CN203838864U - Unmanned aerial vehicle remote control device - Google Patents
Unmanned aerial vehicle remote control device Download PDFInfo
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- CN203838864U CN203838864U CN201420157021.XU CN201420157021U CN203838864U CN 203838864 U CN203838864 U CN 203838864U CN 201420157021 U CN201420157021 U CN 201420157021U CN 203838864 U CN203838864 U CN 203838864U
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 10
- 230000010365 information processing Effects 0.000 claims description 2
- 238000000034 method Methods 0.000 claims description 2
- 238000013461 design Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000003756 stirring Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle remote control device. The unmanned aerial vehicle remote control device comprises a shell, a cover, a lifting handle, control buttons, rotary knobs and a rod piece. The unmanned aerial vehicle remote control device is mainly used for combining traditional aerial vehicle control and control of an image acquisition device which is carried on an aerial vehicle, flight parameters which are returned from the aerial vehicle and image information which are returned from the carried image acquisition device can be displayed on the same screen together, and an operator can conveniently and real-timely control the whole aerial vehicle and know the actual condition messages of the aerial vehicle.
Description
Technical field
The utility model relates to a kind of telepilot, particularly relates to a kind of telepilot of unmanned vehicle.
Background technology
The telepilot of existing unmanned vehicle (unmanned plane) only has remote control function (general this telepilot can show the flight parameter of aircraft passback), if need to obtain the information of the contained image acquisition equipment of aircraft, also need to add in addition an image acquisition equipment, generally also need the telepilot of the contained image acquisition equipment of control aircraft.
If, operator need to control image acquisition equipment and unmanned plane motion simultaneously, need two people to control respectively these two, and the flight parameter of aircraft passback is presented at respectively on different screens from image information, this is unfavorable for the comprehensive grasp of operator to aircraft live state information.
Utility model content
Because the above-mentioned defect of prior art, technical problem to be solved in the utility model is to provide a kind ofly to be controlled the motion control of unmanned vehicle and image acquisition equipment to combine, and can be by flight parameter and the unmanned vehicle telepilot of image information Overlapping display on same screen of aircraft passback.
For achieving the above object, the utility model provides following technical scheme:
A kind of unmanned vehicle telepilot, comprise housing, lid, handle, described handle is arranged on housing, described lid is arranged on housing by screw, on the described lid left side, power switch, charging inlet are installed, described power switch and charging inlet up have image control button, described image control button up has suspender clip, described suspender clip up has head to control rocking bar, and described head is controlled rocking bar up has The Cloud Terrace pitching knob, offline mode change-over switch, speed to pass antenna;
Lid the right is there is start button in the place by telepilot mid-plane symmetry with image control button, start button up has fuselage to control rocking bar, fuselage is controlled rocking bar up has figure to pass antenna, automatic takeoff/landing switch, cloud platform rotation knob, and figure passes antenna for receiving the image information of the image acquisition equipment passback of aircraft lift-launch;
In the middle of lid, there are screen, described screen to be mainly used in showing relevant image information and the flight parameter of passback.
Telepilot inner structure mainly comprises: head is controlled rocking bar base, center-control electroplax, fuselage control rocking bar base, and described head is controlled rocking bar base and is connected with center-control electroplax by electric wire;
Head is controlled rocking bar base down data-interface base and charging inlet base, and data-interface base is connected by electric wire with center-control electroplax respectively with charging inlet base; Head is controlled rocking bar base up The Cloud Terrace pitching knob base, turned left offline mode change-over switch base and speed of The Cloud Terrace pitching knob base passes antenna base, and The Cloud Terrace pitching knob base, offline mode change-over switch base and speed pass antenna base and by electric wire, is connected with center-control electroplax respectively;
Described fuselage is controlled rocking bar base down start button base, and start button base down has battery, and battery is connected by electric wire with center-control electroplax;
Described fuselage is controlled rocking bar base up has figure to pass antenna base, figure biography antenna base has been turned right automatically to open and has been flown/landed switch pedestal, automatically open and fly/land the switch pedestal cloud platform rotation knob of having turned right, figure passes antenna base, automatically opens and fly/land switch pedestal, have cloud platform rotation knob base by electric wire, to be connected with center-control electroplax respectively.
The telepilot back side has data-interface and figure to pass frequency adjustment code switch.
The function of each major part is as follows:
Described image control button be mainly used in controlling the contained vision facilities of unmanned vehicle zoom, take pictures, facility switching etc.;
Described head is controlled rocking bar and can be stirred to " upper and lower, left and right " four direction, controls the lifting of head and turns to;
The Cloud Terrace pitching knob is for the The Cloud Terrace controlling carrying image on aircraft and obtain equipment luffing angle in vertical direction;
Offline mode change-over switch is for switching the real-time flight pattern of aircraft;
Speed passes antenna for the flight parameter to vehicle launch steering order and the passback of reception aircraft;
Start button is used for starting aircraft;
Fuselage is controlled rocking bar for controlling advancing, retreat, move to left, moving to right of aircraft;
Automatic takeoff/landing switch is for controlling taking off or landing of aircraft;
Cloud platform rotation knob is for controlling the rotation in the horizontal direction of carry-on The Cloud Terrace;
Described figure passes frequency adjustment code switch and passes signal frequency for adjusting figure.
Center-control electroplax is mainly used in the information processing of vehicle launch in whole control procedure or reception, and has the function that the flight parameter of aircraft passback and image information are superimposed.
The beneficial effects of the utility model are: the utility model combines the motion control of unmanned vehicle and image acquisition equipment control, and the flight parameter that aircraft can be returned and image information Overlapping display, on same screen, can convenient operator be controlled whole aircraft and the live state information of grasping aircraft in real time.
Accompanying drawing explanation
Fig. 1 is the structural representation of one one kinds of unmanned vehicle telepilot embodiments of the utility model.
Fig. 2 is the inner structure schematic diagram of one one kinds of unmanned vehicle telepilot embodiments of the utility model.
Fig. 3 is the bottom surface structure schematic diagram of one one kinds of unmanned vehicle telepilot embodiments of the utility model.
Fig. 4 is the enlarged drawing of A in Fig. 3.
Embodiment
Below in conjunction with drawings and Examples, the utility model is described in further detail:
As shown in Figure 1, a kind of unmanned vehicle telepilot, comprises housing 1, lid 1a, handle 3, and described handle 3 is arranged on housing 1, and described lid 1a is arranged on housing 1 by screw 2;
Power switch 4, charging inlet 5 are installed on the lid 1a left side, and power switch 4 is for controlling the on/off of whole telepilot, and charging inlet 5 connects external charging line telepilot is charged;
Power switch 4 and charging inlet 5 up have image control button 6, described image control button 6 be mainly used in controlling the contained vision facilities of unmanned vehicle zoom, take pictures, facility switching etc.;
Image control button 6 up has suspender clip 11, and described suspender clip 11 is mainly used in connecting braces, and telepilot is easy to carry;
Suspender clip 11 up has head to control rocking bar 7, and described head is controlled rocking bar 7 and can be stirred to " upper and lower, left and right " four direction, and when stirring toward left and right, aircraft head rotates to corresponding left and right sides; When stirring up and down, aircraft head rises or declines;
Head is controlled rocking bar 7 up has The Cloud Terrace pitching knob 8, offline mode change-over switch 9, speed to pass antenna 10, and The Cloud Terrace pitching knob 8 is for the The Cloud Terrace controlling carrying image on aircraft and obtain equipment luffing angle in vertical direction; Offline mode change-over switch 9 is for switching the real-time flight pattern of aircraft; Speed passes antenna 10 for the flight parameter to vehicle launch steering order or the passback of reception aircraft;
Lid 1a the right is there is start button 17 in the place by telepilot mid-plane symmetry with image control button 6, for starting aircraft;
Start button 17 up has fuselage to control rocking bar 16, for controlling advancing, retreat, move to left, moving to right of aircraft; When fuselage control rocking bar 16 left or rights are stirred, move on the past left side of aircraft meeting or right side; When fuselage controls that rocking bar 16 is upper and lower to be stirred, aircraft can advance or retreat;
Fuselage is controlled rocking bar 16 up has figure to pass antenna 13, automatic takeoff/landing switch 14, cloud platform rotation knob 15, and figure passes antenna 13 for receiving the image information of the image acquisition equipment passback of aircraft lift-launch; Automatic takeoff/landing switch 14 is for controlling taking off or landing of aircraft; Cloud platform rotation knob 15 is for controlling the rotation in the horizontal direction of carry-on The Cloud Terrace;
In the middle of lid 1a, have screen 12, described screen 12 is mainly used in showing relevant image information and the flight parameter of passback.
Fig. 2 is for unliding after 1a, the structural drawing of telepilot, mainly contain three bulks (from left to right): head is controlled rocking bar base 27, center-control electroplax 31, fuselage control rocking bar base 21, and described head is controlled rocking bar base 27 and is connected with center-control electroplax 31 by electric wire 24; Head is controlled rocking bar base 27 down data-interface base 26 and charging inlet base 25, and data-interface base 26 is connected by electric wire 24 with center-control electroplax 31 respectively with charging inlet base 25; Head is controlled rocking bar base 27 up The Cloud Terrace pitching knob base 28, turned left offline mode change-over switch base 9 and speed of The Cloud Terrace pitching knob base 28 passes antenna base 30, and The Cloud Terrace pitching knob base 28, offline mode change-over switch base 9 and speed pass antenna base 30 and by electric wire 24, is connected with center-control electroplax 31 respectively;
Described fuselage is controlled rocking bar base 21 down start button base 22, and start button base 22 down has battery 23, and battery 23 is connected by electric wire 24 with center-control electroplax 31;
Described fuselage is controlled rocking bar base 21 up has figure to pass antenna base 18, figure biography antenna base 18 has been turned right automatically to open and has been flown/landed switch pedestal 19, automatically open and fly/land the switch pedestal 19 cloud platform rotation knob 20 of having turned right, figure passes antenna base 18, automatically opens and fly/land switch pedestal 19, have cloud platform rotation knob base 20 to pass through respectively electric wire 24 to be connected with center-control electroplax 31.
Referring to Fig. 3 to Fig. 4, telepilot bottom surface has data-interface 32 and figure to pass frequency adjustment code switch 33, and described figure passes frequency adjustment code switch 33 and passes signal frequency for adjusting figure.
More than describe preferred embodiment of the present utility model in detail.Should be appreciated that those of ordinary skill in the art just can make many modifications and variations according to design of the present utility model without creative work.Therefore, all technician in the art comply with design of the present utility model on the basis of existing technology by the available technical scheme of logical analysis, reasoning, or a limited experiment, all should be in the determined protection domain by claims.
Claims (4)
1. a unmanned vehicle telepilot, comprise housing (1), lid (1a), handle (3), described handle (3) is arranged on housing (1), described lid (1a) is arranged on housing (1) by screw 2, power switch (4), charging inlet (5) are installed on described lid (1a) left side, it is characterized in that
Described power switch (4) and charging inlet (5) up have image control button (6), described image control button (6) up has suspender clip (11), described suspender clip (11) up has head to control rocking bar (7), and described head is controlled rocking bar (7) up has The Cloud Terrace pitching knob (8), offline mode change-over switch (9), speed to pass antenna (10);
Lid (1a) the right is there is start button (17) in the place by telepilot mid-plane symmetry with image control button (6), start button (17) up has fuselage to control rocking bar (16), fuselage is controlled rocking bar (16) up has figure to pass antenna (13), automatic takeoff/landing switch (14), cloud platform rotation knob (15), and figure passes antenna (13) for receiving the image information of the image acquisition equipment passback of aircraft lift-launch;
In the middle of lid (1a), there is screen (12).
2. a kind of unmanned vehicle telepilot as claimed in claim 1, it is characterized in that, telepilot inner structure mainly comprises: head is controlled rocking bar base (27), center-control electroplax (31), fuselage control rocking bar base (21), and described head is controlled rocking bar base (27) and is connected with center-control electroplax (31) by electric wire (24);
Head is controlled rocking bar base (27) down data-interface base (26) and charging inlet base (25), and data-interface base (26) is connected by electric wire (24) with center-control electroplax (31) respectively with charging inlet base (25); Head is controlled rocking bar base (27) up The Cloud Terrace pitching knob base (28), turned left offline mode change-over switch base (9) and speed of The Cloud Terrace pitching knob base (28) passes antenna base (30), and The Cloud Terrace pitching knob base (28), offline mode change-over switch base (9) and speed biography antenna base (30) are connected with center-control electroplax (31) by electric wire (24) respectively;
Described fuselage is controlled rocking bar base (21) down start button base (22), and start button base (22) down has battery (23), and battery (23) is connected by electric wire (24) with center-control electroplax (31);
Described fuselage is controlled rocking bar base (21) up has figure to pass antenna base (18), figure biography antenna base (18) has been turned right automatically to open and has been flown/landed switch pedestal (19), automatically open and fly/land switch pedestal (19) the cloud platform rotation knob (20) of having turned right, figure passes antenna base (18), automatically opens and fly/land switch pedestal (19), have cloud platform rotation knob base (20) to pass through respectively electric wire (24) to be connected with center-control electroplax (31).
3. a kind of unmanned vehicle telepilot as claimed in claim 1, is characterized in that: the telepilot back side has data-interface (32) and figure to pass frequency adjustment code switch (33).
4. a kind of unmanned vehicle telepilot as claimed in claim 1, is characterized in that: the function of each major part is as follows:
Described image control button (6) be mainly used in controlling the contained vision facilities of unmanned vehicle zoom, take pictures, facility switching etc.;
Described head is controlled rocking bar (7) and can be stirred to " upper and lower, left and right " four direction, controls the lifting of head and turns to;
The Cloud Terrace pitching knob (8) is for the The Cloud Terrace controlling carrying image on aircraft and obtain equipment luffing angle in vertical direction;
Offline mode change-over switch (9) is for switching the real-time flight pattern of aircraft;
Speed passes antenna (10) for the flight parameter to vehicle launch steering order and the passback of reception aircraft;
Start button (17) is for starting aircraft;
Fuselage is controlled rocking bar (16) for controlling advancing, retreat, move to left, moving to right of aircraft;
Automatic takeoff/landing switch (14) is for controlling taking off or landing of aircraft;
Cloud platform rotation knob (15) is for controlling the rotation in the horizontal direction of carry-on The Cloud Terrace;
Described figure passes frequency adjustment code switch (33) and passes signal frequency for adjusting figure;
Center-control electroplax (31) is mainly used in the information processing of vehicle launch in whole control procedure or reception, and has the function that the flight parameter of aircraft passback and image information are superimposed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420157021.XU CN203838864U (en) | 2014-04-02 | 2014-04-02 | Unmanned aerial vehicle remote control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420157021.XU CN203838864U (en) | 2014-04-02 | 2014-04-02 | Unmanned aerial vehicle remote control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203838864U true CN203838864U (en) | 2014-09-17 |
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ID=51516679
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420157021.XU Expired - Lifetime CN203838864U (en) | 2014-04-02 | 2014-04-02 | Unmanned aerial vehicle remote control device |
Country Status (1)
| Country | Link |
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| CN (1) | CN203838864U (en) |
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN104608928A (en) * | 2014-12-12 | 2015-05-13 | 辽宁石油化工大学 | Multifunctional early-warning type aerial photography aircraft |
| WO2016045018A1 (en) * | 2014-09-24 | 2016-03-31 | 深圳市大疆创新科技有限公司 | Remote controller, handle structure thereof, and control method for uav |
| CN105518757A (en) * | 2015-01-06 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Holder remote controller and handheld holder using the same |
| CN105518371A (en) * | 2014-09-30 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Retaining device and remote controller using same |
| CN105513433A (en) * | 2016-01-19 | 2016-04-20 | 清华大学合肥公共安全研究院 | Ground control station based on airborne system of unmanned aerial vehicle |
| WO2016095793A1 (en) * | 2014-12-15 | 2016-06-23 | 优利科技有限公司 | Remote control |
| CN105872336A (en) * | 2016-05-24 | 2016-08-17 | 北京小米移动软件有限公司 | Camera |
| CN105867422A (en) * | 2016-06-08 | 2016-08-17 | 南京钟山苑航空技术有限公司 | Handheld ground control station of unmanned vehicles |
| CN106791430A (en) * | 2017-01-17 | 2017-05-31 | 石家庄高新区天遥航空设备科技有限公司 | A kind of vision composite control apparatus |
| CN106774416A (en) * | 2017-01-11 | 2017-05-31 | 联想(北京)有限公司 | Information processing method and device, control device, UAS |
| CN107437330A (en) * | 2016-05-27 | 2017-12-05 | 北京臻迪机器人有限公司 | No-manned machine distant control system and method |
| CN107754346A (en) * | 2017-11-30 | 2018-03-06 | 广州市华科尔科技股份有限公司 | A kind of foldable unmanned controller |
| CN108513675A (en) * | 2017-08-17 | 2018-09-07 | 深圳市大疆创新科技有限公司 | Remote controler |
| CN108536214A (en) * | 2018-02-24 | 2018-09-14 | 沈阳无距科技有限公司 | A kind of remote controler and flight instruments |
| CN108884961A (en) * | 2017-08-04 | 2018-11-23 | 深圳市大疆灵眸科技有限公司 | Remote controler and capture apparatus |
| CN109983415A (en) * | 2017-07-24 | 2019-07-05 | 深圳市大疆创新科技有限公司 | Remote controler and unmanned vehicle system |
| CN110249373A (en) * | 2017-08-17 | 2019-09-17 | 深圳市大疆创新科技有限公司 | Remote controler |
| CN111090287A (en) * | 2018-10-23 | 2020-05-01 | 深圳市斯威普科技有限公司 | Remote control for controlling an aircraft |
-
2014
- 2014-04-02 CN CN201420157021.XU patent/CN203838864U/en not_active Expired - Lifetime
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| WO2016045018A1 (en) * | 2014-09-24 | 2016-03-31 | 深圳市大疆创新科技有限公司 | Remote controller, handle structure thereof, and control method for uav |
| CN105612468A (en) * | 2014-09-24 | 2016-05-25 | 深圳市大疆创新科技有限公司 | Remote controller, handle structure thereof, and control method for uav |
| US11179650B2 (en) | 2014-09-24 | 2021-11-23 | SZ DJI Technology Co., Ltd. | Remote controller and handle structure thereof, and method for controlling a UAV |
| US10675551B2 (en) | 2014-09-24 | 2020-06-09 | SZ DJI Technology Co., Ltd. | Remote controller and handle structure thereof, and method for controlling a UAV |
| CN105518371A (en) * | 2014-09-30 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Retaining device and remote controller using same |
| US10222794B2 (en) | 2014-09-30 | 2019-03-05 | SZ DJI Technology Co., Ltd. | Remote controller using retaining device |
| CN104608928A (en) * | 2014-12-12 | 2015-05-13 | 辽宁石油化工大学 | Multifunctional early-warning type aerial photography aircraft |
| WO2016095793A1 (en) * | 2014-12-15 | 2016-06-23 | 优利科技有限公司 | Remote control |
| CN105518757B (en) * | 2015-01-06 | 2018-06-12 | 深圳市大疆灵眸科技有限公司 | Holder remote controler and the hand-held holder using the holder remote controler |
| CN105518757A (en) * | 2015-01-06 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Holder remote controller and handheld holder using the same |
| US10347119B2 (en) | 2015-01-06 | 2019-07-09 | Sz Dji Osmo Technology Co., Ltd. | Gimbal remote controller and handheld gimbal using the gimbal remote controller |
| CN105513433A (en) * | 2016-01-19 | 2016-04-20 | 清华大学合肥公共安全研究院 | Ground control station based on airborne system of unmanned aerial vehicle |
| CN105872336A (en) * | 2016-05-24 | 2016-08-17 | 北京小米移动软件有限公司 | Camera |
| CN107437330A (en) * | 2016-05-27 | 2017-12-05 | 北京臻迪机器人有限公司 | No-manned machine distant control system and method |
| CN105867422A (en) * | 2016-06-08 | 2016-08-17 | 南京钟山苑航空技术有限公司 | Handheld ground control station of unmanned vehicles |
| CN106774416A (en) * | 2017-01-11 | 2017-05-31 | 联想(北京)有限公司 | Information processing method and device, control device, UAS |
| CN106791430A (en) * | 2017-01-17 | 2017-05-31 | 石家庄高新区天遥航空设备科技有限公司 | A kind of vision composite control apparatus |
| CN109983415A (en) * | 2017-07-24 | 2019-07-05 | 深圳市大疆创新科技有限公司 | Remote controler and unmanned vehicle system |
| WO2019024119A1 (en) * | 2017-08-04 | 2019-02-07 | 深圳市大疆灵眸科技有限公司 | Remote controller and photographing device |
| CN108884961A (en) * | 2017-08-04 | 2018-11-23 | 深圳市大疆灵眸科技有限公司 | Remote controler and capture apparatus |
| CN111561642A (en) * | 2017-08-04 | 2020-08-21 | 深圳市大疆灵眸科技有限公司 | Remote controller and shooting equipment |
| US11089198B2 (en) | 2017-08-04 | 2021-08-10 | Sz Dji Osmo Technology Co., Ltd. | Remote controller and photographing device |
| CN111561642B (en) * | 2017-08-04 | 2022-08-16 | 深圳市大疆灵眸科技有限公司 | Remote controller and shooting equipment |
| WO2019033343A1 (en) * | 2017-08-17 | 2019-02-21 | 深圳市大疆创新科技有限公司 | Remote control |
| CN110249373A (en) * | 2017-08-17 | 2019-09-17 | 深圳市大疆创新科技有限公司 | Remote controler |
| CN108513675B (en) * | 2017-08-17 | 2020-11-27 | 深圳市大疆创新科技有限公司 | Remote controller |
| CN108513675A (en) * | 2017-08-17 | 2018-09-07 | 深圳市大疆创新科技有限公司 | Remote controler |
| US11226617B2 (en) | 2017-08-17 | 2022-01-18 | SZ DJI Technology Co., Ltd. | Remote control |
| CN107754346A (en) * | 2017-11-30 | 2018-03-06 | 广州市华科尔科技股份有限公司 | A kind of foldable unmanned controller |
| CN108536214A (en) * | 2018-02-24 | 2018-09-14 | 沈阳无距科技有限公司 | A kind of remote controler and flight instruments |
| CN111090287A (en) * | 2018-10-23 | 2020-05-01 | 深圳市斯威普科技有限公司 | Remote control for controlling an aircraft |
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| C14 | Grant of patent or utility model | ||
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| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160316 Address after: 401122 Chongqing city Yubei District northern new cloud Feng Lu No. 2 Patentee after: CHONGQING YIDONG TECHNOLOGY CO.,LTD. Address before: 012000, 1, 1, 69 East Tiger Hill Road, Jining District, the Inner Mongolia Autonomous Region, Wulanchabu Patentee before: Li Bin Patentee before: Zhang Jianren Patentee before: Zhang Jianjun |
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| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20140917 |