CN206648522U - A kind of UAV system fire extinguishing bullet launching device - Google Patents
A kind of UAV system fire extinguishing bullet launching device Download PDFInfo
- Publication number
- CN206648522U CN206648522U CN201720379716.6U CN201720379716U CN206648522U CN 206648522 U CN206648522 U CN 206648522U CN 201720379716 U CN201720379716 U CN 201720379716U CN 206648522 U CN206648522 U CN 206648522U
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- China
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- shell
- electromagnetic lock
- fire extinguisher
- extinguisher bomb
- hole
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- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
It the utility model is related to a kind of UAV system fire extinguishing bullet launching device, including launching tube and fire extinguisher bomb, the fire extinguisher bomb is located in launching tube, also include Electromalgnetic locking mechanism and positioning self-lock device, fire extinguisher bomb is provided with circumferentially positioned groove, the Electromalgnetic locking mechanism includes electromagnetic lock shell, electromagnetic lock component and latch, the electromagnetic lock component is arranged in electromagnetic lock shell, electromagnetic lock shell is provided with pin hole, the latch is connected with electromagnetic lock component, and stretch out outside pin hole, end is stretched into hole insertion locating slot through first, positioning self-lock device includes shell, sealing nut, sensor, spring, piston and hoodle, sealing nut is fixedly connected with shell end face, the sensor is arranged in shell, one end of spring offsets with piston, hoodle is arranged at the mounting hole aperture of shell, and stretch into locating slot.The locking of the utility model fire extinguisher bomb is firm, and when unmanned plane adjusts flight attitude, fire extinguisher bomb will not fall, and during release fire extinguisher bomb, can unlock rapidly.
Description
Technical field
A kind of emitter is the utility model is related to, especially a kind of UAV system fire extinguishing bullet launching device.
Background technology
With the fast development of social economy, living standards of the people improve constantly, and high-rise building building will progressively substitute more
Floor room turns into the main building of city-building.The development of high-rise building construction reduces floor space, has saved space, simultaneously
Also new requirement is highlighted for security against fire lifesaving system.Although to security against fire in the design, building course in high-rise building
Strict requirements are proposed, but deficiency is still suffered from the ability for tackling urgent accident.
This project is intended putting out a fire to building outside building by unmanned plane loading fire extinguisher bomb, and solving high-rise building can not be effective
The difficulty of conveying extinguishing agent, implement efficient quick extinguishing.
As China's skyscraper quantity and height are constantly soaring, fire-fighting and rescue pressure increasingly increases.By operation principle and
Physics limit influences, and the special type fire control vehicle equipment generally existing car body for more than hundred meters high-rise building external rescues is wide
Greatly, developed area is big, supply and the features such as Support Equipment complexity, thus bring it is many limited by rescue site, rescue and its protect
Barrier equipment " enter and do not go ", " Zhan Bukai ", the application problem of " can't reach ", have impact on the performance of rescue outfit performance.
Using unmanned plane carry fire extinguisher bomb, can maneuverability shuttle between building, coordinate optical aiming system, it is parallel
Launch fire extinguisher bomb, carry high-efficiency fire-extinguishant, it is accurate to put into high-rise building scene on fire, stamp out a fire, be particularly suitable for city complexity
Fire-fighting and rescue under environmental condition, can effectively solve elevating fire truck under the complex environment of city " enter and do not go ", " Zhan Bukai ",
The problems such as " can't reach ", high-rise and super high rise building fire hose will be given to carry out significant change.
Unmanned plane carries fire extinguisher bomb in flame range airflight, and flight attitude needs not stop to adjust, if fire extinguisher bomb is not reinforced
It is fixed, it is more likely that to cause to fall, it is therefore desirable to a kind of simple reliable device for positioning and securing.The device is by can free activity orientation
Self-lock pin determines position of the fire extinguisher bomb in cylinder, and instruction electromagnetic lock fixes fire extinguisher bomb.
The content of the invention
The purpose of this utility model is to provide a kind of fire extinguisher bomb locking firmly, when unmanned plane adjusts flight attitude, gone out
Fiery bullet will not fall, and when discharging fire extinguisher bomb, the UAV system fire extinguishing bullet launching device that can unlock rapidly.
In order to achieve the above object, the technical solution of the utility model is：A kind of UAV system fire extinguishing bullet launching device, bag
Launching tube and fire extinguisher bomb are included, the fire extinguisher bomb is located in launching tube, in addition to Electromalgnetic locking mechanism and positioning self-lock device, launching tube
It is provided with and radially first stretches into hole and radially second stretch into hole, fire extinguisher bomb is provided with circumferentially positioned groove, the Electromalgnetic locking mechanism bag
Electromagnetic lock shell, electromagnetic lock component and latch are included, the electromagnetic lock component is arranged in electromagnetic lock shell, and on electromagnetic lock shell
Provided with pin hole, the latch is connected with electromagnetic lock component, and is stretched out outside pin hole, and hole insertion positioning is stretched into end through first
In groove, positioning self-lock device includes shell, sealing nut, sensor, spring, piston and hoodle, and the shell stretches into second
Hole is fixedly connected, and sealing nut is fixedly connected with shell end face, and the sensor is arranged in shell, one end of spring and piston
Offset, the hoodle is arranged at the mounting hole aperture of shell, and is stretched into locating slot.
The electromagnetic lock component includes coil brace, coil, iron core, ring support and coil spring, the coil brace
It is fixedly connected with ring support, the coil winding is on coil brace, the mesopore connection of iron core and coil brace, the coil
Spring is located in ring support, and one end offsets with iron core, and the other end offsets with latch.
The electromagnetic lock component also includes bottom plate, and the bottom plate is fixedly connected in electromagnetic lock shell, and the annular branch
Frame is fixedly connected on bottom plate, and bottom plate is provided with bottom plate hole, and the latch passes through bottom plate hole.
The positioning self-lock device also includes trim ring and cover plate, and the cover plate is fixed in shell, and sensor is arranged on lid
On plate, trim ring is between sealing nut and cover plate.
The positioning self-lock device also includes connecting rod, and the piston is connected by connecting rod with hoodle.
After said structure, before fire extinguisher bomb loads launching tube, the latch of Electromalgnetic locking mechanism be recovered to launching tube inwall with
Outside, the hoodle of positioning self-lock device is reached on the inside of the barrel of launching tube by spring extruding, when fire extinguisher bomb loads from transmitting tube rear end
During launching tube, positioning self-lock device is touched first, and receding returns after hoodle is stressed, and pressure is delivered to positioning self-locking by spring
On the pressure sensor for selling rear end, high level output is produced.When fire extinguisher bomb is passed onwards to assigned position, hoodle can slip into fire extinguishing
The locating slot of bullet, pressure release, sensor recover low level.When sensor output by low level rise to high level be transferred to again it is low
During level, the latch of Electromalgnetic locking mechanism is discharged, inserted in the locating slot of fire extinguisher bomb.Complete the locking task of fire extinguisher bomb.Need
The latch of Electromalgnetic locking mechanism is withdrawn before fire extinguisher bomb transmitting in advance, then starts fire extinguisher bomb engine and is launched.Therefore originally belong to
Fire extinguisher bomb is locked by Electromalgnetic locking mechanism and positioning self-lock device under line, when unmanned plane adjusts flight attitude, fire extinguishing
Bullet will not fall, and during release fire extinguisher bomb, can unlock rapidly.
Brief description of the drawings
Fig. 1 is full sectional view of the present utility model；
Fig. 2 is Electromalgnetic locking mechanism sectional view in Fig. 1；
Fig. 3 is positioning self-lock device sectional view in Fig. 1.
Embodiment
The utility model is described in further detail below in conjunction with the embodiment that accompanying drawing provides.
Referring to shown in Fig. 1,2,3, a kind of UAV system fire extinguishing bullet launching device, including launching tube 1 and fire extinguisher bomb 2, it is described
Fire extinguisher bomb 2 is located in launching tube 1, in addition to Electromalgnetic locking mechanism 3 and positioning self-lock device 4, and launching tube 1 is provided with radial direction first and stretched
Enter hole 11 and radially second stretch into hole 12, fire extinguisher bomb 2 is provided with circumferentially positioned groove 21, and the Electromalgnetic locking mechanism 3 includes electromagnetic lock
Shell 31, electromagnetic lock component 32 and latch 33, the electromagnetic lock component 32 is arranged in electromagnetic lock shell 31, and electromagnetic lock shell
31 are provided with pin hole 311, and the latch 33 is connected with electromagnetic lock component 32, and is stretched out outside pin hole 311, and end passes through first
Stretch into hole 11 to insert in locating slot 21, positioning self-lock device 4 includes shell 41, sealing nut 42, sensor 43, spring 44, work
Plug 45 and hoodle 46, the shell 41 stretch into hole 12 with second and are fixedly connected, and sealing nut 42 is fixedly connected with the end face of shell 41,
The sensor 43 is arranged in shell 41, and one end and the piston 45 of spring 44 offset, and the hoodle 46 is arranged on shell 41
At the aperture of mounting hole 411, and stretch into locating slot 21.
Referring to shown in Fig. 1,2, the electromagnetic lock component 32 includes coil brace 321, coil 322, iron core 323, annular branch
Frame 324 and coil spring 325, the coil brace 321 are fixedly connected with ring support 324, and the coil 322 is wound on coil
On support 321, iron core 323 is connected with the mesopore of coil brace 321, and the coil spring 325 is located in ring support 324, and
One end offsets with iron core 323, and the other end offsets with latch 33.When coil 322 is powered, iron core 323 is with dynamic iron core 323 in annular
Stretching motion is done in the hole of support 324 so that latch 33 can be inserted in locating slot 21.
Referring to shown in Fig. 1,2, the electromagnetic lock component 32 also includes bottom plate 326, and the bottom plate 326 is fixedly connected on electromagnetism
Lock in shell 31, and the ring support 324 is fixedly connected on bottom plate 326, bottom plate 326 is provided with bottom plate hole 327, described to insert
Pin 33 passes through bottom plate hole 327.It in order to install ring support 324, can stretch out latch 33.
Referring to shown in Fig. 1,3, the positioning self-lock device 4 also includes trim ring 47 and cover plate 48, and the cover plate 48 is fixed on
In shell 41, sensor 43 is arranged on cover plate 48, and trim ring 47 is between sealing nut 42 and cover plate 48.In order to which can is consolidated
Determine sensor 43 so that sensor 43 can sense the motion of piston 45, and trim ring 47 can be right by sealing nut 42
Cover plate 48 carry out it is spacing, cover plate 48 also have the function that further increase shell 41 in sealing property.
Referring to shown in Fig. 1,3, the positioning self-lock device 4 also includes connecting rod 49, and the piston 45 passes through connecting rod 49 and bullet
Pearl 46 connects.It is plane with the junction of connecting rod 49 in order to which piston 45 is preferably connected with hoodle 46, and on hoodle 46.
Referring to shown in Fig. 1,2,3, the utility model is in use, Electromalgnetic locking mechanism 3 is arranged on launching tube 1, and positioning is certainly
The shell 41 of locking device 4 is stretched into hole 12 installed in the second of launching tube 1.Fire extinguisher bomb 2 is provided with locating slot 21.Fire extinguisher bomb 2 fills
When entering launching tube 1, the hoodle 46 of positioning self-lock device 4 is fallen into the locating slot 21 on fire extinguisher bomb 2, and fire extinguisher bomb 2 is locked in into rule
Fixed position, to ensure that the latch 33 of Electromalgnetic locking mechanism 3 can be inserted accurately in locating slot 21.
Before fire extinguisher bomb 2 loads launching tube 1, controller provides electric current by lead to coil 322, and generation is more than coil spring
The electromagnetic force of 325 pressure, the latch 33 of Electromalgnetic locking mechanism 3 is recovered in launching tube 1, the hoodle 46 of positioning self-lock device 4 by
Spring 44 is extruded on the inside of the barrel for reaching launching tube 1, when fire extinguisher bomb 2 loads from the rear end of launching tube 1, touches positioning self-locking first
Device 4, receding returns after hoodle 46 is stressed, after promoting piston 45 to transfer the pressure to positioning self-lock device 4 by connecting rod 49
On the sensor 43 at end, caused high level is output to controller by the lead of sensor 43, when fire extinguisher bomb 2 is in launching tube 1
When being inside passed onwards to assigned position, hoodle 46 can slip into the locating slot 21 of fire extinguisher bomb 2, pressure release, and sensor 43 recovers low electricity
Flat output, when controller receive sensor 43 export high level risen to by low level be transferred to low level signal again when, cut
The open close electric current crossed lead and be supplied to coil 322, cancels electromagnetic force, latch 33 enters fire extinguisher bomb 2 in the pressure underthrust of spring 44
In locating slot 21, the locking task of fire extinguisher bomb 2 is completed.Withdraw the latch 33 of Electromalgnetic locking mechanism 3 in advance before fire extinguisher bomb 2 is launched,
Then engine is started.The locking of the utility model fire extinguisher bomb is firm, and when unmanned plane adjusts flight attitude, fire extinguisher bomb will not fall
When falling, and discharging fire extinguisher bomb, it can unlock rapidly.
Above-described is only preferred embodiment of the present utility model, it is noted that for the ordinary skill of this area
For personnel, on the premise of not departing from the utility model and creating design, various modifications and improvements can be made, these all belong to
In the scope of protection of the utility model.
Claims (5)
1. a kind of UAV system fire extinguishing bullet launching device, including launching tube (1) and fire extinguisher bomb (2), the fire extinguisher bomb (2) is positioned at hair
In shooting cylinder (1), it is characterised in that：Also include Electromalgnetic locking mechanism (3) and positioning self-lock device (4), launching tube (1) is provided with radially
First stretches into hole (11) and radially second stretches into hole (12), and fire extinguisher bomb (2) is provided with circumferentially positioned groove (21), the electromagnetic lock dress
Putting (3) includes electromagnetic lock shell (31), electromagnetic lock component (32) and latch (33), and the electromagnetic lock component (32) is arranged on electromagnetism
Lock in shell (31), and electromagnetic lock shell (31) is provided with pin hole (311), the latch (33) connects with electromagnetic lock component (32)
Connect, and stretch out pin hole (311) outside, end is stretched into hole (11) insertion locating slot (21) through first, positioning self-lock device (4)
Including shell (41), sealing nut (42), sensor (43), spring (44), piston (45) and hoodle (46), the shell (41)
Hole (12) is stretched into second to be fixedly connected, sealing nut (42) is fixedly connected with shell (41) end face, sensor (43) peace
In shell (41), one end and the piston (45) of spring (44) offset, and the hoodle (46) is arranged on the installation of shell (41)
At hole (411) aperture, and stretch into locating slot (21).
2. UAV system fire extinguishing bullet launching device according to claim 1, it is characterised in that：The electromagnetic lock component (32)
Including coil brace (321), coil (322), iron core (323), ring support (324) and coil spring (325), the coil branch
Frame (321) is fixedly connected with ring support (324), and the coil (322) is wound on coil brace (321), iron core (323) with
The mesopore connection of coil brace (321), the coil spring (325) is located in ring support (324), and one end and iron core
(323) offset, the other end offsets with latch (33).
3. UAV system fire extinguishing bullet launching device according to claim 2, it is characterised in that：The electromagnetic lock component (32)
Also include bottom plate (326), the bottom plate (326) is fixedly connected in electromagnetic lock shell (31), and the ring support (324) is solid
Surely it is connected on bottom plate (326), bottom plate (326) is provided with bottom plate hole (327), and the latch (33) passes through bottom plate hole (327).
4. UAV system fire extinguishing bullet launching device according to claim 1, it is characterised in that：The positioning self-lock device
(4) trim ring (47) and cover plate (48) are also included, the cover plate (48) is fixed in shell (41), and sensor (43) is arranged on cover plate
(48) on, trim ring (47) is located between sealing nut (42) and cover plate (48).
5. UAV system fire extinguishing bullet launching device according to claim 1, it is characterised in that：The positioning self-lock device
(4) connecting rod (49) is also included, the piston (45) is connected by connecting rod (49) with hoodle (46).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720379716.6U CN206648522U (en) | 2017-04-12 | 2017-04-12 | A kind of UAV system fire extinguishing bullet launching device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720379716.6U CN206648522U (en) | 2017-04-12 | 2017-04-12 | A kind of UAV system fire extinguishing bullet launching device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206648522U true CN206648522U (en) | 2017-11-17 |
Family
ID=60275092
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720379716.6U Withdrawn - After Issue CN206648522U (en) | 2017-04-12 | 2017-04-12 | A kind of UAV system fire extinguishing bullet launching device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206648522U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107388891A (en) * | 2017-04-12 | 2017-11-24 | 江苏溧航航空科技有限公司 | A kind of UAV system fire extinguishing bullet launching device |
| CN110496331A (en) * | 2019-09-06 | 2019-11-26 | 嵊州佳想汽车用品有限公司 | A kind of automatic car launcher of forest foam fire-fighting bullet |
| KR20200006702A (en) * | 2018-07-11 | 2020-01-21 | 주식회사 드론고 | A throwing type fire-extinguisher mounted to unmanned vehicle for fire suppressing |
| CN112402871A (en) * | 2020-11-17 | 2021-02-26 | 王广 | Fire extinguishing device for building site |
| CN115970193A (en) * | 2022-12-27 | 2023-04-18 | 海南政华科技有限公司 | Remote fire extinguishing device |
-
2017
- 2017-04-12 CN CN201720379716.6U patent/CN206648522U/en not_active Withdrawn - After Issue
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107388891A (en) * | 2017-04-12 | 2017-11-24 | 江苏溧航航空科技有限公司 | A kind of UAV system fire extinguishing bullet launching device |
| CN107388891B (en) * | 2017-04-12 | 2023-07-18 | 江苏溧航航空科技有限公司 | Unmanned aerial vehicle carries fire extinguishing bomb emitter |
| KR20200006702A (en) * | 2018-07-11 | 2020-01-21 | 주식회사 드론고 | A throwing type fire-extinguisher mounted to unmanned vehicle for fire suppressing |
| KR102075026B1 (en) * | 2018-07-11 | 2020-02-07 | 하상균 | A throwing type fire-extinguisher mounted to unmanned vehicle for fire suppressing |
| CN110496331A (en) * | 2019-09-06 | 2019-11-26 | 嵊州佳想汽车用品有限公司 | A kind of automatic car launcher of forest foam fire-fighting bullet |
| CN112402871A (en) * | 2020-11-17 | 2021-02-26 | 王广 | Fire extinguishing device for building site |
| CN115970193A (en) * | 2022-12-27 | 2023-04-18 | 海南政华科技有限公司 | Remote fire extinguishing device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CB03 | Change of inventor or designer information |
Inventor after: Chen Jingwang Inventor after: Gui Jing Inventor before: Chen Jingwang Inventor before: Li Jijun Inventor before: Gui Jing |
|
| CB03 | Change of inventor or designer information | ||
| CP02 | Change in the address of a patent holder |
Address after: 213000 No. 8-5 Huashan Road, Xinbei District, Changzhou City, Jiangsu Province Patentee after: JIANGSU LIHANG AVIATION TECHNOLOGY CO.,LTD. Address before: 213000 Dongcheng Mingju Building 801, Tianning District, Changzhou City, Jiangsu Province Patentee before: JIANGSU LIHANG AVIATION TECHNOLOGY CO.,LTD. |
|
| CP02 | Change in the address of a patent holder | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20171117 Effective date of abandoning: 20230718 |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20171117 Effective date of abandoning: 20230718 |
|
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |