CN204489179U - A kind of water life-saving duct unmanned aerial vehicle - Google Patents
A kind of water life-saving duct unmanned aerial vehicle Download PDFInfo
- Publication number
- CN204489179U CN204489179U CN201520179590.9U CN201520179590U CN204489179U CN 204489179 U CN204489179 U CN 204489179U CN 201520179590 U CN201520179590 U CN 201520179590U CN 204489179 U CN204489179 U CN 204489179U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- plane body
- duct
- aerial vehicle
- water
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Alarm Systems (AREA)
Abstract
The utility model discloses a kind of water life-saving duct unmanned aerial vehicle, belong to unmanned plane rescue field.Rescue duct unmanned aerial vehicle of the present utility model, comprises unmanned plane body, and unmanned plane body is provided with GPS registration device and control setup, and described unmanned plane body is provided with duct, installs rotor in described duct; Described unmanned plane body fits, in body water wing, is equipped with buoy quoit and searches camera head on the downside of unmanned plane body, and search camera head is positioned at outside the circle body of buoy quoit.The utility model makes unmanned plane can not because flying power is not enough or faults itself and the bottom that sinks in the process of suing and labouring by the body water wing on unmanned plane body, and protection unmanned plane body can not be intake impaired, is convenient to reclaim, and solves the rescue problem in vast waters.
Description
Technical field
The utility model relates to unmanned plane rescue technique field, more particularly, relates to a kind of water life-saving duct unmanned aerial vehicle.
Background technology
China is the vast country in a waters, and while utilizing water resource, also endure the disaster of aspect, waters to the fullest extent, the property lost because of natural floods every year on average reaches and exceeds 100 billion, and the precious life lost because various accident is drowned every year is also countless.According to relevant data statistics, the personnel that major part loses one's life in water are because do not rescued timely.The reason mainly containing two aspects of above-mentioned situation, is because water environment restriction on the one hand, cannot searches and rescues distress personnel in time; Be on the other hand because rescue group or wrecking equipment limited, cannot take effective measures as distress personnel provides rescue articles for use.Therefore, need a kind of there is function of searching should acute water life-saving equipment.
As everyone knows, unmanned plane is widely applied to rescue field with its motor-driven sensitivity characteristics, unmanned plane small volume, and flying speed is fast, utilizes it that rescuer can be made away from hazardous location, and with the rescue action of speed enforcement more efficiently.According to retrieval, existing relevant technical scheme in prior art, such as application number is 201420553528.7 patents, this application case discloses a kind of unmanned plane emergency rescue device waterborne, comprise input control mechanism, throw in support, detacher, buoy quoit, rope and LED searchlight, throw in control mechanism and comprise remote control receiver, steering wheel, camera and wireless image emission coefficient, remote control receiver and camera are arranged to be thrown on support, camera connects wireless image emission coefficient, remote control receiver is connected with steering wheel input end, remote control receiver is opened by servos control detacher, throw in buoy quoit, throw in support installing bottom unmanned plane, this input support comprises rack beam and support vertical beam, and detacher is arranged on rack beam, and this detacher connects buoy quoit by rope, and buoy quoit is set on support vertical beam.The program accurately controls the input of buoy quoit by camera filmed image, but in some vast waters, this device Chang Yinwei unmanned plane flying power is not enough and cannot return, and can not put into the salvage work in vast waters, and application is restricted.
Utility model content
1. the utility model technical matters that will solve
The purpose of this utility model is to overcome unmanned plane in prior art cannot be applied to the deficiency of the salvage work in vast waters because flying power is not enough, provide a kind of water life-saving duct unmanned aerial vehicle.The utility model makes unmanned plane can not because flying power is not enough or faults itself and the bottom that sinks in the process of suing and labouring by the body water wing on unmanned plane body; protection unmanned plane body is not intake impaired; be convenient to reclaim, can buoy quoit be carried simultaneously, solve the rescue problem in vast waters.
2. technical scheme
For achieving the above object, the technical scheme that the utility model provides is:
A kind of water life-saving duct unmanned aerial vehicle of the present utility model, comprises unmanned plane body, unmanned plane body is provided with GPS registration device and control setup, and described unmanned plane body is provided with duct, installs rotor in described duct; Described unmanned plane body fits, in body water wing, is equipped with buoy quoit and searches camera head on the downside of unmanned plane body, and search camera head is positioned at outside the circle body of buoy quoit.
Further improve as the utility model, described unmanned plane body is circular, and the external diameter of unmanned plane body is greater than the minimum diameter of body water wing.
Further improve as the utility model, the inner ring of described body water wing is symmetrically arranged with two water wing links, on the downside of the upper plate of unmanned plane body, be arranged with two the second detachers, described second detacher is connected with water wing link by stay cord.
Further improve as the utility model, be provided with at least two the first detachers on the downside of the lower shoe of described unmanned plane body, this first detacher is connected with the buoy quoit link on buoy quoit by stay cord.
Further improve as the utility model, described search camera head comprises globoid, circular arc fixed mount, pick up camera and illuminating lamp, described pick up camera and illuminating lamp are fixed on circular arc fixed mount, this circular arc fixed mount and globoid is hinged and the slewing area of circular arc fixed mount is 0 ~ 180 °.
Further improve as the utility model, described unmanned plane body is fixed with crossbeam, carry positioning shooting device on this crossbeam, positioning shooting device is positioned at the circle body of buoy quoit; The structure of described positioning shooting device is identical with the structure of searching camera head.
3. beneficial effect
The technical scheme adopting the utility model to provide, compared with prior art, has following beneficial effect:
(1) a kind of water life-saving duct unmanned aerial vehicle of the present utility model, unmanned plane body is provided with buoy quoit and searches camera head, sue and labour for searching rescue object, by unmanned plane body fits in body water wing, unmanned plane body arranges duct, in duct, rotor is installed, make rotor can not get to body water wing, when flying power is not enough, body water wing protection unmanned plane body is not intake, and is convenient to follow-up recovery and uses;
(2) a kind of water life-saving duct unmanned aerial vehicle of the present utility model, is connected on unmanned plane body by the second detacher and stay cord by body water wing, easy to connect, is easy to carry after taking off body water wing; When buoy quoit is not enough, body water wing can be thrown off and do buoy quoit use, ensure the life security of distress personnel;
(3) a kind of water life-saving duct unmanned aerial vehicle of the present utility model, install search pick up camera in camera head can 180 ° of rotation, search coverage greatly, at the circle body of buoy quoit built with positioning shooting device, contribute to the accurate input of buoy quoit, ensure effectively carrying out of salvage work.
Accompanying drawing explanation
Fig. 1 is the structural representation of a kind of water life-saving duct unmanned aerial vehicle of the present utility model;
Fig. 2 is the installation site schematic diagram of each device on unmanned plane body of the present utility model;
Fig. 3 is the structural representation of body water wing of the present utility model;
Fig. 4 is the structural representation of the second detacher of the present utility model.
Label declaration in schematic diagram: 1, unmanned plane body; 101, duct; 102, rotor; 103, the first detacher; 104, the second detacher; 2, crossbeam; 3, positioning shooting device; 4, camera head is searched; 401, globoid; 402, circular arc fixed mount; 403, pick up camera; 404, illuminating lamp; 5, body water wing; 501, water wing link; 6, buoy quoit; 601, buoy quoit link; 7, stay cord.
Detailed description of the invention
For understanding content of the present utility model further, in conjunction with the accompanying drawings and embodiments the utility model is described in detail.
Embodiment 1
Composition graphs 1 and Fig. 2, a kind of water life-saving duct unmanned aerial vehicle of the present embodiment, comprise unmanned plane body 1, the phenomenon sunk under water because of flying power deficiency or failure problems when flying in wide waters in order to avoid unmanned plane occurs, unmanned plane body 1 is sleeved in body water wing 5 by the present embodiment.Generally; blade meeting High Rotation Speed during unmanned plane work; unmanned plane body 1 can cause body water wing 5 to be broken by blade with the simple combination of body water wing 5; thus duct 101 is set on unmanned plane body 1; in duct 101, rotor 102 is installed; utilize duct 101 to protect body water wing 5, the lift of unmanned plane can be promoted simultaneously.
In the present embodiment, unmanned plane body 1 is circular; the external diameter of unmanned plane body 1 is greater than the minimum diameter of body water wing 5; unmanned plane body 1 is made to be erected at body water wing 5 middle and upper part; even if body water wing 5 floats on the surface; unmanned plane body 1 also can not be intake; still can continue after recovery to use, protection unmanned plane is not damaged.Two the second detachers 104 (as Fig. 4) are arranged with on the downside of the upper plate of unmanned plane body 1, the inner ring of described body water wing 5 is symmetrically arranged with two water wing links 501 (as Fig. 3), by corresponding with the position of water wing link 501 for the second detacher 104, then both are made to be connected by stay cord 7, and make stay cord 7 be in tension, with the fixing position of unmanned plane body 1 on body water wing 5.
Buoy quoit 6 is housed on the downside of unmanned plane body 1 and searches camera head 4, and search camera head 4 is positioned at outside the circle body of buoy quoit 6, prevent buoy quoit 6 from blocking the visual field of searching camera head 4.6 the first detachers 103 are provided with on the downside of the lower shoe of described unmanned plane body 1, first detacher 103 is identical with the structure of the second detacher 104, this first detacher 103 is along the circumferential uniform intervals distribution of unmanned plane body 1, a pair symmetrical first detachers 103 are connected with the buoy quoit link 601 on buoy quoit 6 by stay cord 7, can the buoy quoit 6 that vertically arranges of carry 1 ~ 3, the too many buoy quoit of carry 6 can affect flying speed.The search camera head 4 of the present embodiment comprises globoid 401, circular arc fixed mount 402, pick up camera 403 and illuminating lamp 404, described pick up camera 403 and illuminating lamp 404 are fixed on circular arc fixed mount 402, this circular arc fixed mount 402 is hinged and the slewing area of circular arc fixed mount 402 is 0 ~ 180 ° with globoid 401, when circular arc fixed mount 402 is in 0 ° of position, the lens barrel direction vertical level of pick up camera 403; When circular arc fixed mount 402 goes to 90 ° of positions, the lens barrel direction of pick up camera 403 and plane-parallel; Be positioned at the opposite side of globoid 401 when circular arc fixed mount 402 is in 180 ° of positions, the lens barrel of pick up camera 403 is positioned at vertical direction; Thus reach the object of the angle adjusting circular arc fixed mount 402 in flight course, to change the search visual angle of pick up camera 403.The illuminating lamp 404 installed facilitates unmanned plane to carry out rescue work when visbility is lower.Unmanned plane body 1 is also fixed with crossbeam 2, carry positioning shooting device 3 on this crossbeam 2, positioning shooting device 3 is positioned at the circle body of buoy quoit 6, the structure of described positioning shooting device 3 is identical with the structure of searching camera head 4, and both there is water-proofness, pick up camera 403 shooting direction in positioning shooting device 3, towards the water surface, is mainly used in the accuracy guaranteeing that buoy quoit 6 is thrown in.
Unmanned plane body 1 is also provided with GPS registration device and control setup, the first above-mentioned detacher 103, second detacher 104, positioning shooting device 3, search camera head 4 and GPS registration device etc. are all electrically connected with control setup, wireless signal transceiver is provided with in control setup, carry out data exchange by wireless signal transceiver and ground parametric controller, complete flare maneuver and search and rescue operation.GPS registration device can locate the position of unmanned plane in real time, once find distress personnel, rescue group can find distress personnel present position fast by locating data, carries out corresponding rescue task.In addition, when unmanned plane falls in water because of continue a journey deficiency or other reasons, the data passed by GPS registration device can find overboard unmanned plane fast, continue to utilize after recovery, avoid the wasting of resources.
During use, the good body water wing 5 of carry and buoy quoit 6, drive unmanned plane at water surface flying overhead, and unmanned plane manipulation personnel search scene captured by camera head 4 by the observation of ground parametric controller, the angle of circular arc fixed mount 402 can be changed, adjustment observation visual angle when observing; Once find overboard distress personnel, unmanned plane low latitude is made to hover over above distress personnel, and judge buoy quoit to be put 6 whether accurate positioning by positioning shooting device 3, then the first detacher 103 swing connecting bar is driven by control setup, stay cord 7 is taken off, then buoy quoit 6 is by input to distress personnel, makes distress personnel out of danger, and products for further is rescued.
If unmanned plane flying power is not enough in rescue work, cannot returns in time again, then can unmanned plane be dropped on the water surface, make body water wing 5 when overboard, carry unmanned plane body 1.What deserves to be explained is, before unmanned plane landing, the buoy quoit 6 on unmanned plane is needed all to throw in, otherwise buoy quoit 6 contacts with the water surface after landing, body water wing 5 is supportted aloft, causes the crank of device own, once rollover, then unmanned plane body 1 just can contact with water, larger to the damage rate of unmanned plane.If entrained buoy quoit 6 is not enough when implementing rescue, and situation is relatively more urgent, then can control unmanned plane throws in distress personnel by body water wing 5, completes rescue mission, for the completing of rescue task in vast waters provides strong guarantee.
Schematically above be described the utility model and embodiment thereof, this description does not have restricted, and also just one of the embodiment of the present utility model shown in accompanying drawing, actual structure is not limited thereto.So, if those of ordinary skill in the art enlightens by it, when not departing from the utility model and creating aim, design the frame mode similar to this technical scheme and embodiment without creationary, protection domain of the present utility model all should be belonged to.
Claims (6)
1. a water life-saving duct unmanned aerial vehicle, comprise unmanned plane body (1), unmanned plane body (1) is provided with GPS registration device and control setup, it is characterized in that: described unmanned plane body (1) is provided with duct (101), in described duct (101), rotor (102) is installed; Described unmanned plane body (1) is sleeved in body water wing (5), in unmanned plane body (1) downside, buoy quoit (6) be housed and search camera head (4), and search camera head (4) is positioned at outside the circle body of buoy quoit (6).
2. a kind of water life-saving duct unmanned aerial vehicle according to claim 1, is characterized in that: described unmanned plane body (1) is for circular, and the external diameter of unmanned plane body (1) is greater than the minimum diameter of body water wing (5).
3. a kind of water life-saving duct unmanned aerial vehicle according to claim 2, it is characterized in that: the inner ring of described body water wing (5) is symmetrically arranged with two water wing links (501), on the downside of the upper plate of unmanned plane body (1), be arranged with two the second detachers (104), described second detacher (104) is connected with water wing link (501) by stay cord (7).
4. a kind of water life-saving duct unmanned aerial vehicle according to claim 1 or 3, it is characterized in that: be provided with at least two the first detachers (103) on the downside of the lower shoe of described unmanned plane body (1), this first detacher (103) is connected with the buoy quoit link (601) on buoy quoit (6) by stay cord (7).
5. a kind of water life-saving duct unmanned aerial vehicle according to claim 4, it is characterized in that: described search camera head (4) comprises globoid (401), circular arc fixed mount (402), pick up camera (403) and illuminating lamp (404), described pick up camera (403) and illuminating lamp (404) are fixed on circular arc fixed mount (402), and this circular arc fixed mount (402) and globoid (401) are hinged and slewing area that is circular arc fixed mount (402) is 0 ~ 180 °.
6. a kind of water life-saving duct unmanned aerial vehicle according to claim 5, it is characterized in that: described unmanned plane body (1) is fixed with crossbeam (2), the upper carry positioning shooting device (3) of this crossbeam (2), positioning shooting device (3) is positioned at the circle body of buoy quoit (6); The structure of described positioning shooting device (3) is identical with the structure of searching camera head (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520179590.9U CN204489179U (en) | 2015-03-27 | 2015-03-27 | A kind of water life-saving duct unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520179590.9U CN204489179U (en) | 2015-03-27 | 2015-03-27 | A kind of water life-saving duct unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204489179U true CN204489179U (en) | 2015-07-22 |
Family
ID=53568452
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520179590.9U Expired - Fee Related CN204489179U (en) | 2015-03-27 | 2015-03-27 | A kind of water life-saving duct unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204489179U (en) |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292479A (en) * | 2015-12-11 | 2016-02-03 | 佛山市南海区广工大数控装备协同创新研究院 | Unmanned aerial vehicle life buoy dropping device |
| CN105416526A (en) * | 2015-12-11 | 2016-03-23 | 佛山市南海区广工大数控装备协同创新研究院 | Unmanned aerial vehicle rescue device for water area |
| WO2016203322A3 (en) * | 2016-10-27 | 2017-05-18 | Wasfi Alshdaifat | Search and rescue drone arrangement |
| CN106741734A (en) * | 2016-12-30 | 2017-05-31 | 哈瓦国际航空技术（深圳）有限公司 | A kind of lifebuoy is jettisoninged carry and unmanned plane |
| CN107318638A (en) * | 2017-06-30 | 2017-11-07 | 唐成吉 | Watermelon pollination unmanned plane in greenhouse |
| CN108357676A (en) * | 2018-04-09 | 2018-08-03 | 重庆国飞通用航空设备制造有限公司 | A kind of multifunction emergency rescue multi-rotor unmanned aerial vehicle system |
| CN109552626A (en) * | 2018-12-25 | 2019-04-02 | 广州拓浪智能应急科技有限公司 | A kind of flight lifebuoy |
| CN109665074A (en) * | 2019-01-25 | 2019-04-23 | 深圳市合泰英龙科技有限公司 | A kind of laser guidance water surface rescue aid and its rescue mode |
| CN109808886A (en) * | 2019-04-17 | 2019-05-28 | 孙鲁青 | A kind of unmanned plane waters deliverance apparatus |
| TWI664116B (en) * | 2018-10-17 | 2019-07-01 | Shu-Te University | Rescue device and system of unmanned aerial vehicle |
| CN112660334A (en) * | 2020-01-09 | 2021-04-16 | 广州船舶及海洋工程设计研究院（中国船舶工业集团公司第六0五研究院） | Rescue device |
| CN114771775A (en) * | 2022-05-27 | 2022-07-22 | 浙江大学湖州研究院 | Annular multi-duct water-air amphibious cross-domain unmanned aerial vehicle |
| AU2022263617B1 (en) * | 2022-11-07 | 2023-01-05 | Revolution Ag Pty Ltd | Unmanned Aerial Vehicle for Rescue |
-
2015
- 2015-03-27 CN CN201520179590.9U patent/CN204489179U/en not_active Expired - Fee Related
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292479B (en) * | 2015-12-11 | 2017-12-01 | 佛山市南海区广工大数控装备协同创新研究院 | A kind of unmanned plane lifebuoy delivery device |
| CN105416526A (en) * | 2015-12-11 | 2016-03-23 | 佛山市南海区广工大数控装备协同创新研究院 | Unmanned aerial vehicle rescue device for water area |
| CN105292479A (en) * | 2015-12-11 | 2016-02-03 | 佛山市南海区广工大数控装备协同创新研究院 | Unmanned aerial vehicle life buoy dropping device |
| CN105416526B (en) * | 2015-12-11 | 2017-08-18 | 佛山市南海区广工大数控装备协同创新研究院 | Water area unmanned machine deliverance apparatus |
| WO2016203322A3 (en) * | 2016-10-27 | 2017-05-18 | Wasfi Alshdaifat | Search and rescue drone arrangement |
| CN106741734B (en) * | 2016-12-30 | 2018-12-11 | 哈瓦国际航空技术（深圳）有限公司 | A kind of lifebuoy is jettisoninged carry and unmanned plane |
| CN106741734A (en) * | 2016-12-30 | 2017-05-31 | 哈瓦国际航空技术（深圳）有限公司 | A kind of lifebuoy is jettisoninged carry and unmanned plane |
| CN107318638A (en) * | 2017-06-30 | 2017-11-07 | 唐成吉 | Watermelon pollination unmanned plane in greenhouse |
| CN108357676A (en) * | 2018-04-09 | 2018-08-03 | 重庆国飞通用航空设备制造有限公司 | A kind of multifunction emergency rescue multi-rotor unmanned aerial vehicle system |
| TWI664116B (en) * | 2018-10-17 | 2019-07-01 | Shu-Te University | Rescue device and system of unmanned aerial vehicle |
| CN109552626A (en) * | 2018-12-25 | 2019-04-02 | 广州拓浪智能应急科技有限公司 | A kind of flight lifebuoy |
| CN109552626B (en) * | 2018-12-25 | 2024-03-12 | 广州拓浪智能应急科技有限公司 | Flight life buoy |
| CN109665074A (en) * | 2019-01-25 | 2019-04-23 | 深圳市合泰英龙科技有限公司 | A kind of laser guidance water surface rescue aid and its rescue mode |
| CN109665074B (en) * | 2019-01-25 | 2023-04-18 | 深圳市合泰英龙科技有限公司 | Laser guidance water surface rescue equipment and rescue method thereof |
| CN109808886A (en) * | 2019-04-17 | 2019-05-28 | 孙鲁青 | A kind of unmanned plane waters deliverance apparatus |
| CN112660334A (en) * | 2020-01-09 | 2021-04-16 | 广州船舶及海洋工程设计研究院（中国船舶工业集团公司第六0五研究院） | Rescue device |
| CN114771775A (en) * | 2022-05-27 | 2022-07-22 | 浙江大学湖州研究院 | Annular multi-duct water-air amphibious cross-domain unmanned aerial vehicle |
| AU2022263617B1 (en) * | 2022-11-07 | 2023-01-05 | Revolution Ag Pty Ltd | Unmanned Aerial Vehicle for Rescue |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204489179U (en) | A kind of water life-saving duct unmanned aerial vehicle | |
| CN104494821B (en) | The many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue | |
| CN204078071U (en) | A kind of unmanned plane emergency rescue device waterborne | |
| CN204341394U (en) | The many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue | |
| CN204415734U (en) | The delivery device of wrecking equipment | |
| DK201900074Z6 (en) | Systems and procedures for stability with suspended loads | |
| US9022322B2 (en) | Remotely-controlled emergency aerial vehicle | |
| CN103612756B (en) | The multi-rotor aerocraft of electric power line inspection and based on its system | |
| CN105015732B (en) | Relief type unmanned vehicle waterborne | |
| CN204013920U (en) | A kind of night search and rescue, search system | |
| CN207157538U (en) | A kind of rescue UAS for fire of high-rise building | |
| CN204916187U (en) | Fire control unmanned aerial vehicle | |
| CN105799928A (en) | Fire protection and extinguishing device based on unmanned aerial vehicle | |
| CN205384516U (en) | Unmanned aerial vehicle rescue system | |
| CN112093050B (en) | Modularized unmanned aerial vehicle fire engine | |
| CN108248865A (en) | A kind of uav water emergency rescue device | |
| KR101522516B1 (en) | The life-saving apparatus using drones | |
| CN105584604A (en) | Remotely-controlled waterborne rescue device | |
| CN205070296U (en) | A unmanned aerial vehicle for electric power inspection and debris are clear away | |
| CN204010209U (en) | Forest fire early-warning system based on depopulated helicopter | |
| CN112319835A (en) | Unmanned aerial vehicle descending positioning device and unmanned aerial vehicle nest | |
| CN204979240U (en) | Carry lifesaving articles for use unmanned aerial vehicle | |
| CN215436908U (en) | Unmanned aerial vehicle device and unmanned aerial vehicle of saving oneself on water | |
| CN109466726B (en) | Rescue system and rescue method at sea based on unmanned aerial vehicle platform | |
| CN111674526A (en) | Rescue underwater robot in dangerous water area |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| 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: 20150722 Termination date: 20160327 |