CN219668511U - Fire control unmanned aerial vehicle - Google Patents
Fire control unmanned aerial vehicle Download PDFInfo
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- CN219668511U CN219668511U CN202320992213.1U CN202320992213U CN219668511U CN 219668511 U CN219668511 U CN 219668511U CN 202320992213 U CN202320992213 U CN 202320992213U CN 219668511 U CN219668511 U CN 219668511U
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- aerial vehicle
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- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims abstract description 30
- 235000011089 carbon dioxide Nutrition 0.000 claims abstract description 30
- 238000001816 cooling Methods 0.000 claims abstract description 21
- 238000007789 sealing Methods 0.000 claims description 14
- 238000003466 welding Methods 0.000 claims description 7
- 230000001681 protective effect Effects 0.000 claims 1
- 230000006378 damage Effects 0.000 abstract description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 230000001939 inductive effect Effects 0.000 description 2
- FGRBYDKOBBBPOI-UHFFFAOYSA-N 10,10-dioxo-2-[4-(N-phenylanilino)phenyl]thioxanthen-9-one Chemical compound O=C1c2ccccc2S(=O)(=O)c2ccc(cc12)-c1ccc(cc1)N(c1ccccc1)c1ccccc1 FGRBYDKOBBBPOI-UHFFFAOYSA-N 0.000 description 1
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
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Abstract
The utility model discloses a fire-fighting unmanned aerial vehicle, which comprises an unmanned aerial vehicle main shell, a fire-fighting bottom pipe and a cooling mechanism, wherein the cooling mechanism comprises a top opening, a supporting plate, a heat-conducting plate, a mouth frame, a micro fan, a dry ice box and an inclined protection cover, the fire-fighting bottom pipe is arranged at the bottom end of the unmanned aerial vehicle main shell, the top opening of an embedded heat-conducting plate is arranged at the top end shell of the unmanned aerial vehicle main shell, the supporting plate for supporting the heat-conducting plate is fixed in the unmanned aerial vehicle main shell below the top opening, and the cooling mechanism is arranged at the top end of the unmanned aerial vehicle main shell far away from the fire-fighting bottom pipe, so that when the fire-fighting unmanned aerial vehicle is used for fire extinguishment in a fire scene, the unmanned aerial vehicle main shell of the fire-fighting unmanned aerial vehicle has a guaranteed air-cooling structure to cool the self shell, and high-temperature damage to self electrical elements in the unmanned aerial vehicle main shell in a long time is avoided.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a fire-fighting unmanned aerial vehicle.
Background
Unmanned aerial vehicle is unmanned aerial vehicle that utilizes radio remote control equipment and self-contained program control device to operate, because it can reach many positions that human can not reach, can play very huge auxiliary role to the high building extinguishment, so often can see its figure in the fire control field.
When the unmanned aerial vehicle is applied to fire extinguishment, the unmanned aerial vehicle is generally provided with a fire-fighting pipeline for connecting a water source pipeline of a fire engine at the bottom end of a self shell, then the unmanned aerial vehicle can ascend to spray water to a fire point at a high position for fire extinguishment, when the unmanned aerial vehicle is frequently used for fire extinguishment rescue at a fire scene, the high temperature at the fire scene often damages electronic elements inside the unmanned aerial vehicle, and then the unmanned aerial vehicle frequently suffers from thermal injury faults after fire extinguishment at the fire scene, so that improvement is required for guaranteeing the high-temperature operation of the unmanned aerial vehicle.
Disclosure of Invention
The utility model mainly aims to provide a fire-fighting unmanned aerial vehicle, wherein a cooling mechanism is arranged at the top end of a main shell of the unmanned aerial vehicle, which is far away from a fire-fighting bottom pipe, so that when the fire-fighting unmanned aerial vehicle is used for extinguishing fire in a fire scene, the main shell of the unmanned aerial vehicle is provided with a guaranteed air-cooled cooling structure to cool the self shell, thereby avoiding the damage to self electric elements caused by the high temperature in the fire scene for a long time in the main shell of the unmanned aerial vehicle, and effectively solving the problems in the background art.
In order to achieve the above purpose, the technical scheme adopted by the utility model is as follows:
the utility model provides a fire control unmanned aerial vehicle, includes unmanned aerial vehicle main casing and fire control end tube, still includes cooling mechanism, cooling mechanism includes roof opening, layer board, heat-conducting plate, mouth-shaped frame, miniature fan, dry ice box and oblique guard, the fire control end tube is installed to the bottom of unmanned aerial vehicle main casing, and the roof opening of embedded heat-conducting plate is seted up to the top casing department of unmanned aerial vehicle main casing, the layer board that is used for the support to connect the heat-conducting plate is fixed with to the unmanned aerial vehicle main casing of roof opening below, the plate surface welding of heat-conducting plate has a mouthful shape frame, and mouthful one side framework department of shape frame has seted up the induced air groove of embedded miniature fan, miniature fan locks in dry ice box surface through the fastening bolt, and the box body of dry ice box and the welding of the outer mouth-shaped frame outer wall of induced air groove, the exhaust hole has been seted up on dry ice box surface on miniature fan one side, the other trilateral frame top welding of mouth-shaped frame of leading the air groove has the cover miniature fan and the oblique guard of heat-conducting plate, and mouth-shaped frame is kept away from the opposite side frame wall surface of induced air groove and has been seted up guard window, mouth-shaped bolt, between the heat-conducting plate has the bar-shaped bolt to be seted up to the mouth-shaped bolt.
Further, screw holes for screwing in bolts are correspondingly formed in the surfaces of the inclined shield, the mouth-shaped frame, the heat-conducting plate and the supporting plate; screw holes of the inclined shield, the mouth frame, the heat-conducting plate and the supporting plate can be correspondingly screwed into the bolts for connection.
Further, a sealing cover is plugged into the upper box opening of the dry ice box, and a lifting handle is protruded from the top end of a cover body of the sealing cover; when the dry ice box is not filled with dry ice, the sealing cover can be used for sealing so as to prevent sundries from entering, and the lifting handle at the sealing cover is convenient for lifting the cover body out of the dry ice box.
Further, four groups of supporting plates in the main shell of the unmanned aerial vehicle are symmetrically fixed according to four corner notches of the top opening; four groups of supporting plates are arranged in the unmanned aerial vehicle main shell and can support and connect the heat-conducting plate at four points.
Further, the honeycomb window of the exhaust window is densely penetrated by the frame plate of the through-hole frame; the exhaust window enables the frame plate of the mouth-shaped frame far from the air inducing groove to have an exhaust pore structure.
Compared with the prior art, the utility model has the following beneficial effects:
according to the utility model, the cooling mechanism is arranged at the top end of the main unmanned aerial vehicle shell, which is far away from the fire-fighting bottom pipe, so that when the fire-fighting unmanned aerial vehicle is used for extinguishing fire in a fire scene, the main unmanned aerial vehicle shell of the fire-fighting unmanned aerial vehicle has a guaranteed air-cooled cooling structure to cool the main unmanned aerial vehicle shell, and the main unmanned aerial vehicle shell is prevented from being damaged by high temperature in the fire scene for a long time.
Drawings
Fig. 1 is a schematic structural view of an integrally installed cooling mechanism of a fire-fighting unmanned aerial vehicle.
Fig. 2 is a schematic diagram illustrating the whole of the fire-fighting unmanned aerial vehicle and the detachment of the heat conducting plate.
Fig. 3 is an exploded view of a cooling mechanism of the fire-fighting unmanned aerial vehicle.
In the figure: 1. an unmanned aerial vehicle main shell; 2. a fire bottom pipe; 3. a cooling mechanism; 4. a top opening; 5. a supporting plate; 6. a heat conductive plate; 7. a mouth-shaped frame; 8. an induced draft slot; 9. a micro fan; 10. a dry ice bank; 11. an exhaust hole; 12. a cover; 13. an oblique shield; 14. and an exhaust window.
Detailed Description
The utility model is further described in connection with the following detailed description, in order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the utility model easy to understand.
As shown in fig. 1-3, a fire-fighting unmanned aerial vehicle, including unmanned aerial vehicle main casing 1 and fire-fighting bottom tube 2, still include cooling mechanism 3, cooling mechanism 3 includes roof opening 4, layer board 5, heat-conducting plate 6, mouth-piece frame 7, miniature fan 9, dry ice box 10 and oblique guard 13, fire-fighting bottom tube 2 is installed to the bottom of unmanned aerial vehicle main casing 1, and roof opening 4 of embedded heat-conducting plate 6 is seted up to the top casing department of unmanned aerial vehicle main casing 1, be fixed with layer board 5 that is used for supporting and connecting heat-conducting plate 6 in the unmanned aerial vehicle main casing 1 of roof opening 4 below, the plate body surface welding of heat-conducting plate 6 has mouth-piece frame 7, and mouth-piece frame 7's one side framework department has seted up the air guiding groove 8 of embedded miniature fan 9, miniature fan 9 locks in dry ice box 10 surface through the fastening bolt, and the box body of dry ice box 10 and the outer wall welding of mouth-piece frame 7 of air guiding groove 8, 11 has been seted up on the box 10 surface of miniature fan 9 one side, mouth-piece frame 7 keeps away from the heat-conducting plate 8 top opening 6, and the other side face of the heat-conducting plate 6 has mouth-piece frame 7, and the oblique-piece frame 7 is kept away from face of the heat-conducting plate 6, and the face of the side is kept away from face of the mouth-piece frame 7, and is equipped with mouth-piece frame 7, and the face-piece frame 13 is kept away from between the face of the face-piece frame 6.
Screw holes for screwing in bolts are correspondingly formed in the surfaces of the inclined shield 13, the mouth-shaped frame 7, the heat conducting plate 6 and the supporting plate 5; screw holes of the inclined shield 13, the mouth frame 7, the heat conducting plate 6 and the supporting plate 5 can be correspondingly screwed into bolts for connection.
Wherein, the upper box opening of the dry ice box 10 is plugged with a sealing cover 12, and the top end of the cover body of the sealing cover 12 is protruded with a lifting handle; when the dry ice box 10 is not filled with dry ice, the sealing cover 12 can be used for sealing to prevent sundries from entering, and the lifting handle at the sealing cover 12 is convenient for lifting the cover body out of the dry ice box 10.
Four groups of supporting plates 5 in the unmanned aerial vehicle main shell 1 are symmetrically fixed according to four corner notches of the top opening 4; four groups of supporting plates 5 are arranged in the unmanned aerial vehicle main shell 1 and can be connected with a heat-conducting plate 6 in a supporting mode at four points.
Wherein the honeycomb window of the exhaust window 14 is densely penetrated by the frame plate of the through-hole frame 7; the vent window 14 allows vent aperture structure to exist at the frame plate of the mouth-shaped frame 7 far from the air inducing groove 8.
It should be noted that, the utility model is a fire-fighting unmanned aerial vehicle, after the top opening 4 of the cooling mechanism 3 is arranged at the top end of the main unmanned aerial vehicle shell 1, the heat-conducting plate 6 of the cooling mechanism 3 can enter the main unmanned aerial vehicle shell 1 from the top opening 4 and be supported by the supporting plate 5, then the micro fan 9 is embedded into the air-guiding groove 8 of the opening-shaped frame 7 above the heat-conducting plate 6 and is tightly connected with the dry ice box 10 by using a fastening bolt, the micro fan 9 can extend into the main unmanned aerial vehicle shell 1 from the strip-shaped heat-conducting notch of the heat-conducting plate 6 to be connected with electricity, then the inclined shield 13 is welded above the rest three-side frame plates of the opening-shaped frame 7 far from the air-guiding groove 8 to cover the micro fan 9 and the heat-conducting plate 6, then the inclined shield 13, the opening-shaped frame 7, the screw holes of the heat-conducting plate 6 and the supporting plate 5 can be correspondingly screwed into the bolts to be connected, when the fire-fighting unmanned aerial vehicle is not in use, the sealing cover 12 can be plugged into the dry ice box 10 to be sealed, when the fire-fighting bottom pipe 2 at the bottom of the fire-fighting unmanned aerial vehicle is connected with a water pipe and needs to raise the fire in a fire scene, the sealing cover 12 can be lifted out of the dry ice box 10, then dry ice is put into the dry ice box 10, ventilation gaps exist between the dry ice boxes, the dry ice sublimates in the dry ice box 10 to generate cool air, after the fire-fighting unmanned aerial vehicle is started, the micro fan 9 can be enabled to draw the cool air at the dry ice box 10 into the mouth frame 7 below the inclined shield 13 through the exhaust hole 11, heat in the main shell 1 of the unmanned aerial vehicle enters the mouth frame 7 from the heat conducting plate 6 with strip-shaped heat conducting notches on the surface, and along with the flow of cool wind, the wind force at the mouth frame 7 can take the heat out from the exhaust window 14, so that the heat generated at the main shell 1 of the unmanned aerial vehicle is taken away, and the cooling mechanism 3 with the security performs cooling at the self shell when the fire-fighting fire scene is in fire scene, the unmanned aerial vehicle main shell 1 is prevented from being damaged by high temperature of a fire scene for a long time.
It should be noted that the present utility model is a fire-fighting unmanned aerial vehicle, the components in the present utility model are all known by those skilled in the art, and the structures and principles of the present utility model are all known by those skilled in the art through technical manuals or by conventional experimental methods.
The foregoing has shown and described the basic principles and main features of the present utility model and the advantages of the present utility model. It will be understood by those skilled in the art that the present utility model is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present utility model, and various changes and modifications may be made without departing from the spirit and scope of the utility model, which is defined in the appended claims. The scope of the utility model is defined by the appended claims and equivalents thereof.
Claims (5)
1. The utility model provides a fire control unmanned aerial vehicle, includes unmanned aerial vehicle main casing (1) and fire control bottom tube (2), its characterized in that: still include cooling body (3), cooling body (3) include roof opening (4), layer board (5), heat conduction board (6), mouth shape frame (7), miniature fan (9), dry ice box (10) and oblique shroud (13), fire control bottom tube (2) are installed to the bottom of unmanned aerial vehicle main casing (1), and roof opening (4) of embedded heat conduction board (6) are seted up in the top casing department of unmanned aerial vehicle main casing (1), roof opening (4) below unmanned aerial vehicle main casing (1) internal fixation has layer board (5) that are used for supporting and joining heat conduction board (6), the board surface welding of heat conduction board (6) has mouth shape frame (7), and mouth shape frame (7) one side framework department has seted up air guide groove (8) of embedded miniature fan (9), miniature fan (9) are locked in dry ice box (10) surface through the binding bolt, and the box body of dry ice box (10) and air guide groove (8) outer mouth shape frame (7) outer wall welding, the board (7) of miniature fan (6) are kept away from on the face of mouth shape frame (7) and the oblique shroud (13), and the other side frame wall surface of the mouth-shaped frame (7) far away from the induced air groove (8) is penetrated and provided with an exhaust window (14), bolts are locked among the inclined shield (13), the mouth-shaped frame (7), the heat conducting plate (6) and the supporting plate (5), and the plate surface of the heat conducting plate (6) is penetrated and provided with a strip-shaped heat conducting notch.
2. The fire fighting unmanned aerial vehicle of claim 1, wherein: screw holes for screwing in bolts are correspondingly formed in the surfaces of the inclined protective cover (13), the mouth-shaped frame (7), the heat conducting plate (6) and the supporting plate (5).
3. The fire fighting unmanned aerial vehicle of claim 1, wherein: a sealing cover (12) is plugged into the upper box opening of the dry ice box (10), and a lifting handle is protruded from the top end of the cover body of the sealing cover (12).
4. The fire fighting unmanned aerial vehicle of claim 1, wherein: four groups of supporting plates (5) in the unmanned aerial vehicle main shell (1) are symmetrically fixed according to four corner notches of the top opening (4).
5. The fire fighting unmanned aerial vehicle of claim 1, wherein: the honeycomb window of the exhaust window (14) is densely penetrated by the frame plate of the through-hole frame (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320992213.1U CN219668511U (en) | 2023-04-27 | 2023-04-27 | Fire control unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320992213.1U CN219668511U (en) | 2023-04-27 | 2023-04-27 | Fire control unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219668511U true CN219668511U (en) | 2023-09-12 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320992213.1U Active CN219668511U (en) | 2023-04-27 | 2023-04-27 | Fire control unmanned aerial vehicle |
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| Country | Link |
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| CN (1) | CN219668511U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117861101A (en) * | 2024-03-12 | 2024-04-12 | 山东龙翼航空科技有限公司 | Unmanned aerial vehicle for firefighting rescue and application method thereof |
-
2023
- 2023-04-27 CN CN202320992213.1U patent/CN219668511U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117861101A (en) * | 2024-03-12 | 2024-04-12 | 山东龙翼航空科技有限公司 | Unmanned aerial vehicle for firefighting rescue and application method thereof |
| CN117861101B (en) * | 2024-03-12 | 2024-05-10 | 山东龙翼航空科技有限公司 | Unmanned aerial vehicle for firefighting rescue and application method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240425 Address after: 2715, Duhuixuan, No. 3018 Shennan Middle Road, Huahang Community, Huaqiangbei Street, Futian District, Shenzhen City, Guangdong Province, 518000 Patentee after: Shenzhen Tianfeng Investment Development Co.,Ltd. Country or region after: China Patentee after: Xiao Bixiong Address before: 417500 Shatangwan Street, Lengshuijiang City, Loudi City, Hunan Province Patentee before: Zhang Xiangwan Country or region before: China |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240529 Address after: 1923, Tianjian Entrepreneurship Building, No. 7 Shangbao Road, Shiling Community, Lianhua Street, Futian District, Shenzhen City, Guangdong Province, 518000 Patentee after: Shenzhen neng'an fire Decoration Engineering Equipment Co.,Ltd. Country or region after: China Address before: 2715, Duhuixuan, No. 3018 Shennan Middle Road, Huahang Community, Huaqiangbei Street, Futian District, Shenzhen City, Guangdong Province, 518000 Patentee before: Shenzhen Tianfeng Investment Development Co.,Ltd. Country or region before: China Patentee before: Xiao Bixiong |