CN204596856U - Power brick and unmanned plane - Google Patents
Power brick and unmanned plane Download PDFInfo
- Publication number
- CN204596856U CN204596856U CN201520236752.8U CN201520236752U CN204596856U CN 204596856 U CN204596856 U CN 204596856U CN 201520236752 U CN201520236752 U CN 201520236752U CN 204596856 U CN204596856 U CN 204596856U
- Authority
- CN
- China
- Prior art keywords
- battery pack
- plate
- connecting portion
- housing
- power brick
- 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 - Lifetime
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Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
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- Casings For Electric Apparatus (AREA)
Abstract
本实用新型公开了一种电池包，安装于无人机上，所述电池包括锁扣件及壳体，所述壳体包括前端部、后端部、左侧部、右侧部、上侧部及下侧部；所述锁扣件包括固定连接于所述前端部的连接部及位于所述连接部两端的两卡持部，所述两卡持部分别位于所述左侧部和所述右侧部的外侧，所述卡持部包括自所述连接部向所述后端部方向延伸出的内侧板及由所述内侧板向所述连接部方向弯折而成的、且与所述内侧板具有一间距的外侧板，所述外侧板上设有用于卡入外部构件的凹槽中的凸起。本实用新型还提供一种无人机。本实用新型的电池包通过锁扣件卡持安装于无人机的收容室内，使电池包的安装及拆卸极为方便、快捷。
The utility model discloses a battery pack, which is installed on an unmanned aerial vehicle. The battery includes a locking member and a casing, and the casing includes a front end, a rear end, a left side, a right side, and an upper side. and the lower side part; the locking member includes a connecting part fixedly connected to the front end part and two clamping parts located at both ends of the connecting part, and the two clamping parts are respectively located on the left side part and the On the outer side of the right side, the clamping portion includes an inner plate extending from the connecting portion toward the rear end, and an inner plate bent from the inner plate toward the connecting portion, and is connected to the The inner side plate has an outer side plate with a distance, and the outer side plate is provided with protrusions for snapping into the grooves of the outer member. The utility model also provides an unmanned aerial vehicle. The battery pack of the utility model is clamped and installed in the containment room of the drone through the locking member, so that the installation and disassembly of the battery pack are extremely convenient and fast.
Description
Technical field
The utility model relates to unmanned plane field.
Background technology
Unmanned plane with its action flexibly, landing environmental requirement is lower, and has good operating characteristics etc., be widely used in take photo by plane, monitor, investigate, the numerous areas such as search and rescue.All battery is provided with in unmanned plane, battery plays vital effect to unmanned plane, but, the fuselage of existing unmanned plane has for the battery chamber of battery installation with by the cover plate of battery chamber's capping, when mounted, need battery to install to be placed in battery chamber, with cover plate by battery chamber's capping, then by screw, cover plate is fixed on fuselage.Although the mounting means of this battery is very firm, can prevent battery from getting loose in battery chamber, for the installation and removal of battery, aforesaid way and trouble thereof, and lose time.
Utility model content
Main purpose of the present utility model, for providing a kind of battery, is intended to the problem of the assembling complexity solving power brick in existing unmanned plane.
The utility model proposes a kind of power brick, be installed on unmanned plane, described power brick comprises snap close piece and housing, and described housing comprises leading section, rearward end, left side, right side, upper lateral part and following side; Described snap close piece comprises the connecting portion being fixedly connected on described leading section and two holding sections being positioned at described connecting portion two ends, described two holding sections lay respectively at the outside of described left side and described right side, described holding section comprise the interior plate that extends to described rearward end direction from described connecting portion and by described interior plate bend to described connecting portion direction and with described interior plate, there is the outer panel of a spacing, described outer panel is provided with the projection for snapping in the groove of external member.
Preferably, described connecting portion is fixedly connected on the inner surface of described leading section, and described left side and described right side are respectively equipped with the mouth of stepping down stretching out described housing for holding section described in two.
Preferably, described interior plate comprises the first interior plate be connected with described connecting portion and the second interior plate extended towards described rearward end by described leading section formed to infolding by described first interior plate, and described outer panel is outwards bent to form by described second interior plate.
Preferably, described first side plate is parallel with described second side plate.
Preferably, described leading section becomes cabochon, and described connecting portion and described leading section are contoured design.
Preferably, the plate face deviating from described interior plate of the free end of described outer panel is provided with some convex tendons.
Preferably, described housing is the fine housing of carbon.
Preferably, described projection has the chamfering for described projection being imported in the groove of external member near the part of described rearward end.
For achieving the above object, the utility model also provides a kind of power brick, is installed on unmanned plane, and described power brick comprises snap close piece and housing, and described housing comprises leading section, rearward end, left side, right side, upper lateral part and following side; Described snap close piece comprises two holding sections, described two holding sections lay respectively at the outside of described left side and described right side, described holding section comprise the interior plate that extends to described rearward end direction along described leading section and by described interior plate bend to described connecting portion direction and with described interior plate, there is the outer panel of a spacing, the interior plate of described two holding sections connects described left side and described right side respectively, and the plate face deviating from described interior plate of described outer panel is provided with the projection for snapping in the groove of external member.
For achieving the above object, the utility model provides a kind of unmanned plane further, described unmanned plane comprises the power brick described in above-mentioned any one, the fuselage of described unmanned plane is provided with one for accommodating the reception room of described power brick, and the both sides of described reception room are provided with the reeded holding part of tool.
Power brick of the present utility model is held by described snap close piece and is installed in the reception room of unmanned plane, decreases the installation steps of power brick, improves the installation effectiveness of power brick, makes the installation of described power brick and dismantles very convenient, fast.
Accompanying drawing explanation
Fig. 1 is the structural representation of an embodiment of the utility model power brick;
Fig. 2 is the structural representation of the snap close piece of power brick in Fig. 1;
Fig. 3 is the structural representation of the housing of power brick in Fig. 1;
Fig. 4 is the A portion structure for amplifying schematic diagram of snap close piece in Fig. 2;
Fig. 5 is the structural representation of this practical vivid another embodiment of power brick;
Fig. 6 is the structural representation of the snap close piece of power brick in Fig. 5;
Fig. 7 is the structural representation of the utility model aircraft one embodiment, and wherein, power brick is also unkitted and is loaded in fuselage;
Fig. 8 is the B portion structure for amplifying schematic diagram of unmanned plane in Fig. 7.
The realization of the utility model object, functional characteristics and advantage will in conjunction with the embodiments, are described further with reference to accompanying drawing.
Embodiment
Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
As shown in Figure 1, the utility model provides a kind of for being installed on power brick on unmanned plane, and this power brick comprises snap close piece 10 and housing 20, and wherein, housing 10 comprises leading section, rearward end, left side, right side, upper lateral part and following side; Snap close piece 10 comprises the connecting portion 11 being fixedly connected on leading section and two holding sections 12 being positioned at connecting portion 11 two ends, two holding sections 12 lay respectively at the outside of left side and right side, holding section 12 comprise from connecting portion 11 backward the interior plate 121 that extends of end direction and by interior plate 121 bend to connecting portion 11 direction and with interior plate 121, there is the outer panel 122 of a spacing, outer panel 122 is provided with the projection 123 for snapping in the groove of external member.
For holding battery body 30 in housing 20, snap close piece 10 is inserted in housing 20 by mouth 210 of stepping down, and connecting portion 11 is arranged between leading section and battery body 30.Be understandable that, can not arrange mouth 210 of stepping down, directly connecting portion 11 is fixed on the outer surface of leading section, namely snap close piece 10 is located at the outside of housing 20.
With reference to Fig. 7 and Fig. 8, the fuselage 40 of unmanned plane is provided with the reception room 41 of collecting power brick, the holding part 410 of the opening part of reception room 41 is provided with the groove 411 corresponding with protruding 123 positions, and power brick is fastened in reception room 41 with coordinating of groove 411 by protruding 123.Concrete, with reference to Fig. 2, holding section 12 arranges in " U " type, and when assembling this power brick, the rearward end of power brick passes the opening of reception room 41, protruding 123 abut with the holding part 410 of reception room 41, after the outer panel 122 of holding section 12 is squeezed, elastic deformation occurs, outer panel 122 offsets towards the direction of interior plate 121, until after projection 123 accommodates by groove 411, outer panel 122 recovers elastic deformation, towards the direction skew deviating from interior plate 121.So far, power brick is closely fastened in reception room 41 with coordinating of groove 411 by protruding 123.When this power brick dismantled by needs time, only need, towards the direction pressing outer panel 122 of interior plate 121, to make protruding 123 to deviate from groove 411, then extract de-for power brick.
Power brick of the present utility model is held by snap close piece 10 and is installed in the reception room 41 of unmanned plane, decreases the installation steps of power brick, improves the installation effectiveness of power brick, makes the installation of power brick and dismantles very convenient, fast.
Further, connecting portion 11 is fixedly connected on the inner surface of leading section, and left side and right side are respectively equipped with the mouth 210 of stepping down stretching out housing 20 for two holding sections.
Concrete, left side and right side all have the first side plate 21, and mouth 210 of stepping down is arranged on the first side plate 21, and through first side plate 21 of mouth 210 of stepping down, so that the installation of snap close piece 10.
Further, interior plate 121 comprises the first interior plate 1211 be connected with connecting portion 11 and the second interior plate 1212 extended towards rearward end by leading section formed to infolding by the first interior plate 1211, and outer panel 122 is outwards bent to form by the second interior plate 1212.
Continue with reference to Fig. 2 and Fig. 3, interior plate 121 also comprises and is arranged at the first interior plate 1211, second interior plate 1212, and transition plate 1213, one plate of the first interior plate 1211 is facing to the first side plate 21, one end of first interior plate 1211 connects described connecting portion 11, the other end of the first interior plate 1211 connects one end of transition plate 112, and the other end of transition plate 112 connects one end towards connecting portion 11 of the second interior plate 1212.
In the present embodiment, by the compactness be connected between this snap close piece 10 with housing 20 can be strengthened after arranging the first interior plate 1211.Concrete, in a upper embodiment, the connected mode between connecting portion 11 and housing 20 has multiple, as connecting portion 11 is bonded in housing 20, certain connecting portion 11 also can be connected by playing screw with between housing 20, and connects relatively complicated by playing screw, and dismounting is inconvenient.By after the arranging of the first interior plate 1211, when this snap close piece 10 is inserted in housing 20 by mouth 210 of stepping down, first interior plate 1211 can abut with the medial surface of the first side plate 21, which adds snap close piece 10 and the contact area of housing 20, make this snap close piece 10 installation in housing 20 more stable.
Further, continue referring to Fig. 2 and Fig. 8, leading section becomes cabochon, and connecting portion 11 and leading section are contoured design, and what connecting portion 11 and leading section can be made like this to bond is more firm.That is, leading section has one day to the cambered outwards cambered surface in the side deviating from holding section 12, and connecting portion 11 is arranged in the arc similar with leading section.
If when connecting portion 11 and leading section are spirally connected fixing, due to installation and when dismantling this power brick, holding section 12 can extrude because being subject to holding part 410 and elastic deformation occur, in the process, holding section 12 entirety all has the trend towards this housing 20 internal blas, is fastened in groove 411 to make protruding 123.This arc of connecting portion 11 arranges the elasticity that further enhancing this snap close piece 10 entirety; Concrete, the connecting portion 11 that arc is arranged adds the elastically-deformable performance of this connecting portion 11, when holding section 12 is subject to the extruding force towards this housing 20 inside, also there is elastic deformation in connecting portion 11, the two ends of connecting portion 11 are all towards the internal blas of this housing 20, so just further enhancing the elasticity of this snap close piece 10 entirety, just make power brick more easily mount and dismount.
Further, continue with reference to Fig. 2, the plate face deviating from interior plate 121 of the free end of outer panel 122 is provided with some convex tendons.
Concrete, arranging of convex tendon 124 can make the finger of user more convenient when clamping holding section 12, can prevent user from skidding with during hand clamping holding section 12.
Further, with reference to Fig. 3, housing 20 is the fine housing of carbon.
Concrete, generally, in order to prevent housing 20 from conducting electricity, the material of housing 20 is often plastics.Consider that the quality of general plastics is relatively large, the overall weight impact of housing 20 on power brick that quality is larger is larger, so will strengthen the heavy burden of unmanned plane, in the present embodiment, the material of housing 20 is that carbon is fine, just greatly reduces the weight of housing 20 thus, also the heavy burden of unmanned plane is just reduced, make the flight of unmanned plane more brisk, also reduce the consumption of unmanned plane to electric energy, extend the power-on time of power brick.
Further, with reference to Fig. 2 and Fig. 4, protruding 123 have the chamfering for importing protruding 123 in the groove 411 of external member towards the part of rearward end, this chamfering can be rounding or the hypotenuse that falls.
Concrete, protruding 123 comprise a guide part 1231, the cross-sectional area that guide part 1231 intercepts via the plane perpendicular to outer panel 122, and the one end along the one end deviating from connecting portion 11 close connecting portion 11 of side plate 122 toward the outside of outer panel 122 increases gradually.Like this, when power brick is installed on reception room 41, guide part 1231 can make this projection 123 enter in groove 411 more convenient, adds the efficiency of assembling of power brick.
With reference to Fig. 5 and Fig. 6, the utility model also provides another kind of power brick, and power brick comprises snap close piece 10 ' and housing 20 ', and housing 20 ' comprises leading section, rearward end, left side, right side, upper lateral part and following side; Snap close piece 10 ' comprises two holding sections 12 ', two holding sections 12 ' lay respectively at the outside of left side and right side, holding section 12 ' comprise along leading section backward end direction extend interior plate 121 ' and by interior plate 121 ' bend to connecting portion direction and with interior plate 121 ', there is the outer panel 122 ' of a spacing, the interior plate 121 ' of two holding sections 12 ' connects left side and right side respectively, and the plate face deviating from interior plate 121 ' of outer panel 122 ' is provided with the projection 123 ' for snapping in the groove 411 of external member.Being understandable that the power brick in the present embodiment is the distortion of above-mentioned any embodiment to snap close piece, only otherwise the technical scheme in conflicting above-mentioned any embodiment can move on in the present embodiment equally, and in order to meet succinct requirement, not repeating them here.
With reference to Fig. 7, for achieving the above object, the utility model also provides a kind of unmanned plane, and unmanned plane comprises the power brick of above-mentioned any embodiment, the fuselage 40 of unmanned plane is provided with one for accommodating the reception room 41 of power brick, the both sides of reception room 41 are provided with the holding part 410 with groove 411.
Concrete, owing to being provided with any embodiment of above-mentioned power brick in this unmanned plane, therefore, all these unmanned planes of beneficial effect of above-mentioned power brick also Ying Yiying have, and do not repeat one by one at this.
The foregoing is only preferred embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every utilize the utility model specification and accompanying drawing content to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present utility model.
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520236752.8U CN204596856U (en) | 2015-04-17 | 2015-04-17 | Power brick and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520236752.8U CN204596856U (en) | 2015-04-17 | 2015-04-17 | Power brick and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204596856U true CN204596856U (en) | 2015-08-26 |
Family
ID=53932976
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520236752.8U Expired - Lifetime CN204596856U (en) | 2015-04-17 | 2015-04-17 | Power brick and unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204596856U (en) |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105514315A (en) * | 2016-01-11 | 2016-04-20 | 无锡觅睿恪科技有限公司 | Cell structure for unmanned plane |
| CN105529419A (en) * | 2015-12-08 | 2016-04-27 | 深圳市数码时代科技有限公司 | Universal type quick battery plugging and unplugging device for unmanned aerial vehicle |
| CN105539857A (en) * | 2016-01-22 | 2016-05-04 | 无锡觅睿恪科技有限公司 | Battery clamping structure for unmanned aerial vehicle |
| CN105826488A (en) * | 2016-05-24 | 2016-08-03 | 北京小米移动软件有限公司 | Multi-channel power supply cell structure, cell system and air vehicle |
| WO2017101589A1 (en) * | 2015-12-14 | 2017-06-22 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle battery and unmanned aerial vehicle |
| CN107031841A (en) * | 2016-04-07 | 2017-08-11 | 广州极飞科技有限公司 | Aircraft |
| WO2018152835A1 (en) * | 2017-02-27 | 2018-08-30 | Tti (Macao Commercial Offshore) Limited | Handheld vacuum cleaner |
| CN108513564A (en) * | 2017-04-26 | 2018-09-07 | 深圳市大疆创新科技有限公司 | Electronic equipment |
| WO2019134406A1 (en) * | 2018-01-05 | 2019-07-11 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| US10442533B2 (en) | 2015-12-14 | 2019-10-15 | Autel Robotics Co., Ltd. | Battery used for unmanned aerial vehicle and unmanned aerial vehicle |
| US10525832B2 (en) | 2013-12-06 | 2020-01-07 | SZ DJI Technology Co., Ltd. | Battery and unmanned aerial vehicle with the battery |
| WO2022141416A1 (en) * | 2020-12-31 | 2022-07-07 | 深圳市大疆创新科技有限公司 | Housing structure, battery, electronic device, and mobile platform |
| CN115498350A (en) * | 2021-06-17 | 2022-12-20 | 启碁科技股份有限公司 | Engagement member and battery accommodation device |
-
2015
- 2015-04-17 CN CN201520236752.8U patent/CN204596856U/en not_active Expired - Lifetime
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| US11607972B2 (en) | 2013-12-06 | 2023-03-21 | SZ DJI Technology Co., Ltd. | Battery and unmanned aerial vehicle with battery indicator and venting opening |
| US10906427B2 (en) | 2013-12-06 | 2021-02-02 | SZ DJI Technology Co., Ltd. | Battery and unmanned aerial vehicle with the battery |
| US10625613B2 (en) | 2013-12-06 | 2020-04-21 | SZ DJI Technology Co., Ltd. | Battery and unmanned aerial vehicle with the battery |
| US10525832B2 (en) | 2013-12-06 | 2020-01-07 | SZ DJI Technology Co., Ltd. | Battery and unmanned aerial vehicle with the battery |
| CN105529419B (en) * | 2015-12-08 | 2018-07-10 | 深圳市数码时代科技有限公司 | A kind of universal unmanned plane fast insert-pull cell apparatus |
| CN105529419A (en) * | 2015-12-08 | 2016-04-27 | 深圳市数码时代科技有限公司 | Universal type quick battery plugging and unplugging device for unmanned aerial vehicle |
| US10090496B2 (en) | 2015-12-14 | 2018-10-02 | Autel Robotics Usa Llc | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
| US10074836B2 (en) | 2015-12-14 | 2018-09-11 | Autel Robotics Usa Llc | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
| US9979000B2 (en) | 2015-12-14 | 2018-05-22 | Autel Robotics Co., Ltd. | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
| WO2017101589A1 (en) * | 2015-12-14 | 2017-06-22 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle battery and unmanned aerial vehicle |
| US10044013B2 (en) | 2015-12-14 | 2018-08-07 | Autel Robotics Usa Llc | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
| US11254429B2 (en) | 2015-12-14 | 2022-02-22 | Autel Robotics Co., Ltd. | Battery used for unmanned aerial vehicle and unmanned aerial vehicle |
| EP3244468A4 (en) * | 2015-12-14 | 2017-12-13 | Autel Robotics Co., Ltd. | Unmanned aerial vehicle battery and unmanned aerial vehicle |
| US10745128B2 (en) | 2015-12-14 | 2020-08-18 | Autel Robotics Co., Ltd. | Battery used for unmanned aerial vehicle and unmanned aerial vehicle |
| US10442533B2 (en) | 2015-12-14 | 2019-10-15 | Autel Robotics Co., Ltd. | Battery used for unmanned aerial vehicle and unmanned aerial vehicle |
| US10115944B2 (en) | 2015-12-14 | 2018-10-30 | Autel Robotics Usa Llc | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
| US10224526B2 (en) | 2015-12-14 | 2019-03-05 | Autel Robotics Usa Llc | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
| EP3840111A1 (en) * | 2015-12-14 | 2021-06-23 | Autel Robotics Co., Ltd. | A battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
| CN105514315A (en) * | 2016-01-11 | 2016-04-20 | 无锡觅睿恪科技有限公司 | Cell structure for unmanned plane |
| CN105539857A (en) * | 2016-01-22 | 2016-05-04 | 无锡觅睿恪科技有限公司 | Battery clamping structure for unmanned aerial vehicle |
| CN105539857B (en) * | 2016-01-22 | 2017-09-12 | 无锡觅睿恪科技有限公司 | Unmanned plane battery interface arrangment |
| CN107031841A (en) * | 2016-04-07 | 2017-08-11 | 广州极飞科技有限公司 | Aircraft |
| CN107031841B (en) * | 2016-04-07 | 2024-02-13 | 广州极飞科技股份有限公司 | Aircraft with a plurality of aircraft body |
| CN105826488A (en) * | 2016-05-24 | 2016-08-03 | 北京小米移动软件有限公司 | Multi-channel power supply cell structure, cell system and air vehicle |
| WO2018152835A1 (en) * | 2017-02-27 | 2018-08-30 | Tti (Macao Commercial Offshore) Limited | Handheld vacuum cleaner |
| CN108513564A (en) * | 2017-04-26 | 2018-09-07 | 深圳市大疆创新科技有限公司 | Electronic equipment |
| WO2019134406A1 (en) * | 2018-01-05 | 2019-07-11 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| WO2022141416A1 (en) * | 2020-12-31 | 2022-07-07 | 深圳市大疆创新科技有限公司 | Housing structure, battery, electronic device, and mobile platform |
| CN115498350A (en) * | 2021-06-17 | 2022-12-20 | 启碁科技股份有限公司 | Engagement member and battery accommodation device |
| CN115498350B (en) * | 2021-06-17 | 2023-05-19 | 启碁科技股份有限公司 | Engaging member and battery accommodating device |
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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: 20160307 Address after: Baoan District Shiyan street Shenzhen city Guangdong province 518108 Songbai road Tangtou junctions electric science and Technology Park Patentee after: Shenzhen Aee Technology Co., Ltd. Address before: Baoan District Shiyan street Shenzhen city Guangdong province 518108 Songbai road Tangtou junctions electric science and Technology Park Patentee before: Shenzhen Aee Technology Co., Ltd. Patentee before: Shenzhen Aee Technology Co., Ltd. |
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| TR01 | Transfer of patent right |
Effective date of registration: 20191213 Address after: Room 812, enterprise service center, No. 17, section 3, west section of Changjiang North Road, Lingang Economic Development Zone, Yibin City, Sichuan Province Patentee after: Sichuan Yidian Aviation Technology Co., Ltd Address before: Baoan District Shiyan street Shenzhen city Guangdong province 518108 Songbai road Tangtou junctions electric science and Technology Park Patentee before: Shenzhen Yidian Aviation Technology Co., Ltd. |
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| TR01 | Transfer of patent right |