CN205145454U - Infrared homing vector machine carries guided missile of putting out a fire - Google Patents

Infrared homing vector machine carries guided missile of putting out a fire Download PDF

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Publication number
CN205145454U
CN205145454U CN201520948980.8U CN201520948980U CN205145454U CN 205145454 U CN205145454 U CN 205145454U CN 201520948980 U CN201520948980 U CN 201520948980U CN 205145454 U CN205145454 U CN 205145454U
Authority
CN
China
Prior art keywords
guided missile
fire
head
wing
infrared
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201520948980.8U
Other languages
Chinese (zh)
Inventor
徐健飞
马聪颖
徐健茹
徐子涵
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhejiang Tianwen Cci Capital Ltd
Original Assignee
ZHEJIANG YOUAN GAOKE FIRE-FIGHTING SYSTEM Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by ZHEJIANG YOUAN GAOKE FIRE-FIGHTING SYSTEM Co Ltd filed Critical ZHEJIANG YOUAN GAOKE FIRE-FIGHTING SYSTEM Co Ltd
Priority to CN201520948980.8U priority Critical patent/CN205145454U/en
Application granted granted Critical
Publication of CN205145454U publication Critical patent/CN205145454U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses an infrared homing vector machine carries guided missile of putting out a fire, including the body, the welding of body middle part has the mounted frame of two " T " fonts, be provided with the guide vane on the body, turn to the wing and the balanced wing, guide vane welding is at the body front end, and balanced wing welding is in the body rear end, and balanced wing rear end is with to turn to wing front end articulated, be provided with in the body and put the thing cavity, should put and be provided with the fire extinguishing agent in the thing cavity and scatter the trigger, fixed infrared ray camera, temperature detect ware and the wireless transmission device of being provided with of body front end, the last connecting wire that is provided with of wireless transmission device, and wireless transmission device pass through connecting wire respectively with temperature detect ware and infrared ray camera connection. Above -mentioned technical scheme, structural design is reasonable, simple structure, convenient to use, fire control effect are good.

Description

Infrared homing vector airborne fire extinguishing guided missile
Technical field
The utility model relates to fire extinguishing appliance technical field, is specifically related to a kind of infrared homing vector airborne fire extinguishing guided missile.
Background technology
Fire is arch enemy of man, and certainly from ancient times to now by now, it is always all at the property endangering people and life.Even to this day, modern science and technology and modern civilization have had the development of height, but, still have the fire of 100,000 times in China every year and even wreak havoc all over the world, people being caused and passes away greatly.
Closely for many years, though there is the fire extinguishing appliance of many indoor in-plant automatic spraying extinguishing chemicals to come out, (as: utility model patent ZLO1247004.X " infrared ray induces target-seeking Full automatic fire fighting device " etc.), occur with some technology for improving its target-seeking pointing accuracy, (as: utility model patent ZL200720114296.5 " segment compensate type horizontal scanning positioning apparatus " etc.), the target-seeking fire-fighting technique of the automation of indoor large space is developed, the fire gripping short range of going out in time is really had large improvement.But, for the fire under large wilderness, open air and open-air atmosphere, as the outdoor storage of paper mill, the pharmaceutical factory of traditional Chinese medicine, velveteen factory, the reaction tower group in oil plant, chemical plant, train, automobile, ship cargo transporting something containerized field, urban skyscraper, grassland, mountain forest ... just obviously helpless etc. numerous fire, firefighters, because not understanding fire zone temperature and the intensity of a fire, easily occurs unexpected and sacrifices in fire extinguishing procedure.
Summary of the invention
For the deficiency that prior art exists, the purpose of this utility model is to provide that a kind of reasonable in design, structure are simple, easy to use, the infrared homing vector airborne fire extinguishing guided missile of good extinguishing effect.
For achieving the above object, the utility model provides following technical scheme: a kind of infrared homing vector airborne fire extinguishing guided missile, comprise body, the hanger bracket of two " T " fonts is welded with in the middle part of described body, described body is provided with guide vane, turns to the wing and balance wing, described guide vane is welded on body front end, and balance wing is welded on body rear end, and balance wing rear end with turn to wing front end hinged; Be provided with glove cavity in described body, be provided with extinguishing chemical in this glove cavity and sow trigger; Described body front end is fixedly installed infrared pick-up head, hygrosensor and radio transmitting device, described radio transmitting device is provided with connection wire, and radio transmitting device is connected with hygrosensor and infrared pick-up head respectively by connecting wire.
By adopting technique scheme, hanger bracket arranges rationally, can be suspended on existing unmanned plane, after sending dangerous burning things which may cause a fire disaster overhead to, sows extinguishing chemical and puts out a fire, good extinguishing effect by unmanned plane; Be applicable to the fire zone such as open air, forest zone, hygrosensor is used for the temperature in detection of fires district, infrared pick-up head is for taking fire zone intensity of a fire situation, and the temperature data of fire zone and fire zone intensity of a fire video are transferred in on-the-spot existing fire fighting command car computer by radio transmitting device, so that commanding makes correct commander, to ensureing that the life security of firefighters has very important meaning.
The utility model is set to further: described body cylindrically structure, and the diameter of described body is 20-80cm.By this setting, diameter of the projectile body is arranged rationally, uses convenient.
The utility model is also set to further: described body nose threads is connected with guided missile head, and described radio transmitting device is embedded to be arranged in guided missile head.By this setting, radio transmitting device position is arranged rationally, uses convenient.
The utility model is also set to further: be connected by screw between described infrared pick-up head and guided missile head outer surface, and infrared pick-up head is arranged near radio transmitting device.By this setting, infrared pick-up head position arranges rationally, connects reliable.
The utility model is also set to further: be connected by screw between described hygrosensor and guided missile head outer surface, and hygrosensor is arranged near radio transmitting device.By this setting, hygrosensor position arranges rationally, connects reliable.
The utility model is also set to further: described body rear end is embedded is provided with power set.By this setting, power set arrange rationally, and fire extinguishing missile air range is farther.
The utility model has the advantages that: compared with prior art, the utility model vibrational power flow is more reasonable, can be suspended on existing unmanned plane, after sending dangerous burning things which may cause a fire disaster overhead to by unmanned plane by fire extinguishing guided missile by hanger bracket, sow extinguishing chemical to put out a fire, good extinguishing effect; Be applicable to the fire zone such as open air, forest zone, hygrosensor is used for the temperature in detection of fires district, infrared pick-up head is for taking fire zone intensity of a fire situation, and the temperature data of fire zone and fire zone intensity of a fire video are transferred in on-the-spot existing fire fighting command car computer by radio transmitting device, so that commanding makes correct commander, to ensureing that the life security of firefighters has very important meaning.
Below in conjunction with Figure of description and specific embodiment, the utility model is described in further detail.
Accompanying drawing explanation
Fig. 1 is the structural representation of the utility model embodiment.
Detailed description of the invention
See Fig. 1, the disclosed a kind of infrared homing vector airborne fire extinguishing guided missile of the utility model, comprise body 1, the hanger bracket 2 of two " T " fonts is welded with in the middle part of described body 1, described body 1 is provided with guide vane 3, turns to the wing 4 and balance wing 5, described guide vane 3 is welded on body 1 front end, and balance wing 5 is welded on body 1 rear end, and balance wing 5 rear end with turn to the wing 4 front end hinged; Be provided with glove cavity 11 in described body 1, be provided with extinguishing chemical 12 in this glove cavity 11 and sow trigger 13; Described body 1 front end is fixedly installed infrared pick-up head 6, hygrosensor 7 and radio transmitting device 8, described radio transmitting device 8 is provided with connection wire, and radio transmitting device 8 is connected with hygrosensor 7 and infrared pick-up head 6 respectively by connecting wire.
As preferably, described balance wing 5 rear end and turn to that to adopt bearing pin to form between the wing 4 front end hinged; Described trigger 13 of sowing is arranged on extinguishing chemical 12 medium position.
For making the utility model structure more reasonable, as preferably, body 1 cylindrically structure described in the present embodiment, the diameter of described body 1 is 20-80cm.
Described body 1 nose threads is connected with guided missile head 9, and described radio transmitting device 8 is embedded to be arranged in guided missile head 9.Be connected by screw between described infrared pick-up head 6 and guided missile head 9 outer surface, and infrared pick-up head 6 is arranged near radio transmitting device 8.Be connected by screw between described hygrosensor 7 and guided missile head 9 outer surface, and hygrosensor 7 is arranged near radio transmitting device 8.
Described body 1 rear end is embedded is provided with power set 10.Power set 10 by housing, be contained in fuel column in housing and igniter and nozzle and form.During transmitting, by existing emitter trigger point firearm pilot fuel post, high velocity air is just from nozzle ejection, and the reaction force produced orders about whole body and flies to forward.
During practical application, can fire extinguishing guided missile be suspended on existing unmanned plane by hanger bracket, after sending dangerous burning things which may cause a fire disaster overhead to by unmanned plane, sow extinguishing chemical and put out a fire, good extinguishing effect; Be applicable to the fire zone such as open air, forest zone, hygrosensor is used for the temperature in detection of fires district, infrared pick-up head is for taking fire zone intensity of a fire situation, and the temperature data of fire zone and fire zone intensity of a fire video are transferred in on-the-spot existing fire fighting command car computer by radio transmitting device, so that commanding makes correct commander, to ensureing that the life security of firefighters has very important meaning.
Above-described embodiment is to specific descriptions of the present utility model; only for being further described the utility model; can not be interpreted as the restriction to the utility model protection domain, the technician of this area makes some nonessential improvement according to the content of above-mentioned utility model to the utility model and adjustment all falls within protection domain of the present utility model.

Claims (6)

1. one kind infrared homing vector airborne fire extinguishing guided missile, comprise body (1), it is characterized in that: described body (1) middle part is welded with the hanger bracket (2) of two " T " fonts, described body (1) is provided with guide vane (3), turns to the wing (4) and balance wing (5), described guide vane (3) is welded on body (1) front end, balance wing (5) is welded on body (1) rear end, and balance wing (5) rear end with turn to the wing (4) front end hinged; Be provided with glove cavity (11) in described body (1), be provided with extinguishing chemical (12) in this glove cavity (11) and sow trigger (13); Described body (1) front end is fixedly installed infrared pick-up head (6), hygrosensor (7) and radio transmitting device (8), (8) are provided with connection wire with described radio transmitting device, and radio transmitting device (8) is connected with hygrosensor (7) and infrared pick-up head (6) respectively by connecting wire.
2. the infrared homing vector airborne fire extinguishing guided missile of one according to claim 1, it is characterized in that: described body (1) cylindrically structure, the diameter of described body (1) is 20-80cm.
3. the infrared homing vector airborne fire extinguishing guided missile of one according to claim 1 and 2, it is characterized in that: described body (1) nose threads is connected with guided missile head (9), described radio transmitting device (8) is embedded to be arranged in guided missile head (9).
4. the infrared homing vector airborne fire extinguishing guided missile of one according to claim 3, it is characterized in that: be connected by screw between described infrared pick-up head (6) and guided missile head (9) outer surface, and infrared pick-up head (6) is arranged near radio transmitting device (8).
5. the infrared homing vector airborne fire extinguishing guided missile of one according to claim 4, it is characterized in that: be connected by screw between described hygrosensor (7) and guided missile head (9) outer surface, and hygrosensor (7) is arranged near radio transmitting device (8).
6. the infrared homing vector airborne fire extinguishing guided missile of one according to claim 5, is characterized in that: described body (1) rear end is embedded is provided with power set (10).
CN201520948980.8U 2015-11-24 2015-11-24 Infrared homing vector machine carries guided missile of putting out a fire Expired - Fee Related CN205145454U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520948980.8U CN205145454U (en) 2015-11-24 2015-11-24 Infrared homing vector machine carries guided missile of putting out a fire

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520948980.8U CN205145454U (en) 2015-11-24 2015-11-24 Infrared homing vector machine carries guided missile of putting out a fire

Publications (1)

Publication Number Publication Date
CN205145454U true CN205145454U (en) 2016-04-13

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Family Applications (1)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110420412A (en) * 2019-08-21 2019-11-08 江苏汇通新能源有限公司 A kind of light-duty high-precision fire extinguisher bomb
CN112977825A (en) * 2021-03-23 2021-06-18 哈尔滨工业大学 Ejection fixed wing flying robot

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110420412A (en) * 2019-08-21 2019-11-08 江苏汇通新能源有限公司 A kind of light-duty high-precision fire extinguisher bomb
CN112977825A (en) * 2021-03-23 2021-06-18 哈尔滨工业大学 Ejection fixed wing flying robot

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20160614

Address after: 403, 325200 head, room 4, Taoyuan garden, Xincheng Road, Lucheng District, Zhejiang, Wenzhou

Patentee after: Zhejiang Tianwen Cci Capital Ltd

Address before: 325000 Zhejiang city of Wenzhou Province Jiao Feng Road No. 108 6 floor

Patentee before: Zhejiang Youan GaoKe Fire-fighting System Co., Ltd.

CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160413

Termination date: 20171124

CF01 Termination of patent right due to non-payment of annual fee