CN215098277U

CN215098277U - High-altitude multi-emission fire-fighting unmanned aerial vehicle

Info

Publication number: CN215098277U
Application number: CN202121168774.7U
Authority: CN
Inventors: 陈春燕
Original assignee: Jiangsu Xinyan Fire Fighting Equipment Co ltd
Current assignee: Jiangsu Xinyan Fire Fighting Equipment Co ltd
Priority date: 2021-05-27
Filing date: 2021-05-27
Publication date: 2021-12-10
Anticipated expiration: 2031-05-27

Abstract

The utility model relates to a fire control unmanned aerial vehicle technical field that puts out a fire specifically is high altitude multiple-emission unmanned aerial vehicle that puts out a fire, including the unmanned aerial vehicle main part, the unmanned aerial vehicle main part is including being used for this accurate location structure of going on fixing a position to the conflagration scene, location structure both sides all are equipped with branch along width direction's both ends, the one end that location structure was kept away from to branch is equipped with the screw, four corners in location structure bottom all are equipped with the undercarriage, the undercarriage bottom is equipped with the buffer structure who is used for improving this unmanned aerial vehicle buffer power when descending, location structure bottom and the position that is located between four undercarriages are equipped with the mounting panel, the mounting panel bottom is equipped with the emission structure who is used for improving fire extinguishing efficiency, through setting up buffer structure, make this unmanned aerial vehicle's shock resistance by effectual improvement, thereby can effectively avoid descending in-process unmanned aerial vehicle main part impaired risk.

Description

High-altitude multi-emission fire-fighting unmanned aerial vehicle

Technical Field

The utility model relates to a fire control unmanned aerial vehicle technical field specifically is high altitude multi-launch formula fire control unmanned aerial vehicle that puts out a fire.

Background

Unmanned aerial vehicle fire control is taken as a novel industrial technology, widely applied to various fields, at home, many fire-fighting institutions have used unmanned aerial vehicles to successfully perform fire scene investigation monitoring, throwing rescue goods and materials and other attempts, the effect is very obvious, in Tianjin explosion accident rescue, all departments also use unmanned aerial vehicles to perform high-altitude investigation on accident sites, partial reference basis is provided for rescue decision making, the unmanned aerial vehicles gradually enter the visual field of people along with the popularization of science and technology, the industrial unmanned aerial vehicles are also gradually applied to all the fields to play the own role, particularly in the high-risk field mainly taking fire control, the unmanned aerial vehicles are used for replacing partial manpower action, and the importance of the fire-fighting industry is self-evident.

However, the existing fire-fighting unmanned aerial vehicle still has a lot of defects, in the prior art, the fire-fighting unmanned aerial vehicle can be used for throwing fire extinguishing bomb in the process of fire fighting, but usually cannot realize accurate positioning, so that sometimes the fire extinguishing bomb cannot be accurately thrown to the vicinity of a fire source; the landing gear of the existing fire-fighting unmanned aerial vehicle is poor in shock resistance generally, and when the fire-fighting unmanned aerial vehicle lands on the ground, a large force is generated generally, so that the risk of damaging the unmanned aerial vehicle body exists; and present unmanned aerial vehicle of putting out a fire can only realize single-shot technique usually to make current unmanned aerial vehicle of putting out a fire's efficiency of putting out a fire not high.

Therefore, there is a need to design a high altitude multi-launch fire fighting unmanned aerial vehicle to solve the above problems in the background art.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a many transmission of high altitude unmanned aerial vehicle that disappears to solve the problem that proposes in the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme:

high altitude multi-launch formula fire control unmanned aerial vehicle that puts out a fire, including the unmanned aerial vehicle main part, the unmanned aerial vehicle main part is including being used for this unmanned aerial vehicle accurate location structure of going on fixing a position to the scene of conflagration, location structure both sides all are equipped with branch along width direction's both ends, the one end that location structure was kept away from to branch is equipped with the screw, four corners in location structure bottom all are equipped with the undercarriage, the undercarriage bottom is equipped with the buffer structure who is used for improving this unmanned aerial vehicle buffer power when descending, location structure bottom and the position that is located between four undercarriage are equipped with the mounting panel, the mounting panel bottom is equipped with the launch structure that is used for improving fire extinguishing efficiency.

As the utility model discloses preferred scheme, location structure includes the mounting box, and the mounting box top is equipped with the installation lid, inside controller and the GPS orientation module of being equipped with of mounting box, and one side that the mounting box is adjacent with the undercarriage is equipped with infrared camera and heat source sensor.

As the preferred scheme of the utility model, be electric connection between controller, GPS orientation module, infrared camera and the heat source sensor, and the GPS orientation module model is SKM66, and infrared camera is the camera device of J-DP-8015 series.

As the utility model discloses preferred scheme, buffer structure is equipped with two sets ofly, and buffer structure includes the buffer board, and buffer board bottom array distribution has a plurality of fixed slots, and the fixed slot is inside to be equipped with the telescopic link, and the telescopic link outside is equipped with buffer spring, and the telescopic link bottom is equipped with the steadying plate, and the steadying plate top is equipped with a plurality of array distribution and with the corresponding fixed slot of buffer board, and the steadying plate bottom is equipped with anti-skidding rubber pad.

As the utility model discloses preferred scheme, the transmission structure includes the locker room, the locker room passes through bolted connection and installs in the mounting panel bottom, the locker room is installed through hinged joint with one side that the undercarriage is adjacent and is opened the door, inside both sides adjacent with opening the door of locker room all are equipped with the guide block, and locker room bottom center department is equipped with quantitative chamber, locker room bottom all is equipped with the mounting bracket with the both sides adjacent that open the door, the mounting bracket is close to one side in quantitative chamber and the inside one side of keeping away from the locker room of guide block all is equipped with keeps off the material structure, and keep off the material structure and arrange the bottom and the top in quantitative chamber respectively, the inside shell of putting out a fire that all is equipped with in quantitative intracavity portion and locker room.

As the utility model discloses preferred scheme, keep off the material structure and include the mounting groove, the mounting groove is established respectively in the inside both sides that are close to quantitative chamber of mounting bracket and is led the both sides that the locker room was kept away from to the slider, the inside hydraulic stem that is equipped with of mounting groove, one side that the mounting groove was kept away from to the hydraulic stem is equipped with the installation piece, one side that the hydraulic stem was kept away from to the installation piece is equipped with the baffler.

Compared with the prior art, the beneficial effects of the utility model are that:

1. the utility model discloses in, through setting up location structure, when fire control unmanned aerial vehicle in the course of the work, unmanned aerial vehicle passes through infrared camera and surveys in real time, and heat source sensor work searches for the conflagration source simultaneously to through GPS orientation module's effect, make that this unmanned aerial vehicle can be accurate find the conflagration scene of taking place, and the accurate bullet of will putting out a fire puts in.

2. The utility model discloses in, through setting up buffer structure, when the fire control unmanned aerial vehicle descends to the ground, the steadying plate makes unmanned aerial vehicle main part and the stable support in ground, and under telescopic link, buffer board and buffer spring's combined action for this unmanned aerial vehicle's shock resistance is by effectual improvement, thereby can effectively avoid descending the impaired risk of in-process unmanned aerial vehicle main part.

3. The utility model discloses in, through setting up the transmission structure, before the unmanned aerial vehicle work of putting out a fire in the fire control, can be earlier through opening the door to the inside a plurality of bullets of putting out a fire of locker room, thereby at the unmanned aerial vehicle during operation of putting out a fire, can put in many pieces of bullets of putting out a fire to the fire disaster area, thereby make this unmanned aerial vehicle of putting out a fire efficiency by effectual improvement, and the flexible fire source area that makes the bullet of putting out a fire accurate of accessible controller autonomous control hydraulic stem in the course of the work, make more convenient of putting out a fire.

Drawings

Fig. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a schematic view of the internal structure of the present invention;

fig. 3 is an enlarged view of the region a of the present invention.

In the figure: 1. an unmanned aerial vehicle main body; 11. a positioning structure; 111. an infrared camera; 112. a heat source sensor; 113. installing a cover; 114. a controller; 115. a GPS positioning module; 116. mounting a box; 12. a strut; 13. a propeller; 14. a landing gear; 15. a buffer structure; 151. a buffer plate; 152. fixing grooves; 153. a buffer spring; 154. a telescopic rod; 155. a stabilizing plate; 16. mounting a plate; 2. an emitting structure; 21. a storage chamber; 22. opening the door; 23. a mounting frame; 24. a guide slider; 25. a dosing chamber; 26. fire extinguishing bombs; 27. a material blocking structure; 271. a barrier plate; 272. mounting blocks; 273. a hydraulic lever; 274. and (4) mounting the groove.

Detailed Description

The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, rather than all embodiments, and all other embodiments obtained by a person of ordinary skill in the art without creative work belong to the protection scope of the present invention based on the embodiments of the present invention.

In order to facilitate understanding of the present invention, the present invention will be described more fully hereinafter with reference to the accompanying drawings. Several embodiments of the invention are given in the accompanying drawings. The invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.

It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. The terms "vertical," "horizontal," "left," "right," and the like as used herein are for illustrative purposes only.

Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.

Please refer to fig. 1-3, the present invention provides a technical solution:

an aerial multi-launch fire-fighting unmanned aerial vehicle comprises an unmanned aerial vehicle main body 1, wherein the unmanned aerial vehicle main body 1 comprises a positioning structure 11 for accurately positioning a fire scene, supporting rods 12 are arranged at two ends of two sides of the positioning structure 11 along the width direction, propellers 13 are arranged at one ends of the supporting rods 12 far away from the positioning structure 11, landing gears 14 are arranged at four corners of the bottom of the positioning structure 11, a buffer structure 15 for improving the buffer force when the unmanned aerial vehicle lands is arranged at the bottom of the landing gear 14, a mounting plate 16 is arranged at the bottom of the positioning structure 11 and between the four landing gears 14, a launch structure 2 for improving the fire-fighting efficiency is arranged at the bottom of the mounting plate 16, the unmanned aerial vehicle can accurately find the fire scene by arranging the positioning structure 11, and accurately put fire-fighting bombs 26 in, and the shock resistance of the unmanned aerial vehicle is effectively improved by arranging the buffer structure 15, thereby can effectively avoid descending the impaired risk of in-process unmanned aerial vehicle main part, through setting up emission structure 2 for this fire control unmanned aerial vehicle that puts out a fire efficiency of putting out a fire is by effectual improvement.

In the embodiment, referring to fig. 1 and 2, the positioning structure 11 includes a mounting box 116, a mounting cover 113 is disposed on the top of the mounting box 116, a controller 114 and a GPS positioning module 115 are disposed inside the mounting box 116, an infrared camera 111 and a heat source sensor 112 are disposed on one side of the mounting box 116 adjacent to the landing gear 14, the controller 114, the GPS positioning module 115, the infrared camera 111 and the heat source sensor 112 are electrically connected, the model of the GPS positioning module 115 is SKM66, the infrared camera 111 is a J-DP-8015 series camera device, by disposing the positioning structure 11, the unmanned aerial vehicle can accurately position a fire scene, when the unmanned aerial vehicle is actually used, the unmanned aerial vehicle observes in real time through the infrared camera 111 during operation, and the heat source sensor 112 searches for a fire source during operation, and through the function of the GPS positioning module 115, make this unmanned aerial vehicle can be accurate find the conflagration scene of taking place to accurate will put in fire extinguishing bomb.

In an embodiment, referring to fig. 1 and 2, two sets of buffer structures 15 are provided, each buffer structure 15 includes a buffer plate 151, a plurality of fixing slots 152 are distributed at the bottom of the buffer plate 151 in an array manner, a telescopic rod 154 is disposed inside the fixing slot 152, a buffer spring 153 is disposed outside the telescopic rod 154, a stabilizing plate 155 is disposed at the bottom of the telescopic rod 154, a plurality of fixing slots 152 are distributed at the top of the stabilizing plate 155 in an array manner and correspond to the buffer plate 151, and the bottom of the stabilizing plate 155 is provided with the anti-skidding rubber pad, the shock resistance of the device is effectively improved by arranging the buffer structure 15, in actual use, when the fire fighting unmanned aerial vehicle lands on the ground, the stabilizing plate 155 enables the main body 1 of the unmanned aerial vehicle to be stably supported with the ground, and under the combined action of the telescopic rod 154, the buffer plate 151 and the buffer spring 153, make this unmanned aerial vehicle's shock resistance by effectual improvement to can effectively avoid descending impaired risk of in-process unmanned aerial vehicle main part 1.

In the embodiment, please refer to fig. 1 and 2, the launching structure 2 includes a storage chamber 21, the storage chamber 21 is installed at the bottom of the mounting plate 16 by bolt connection, the door 22 is installed at one side of the storage chamber 21 adjacent to the landing gear 14 by hinge connection, the two sides of the interior of the storage chamber 21 adjacent to the door 22 are both provided with guide blocks 24, the center of the bottom of the storage chamber 21 is provided with a quantitative chamber 25, the two sides of the bottom of the storage chamber 21 adjacent to the door 22 are both provided with mounting frames 23, one side of the mounting frame 23 close to the quantitative chamber 25 and one side of the interior of the guide blocks 24 away from the storage chamber 21 are both provided with material blocking structures 27, the material blocking structures 27 are respectively arranged at the bottom and the top of the quantitative chamber 25, the interior of the quantitative chamber 25 and the interior of the storage chamber 21 are both provided with fire extinguishing bombs 26, by arranging the launching structure 2, the fire extinguishing efficiency of the unmanned aerial vehicle is effectively improved, in practical use, before the fire extinguishing unmanned aerial vehicle works, can be earlier through opening door 22 and put into a plurality of shells 26 of putting out a fire to locker room 21 inside to at the unmanned aerial vehicle during operation of putting out a fire, can put in many pieces of shells 26 of putting out a fire to the fire disaster area, thereby make this unmanned aerial vehicle of putting out a fire of fire control put out a fire efficiency by effectual improvement, and accessible controller 114 autonomous control hydraulic stem 273 stretches out and draws back in the fire source area that makes the shell 26 of putting out a fire accurate in the course of the work, makes more convenient of putting out a fire.

In an embodiment, referring to fig. 3, the material blocking structure 27 includes a mounting groove 274, the mounting groove 274 is respectively disposed on two sides of the mounting frame 23 near the quantitative cavity 25 and two sides of the guiding slider 24 far away from the storage chamber 21, a hydraulic rod 273 is disposed in the mounting groove 274, a mounting block 272 is disposed on one side of the hydraulic rod 273 far away from the mounting groove 274, and a blocking plate 271 is disposed on one side of the mounting block 272 far away from the hydraulic rod 273.

The working principle is as follows: when the unmanned aerial vehicle is used, before the unmanned aerial vehicle for fire fighting works, a plurality of fire extinguishing bombs 26 can be put into the storage chamber 21 through the door 22, when the unmanned aerial vehicle for fire fighting works, the unmanned aerial vehicle can observe in real time through the infrared camera 111, meanwhile, the heat source sensor 112 works to search for the fire source, and through the action of the GPS positioning module 115, the unmanned aerial vehicle can accurately find the fire scene, when the unmanned aerial vehicle is positioned above the fire source, the hydraulic rods 273 at the top and the bottom of the quantitative cavity 25 can be respectively controlled to shrink through the controller 114, so that the fire extinguishing bombs 26 are accurately put into the fire source region, when the unmanned aerial vehicle for fire fighting lands on the ground, the stabilizing plate 155 enables the main body 1 of the unmanned aerial vehicle to be stably supported with the ground, and under the combined action of the telescopic rod 154, the buffer plate 151 and the buffer spring 153, the anti-shock capacity of the unmanned aerial vehicle is effectively improved, thereby can effectively avoid descending the impaired risk of in-process unmanned aerial vehicle main part 1.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. High altitude many transmission formula fire control unmanned aerial vehicle of putting out a fire, including unmanned aerial vehicle main part (1), its characterized in that: unmanned aerial vehicle main part (1) all is equipped with branch (12) including being used for this accurate location structure (11) of going on fixing a position to the scene of fire of unmanned aerial vehicle, location structure (11) both sides along width direction's both ends, the one end that location structure (11) were kept away from in branch (12) is equipped with screw (13), four corners in location structure (11) bottom all are equipped with undercarriage (14), undercarriage (14) bottom is equipped with buffer structure (15) that are used for improving this unmanned aerial vehicle buffer power when descending, location structure (11) bottom and the position that is located between four undercarriage (14) are equipped with mounting panel (16), mounting panel (16) bottom is equipped with emission structure (2) that are used for improving fire extinguishing efficiency.

2. The high altitude multi-launch formula fire control unmanned aerial vehicle of claim 1, characterized in that: the positioning structure (11) comprises a mounting box (116), a mounting cover (113) is arranged at the top of the mounting box (116), a controller (114) and a GPS positioning module (115) are arranged inside the mounting box (116), and an infrared camera (111) and a heat source sensor (112) are arranged on one side, adjacent to the landing gear (14), of the mounting box (116).

3. The high altitude multi-launch formula fire control unmanned aerial vehicle of claim 2, characterized in that: the controller (114), the GPS positioning module (115), the infrared camera (111) and the heat source sensor (112) are electrically connected, the model of the GPS positioning module (115) is SKM66, and the infrared camera (111) is a J-DP-8015 series camera.

4. The high altitude multi-launch formula fire control unmanned aerial vehicle of claim 1, characterized in that: buffer structure (15) are equipped with two sets ofly, and buffer structure (15) include buffer board (151), and buffer board (151) bottom array distribution has a plurality of fixed slots (152), and fixed slot (152) inside is equipped with telescopic link (154), and telescopic link (154) outside is equipped with buffer spring (153), and telescopic link (154) bottom is equipped with stabilising plate (155), and stabilising plate (155) top is equipped with a plurality of array distributions and with buffer board (151) corresponding fixed slot (152), and stabilising plate (155) bottom is equipped with anti-skidding rubber pad.

5. The high altitude multi-launch formula fire control unmanned aerial vehicle of claim 1, characterized in that: the launching structure (2) comprises a storage chamber (21), the storage chamber (21) is installed at the bottom of the installation plate (16) through bolt connection, one side of the storage chamber (21) adjacent to the undercarriage (14) is provided with a door opening (22) through hinge connection, two sides of the interior of the storage chamber (21) adjacent to the door opening (22) are respectively provided with a guide sliding block (24), a quantitative cavity (25) is arranged at the center of the bottom of the storage chamber (21), mounting frames (23) are arranged on two sides of the bottom of the storage chamber (21) adjacent to the door opening (22), material blocking structures (27) are arranged on one side of each mounting frame (23) close to the quantitative cavity (25) and one side of the interior of each guide slider (24) far away from the storage chamber (21), and the material blocking structure (27) is respectively arranged at the bottom and the top of the quantitative cavity (25), and fire extinguishing bombs (26) are respectively arranged inside the quantitative cavity (25) and inside the storage chamber (21).

6. The high altitude multi-launch formula fire control unmanned aerial vehicle of claim 5, characterized in that: keep off material structure (27) including mounting groove (274), mounting groove (274) are established respectively in mounting bracket (23) inside both sides that are close to ration chamber (25) and guide slider (24) and keep away from the both sides of locker room (21), and mounting groove (274) inside is equipped with hydraulic stem (273), and one side that mounting groove (274) were kept away from to hydraulic stem (273) is equipped with installation piece (272), and one side that hydraulic stem (273) were kept away from to installation piece (272) is equipped with separation board (271).