The gist of the configuration is that the warhead 10 has a streamlined shape similar to a general military shell, has several wings 11, forms a plurality of incision grooves 12 on the surface, and a control device in front of the warhead 10. After the device space 16 is installed, a timer 13 for starting operation at the same time as the ignition of the ignition device 21 for firing the fire rocket bullet 1 is installed, and the remaining warhead 10 is installed inside. The extinguishing agent 17 in a liquid or powder form is filled in a compressed state, and an explosive charge 18 is mounted at the center of the extinguishing agent 17 and connected to the timer 13 to signal an operation completion signal of the timer 13. Receiving and ignited electron primer 19 is mounted on the explosives 18, the rear end of the warhead 10 forms a rocket propeller 20 is filled with a propulsion fuel for long-distance propulsion, inside the rear end of the warhead 10 Excellent heat insulation and heat resistance to block the heat generated from the rocket propeller 20 The heat shield plate 30 is made of a non-metallic material having excellent properties.

Description

장거리 화재 진화용 소화로켓탄{Fire extinguishing rocket bomb for long distance fire extinguish}Fire extinguishing rocket bomb for long distance fire extinguish}

도 1은 본 발명에 의한 소화로켓탄의 정면도1 is a front view of a fire rocket bullet according to the present invention.

도 2는 본 발명에 의한 소화로켓탄의 부분 단면도2 is a partial cross-sectional view of the fire rocket bullet according to the present invention.

도 3은 본 발명의 소화로켓탄을 발사하기 위한 발사장치 예시도 Figure 3 is an illustration of a launch device for firing a rocket fire of the present invention

***도면 중 주요 부분에 대한 부호의 설명****** Description of the symbols for the main parts of the drawings ***

1: 소화로켓탄1: fire rocket

10: 탄두10: warhead

11: 날개11: wings

12: 절개홈12: incision groove

13: 타이머13: timer

14: 센서14: sensor

15: 회로기판15: circuit board

16: 장치공간16: device space

17: 소화약제 17: extinguishing agent

18: 폭약18: explosive

19: 뇌관19: primer

20: 로켓추진체20: rocket prop

21: 점화장치21: igniter

30: 차열판30: heat shield

본 발명은 소방차량이나 화재진압을 위한 인원이 근접하기 어려운 위치이거나 긴급한 상태에서 매우 먼 거리의 화재를 진압하여야 하는 경우에, 로켓탄과 같은 형태로 발사하여 먼 거리에 있는 화재장소의 바로 위 공중에서 소화용 약제가 폭발에 의해 산포되도록 함으로써 유용하게 화재를 진압할 수 있는 화재 진화용 소화(消火)로켓탄에 관한 것이다. The present invention is to fire in the form of a rocket bullet in the air immediately above the place of fire in the case of fire trucks or fire extinguishing personnel or in case of emergency to extinguish very long distance fire in the emergency state The present invention relates to a fire extinguishing rocket fire for extinguishing a fire usefully by causing a fire extinguishing agent to be dispersed by an explosion.

주지된 바와 같이 대규모의 산불이 발생하거나 차량 또는 사람이 근접하기 어려운 위치에서 화재가 발생할 경우에는 화재를 진압하는데 많은 어려움을 겪고 신속히 진압할 방법이 없어 엄청난 피해를 초래하게 되었던 것이다.As is well known, when a large-scale forest fire occurs or a fire occurs in a location where a vehicle or a person is difficult to approach, it is difficult to extinguish the fire and there is no way to extinguish it quickly, which causes enormous damage.

즉, 통상적인 화재진압 방법에 의하면 물이나 소화약재를 필요한 위치에 뿌려주는 정도에 불과하여 대규모이거나 강력한 화재 시에는 효과적인 진화가 불가능하다 할 수 있다.In other words, according to the conventional fire suppression method, the water or extinguishing agent is sprayed only in the required position, and in the case of a large-scale or strong fire, an effective extinguishing may not be possible.

이러한 경우에는 통상 소방용 헬기를 이용하여 화재를 진압하기도 하지만 이러한 헬기는 악천후 시에나 야간에는 위험성 때문에 출동하기가 어려우며, 물이 많은 저수지나 강까지 왕복하면서 물을 채워 화재현장에 투하하여야 하는 번거로움이 있어서 효율적이지 못한 단점이 있는 것이다.In this case, firefighting helicopters are usually used to extinguish the fire. However, such helicopters are difficult to operate due to dangers during bad weather or at night. The disadvantage is that it is not efficient.

상기한 문제점에 의해 안출된 본 발명은 탄두부분에 압축된 소화약제와 폭발용 폭약을 구비하고 후단에는 추진연료를 충진한 로켓추진체를 구비하며, 별도의 발사장치를 이용하여 발사시킴으로써 로켓추진체의 추진연료에 의해 장거리까지 비행하여 원하는 지점의 공중에서 폭발하여 소화약제가 산포되도록 함으로써 원거리의 화재를 효과적으로 진화하도록 함을 목적으로 하는 것이다. The present invention devised by the above problems is provided with a fire extinguishing agent and explosive explosives compressed in the warhead portion and provided with a rocket propeller filled with a propellant fuel at the rear end, the propulsion of the rocket propeller by firing using a separate launch device. It aims to effectively extinguish a long-distance fire by flying a long distance by fuel, exploding in the air at a desired point, and dispersing extinguishing agent.

본 발명은 로켓형으로 발사되는 소화로켓탄을 구성하되, 전방에는 소화약제가 압축 내장된 소화탄두가 형성되고 내부에는 폭파용 화약이 내장되며, 후단에는 원거리까지 추진을 가능하게 하도록 연료를 채운 추진체가 구성되고 내부에는 타이머장치 및 그와 연결되는 뇌관이 구성되어, 발사장치에 의해 발사되면 먼 거리에 있는 화재장소까지 비행한 후 화재장소의 상공 일정 높이에서 폭파되어 소화약제를 살포토록 하는 것을 특징으로 하는 것이다.The present invention constitutes a rocket-type fire rocket fired, the front is formed with a fire extinguishing extinguisher is built-in extinguishing warhead and the blasting gun is built in, the rear end of the propellant filled with fuel to enable propulsion to a long distance. It is composed of a timer device and a primer connected therein, and when fired by the launching device is characterized by flying to a fire place at a distant place and then blasted at a certain height above the fire place to examine the extinguishing agent. It is.

이하 첨부된 도면에 의거 본 발명의 바람직한 구성 실시 예를 살펴보면 다음과 같다.Looking at a preferred embodiment of the present invention based on the accompanying drawings as follows.

도 1은 본 발명에 의한 소화로켓탄의 정면도, 도 2는 본 발명에 의한 소화로켓탄의 부분 단면도이다.1 is a front view of a fire rocket bullet according to the present invention, Figure 2 is a partial cross-sectional view of the fire rocket bullet according to the present invention.

본 발명의 소화로켓탄(1)은 탄두(10)가 일반적인 군사용 포탄과 유사하게 유선형을 가지면서 후단 쪽에 수개의 날개(11)를 갖고, 표면에는 폭발시 균일하게 잘 파손되도록 하는 절개홈(12)을 다수 형성하였다. Extinguishing rocket bullet 1 of the present invention has a plurality of wings 11 at the rear end while having a warhead 10 has a streamlined similar to a general military shell, the incision groove 12 to be uniformly well broken during the explosion on the surface A large number was formed.

탄두(10)의 앞쪽에는 타이머(13)와 센서(14), 회로기판(15) 등의 제어장치를 설치할 장치공간(16)을 마련하였고, 그 나머지 탄두(10)의 내부에는 액체 또는 분말 형태의 소화약제(17)가 압축된 상태로 충진되며, 소화약제(17)가 분산되도록 폭약(18)을 중앙에 장착하고 상기 타이머(13)와 연결되어 점화하는 전자뇌관(19)을 폭약(18)에 장착한다.In front of the warhead 10, a device space 16 for installing a control device such as a timer 13, a sensor 14, and a circuit board 15 is provided, and the remaining warhead 10 has a liquid or powder form. The fire extinguishing agent 17 is filled in a compressed state, and the explosive agent 17 is mounted in the center so that the fire extinguishing agent 17 is dispersed, and the electron primer 19 which is connected to the timer 13 and ignited explodes (18). )).

탄두(10) 선단의 장치공간(16)에는 소화로켓탄(1)의 발사를 위한 점화장치(21)의 점화와 동시에 작동을 시작하는 타이머(13)가 구비되며, 상기 전자뇌관(19)이 타이머(13)의 작동완료 신호를 받아 작동함으로써 폭약(18)을 폭발시키도록 구성하였다. The device space 16 at the tip of the warhead 10 is provided with a timer 13 for starting operation at the same time as the ignition of the ignition device 21 for firing the fire rocket bomb 1, and the electron primer 19 is a timer. It was configured to explode the explosive (18) by receiving the operation completion signal of (13).

탄두(10)의 후단에는 장거리 추진을 위해 로켓추진체(20)가 형성되는데 내부에는 추진용 연료가 충진되고 후단 끝에는 점화장치(21)가 구성된다. The rear end of the warhead 10 is formed with a rocket propulsion body 20 for long-distance propulsion, the fuel for propulsion is filled therein and the ignition device 21 is configured at the rear end.

탄두(10)의 후단 내부에는 로켓추진체(20)에서 발생하는 열을 차단하기 위한 단열성능이 뛰어나고 내열성이 뛰어난 비금속 재질로 된 차열판(30)을 구성하였다. Inside the rear end of the warhead 10 was configured a heat shield plate 30 made of a non-metallic material having excellent heat insulating performance and excellent heat resistance to block heat generated from the rocket propeller 20.

도면 중 미설명된 부호 100은 발사장치이다. Reference numeral 100 in the drawings is a launch device.

이러한 구성으로 된 본 발명의 소화로켓탄(1)은 별도의 발사장치(100)에 의해 발사되는데, 발사장치의 한 예로는 도 3과 같다.Fire extinguisher rocket (1) of the present invention having such a configuration is launched by a separate launch device 100, an example of the launch device is shown in FIG.

발사장치(100)에 본 발명의 소화로켓탄(1)을 장전한 후에 점화장치(21)를 이용하여 점화를 하게 되면, 점화장치에 의해 로켓추진체(20)의 연료가 연소되면서 그 힘으로 소화로켓탄(1)이 발사되어 날아가게 되는 것이다.When the fire ignition rocket ignition using the ignition device 21 after loading the fire rocket rocket (1) of the present invention to the launch device 100, the rocket propulsion fuel 20 is burned by the ignition device with the power to fire rocket bullet (1) is fired to fly.

이와 같은 점화순간을 감지하여 타이머(13)의 작동을 시작하게 되는데, 미리 발사장소로부터 화재 장소의 공중까지의 거리를 파악하여 발사시간부터 폭발할 시간을 설정하여 두는 것이고, 따라서 화재 장소의 공중에 도달하였을 때 타이머(13)는 뇌관(19)을 작동시켜 폭약을 폭파시키게 된다. By detecting such an ignition moment, the operation of the timer 13 is started. The distance from the launching place to the air of the fire place is determined in advance to set the time to explode from the firing time. When reached, the timer 13 operates the primer 19 to explode the explosive.

폭약이 폭파되면서 탄두(1)가 조각이 나게 되며 이에 따라 내부에 충진된 소화약제가 분산되면서 화재를 진화하게 되는 것이다.As explosives are exploded, warheads (1) are fragmented, thus extinguishing fires as the extinguishing agent filled inside is dispersed.

그리고 본 발명에 의하면 탄두(10)의 후미 내부에 차열판(30)을 구성하였으므로 상기 로켓추진체(20)의 연료가 연소되면서 날아가는 도중에 로켓추진체(20)에서 발생하는 열이 탄두(10) 내부의 소화약제(17)나 폭약(18)에 영향을 주지 않게 된다.In addition, according to the present invention, since the heat shield plate 30 is formed inside the rear of the warhead 10, the heat generated from the rocket propeller 20 during the flight of the fuel of the rocket propeller 20 is burned. It does not affect the extinguishing agent (17) or explosives (18).

이상 설명한 바와 같은 본 발명에 의하면, 로켓추진체에 의해 원거리를 비행한 후 화재장소의 공중에서 폭파하면서 소화약제를 분산시키게 되므로 효과적으로 화재를 진압하게 되는 것으로, 신속한 출동이 어렵거나 근접하여 진화가 어려운 산불이나 특수한 여건에서 발생한 화재를 진화하기에 매우 용이하게 되어 새로운 화재진압의 수단으로 유용하게 사용될 뛰어난 발명이라 할 것이다.According to the present invention as described above, since the rocket propulsion to fly a long distance and to explode the fire extinguishing agent while blowing in the air of the fire place to effectively extinguish the fire, it is difficult to move quickly or difficult to close forest fire However, it is very easy to extinguish a fire that occurred in a special condition, so it is an excellent invention to be used as a means of extinguishing a new fire.

Claims (1)

탄두(10)가 일반적인 군사용 포탄과 유사하게 유선형을 가지면서 후단 쪽에 수개의 날개(11)를 갖고, 표면에는 절개홈(12)을 다수 형성하며, The warhead 10 has a streamlined shape similar to a general military shell, has several wings 11 at the rear end, and forms a plurality of incision grooves 12 on the surface thereof. 탄두(10)의 앞쪽에는 제어장치를 설치할 장치공간(16)을 마련한 후, 소화로켓탄(1)의 발사를 위한 점화장치(21)의 점화와 동시에 작동을 시작하는 타이머(13)를 설치하고, In front of the warhead 10 is provided with a device space 16 for installing the control device, a timer 13 for starting operation at the same time as the ignition of the ignition device 21 for the firing of the fire rocket shell (1) is installed, 그 나머지 탄두(10)의 내부에는 액체 또는 분말 형태의 소화약제(17)를 압축된 상태로 충진하고, The remaining warhead 10 is filled with a compressed extinguishing agent 17 in a liquid or powder form in a compressed state, 소화약제(17)의 중앙에 폭약(18)을 장착하고 상기 타이머(13)와 연결되어 타이머(13)의 작동완료 신호를 받아 점화하는 전자뇌관(19)을 폭약(18)에 장착하며,Equipped with an explosive (18) in the center of the extinguishing agent (17) and is connected to the timer (13) is equipped with an electrodetonator (19) to receive the operation completion signal of the timer 13 to the explosive (18), 탄두(10)의 후단에는 장거리 추진을 위해 추진용 연료가 충진되는 로켓추진체(20)를 형성하며, The rear end of the warhead 10 forms a rocket propulsion body 20 filled with a propulsion fuel for long-distance propulsion, 탄두(10)의 후단 내부에는 로켓추진체(20)에서 발생하는 열을 차단하기 위한 단열성능이 뛰어나고 내열성이 뛰어난 비금속 재질로 된 차열판(30)을 구성함을 특징으로 하는 장거리 화재 진화용 소화로켓탄. The rear end of the warhead (10) fire extinguishing rocket fire for long-distance fire, characterized in that the heat shield to block the heat generated from the rocket propeller 20, and the heat shield plate 30 made of a non-metal material excellent in heat resistance .
KR1020060033047A 2006-04-12 2006-04-12 Fire extinguishing rocket fire for long distance fire extinguishing Ceased KR20070101675A (en)

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2403931C1 (en) * 2009-09-29 2010-11-20 Сергей Петрович Белоконь Method of fire extinguisting with application of armoured vehicle
RU2403932C1 (en) * 2009-09-21 2010-11-20 Сергей Петрович Белоконь Method of fire extinguisting with application of armoured vehicle
KR101037659B1 (en) * 2010-07-14 2011-05-27 (주)오티에스 Fire extinguishers
CN106890413A (en) * 2017-04-28 2017-06-27 成都谍翼科技有限公司 Fire-fighting rocket projectile and fire-fighting system
CN106955442A (en) * 2017-04-28 2017-07-18 成都谍翼科技有限公司 Fire-fighting rocket projectile and fire-fighting system
CN107551422A (en) * 2017-09-13 2018-01-09 成都谍翼科技有限公司 Fire extinguisher bomb, fire-fighting system and control method
CN107670201A (en) * 2017-08-31 2018-02-09 上海机电工程研究所 UAV system type fire extinguishing system
KR20190123393A (en) 2018-04-24 2019-11-01 정재성 Grenade for fire extinguish structure of high buildings
WO2021107261A1 (en) * 2019-11-27 2021-06-03 아이브에어크레프트(주) Powder fire-extinguishing agent-filled bullet starch fire extinguisher for extinguishing fires
KR20210073837A (en) 2019-12-11 2021-06-21 김진영 Fire suppression equipment and fire suppression method using thereof
KR20210125390A (en) 2020-04-08 2021-10-18 김진영 Grenade launching equipment for fire suppression and fire suppression method using thereof
CN115869568A (en) * 2023-01-18 2023-03-31 太原理工大学 Reusable non-explosive fire extinguishing bomb and fire extinguishing system
KR102663254B1 (en) * 2023-03-13 2024-05-03 홍권표 Fire extinguishing device using long-range projectile

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2403932C1 (en) * 2009-09-21 2010-11-20 Сергей Петрович Белоконь Method of fire extinguisting with application of armoured vehicle
RU2403931C1 (en) * 2009-09-29 2010-11-20 Сергей Петрович Белоконь Method of fire extinguisting with application of armoured vehicle
KR101037659B1 (en) * 2010-07-14 2011-05-27 (주)오티에스 Fire extinguishers
CN106890413A (en) * 2017-04-28 2017-06-27 成都谍翼科技有限公司 Fire-fighting rocket projectile and fire-fighting system
CN106955442A (en) * 2017-04-28 2017-07-18 成都谍翼科技有限公司 Fire-fighting rocket projectile and fire-fighting system
CN107670201A (en) * 2017-08-31 2018-02-09 上海机电工程研究所 UAV system type fire extinguishing system
CN107551422A (en) * 2017-09-13 2018-01-09 成都谍翼科技有限公司 Fire extinguisher bomb, fire-fighting system and control method
KR20190123393A (en) 2018-04-24 2019-11-01 정재성 Grenade for fire extinguish structure of high buildings
WO2021107261A1 (en) * 2019-11-27 2021-06-03 아이브에어크레프트(주) Powder fire-extinguishing agent-filled bullet starch fire extinguisher for extinguishing fires
KR20210073837A (en) 2019-12-11 2021-06-21 김진영 Fire suppression equipment and fire suppression method using thereof
KR20210125390A (en) 2020-04-08 2021-10-18 김진영 Grenade launching equipment for fire suppression and fire suppression method using thereof
CN115869568A (en) * 2023-01-18 2023-03-31 太原理工大学 Reusable non-explosive fire extinguishing bomb and fire extinguishing system
CN115869568B (en) * 2023-01-18 2023-06-30 太原理工大学 A reusable non-explosive fire extinguishing bomb and fire extinguishing system
KR102663254B1 (en) * 2023-03-13 2024-05-03 홍권표 Fire extinguishing device using long-range projectile

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