CN204056311U - The steady cradle head structure of a kind of increasing - Google Patents
The steady cradle head structure of a kind of increasing Download PDFInfo
- Publication number
- CN204056311U CN204056311U CN201420584295.7U CN201420584295U CN204056311U CN 204056311 U CN204056311 U CN 204056311U CN 201420584295 U CN201420584295 U CN 201420584295U CN 204056311 U CN204056311 U CN 204056311U
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- roll axle
- cloud terrace
- carbon pipe
- pitch axis
- adapter plate
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- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 39
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 39
- 238000009434 installation Methods 0.000 claims description 6
- 238000000034 method Methods 0.000 abstract description 4
- 230000008569 process Effects 0.000 abstract description 4
- 238000010521 absorption reaction Methods 0.000 abstract description 2
- 230000035939 shock Effects 0.000 abstract description 2
- 230000000694 effects Effects 0.000 description 6
- 238000010586 diagram Methods 0.000 description 3
- 238000013016 damping Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000017105 transposition Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000012512 characterization method Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000003351 stiffener Substances 0.000 description 1
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Abstract
The steady cradle head structure of the open a kind of increasing of the utility model, comprise quick detach adapter plate, The Cloud Terrace support, The Cloud Terrace adapter plate, lay the erecting stage of picture pick-up device, quick detach adapter plate is fixedly mounted on The Cloud Terrace support, and The Cloud Terrace adapter plate is fixedly mounted on below The Cloud Terrace support, between The Cloud Terrace adapter plate and The Cloud Terrace support, be provided with shock-absorbing ball; Carbon pipe under The Cloud Terrace adapter plate is extended with yaw axis downwards, under yaw axis, carbon pipe is fixedly connected with roll bearing housing, roll axle is arranged on roll bearing housing, roll axle is fixedly connected with roll axle sleeve, U-shaped roll axle carbon pipe support is socketed in roll axle sleeve, and described erecting stage is arranged on U-shaped roll axle carbon pipe support.The mechanical shock absorption mode that the utility model adopts shock-absorbing ball to connect, the most low-frequency vibration that aircraft produces can be eliminated, and make pick up camera keep stable, necessary shooting angle in boat process by the angle state of carbon pipe, pitch axis swinging strut plate in motor adjustment roll axle, increase surely effective.
Description
Technical field
The utility model relates to unmanned vehicle technical field, more particularly, relates to the steady cradle head structure of a kind of increasing.
Background technology
Now, unmanned vehicle because of itself light structure, need not be manned, badly, complete the activities such as shooting, detection in even dangerous environment, and the field of taking photo by plane can be widely used in, comprise photography, transport development, hydraulic engineering, ecological Studies, city planning etc.Usually, the pick up camera of taking photo by plane is controlled by the photographer on ground, to obtaining gratifying image, but, in the process of taking photo by plane, because of situations such as airflow influence or aircraft fuselage inclination, vibrations, all can affect the effect of capture apparatus.
Utility model content
The utility model object is to overcome the deficiencies in the prior art, provides a kind of increasing be applied on unmanned vehicle steady cradle head structure, effectively to solve the problems of the technologies described above.
The technical solution of the utility model is: the steady cradle head structure of a kind of increasing, comprise quick detach adapter plate, The Cloud Terrace support, The Cloud Terrace adapter plate, lay the erecting stage of picture pick-up device, described quick detach adapter plate is fixedly mounted on The Cloud Terrace support, and described The Cloud Terrace adapter plate is fixedly mounted on below The Cloud Terrace support, between The Cloud Terrace adapter plate and The Cloud Terrace support, be provided with shock-absorbing ball; Carbon pipe under The Cloud Terrace adapter plate is extended with yaw axis downwards, under yaw axis, carbon pipe is fixedly connected with roll bearing housing, roll axle is arranged on roll bearing housing, roll axle is fixedly connected with roll axle sleeve, U-shaped roll axle carbon pipe support is socketed in roll axle sleeve, described in lay picture pick-up device erecting stage be arranged on U-shaped roll axle carbon pipe support.
Preferably, described roll bearing housing is provided with roll axle brushless motor, the output shaft of roll axle brushless motor connects roll axle; Be installed with control desk shell in the side of described U-shaped roll axle carbon pipe support, the sensor for responding to roll Spindle Status is set in control desk shell.
Preferably, described erecting stage both sides of laying picture pick-up device are fixedly connected with pitch axis swinging strut plate, the top of pitch axis swinging strut plate is hinged on the both sides carbon pipe of U-shaped roll axle carbon pipe support, the top of pitch axis swinging strut plate is fixedly connected with pitch axis, the wherein side carbon pipe of U-shaped roll axle carbon pipe support is provided with pitch axis brushless motor, and the output shaft of pitch axis brushless motor connects described pitch axis.
Preferably, the sensor for responding to pitch axis state is provided with in the erecting stage laying picture pick-up device described in.
Preferably, described in lay picture pick-up device erecting stage be comprise the double-decked platform structure of installing upper plate, installing lower plate, between two plates, some brace panels are set; Right angle rack connection is arranged on installation upper plate and installs in the gap between lower plate, and the sidewall of right angle rack is fixed on pitch axis swinging strut plate and makes pitch axis swinging strut plate be vertically fixed on the erecting stage both sides of laying picture pick-up device.
The utility model has following beneficial effect: the mechanical shock absorption mode that the steady cradle head structure of increasing of the present utility model adopts shock-absorbing ball to connect, the most low-frequency vibration that aircraft produces can be eliminated, and make pick up camera keep stable, necessary shooting angle in boat process by the angle state of carbon pipe, pitch axis swinging strut plate in motor adjustment roll axle, increase surely effective.
The steady cradle head structure of increasing of the present utility model can also control the shooting angle of picture pick-up device, makes the convenient freedom of shooting.
Accompanying drawing explanation
Fig. 1 is that the utility model increases steady cradle head structure block diagram.
Fig. 2 is that the utility model increases steady cradle head structure face upwarding stereogram.
Fig. 3 is that the utility model increases steady cradle head structure side isometric view.
Fig. 4 is the mounting structure schematic diagram of roll axle brushless motor.
Fig. 5 is the side isometric view of the erecting stage laying shooting DV.
Fig. 6 is the block diagram of the erecting stage of another angle.
Fig. 7 is the structural representation of the erecting stage concealing upper plate.
Detailed description of the invention
Be described below in detail embodiment of the present utility model, the example of described embodiment is shown in the drawings, and wherein same or similar label represents same or similar element or has element that is identical or similar functions from start to finish.Being exemplary below by the embodiment be described with reference to the drawings, only for explaining the utility model, and can not being interpreted as restriction of the present utility model.
In description of the present utility model, it will be appreciated that, term " " center ", " transverse direction ", " on ", D score, "left", "right", etc. the orientation of instruction or position relationship be based on orientation shown in the drawings or position relationship; be only the utility model and simplified characterization for convenience of description; instead of instruction or imply the device of indication or element must have specific orientation, with specific azimuth configuration and operation, therefore can not be interpreted as restriction of the present utility model.
See Fig. 1-3, the utility model one increases steady cradle head structure, comprise connecting portion and carrier, the effect of connecting portion be connected with the fuselage of unmanned plane and with the connection of carrier, it comprises The Cloud Terrace quick detach adapter plate 1, The Cloud Terrace support 2, The Cloud Terrace support is criss-cross, and it is fixedly connected with The Cloud Terrace quick detach adapter plate by pillar stiffener 3.In the parallel beneath of The Cloud Terrace support, a pair The Cloud Terrace adapter plate 4 is set, The Cloud Terrace support is fixedly connected with by Anti-off bolt 6, anti-dropping gasket 7 with The Cloud Terrace adapter plate, and between two plates, be provided with some shock-absorbing balls 5, shock-absorbing ball 5 profile approximate spheres, it is obtained by damping materials such as rubber, has good damping effect.Its line of centers is provided with through hole from top to bottom, and anti-drop screw can be allowed to pass.Shock-absorbing ball can eliminate the most low-frequency vibration by a small margin that aircraft produces, and picture pick-up device is taken more stable.
Fixedly mount carbon pipe 9 on a yaw axis in the below of The Cloud Terrace adapter plate 4 by pipe clamp 8, under yaw axis, carbon pipe 10 is connected with on yaw axis, carbon pipe 9 is vertical by 90 degree of coupler 11, connects the carrier of load equipment by carbon pipe 10 under yaw axis.
See Fig. 1, Fig. 4, carrier comprises erecting stage, pitch axis swinging strut plate 12, U-shaped roll axle carbon pipe support for laying shooting DV, under yaw axis, carbon pipe 10 is arranged in the sleeve of roll bearing housing 13, roll axle is arranged on the base portion of roll bearing housing, the motor fixing plate 141 of roll axle brushless motor 14, motor mounting plate 142 are fixed on roll bearing housing 13, the output shaft of roll axle brushless motor 14 connects roll axle 15, and roll axle sleeve 16 is screwed on the axis body of roll axle 15.Roll axle coupler 40 is connected with the rotor of roll axle brushless motor 14.U-shaped roll axle carbon pipe support is made up of carbon pipe 17, roll axle left carbon pipe 18, the right carbon pipe 19 of roll axle in roll axle, is connected, surround the pipe support of a U-shaped between them by 90 degree of coupler.In roll axle, carbon pipe 17 is through roll axle sleeve 16, and both are screwed.Therefore, when roll axle 15 rotates certain angular transposition under the driving of roll axle brushless motor 14, carbon pipe 17 will to be driven in roll axle with roll axle 15 for axis rotates, its direct effect is: the left and right carbon pipe of roll axle axis centered by roll axle 15 is rotated, and the left and right carbon pipe of roll axle connects pitch axis swinging strut plate 12 respectively.
See Fig. 1, Fig. 5-7, the framework platform that the erecting stage laying shooting DV is made up of plate 24, brace panel 25 etc. after pitch axis DV installation header board 21, pitch axis DV installation upper plate 22, pitch axis DV installation lower plate 23, pitch axis DV installation, pitch axis swinging strut plate 12 is connected to the both sides of framework platform, in order to strengthen the connection of pitch axis swinging strut plate and erecting stage, pitch axis DV installs upper plate 22, pitch axis DV installs in lower plate 23 by right angle rack 26, pitch axis swinging strut plate 12 to be fixed on.Install on upper plate 22 at DV and DV registration mast 27 is set, have pitch axis swinging strut backing plate 28 in pitch axis swinging strut plate 12 arranged outside of installing pitch axis motor.See Fig. 5, pitch axis 29 is arranged in pitch axis bearing 30, the axis body of pitch axis 29 is fixedly connected with pitch axis swinging strut plate 12, therefore, when pitch axis 29 rotates certain angular transposition under the driving of pitch axis brushless motor 31, to drive pitch axis swinging strut plate 12 with pitch axis 29 for axis rotates, its direct effect is that the erecting stage laying shooting DV is rotated.
See Fig. 1, pitch axis brushless motor 31 is arranged on roll axle right carbon pipe 19 side, and it is outer is control desk shell 32.See Fig. 7, install in lower plate at pitch axis DV and be provided with pitch axis sensor board 33, plate is installed the sensor of pitch axis, and the sensor setting of roll axle is in control desk shell, two sensors is for responding to cireular frequency and the angle state of roll axle/pitch axis, sensor connection control circuit card, in the process of taking photo by plane, micro controller system carries out computing to the sensor information collected, when operation result display roll axle/pitch axis has departed from the location status of setting, micro controller system calculates a compensation value, export control signal, make roll axle/pitch axes, to balance the deflection of diaxon.
See Fig. 1, Fig. 3, install on header board 21 at pitch axis DV and arrange steering wheel mount pad 34, it is provided with focusing steering wheel 35, shooting DV36 is arranged on erecting stage, and its focusing ring big gear wheel 37 engages with the focusing gear 38 of focusing steering wheel.
Although illustrate and described embodiment of the present utility model; those of ordinary skill in the art is to be understood that: can carry out multiple change, amendment, replacement and modification to these embodiments when not departing from principle of the present utility model and aim; scope of the present utility model limited by claim and equivalent replacement thereof; in the improvement etc. done without creative work, all should be included within protection domain of the present utility model.
Claims (5)
1. one kind increases steady cradle head structure, comprise quick detach adapter plate, The Cloud Terrace support, The Cloud Terrace adapter plate, lay the erecting stage of picture pick-up device, described quick detach adapter plate is fixedly mounted on The Cloud Terrace support, it is characterized in that: described The Cloud Terrace adapter plate is fixedly mounted on below The Cloud Terrace support, between The Cloud Terrace adapter plate and The Cloud Terrace support, be provided with shock-absorbing ball; Carbon pipe under The Cloud Terrace adapter plate is extended with yaw axis downwards, under yaw axis, carbon pipe is fixedly connected with roll bearing housing, roll axle is arranged on roll bearing housing, roll axle is fixedly connected with roll axle sleeve, U-shaped roll axle carbon pipe support is socketed in roll axle sleeve, described in lay picture pick-up device erecting stage be arranged on U-shaped roll axle carbon pipe support.
2. one according to claim 1 increases steady cradle head structure, it is characterized in that: on described roll bearing housing, be provided with roll axle brushless motor, and the output shaft of roll axle brushless motor connects roll axle; Be installed with control desk shell in the side of described U-shaped roll axle carbon pipe support, the sensor for responding to roll Spindle Status is set in control desk shell.
3. one according to claim 1 increases steady cradle head structure, it is characterized in that: described in lay picture pick-up device erecting stage both sides be fixedly connected with pitch axis swinging strut plate, the top of pitch axis swinging strut plate is hinged on the both sides carbon pipe of U-shaped roll axle carbon pipe support, the top of pitch axis swinging strut plate is fixedly connected with pitch axis, the wherein side carbon pipe of U-shaped roll axle carbon pipe support is provided with pitch axis brushless motor, and the output shaft of pitch axis brushless motor connects described pitch axis.
4. one according to claim 3 increases steady cradle head structure, it is characterized in that: described in lay picture pick-up device erecting stage in be provided with sensor for responding to pitch axis state.
5. the one according to claim 2 or 4 increases steady cradle head structure, it is characterized in that: described in lay picture pick-up device erecting stage be comprise the double-decked platform structure of installing upper plate, installing lower plate, between two plates, some brace panels are set; Right angle rack connection is arranged on installation upper plate and installs in the gap between lower plate, and the sidewall of right angle rack is fixed on pitch axis swinging strut plate and makes pitch axis swinging strut plate be vertically fixed on the erecting stage both sides of laying picture pick-up device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420584295.7U CN204056311U (en) | 2014-10-11 | 2014-10-11 | The steady cradle head structure of a kind of increasing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420584295.7U CN204056311U (en) | 2014-10-11 | 2014-10-11 | The steady cradle head structure of a kind of increasing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204056311U true CN204056311U (en) | 2014-12-31 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420584295.7U Expired - Fee Related CN204056311U (en) | 2014-10-11 | 2014-10-11 | The steady cradle head structure of a kind of increasing |
Country Status (1)
| Country | Link |
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| CN (1) | CN204056311U (en) |
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104696690A (en) * | 2015-03-18 | 2015-06-10 | 零度智控（北京）智能科技有限公司 | Onboard holder |
| CN105042299A (en) * | 2015-04-22 | 2015-11-11 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle mounted pan-tilt |
| CN105217051A (en) * | 2015-10-29 | 2016-01-06 | 中国科学院遥感与数字地球研究所 | Unmanned plane one camera multi-angled shooting bracing or strutting arrangement |
| CN105277177A (en) * | 2015-10-17 | 2016-01-27 | 佛山市安尔康姆航空科技有限公司 | Oblique photography system adopting multi-rotor unmanned aerial vehicle |
| CN105516688A (en) * | 2016-01-20 | 2016-04-20 | 北京航空航天大学 | Resolution-transforming type eagle eye-mimic visual imaging device and imaging method thereof |
| CN105599915A (en) * | 2016-01-15 | 2016-05-25 | 中国人民解放军国防科学技术大学 | Steering engine driven flexible cable transmission two-shaft cradle head structure |
| CN105605388A (en) * | 2015-10-20 | 2016-05-25 | 西京学院 | Variable-focus aerial photography cradle head device |
| CN105599914A (en) * | 2016-01-05 | 2016-05-25 | 零度智控（北京）智能科技有限公司 | Cradle head |
| CN105954959A (en) * | 2016-07-15 | 2016-09-21 | 成都睿铂科技有限责任公司 | Single-lens aerial photographic instrument bracket, aerial photographic instrument and unmanned aerial vehicle |
| CN106200216A (en) * | 2016-08-28 | 2016-12-07 | 浙江尚友智能科技有限公司 | A kind of shooting regulator with auto-focusing |
| CN106292741A (en) * | 2016-09-27 | 2017-01-04 | 成都普诺思博科技有限公司 | A kind of mobile machine user tripod head system based on brushless electric machine |
| CN106325305A (en) * | 2015-06-29 | 2017-01-11 | 优利科技有限公司 | Geo-location or navigation type camera, aircraft, and navigation method and system thereof |
| CN107380472A (en) * | 2017-07-25 | 2017-11-24 | 芜湖超源力工业设计有限公司 | A kind of unmanned plane of taking photo by plane that there is shooting to increase steady cradle head device |
| CN108349593A (en) * | 2015-11-02 | 2018-07-31 | 三星电子株式会社 | The adjustable small-sized holder of three axis |
| CN109061875A (en) * | 2018-07-27 | 2018-12-21 | 长安大学 | A kind of superman's eye rotation zoom monocular vision device |
| CN109562845A (en) * | 2017-12-12 | 2019-04-02 | 深圳市大疆创新科技有限公司 | A kind of unmanned plane and its holder damping, head assembly |
| US10386188B2 (en) | 2015-06-29 | 2019-08-20 | Yuneec Technology Co., Limited | Geo-location or navigation camera, and aircraft and navigation method therefor |
| CN110771136A (en) * | 2018-04-12 | 2020-02-07 | 深圳市大疆创新科技有限公司 | Image pickup system |
| CN114435611A (en) * | 2016-01-26 | 2022-05-06 | 深圳市大疆创新科技有限公司 | Stability augmentation platform |
-
2014
- 2014-10-11 CN CN201420584295.7U patent/CN204056311U/en not_active Expired - Fee Related
Cited By (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104696690A (en) * | 2015-03-18 | 2015-06-10 | 零度智控（北京）智能科技有限公司 | Onboard holder |
| CN104696690B (en) * | 2015-03-18 | 2017-05-24 | 零度智控（北京）智能科技有限公司 | Onboard holder |
| CN105042299A (en) * | 2015-04-22 | 2015-11-11 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle mounted pan-tilt |
| CN105042299B (en) * | 2015-04-22 | 2017-05-31 | 零度智控（北京）智能科技有限公司 | Unmanned vehicle airborne tripod head |
| CN106325305A (en) * | 2015-06-29 | 2017-01-11 | 优利科技有限公司 | Geo-location or navigation type camera, aircraft, and navigation method and system thereof |
| CN106325305B (en) * | 2015-06-29 | 2020-03-20 | 优利科技有限公司 | Camera for ground positioning or navigation, aircraft and navigation method and system thereof |
| US10386188B2 (en) | 2015-06-29 | 2019-08-20 | Yuneec Technology Co., Limited | Geo-location or navigation camera, and aircraft and navigation method therefor |
| CN105277177A (en) * | 2015-10-17 | 2016-01-27 | 佛山市安尔康姆航空科技有限公司 | Oblique photography system adopting multi-rotor unmanned aerial vehicle |
| CN105605388A (en) * | 2015-10-20 | 2016-05-25 | 西京学院 | Variable-focus aerial photography cradle head device |
| CN105217051B (en) * | 2015-10-29 | 2017-07-07 | 中国科学院遥感与数字地球研究所 | Unmanned plane one camera multi-angled shooting support meanss |
| CN105217051A (en) * | 2015-10-29 | 2016-01-06 | 中国科学院遥感与数字地球研究所 | Unmanned plane one camera multi-angled shooting bracing or strutting arrangement |
| CN108349593B (en) * | 2015-11-02 | 2022-03-22 | 三星电子株式会社 | Three-axis adjustable small-sized pan-tilt |
| CN108349593A (en) * | 2015-11-02 | 2018-07-31 | 三星电子株式会社 | The adjustable small-sized holder of three axis |
| CN105599914A (en) * | 2016-01-05 | 2016-05-25 | 零度智控（北京）智能科技有限公司 | Cradle head |
| CN105599915A (en) * | 2016-01-15 | 2016-05-25 | 中国人民解放军国防科学技术大学 | Steering engine driven flexible cable transmission two-shaft cradle head structure |
| CN105516688A (en) * | 2016-01-20 | 2016-04-20 | 北京航空航天大学 | Resolution-transforming type eagle eye-mimic visual imaging device and imaging method thereof |
| CN114435611A (en) * | 2016-01-26 | 2022-05-06 | 深圳市大疆创新科技有限公司 | Stability augmentation platform |
| CN105954959A (en) * | 2016-07-15 | 2016-09-21 | 成都睿铂科技有限责任公司 | Single-lens aerial photographic instrument bracket, aerial photographic instrument and unmanned aerial vehicle |
| CN106200216A (en) * | 2016-08-28 | 2016-12-07 | 浙江尚友智能科技有限公司 | A kind of shooting regulator with auto-focusing |
| CN106292741A (en) * | 2016-09-27 | 2017-01-04 | 成都普诺思博科技有限公司 | A kind of mobile machine user tripod head system based on brushless electric machine |
| CN107380472A (en) * | 2017-07-25 | 2017-11-24 | 芜湖超源力工业设计有限公司 | A kind of unmanned plane of taking photo by plane that there is shooting to increase steady cradle head device |
| WO2019113775A1 (en) * | 2017-12-12 | 2019-06-20 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and pan-tilt shock-absorbing mechanism and pan-tilt assembly therefor |
| CN109562845A (en) * | 2017-12-12 | 2019-04-02 | 深圳市大疆创新科技有限公司 | A kind of unmanned plane and its holder damping, head assembly |
| CN109562845B (en) * | 2017-12-12 | 2021-11-16 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and cloud platform damper, cloud platform subassembly thereof |
| CN110771136A (en) * | 2018-04-12 | 2020-02-07 | 深圳市大疆创新科技有限公司 | Image pickup system |
| CN109061875A (en) * | 2018-07-27 | 2018-12-21 | 长安大学 | A kind of superman's eye rotation zoom monocular vision device |
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Legal Events
| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 528300 No. 7 Jianye Middle Road, Shunde High-tech Zone, Foshan City, Guangdong Province Patentee after: Magnesium Kezhongsi Technology (Foshan) Co.,Ltd. Address before: 528300 No. 7 Jianye Middle Road, Shunde High-tech Zone, Foshan City, Guangdong Province Patentee before: Foshan Anlcom Technology Co.,Ltd. Address after: 528300 No. 7 Jianye Middle Road, Shunde High-tech Zone, Foshan City, Guangdong Province Patentee after: Foshan Anlcom Technology Co.,Ltd. Address before: 528300 No. 7 Jianye Middle Road, Shunde High-tech Zone, Foshan City, Guangdong Province Patentee before: FOSHAN AIRCAM UAV TECHNOLOGY Corp. |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141231 |