CN105667795A - Fire extinguishing bomb launching system for unmanned aerial vehicle - Google Patents
Fire extinguishing bomb launching system for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN105667795A CN105667795A CN201610165872.2A CN201610165872A CN105667795A CN 105667795 A CN105667795 A CN 105667795A CN 201610165872 A CN201610165872 A CN 201610165872A CN 105667795 A CN105667795 A CN 105667795A
- Authority
- CN
- China
- Prior art keywords
- guide rail
- fire
- man
- machine
- hook
- 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.)
- Granted
Links
- 230000008878 coupling Effects 0.000 claims description 23
- 238000010168 coupling process Methods 0.000 claims description 23
- 238000005859 coupling reaction Methods 0.000 claims description 23
- 239000011159 matrix material Substances 0.000 claims description 14
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 10
- 229910052799 carbon Inorganic materials 0.000 claims description 10
- 238000004891 communication Methods 0.000 abstract description 4
- 238000005516 engineering process Methods 0.000 description 7
- 230000000694 effects Effects 0.000 description 3
- 239000003981 vehicle Substances 0.000 description 3
- 238000009434 installation Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 206010057071 Rectal tenesmus Diseases 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000000412 dendrimer Substances 0.000 description 1
- 229920000736 dendritic polymer Polymers 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 239000000806 elastomer Substances 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 208000012271 tenesmus Diseases 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
Landscapes
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Train Traffic Observation, Control, And Security (AREA)
Abstract
The invention provides a fire extinguishing bomb launching system for an unmanned aerial vehicle. The fire extinguishing bomb launching system comprises a ground station as well as the unmanned aerial vehicle, a hanging rack and fire extinguishing bombs which are sequentially connected from top to bottom, wherein the hanging rack comprises a launch platform, batteries which are in line connection with the unmanned aerial vehicle are arranged above the launch platform, a guide rail assembly is arranged below the launch platform, the fire extinguishing bombs are hung below the guide rail assembly, the ground station comprises a ground portable computer and a ground radio station, and the ground portable computer is connected with the ground radio station through a data connecting line. According to the fire extinguishing bomb launching system for the unmanned aerial vehicle, provided by the invention, fire-fighting fire extinguishing and relief operations for high-rise buildings are implemented by adopting the unmanned aerial vehicle to carry the fire extinguishing bombs, so that ground obstacles can be effectively evaded; the unmanned aerial vehicle flexibly shuttles among the buildings, maintains unimpeded communication contact with the ground, transmits information on a fire scene to a ground command center by means of images and data, receives ground commands and implements window breaking, aiming and fire extinguishing bomb launching so as to implement fire extinguishing.
Description
Technical field
The present invention relates to without man-machine fire-fighting technique field, particularly relate to a kind of without man-machine fire-extinguishing bullet launching system.
Background technology
Along with China's Highrise buildings quantity with highly constantly rise, fire-fighting and rescue pressure increases day by day. With existing fire-fighting fire extinguishing means, the demand of China's city high-rise building fire-fighting fire extinguishing can not be adapted to. Affect by principle of work and physics limit, generally have that car body is roomy, expanded area big for Special fire fighting vehicle the equipment of more than hundred meters high-rise buildings outside rescue, supply and ensure the features such as equipment is complicated, thus bring and many limit by rescue site, be badly in need of a kind of accurately judging within the short period of time, the equipment of timely fire fighting and rescue, implement fire-fighting fire extinguishing, solve rescue and ensure the problem of equipment " enter and do not go ", " Zhan Bukai ", " can't reach ".
Adopting without man-machine enforcement elevation building fire fighting and rescue action is the problem starting research in recent years, although fire-extinguishing bullet and all more ripe without man-machine technology, but also well the technology characteristic sum of fire-extinguishing bullet is not linked effectively without man-machine technology feature at present, form practical high-tech product. Therefore, without the research and development of man-machine fire-fighting fire extinguishing platform, it is very necessary.
Summary of the invention
Technical problem to be solved by this invention is: the deficiency being equipped in the high-rise building fire-fighting fire extinguishing of city to exist " enter and do not go ", " Zhan Bukai ", " can't reach " in order to overcome Special fire fighting vehicle in prior art, the present invention provides a kind of without man-machine fire-extinguishing bullet launching system.
The present invention solves the technical scheme that its technical problem to be adopted: a kind of without man-machine fire-extinguishing bullet launching system, comprise terrestrial station and connect successively from top to bottom without man-machine, hanger and fire-extinguishing bullet, described hanger comprises flat pad, it is provided with above described flat pad and the battery that described unmanned machine circuit is connected, it is provided with guide assembly below described flat pad, described fire-extinguishing bullet is suspended on below described guide assembly, described terrestrial station comprises ground portable machine and terrestrial wireless radio station, and described ground portable machine is connected with described terrestrial wireless radio station by data connecting line.
Adopt and implement high-rise building fire-fighting fire extinguishing rescue action without the man-machine fire-extinguishing bullet that carries, can effectively avoid ground obstacle, shuttle back and forth flexibly between building, and and ground keep unimpeded communication contact, the information of scene of fire is transferred to ground command center in the way of image, data, accept surface instruction, implement broken window, aim at and launch fire-extinguishing bullet enforcement fire extinguishing.
Require steadily when hanging frame type fire-extinguishing bullet is launched. During from beam, fire-extinguishing bullet direction of motion requires consistent with rocket thrust direction, prevents fire-extinguishing bullet from departing from intended target; And form side force and impact without man-machine flight.
Further, described guide assembly comprises guide rail matrix and hook, described guide rail matrix is provided with front guide rail and rear guide rail, described front guide rail and described rear guide rail parallel are arranged, described hook comprises front guide rail hook and rear guide rail hook, described front guide rail hook is suspended on front guide rail, and described rear guide rail hook is suspended on rear guide rail, and described front guide rail hook is equal apart from front guide rail distance and the described rear guide rail hook of the end distance held that comes off apart from rear guide rail that comes off.
The double-buckle internally and externally guide rail adopting the front and back of parallel setting to arrange ensures the stability during transmitting of UAV system fire-extinguishing bullet, reduces front end tenesmus, ensures that elastomer axis is parallel with working direction. Front guide rail adopts the T-shaped chute of internal fastening type, for hanging the front end of fire-extinguishing bullet, rear guide rail adopts exterior buckle type straight, for hanging the rear end of fire-extinguishing bullet, the hanging position of front guide rail hook and the hanging position of rear guide rail hook are at a distance of certain distance, and two hook hanging positions apart from its separately come off end distance equal, ensure before and after hook can come off simultaneously not influenced.
The guide assembly of this hanger by integral for front and back set of rails, respectively with front and back guide rail hook with the use of, the alignment of guide rail before and after being ensured by mechanical workout equipment, difficulty when reducing installation.
Adopting double-buckle internally and externally guide rail in flight course, interior outer guide hook activity direction in chute restricts mutually, further ensures when body runs at a high speed and does not produce side force, ensures without man-machine flight attitude, it is achieved fall simultaneously, ensures that fire-extinguishing bullet launches precision.
Concrete, described front guide rail is the T-shaped chute of internal fastening type, described front guide rail hook comprises front guide rail hook suspended end and front guide rail hook body coupling end, described front guide rail hook suspended end is the T-type structure mated with the T-shaped chute of described internal fastening type, the lower surface of described front guide rail hook body coupling end is arc, the radian of described arc is identical with fire-extinguishing bullet surface radian, and the bottom of described front guide rail hook suspended end is positioned at the central point of front guide rail hook body coupling end upper surface;
Described rear guide rail is the exterior buckle type line slideway of two parallel settings, and lay respectively at the both sides of described front guide rail, described rear guide rail hook comprises rear guide rail hook suspended end and rear guide rail hook body coupling end, described rear guide rail hook suspended end inside is provided with and the exterior buckle type straight that described exterior buckle type line slideway mates, the lower surface of described rear guide rail hook body coupling end is arc, the radian of described arc is identical with fire-extinguishing bullet surface radian, and the both ends that body coupling end upper surface is linked up with rear guide rail respectively in the bottom of described rear guide rail hook suspended end are connected.
In order to reduce the resistance of motion on slide rail when fire-extinguishing bullet is launched, will reducing the frictional force between hook and hanger, fire-extinguishing bullet can arbitrarily slide on slide rail as far as possible. But, have the danger come off when unmanned plane during flying, it is necessary to have a stationary installation flexibly. Therefore, described guide assembly also comprises the firm device of electromagnetism, the firm device of described electromagnetism comprises firm pin and firm pin-and-hole, described firm pin-and-hole comprises the firm pin-and-hole of hanger matrix and the firm pin-and-hole of fire-extinguishing bullet, the described firm pin-and-hole of hanger matrix and the firm pin-and-hole of fire-extinguishing bullet align up and down and all with firm bayonet fittings. Steady brace adopts electromagnetism adhesive technology, is convenient to the safety before the fixing of fire-extinguishing bullet and transmitting and unlocks.
Further, in order to realize guide assembly with without man-machine connection, described hanger also comprises guide rail fixing element, and described guide rail fixing element is provided with multiple guide rail set screw, and described guide assembly is fixedly connected with described flat pad by guide rail fixing element.
Further, in order to gather the graphic information of scene of fire in real time, the front end of described guide rail fixing element is provided with camera.
Further, described comprising without man-machine body without man-machine, described be circumferentially evenly provided with multiple rotor without man-machine body, described rotor is connected without man-machine body with described by carbon pipe, described carbon pipe and described be provided with folding arm without man-machine body coupling end, described is provided with covering without man-machine bodies top.
It is light that carbon pipe has weight, the feature of Stability Analysis of Structures, adopts carbon pipe to do rotor and the web member without man-machine body, it is possible to reduce without man-machine weight; Employing folding arm connects, it is possible to makes to be folded up by rotor when not using without man-machine, to reduce floor space, is convenient to deposit; Covering for the protection of without man-machine internal mechanical structure and electronic component, prevents in flight air-flow on the impact of the GPS locating device of fuselage interior, to improve the accuracy of the positioning precision without man-machine and flight path; When assumed load is identical, adopting carbon fibre material compared with other materials, fuselage weight is light, and hardness strength can reach design requirements, can meet the requirement born a heavy burden; Meanwhile, also there is effect attractive in appearance.
Further, in order to realize without man-machine location and accurately put out a fire, send the various information that scene of fire gathers in real time, described on man-machine, also it is provided with GPS locating device and wireless transmitter, described terrestrial wireless radio station is provided with ground receiving antenna, and described wireless transmitter is connected with described ground receiving antenna signal.
Further, rising and falling without man-machine in order to convenient, also comprise and be located at the described landing gear without man-machine lower section, described flat pad is fixedly connected with described landing gear.
The invention has the beneficial effects as follows: one provided by the invention is without man-machine fire-extinguishing bullet launching system, adopt and implement high-rise building fire-fighting fire extinguishing rescue action without the man-machine fire-extinguishing bullet that carries, pass through unmanned air vehicle technique, communication technology, effective link of fire-extinguishing bullet technology, form UAV system fire-extinguishing bullet fire-fighting fire extinguishing system platform, can effectively avoid ground obstacle, shuttle back and forth flexibly between building, and and ground keep unimpeded communication contact, by the information of scene of fire with image, the mode of data is transferred to ground command center, accept surface instruction, implement broken window, aim at and launch fire-extinguishing bullet enforcement fire extinguishing, and by next step action of the Evaluation operation according to extinguishing effect, can thoroughly solve current fire-fighting equipment " enter and do not go ", " Zhan Bukai ", the problem " can't reach ".
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the invention will be further described.
Fig. 1 is the structural representation of most preferred embodiment of the present invention;
The structural representation of Tu2Shi Tu1Zhong terrestrial station;
Fig. 3 is the structural representation of hanger and landing gear in Fig. 1;
Fig. 4 is the structural representation of Fig. 1 middle guide matrix;
Fig. 5 is the upward view of Fig. 4;
Fig. 6 is the structural representation of front guide rail hook;
Fig. 7 is the structural representation of rear guide rail hook.
In figure: 1, terrestrial station, 11, ground portable machine, 12, terrestrial wireless radio station, 13, data connecting line, 14, ground receiving antenna, 2, without man-machine, 21, without man-machine body, 22, rotor, 23, carbon pipe, 24, folding arm, 25, covering, 26, GPS locating device, 27, motor, 3, hanger, 31, flat pad, 32, battery, 33, guide assembly, 331, guide rail matrix, 332, front guide rail, 333, rear guide rail, 334, front guide rail is linked up with, 3341, front guide rail hook suspended end, 3342, front guide rail hook body coupling end, 335, rear guide rail is linked up with, 3351, rear guide rail hook suspended end, 3352, rear guide rail hook body coupling end, 336, firm pin-and-hole, 34, guide rail fixing element, 35, guide rail set screw, 36, camera, 4, fire-extinguishing bullet, 5, landing gear, 51, lateral connection bar, 52, support, 53, platform.
Embodiment
The present invention is described in detail by reference to the accompanying drawings now. This figure is the schematic diagram simplified, and the basic structure of the present invention is only described with illustration, and therefore it only shows the formation relevant with the present invention.
As shown in figs. 1-7, the one of the present invention, without man-machine fire-extinguishing bullet launching system, comprises terrestrial station 1, connect successively from top to bottom without man-machine 2, hanger 3 and fire-extinguishing bullet 4 and be located at described without the landing gear 5 below man-machine 2.
As shown in Figure 1, described comprise without man-machine body 21 without man-machine 2, described circumferentially evenly it is provided with multiple rotor 22 without man-machine body 21, described rotor 22 is connected without man-machine body 21 with described by carbon pipe 23, described carbon pipe 23 is provided with folding arm 24 with described without man-machine body 21 coupling end, described being provided with covering 25 without man-machine body 21 top, described be also provided with GPS locating device 26 and wireless transmitter on man-machine 2, described wireless transmitter is connected with described ground receiving antenna 14 signal. In the present embodiment, rotor 22 is 8, and each rotor 22 is driven by a motor 27.
As shown in Figure 2, described terrestrial station 1 comprises ground portable machine 11 and terrestrial wireless radio station 12, and described ground portable machine 11 is connected with described terrestrial wireless radio station 12 by data connecting line 13, and described terrestrial wireless radio station 12 is provided with ground receiving antenna 14.
As shown in Figure 3, described hanger 3 comprises and is fixedly connected with flat pad 31 with described landing gear 5, it is provided with above described flat pad 31 and the described battery 32 without man-machine 2 connections, it is provided with guide assembly 33 below described flat pad 31, described fire-extinguishing bullet 4 is suspended on below described guide assembly 33, described hanger 3 also comprises guide rail fixing element 34, described guide rail fixing element 34 is provided with six guide rail set screws 35, described guide assembly 33 is fixedly connected with described flat pad 31 by guide rail fixing element 34, and the front end of described guide rail fixing element 34 is provided with camera 36.
As shown in figs. 4-7, described guide assembly 33 comprises guide rail matrix 331 and hook, described guide rail matrix 331 is provided with front guide rail 332 and rear guide rail 333, the setting parallel with described rear guide rail 333 of described front guide rail 332, described hook comprises front guide rail hook 334 and rear guide rail hook 335, described front guide rail hook 334 is suspended on front guide rail 332, described rear guide rail hook 335 is suspended on rear guide rail 333, and described front guide rail hook 334 is equal apart from front guide rail 332 distance and the described rear guide rail hook 335 of the end distance held that comes off apart from rear guide rail 333 that comes off.
As shown in Figure 6, described front guide rail 332 is the T-shaped chute of internal fastening type, described front guide rail hook 334 is T-shaped hook, comprise front guide rail hook suspended end 3341 and front guide rail hook body coupling end 3342, described front guide rail hook suspended end 3341 is the T-type structure mated with the T-shaped chute of described internal fastening type, the lower surface of described front guide rail hook body coupling end 3342 is arc, the radian of described arc is identical with fire-extinguishing bullet 4 surface radian, and the bottom of described front guide rail hook suspended end 3341 is positioned at the central point of front guide rail hook body coupling end 3342 upper surface.
As shown in Figure 7, described rear guide rail 333 is the exterior buckle type line slideway of two parallel settings, and lay respectively at the both sides of described front guide rail 332, described rear guide rail hook 335 comprises rear guide rail hook suspended end 3351 and rear guide rail hook body coupling end 3352, described rear guide rail hook suspended end 3351 inside is provided with and the exterior buckle type straight that described exterior buckle type line slideway mates, the lower surface of described rear guide rail hook body coupling end 3352 is arc, the radian of described arc is identical with fire-extinguishing bullet 4 surface radian, the both ends that body coupling end 3352 upper surface is linked up with rear guide rail respectively in the bottom of described rear guide rail hook suspended end 3351 are connected.
Described guide assembly (33) also comprises the firm device of electromagnetism, the firm device of described electromagnetism comprises firm pin and firm pin-and-hole (336), described firm pin-and-hole (336) comprises the firm pin-and-hole of hanger matrix and the firm pin-and-hole of fire-extinguishing bullet, the described firm pin-and-hole of hanger matrix and the firm pin-and-hole of fire-extinguishing bullet align up and down and all with firm bayonet fittings.
As shown in Figure 3, described landing gear 5 comprises two lateral connection bars 51 and two supports 52, support 52 is U-shaped frame, and U-shaped frame is from bottom to opening end to contract, forming up-small and down-big trapezoidal shape, two supports 52 are symmetrically set in the both sides of fire-extinguishing bullet 4, the opening end of lateral connection bar 51 connected symmetrical dendrimer position support 52, and the distance b that the length a of lateral connection bar 51 is less than between bottom two stands 52, it is up-small and down-big prismoid shaped framework that landing gear 5 forms profile on the whole. The platform 53 that the mid-way of U-shaped frame is provided with U-shaped frame both sides are connected, the platform 53 on each support 52 is two, and parallel setting.
Taking the above-mentioned desirable embodiment according to the present invention as enlightenment, by above-mentioned description, relevant staff in the scope not deviateing the present invention, can carry out various change and amendment completely. The technical scope of this invention is not limited to the content on specification sheets, it is necessary to determine its technical scope according to right.
Claims (9)
1. one kind without man-machine fire-extinguishing bullet launching system, it is characterized in that: comprise terrestrial station (1) and connect successively from top to bottom without man-machine (2), hanger (3) and fire-extinguishing bullet (4), described hanger (3) comprises flat pad (31), described flat pad (31) top is provided with and the described battery (32) without man-machine (2) connection, described flat pad (31) lower section is provided with guide assembly (33), described fire-extinguishing bullet (4) is suspended on described guide assembly (33) lower section, described terrestrial station (1) comprises ground portable machine (11) and terrestrial wireless radio station (12), described ground portable machine (11) is connected with described terrestrial wireless radio station (12) by data connecting line (13).
2. as claimed in claim 1 without man-machine fire-extinguishing bullet launching system, it is characterized in that: described guide assembly (33) comprises guide rail matrix (331) and hook, described guide rail matrix (331) is provided with front guide rail (332) and rear guide rail (333), the setting parallel with described rear guide rail (333) of described front guide rail (332), described hook comprises front guide rail hook (334) and rear guide rail hook (335), described front guide rail hook (334) is suspended on front guide rail (332), described rear guide rail hook (335) is suspended on rear guide rail (333), described front guide rail hook (334) comes off apart from front guide rail (332), and link up with (335) distance held that comes off apart from rear guide rail (333) with described rear guide rail equal for the distance of end.
3. as claimed in claim 2 without man-machine fire-extinguishing bullet launching system, it is characterized in that: described front guide rail (332) is the T-shaped chute of internal fastening type, described front guide rail hook (334) comprises front guide rail hook suspended end (3341) and front guide rail hook body coupling end (3342), described front guide rail hook suspended end (3341) is the T-type structure mated with the T-shaped chute of described internal fastening type, the lower surface of described front guide rail hook body coupling end (3342) is arc, the radian of described arc is identical with fire-extinguishing bullet (4) surface radian, the bottom of described front guide rail hook suspended end (3341) is positioned at the central point of front guide rail hook body coupling end (3342) upper surface,
Described rear guide rail (333) is the exterior buckle type line slideway of two parallel settings, and lay respectively at the both sides of described front guide rail (332), described rear guide rail hook (335) comprises rear guide rail hook suspended end (3351) and rear guide rail hook body coupling end (3352), described rear guide rail hook suspended end (3351) inside is provided with and the exterior buckle type straight that described exterior buckle type line slideway mates, the lower surface of described rear guide rail hook body coupling end (3352) is arc, the radian of described arc is identical with fire-extinguishing bullet (4) surface radian, the both ends that body coupling end (3352) upper surface is linked up with rear guide rail respectively in the bottom of described rear guide rail hook suspended end (3351) are connected.
4. as claimed in claim 3 without man-machine fire-extinguishing bullet launching system, it is characterized in that: described guide assembly (33) also comprises the firm device of electromagnetism, the firm device of described electromagnetism comprises firm pin and firm pin-and-hole (336), described firm pin-and-hole (336) comprises the firm pin-and-hole of hanger matrix and the firm pin-and-hole of fire-extinguishing bullet, the described firm pin-and-hole of hanger matrix and the firm pin-and-hole of fire-extinguishing bullet align up and down and all with firm bayonet fittings.
5. as claimed in claim 1 without man-machine fire-extinguishing bullet launching system, it is characterized in that: described hanger (3) also comprises guide rail fixing element (34), described guide rail fixing element (34) is provided with multiple guide rail set screw (35), and described guide assembly (33) is fixedly connected with described flat pad (31) by guide rail fixing element (34).
6. as claimed in claim 5 without man-machine fire-extinguishing bullet launching system, it is characterised in that: the front end of described guide rail fixing element (34) is provided with camera (36).
7. as claimed in claim 1 without man-machine fire-extinguishing bullet launching system, it is characterized in that: described comprise without man-machine body (21) without man-machine (2), described circumferentially evenly it is provided with multiple rotor (22) without man-machine body (21), described rotor (22) is connected without man-machine body (21) with described by carbon pipe (23), described carbon pipe (23), with described being provided with folding arm (24) without man-machine body (21) coupling end, described is provided with covering (25) without man-machine body (21) top.
8. as claimed in claim 1 without man-machine fire-extinguishing bullet launching system, it is characterized in that: described without man-machine (2) are also provided with GPS locating device (26) and wireless transmitter, described terrestrial wireless radio station (12) is provided with ground receiving antenna (14), and described wireless transmitter is connected with described ground receiving antenna (14) signal.
9. as claimed in claim 1 without man-machine fire-extinguishing bullet launching system, it is characterized in that: also comprising and be located at the described landing gear (5) without man-machine (2) lower section, described flat pad (31) is fixedly connected with described landing gear (5).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610032100 | 2016-01-18 | ||
| CN2016100321001 | 2016-01-18 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105667795A true CN105667795A (en) | 2016-06-15 |
| CN105667795B CN105667795B (en) | 2018-09-07 |
Family
ID=56215335
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610165872.2A Expired - Fee Related CN105667795B (en) | 2016-01-18 | 2016-03-22 | Unmanned plane fire extinguisher bomb emission system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105667795B (en) |
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105963882A (en) * | 2016-06-24 | 2016-09-28 | 河南沃野智能科技有限公司 | Air-to-surface rocket fire extinguisher and method |
| CN105999587A (en) * | 2016-06-28 | 2016-10-12 | 安徽扫宝智能科技有限公司 | Fire fighting unmanned aerial vehicle for power high-voltage overhead line |
| CN106506059A (en) * | 2016-10-28 | 2017-03-15 | 易瓦特科技股份公司 | Hand-held unmanned aerial vehicle station |
| CN106569506A (en) * | 2016-10-19 | 2017-04-19 | 广东容祺智能科技有限公司 | Automatic and accurate fire extinguishing system for unmanned aerial vehicle |
| CN106585968A (en) * | 2016-12-19 | 2017-04-26 | 南京理工大学 | Multi-rotor unmanned aerial vehicle fire extinguishing method based on low-temperature hot aerosol fire extinguishing agent |
| CN108051163A (en) * | 2017-12-28 | 2018-05-18 | 顺丰科技有限公司 | A kind of unmanned plane mechanical testing equipment |
| CN108082487A (en) * | 2017-12-15 | 2018-05-29 | 佛山市神风航空科技有限公司 | A kind of disaster relief unmanned plane |
| CN108248838A (en) * | 2017-12-20 | 2018-07-06 | 江苏天域航空科技集团股份有限公司 | Fire-fighting fire extinguishing unmanned helicopter system |
| CN108674658A (en) * | 2018-07-09 | 2018-10-19 | 陈福敏 | A kind of manned fire-fighting aircraft and the method using aircraft progress high-altitude fire extinguishing |
| CN108688807A (en) * | 2018-04-26 | 2018-10-23 | 西北工业大学 | A kind of high building fire fighting unmanned plane and fire-extinguishing |
| CN108771803A (en) * | 2018-08-10 | 2018-11-09 | 中国人民解放军火箭军工程大学 | Control system and fire extinguishing system for the fire extinguishing of skyscraper rotor wing unmanned aerial vehicle |
| CN108791846A (en) * | 2018-06-04 | 2018-11-13 | 西北工业大学 | A kind of six rotor unmanned plane and fire-extinguishing of single-shot |
| CN109334981A (en) * | 2018-11-22 | 2019-02-15 | 东北大学秦皇岛分校 | A kind of unmanned plane equipped with fire extinguishing bullet launching device |
| WO2020052103A1 (en) * | 2018-09-14 | 2020-03-19 | 广州市华科尔科技股份有限公司 | Firefighting method using firefighting unmanned aerial vehicle |
| WO2020052100A1 (en) * | 2018-09-14 | 2020-03-19 | 广州市华科尔科技股份有限公司 | Method for triggering fire-fighting unmanned aerial vehicle to launch fire-fighting bomb |
| CN112386832A (en) * | 2020-12-01 | 2021-02-23 | 安徽信息工程学院 | Fire rescue unmanned aerial vehicle |
| CN114699684A (en) * | 2022-03-31 | 2022-07-05 | 湖南神州防务科技有限公司 | Window breaking fire extinguishing bomb for high-rise building |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4870885A (en) * | 1987-06-05 | 1989-10-03 | R. Alkan & Cie | Device for carrying and releasing a load such as a missile |
| CN203944052U (en) * | 2014-06-11 | 2014-11-19 | 江苏数字鹰科技发展有限公司 | The police fire extinguishing unmanned plane of high building |
| CN204161623U (en) * | 2014-09-05 | 2015-02-18 | 徐伟佳 | A kind of unmanned plane air attack bullet dispenser |
| CN204750571U (en) * | 2015-05-29 | 2015-11-11 | 沈阳航空航天大学 | A flight machine people for high -rise building fire control is put out a fire |
| CN105129091A (en) * | 2015-08-13 | 2015-12-09 | 王清洁 | Extinguishing device for unmanned aerial vehicle |
| CN205652362U (en) * | 2016-01-18 | 2016-10-19 | 江苏顶飞航空科技有限公司 | Unmanned aerial vehicle fire extinguishing bomb transmitting system |
-
2016
- 2016-03-22 CN CN201610165872.2A patent/CN105667795B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4870885A (en) * | 1987-06-05 | 1989-10-03 | R. Alkan & Cie | Device for carrying and releasing a load such as a missile |
| CN203944052U (en) * | 2014-06-11 | 2014-11-19 | 江苏数字鹰科技发展有限公司 | The police fire extinguishing unmanned plane of high building |
| CN204161623U (en) * | 2014-09-05 | 2015-02-18 | 徐伟佳 | A kind of unmanned plane air attack bullet dispenser |
| CN204750571U (en) * | 2015-05-29 | 2015-11-11 | 沈阳航空航天大学 | A flight machine people for high -rise building fire control is put out a fire |
| CN105129091A (en) * | 2015-08-13 | 2015-12-09 | 王清洁 | Extinguishing device for unmanned aerial vehicle |
| CN205652362U (en) * | 2016-01-18 | 2016-10-19 | 江苏顶飞航空科技有限公司 | Unmanned aerial vehicle fire extinguishing bomb transmitting system |
Cited By (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105963882A (en) * | 2016-06-24 | 2016-09-28 | 河南沃野智能科技有限公司 | Air-to-surface rocket fire extinguisher and method |
| CN105963882B (en) * | 2016-06-24 | 2022-03-04 | 河南沃野智能科技有限公司 | Air-to-ground rocket fire extinguisher and method |
| CN105999587A (en) * | 2016-06-28 | 2016-10-12 | 安徽扫宝智能科技有限公司 | Fire fighting unmanned aerial vehicle for power high-voltage overhead line |
| CN105999587B (en) * | 2016-06-28 | 2019-05-14 | 新疆博新智航航空科技有限责任公司 | A kind of power high voltage overhead transmission line fire attack unmanned plane |
| CN106569506A (en) * | 2016-10-19 | 2017-04-19 | 广东容祺智能科技有限公司 | Automatic and accurate fire extinguishing system for unmanned aerial vehicle |
| CN106506059A (en) * | 2016-10-28 | 2017-03-15 | 易瓦特科技股份公司 | Hand-held unmanned aerial vehicle station |
| CN106585968A (en) * | 2016-12-19 | 2017-04-26 | 南京理工大学 | Multi-rotor unmanned aerial vehicle fire extinguishing method based on low-temperature hot aerosol fire extinguishing agent |
| CN106585968B (en) * | 2016-12-19 | 2019-07-02 | 南京理工大学 | Multi-rotor unmanned aerial vehicle extinguishing method based on low temperature hot-gas sol fire extinguishing agent |
| CN108082487A (en) * | 2017-12-15 | 2018-05-29 | 佛山市神风航空科技有限公司 | A kind of disaster relief unmanned plane |
| CN108248838A (en) * | 2017-12-20 | 2018-07-06 | 江苏天域航空科技集团股份有限公司 | Fire-fighting fire extinguishing unmanned helicopter system |
| CN108051163A (en) * | 2017-12-28 | 2018-05-18 | 顺丰科技有限公司 | A kind of unmanned plane mechanical testing equipment |
| CN108688807A (en) * | 2018-04-26 | 2018-10-23 | 西北工业大学 | A kind of high building fire fighting unmanned plane and fire-extinguishing |
| CN108791846A (en) * | 2018-06-04 | 2018-11-13 | 西北工业大学 | A kind of six rotor unmanned plane and fire-extinguishing of single-shot |
| CN108674658A (en) * | 2018-07-09 | 2018-10-19 | 陈福敏 | A kind of manned fire-fighting aircraft and the method using aircraft progress high-altitude fire extinguishing |
| CN108771803A (en) * | 2018-08-10 | 2018-11-09 | 中国人民解放军火箭军工程大学 | Control system and fire extinguishing system for the fire extinguishing of skyscraper rotor wing unmanned aerial vehicle |
| CN108771803B (en) * | 2018-08-10 | 2023-09-15 | 李�杰 | Control system for high-rise building rotor unmanned aerial vehicle fire extinguishment and fire extinguishing system |
| WO2020052103A1 (en) * | 2018-09-14 | 2020-03-19 | 广州市华科尔科技股份有限公司 | Firefighting method using firefighting unmanned aerial vehicle |
| WO2020052100A1 (en) * | 2018-09-14 | 2020-03-19 | 广州市华科尔科技股份有限公司 | Method for triggering fire-fighting unmanned aerial vehicle to launch fire-fighting bomb |
| CN109334981A (en) * | 2018-11-22 | 2019-02-15 | 东北大学秦皇岛分校 | A kind of unmanned plane equipped with fire extinguishing bullet launching device |
| CN109334981B (en) * | 2018-11-22 | 2023-09-05 | 东北大学秦皇岛分校 | Unmanned aerial vehicle carrying fire extinguishing bomb launching device |
| CN112386832A (en) * | 2020-12-01 | 2021-02-23 | 安徽信息工程学院 | Fire rescue unmanned aerial vehicle |
| CN114699684A (en) * | 2022-03-31 | 2022-07-05 | 湖南神州防务科技有限公司 | Window breaking fire extinguishing bomb for high-rise building |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105667795B (en) | 2018-09-07 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105667795A (en) | Fire extinguishing bomb launching system for unmanned aerial vehicle | |
| CN107472536B (en) | Unmanned aerial vehicle for high-altitude fire extinguishment | |
| CN108820214B (en) | Aircraft scouting control transmitting system | |
| US20170369169A1 (en) | Unmanned aerial vehicle system having multi-rotor type rotary wing | |
| CN108771803B (en) | Control system for high-rise building rotor unmanned aerial vehicle fire extinguishment and fire extinguishing system | |
| CN107738750B (en) | Aerial towline towing target system-based unmanned aerial vehicle air-based accurate recovery device and method | |
| CN207173951U (en) | The unmanned fire extinguishing system of high altitude kite balloon formula | |
| CN102785778A (en) | Tubular transmitting fire-extinguishing unmanned plane and fire-extinguishing control methods | |
| CN107487444B (en) | High-altitude mooring unmanned fire extinguishing system | |
| CN105963882A (en) | Air-to-surface rocket fire extinguisher and method | |
| CN103112385A (en) | Fire rescue device based on unmanned aerial vehicle | |
| CN109305364B (en) | Aiming method of fire-fighting unmanned aerial vehicle | |
| WO2020052100A1 (en) | Method for triggering fire-fighting unmanned aerial vehicle to launch fire-fighting bomb | |
| CN105126278B (en) | A kind of suspension type skyscraper automatic fire extinguisher | |
| CN113926106A (en) | Air-drop forest fire extinguishing bomb | |
| CN105667796B (en) | Unmanned plane fire extinguisher bomb hanger | |
| CN205652362U (en) | Unmanned aerial vehicle fire extinguishing bomb transmitting system | |
| CN203280949U (en) | Drone-based fire rescue device | |
| CN207889999U (en) | A kind of carry for unmanned plane and hit net integral type retracting device | |
| CN107600427A (en) | A kind of unmanned plane airdrop platform | |
| CN104724304A (en) | Space photoelectric location-awareness wireless control accurate release device and release method | |
| CN203864994U (en) | Unmanned patrolling airplane for power transmission line | |
| CN208882113U (en) | A kind of aircraft, which is examined, beats control emission system | |
| CN102029036B (en) | Four-DOF fire-fighting spray gun | |
| CN206968991U (en) | Unmanned plane for high altitude firefighting fire extinguishing |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20201027 Address after: 213103 Jiangsu Province, Changzhou city Wujin District Henglin town Cui Village Patentee after: Changzhou Ding Ding cemented carbide Co.,Ltd. Address before: 213103 Jiangsu Province, Changzhou City Economic Development Zone Cui Henglin Road No. 9 Patentee before: JIANGSU DINGFEI AVIATION TECHNOLOGY Co.,Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180907 |