CN204223178U - A kind of folding unmanned plane - Google Patents
A kind of folding unmanned plane Download PDFInfo
- Publication number
- CN204223178U CN204223178U CN201420608793.0U CN201420608793U CN204223178U CN 204223178 U CN204223178 U CN 204223178U CN 201420608793 U CN201420608793 U CN 201420608793U CN 204223178 U CN204223178 U CN 204223178U
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- horn
- cylindrical bar
- rest
- unmanned plane
- connection block
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Abstract
The utility model relates to a kind of folding unmanned plane, comprise center am rest, the horn be connected with center am rest, the foot rest be connected with center am rest, the screw propeller be located on horn, drive the motor of screw propeller and provide the battery of power supply for motor, center am rest is provided with Connection Block, Connection Block is provided with cylindrical bar, and horn and foot rest are flexibly connected with cylindrical bar respectively.The each horn of this unmanned plane adopts folding structure, greatly can increase the portability of unmanned plane.Horn take cylindrical bar as S. A., realizes folding downwards.Cylindrical bar can realize the fast assembling-disassembling of horn simultaneously.The replacing construction of horn can be saved.Battery is placed on the upper end of shell, adopts snap close to be fastened by battery case lid, can ensure that the installation of battery is reliable, can realize again the fast assembling-disassembling of battery.Just because of portability and the fast assembling-disassembling requirement of unmanned plane, this unmanned plane is particularly suitable for the fields such as scouting.
Description
Technical field
The utility model relates to a kind of collapsible unmanned plane, especially can realize the unmanned plane of fast assembling-disassembling.
Background technology
Unmanned plane center am rest can support bearing thing.Such as: carrier be photographic camera or camera time, its to be mounted on support can differing heights, different visual angles shooting; When carrier is headset, it is mounted in the transmission that support can realize sound.But the horn of correlation technique does not have folder function, namely enable realization has the horn of folder function to realize fast assembling-disassembling.In addition, battery can not realize fast assembling-disassembling.For the unmanned plane being applied to scouting field, its fast assembling-disassembling seems particularly important.Therefore, be necessary to provide a kind of new unmanned plane to overcome above-mentioned shortcoming.
Utility model content
The purpose of this utility model is: provide a kind of collapsible unmanned plane.
In order to realize foregoing invention object, the utility model provides a kind of folding unmanned plane, comprise center am rest, the horn be connected with center am rest, the foot rest be connected with center am rest, the screw propeller be located on horn, drive the motor of screw propeller and provide the battery of power supply for motor, center am rest is provided with Connection Block, Connection Block is provided with cylindrical bar, and horn and foot rest are flexibly connected with cylindrical bar respectively.
The coupling end of described horn and cylindrical bar is provided with plush copper one, and the coupling end of foot rest and cylindrical bar is provided with plush copper two, and plush copper one and plush copper two are on same circular path.Extension spring is provided with between horn and foot rest.Described Connection Block is provided with a spinner, horn is provided with the plush copper three locked with spinner.
Described Connection Block is provided with cylinder rod aperture, and cylinder rod aperture one end is circumferentially provided with groove and keyway, and described cylindrical bar head arranges a plush copper four, and plush copper four is located by connecting with Connection Block to keyway through rotating after groove.
Described cylindrical bar is arranged with and makes cylindrical bar be fastened on Compress Spring on Connection Block.Cylindrical bar has certain precompressed compression to spring when installing, to ensure cylindrical bar not because unmanned plane rocking and get loose when flying.
Described center am rest be provided with put battery battery case lid and by snap close fastening for battery case lid.
Compare with correlation technique, unmanned plane of the present utility model can realize horn and fold, and can realize fast assembling-disassembling on this basis in addition.
Accompanying drawing explanation
Fig. 1 is the block diagram of the utility model unmanned plane.
Fig. 2 is the exploded view of the utility model unmanned plane horn part fast assembling disassembling structure.
Fig. 3 is the utility model unmanned plane horn part fast assembling disassembling structure partial enlarged drawing.
Fig. 4 is the exploded view of the utility model unmanned plane battery compartment fast assembling disassembling structure.
Fig. 5 is the installation exploded view of the utility model unmanned plane mount pad and foot rest.
Detailed description of the invention
As Figure 1-3, the utility model provides a kind of collapsible unmanned plane realizing fast assembling-disassembling.Comprising center am rest 4, the folding horn 1 be connected with center am rest, battery rapid dismounting apparatus 2, the foot rest 3 be connected with center am rest 4, the screw propeller 5 be located on horn 1, drive the motor 6 of screw propeller 5, center am rest 4 is provided with Connection Block 4a.Connection Block 4a is provided with cylindrical bar 4c, and horn 1 and foot rest 3 are flexibly connected (as in hinged way) respectively on cylindrical bar 4c, and folding horn 1 can rotate around cylindrical bar 1c.Described Connection Block is provided with spinner 4b, horn is provided with the plush copper 7 locked with spinner; When horn 1 level, rotate spinner 4b and can fasten plush copper 7 on mount pad, thus realize the level locking of horn 1.
see Fig. 3, described Connection Block 4a is provided with cylinder rod aperture 8, and cylinder rod aperture 8 one end is circumferentially provided with groove 9 and keyway 10, and described cylindrical bar head arranges a plush copper 11, and plush copper 11 is located by connecting with Connection Block 4a to keyway 10 through rotating after groove 9.
See Fig. 2, on described cylindrical bar 4c, cover has and makes cylindrical bar 4c be fastened on Compress Spring 4d on Connection Block 4a.Cylindrical bar has certain precompressed compression to spring when installing, to ensure cylindrical bar not because unmanned plane rocking and get loose when flying.
As shown in Figure 2 and Figure 3, present embodiment realizes the fast assembling-disassembling of folding horn 1.During installation, the connecting bore of mount pad 1a and Connection Block 4a is alignd, cylindrical bar 4c is through the connecting bore of mount pad 1a and Connection Block 4a, the key of cylindrical bar 4c head passes from the groove 9 of Connection Block 4a, again by cylindrical bar 4c left-hand revolution 90 degree, by in the key Snap joint seat 4a groove 10 of cylindrical bar 4c head, provide certain predetermincd tension by spring 4d, by the key of cylindrical bar 4c head tightly Snap joint seat 4a groove 10.
Unloading process is then contrary, firmly pin cylindrical bar 4c, overcome the tensile force of spring 4d, the key of cylindrical bar 4c head is exited from the groove 10 of Connection Block 4b, again cylindrical bar 4c dextrorotation is turn 90 degrees, the key of cylindrical bar 4c head is thoroughly exited from groove 9, thus cylindrical bar 4c can be extracted from the connecting bore of mount pad 1a.Can by mount pad 1a, Connection Block 4a, foot rest 3 all dismounting is complete.
As shown in Figure 4, present embodiment realizes the fast assembling-disassembling of battery.Shell 2d is arranged a groove, for placing battery 2b, battery 2b pushes down by battery cover 2a, and battery cover 2a fastens by snap close 2c again, realizes the firm installation of battery 2b.During dismounting battery 2b, only opened by snap close 2c, battery cover 2a can pull down, and battery 2b can take out.
As shown in Figure 5, when the folding horn 1 of present embodiment realization launches, foot rest 3 is launched together with folding horn 1.Horn 1 is provided with plush copper 12 with the coupling end of cylindrical bar 4c, and foot rest 3 is provided with plush copper 13 with the coupling end of cylindrical bar 4c, and plush copper 12 and plush copper 13 are on same circular path.Be provided with extension spring 14 between horn 1 and foot rest 3, when horn 1 launches, foot rest 3 together launches under the effect of extension spring 14, and plush copper 12 can prop up the plush copper 13 on foot rest 3, and extension spring 14 provides certain pulling force that plush copper 13 is pushed down plush copper 12.Foot rest 3 is avoided to rotate because of gravity and vibration.
The foregoing is only better embodiment of the present utility model; protection domain of the present utility model is not limited with above-mentioned embodiment; in every case those of ordinary skill in the art modify or change according to the equivalence that the utility model institute disclosure is done, and all should include in the protection domain recorded in claims.
Claims (5)
1. a folding unmanned plane, comprise center am rest, the horn be connected with center am rest, the foot rest be connected with center am rest, the screw propeller be located on horn, drive the motor of screw propeller and provide the battery of power supply for motor, it is characterized in that: center am rest is provided with Connection Block, Connection Block is provided with cylindrical bar, and horn and foot rest are flexibly connected with cylindrical bar respectively.
2. folding unmanned plane according to claim 1, is characterized in that: the coupling end of described horn and cylindrical bar is provided with plush copper one, and the coupling end of foot rest and cylindrical bar is provided with plush copper two, and plush copper one and plush copper two are on same circular path; Extension spring is provided with between horn and foot rest; Described Connection Block is provided with a spinner, horn is provided with the plush copper three locked with spinner.
3. folding unmanned plane according to claim 1 and 2, it is characterized in that: described Connection Block is provided with cylinder rod aperture, cylinder rod aperture one end is circumferentially provided with groove and keyway, described cylindrical bar head is provided with plush copper four, and plush copper four is located by connecting with Connection Block to keyway through rotating after groove.
4. folding unmanned plane according to claim 3, is characterized in that: described cylindrical bar is arranged with and makes cylindrical bar be fastened on Compress Spring on Connection Block.
5. folding unmanned plane according to claim 1 and 2, is characterized in that: described center am rest be provided with put battery battery case lid and by snap close fastening for battery case lid.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420608793.0U CN204223178U (en) | 2014-10-21 | 2014-10-21 | A kind of folding unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420608793.0U CN204223178U (en) | 2014-10-21 | 2014-10-21 | A kind of folding unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204223178U true CN204223178U (en) | 2015-03-25 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420608793.0U Expired - Fee Related CN204223178U (en) | 2014-10-21 | 2014-10-21 | A kind of folding unmanned plane |
Country Status (1)
| Country | Link |
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| CN (1) | CN204223178U (en) |
Cited By (17)
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| CN104859837A (en) * | 2015-04-30 | 2015-08-26 | 深圳一电科技有限公司 | Foldable propeller arm assembly and unmanned aerial vehicle |
| CN104986324A (en) * | 2015-07-15 | 2015-10-21 | 广州天翔航空科技有限公司 | Rotary locking mechanism and plant protection unmanned aerial vehicle with the same |
| CN105035318A (en) * | 2015-09-01 | 2015-11-11 | 湖南云顶智能科技有限公司 | Multi-rotor unmanned aerial vehicle |
| CN105539810A (en) * | 2016-02-01 | 2016-05-04 | 张琬彬 | Irregularly-shaped arm folding device for unmanned aerial vehicle |
| CN105599895A (en) * | 2016-01-29 | 2016-05-25 | 浙江智天科技有限公司 | Multi-axis aircraft |
| CN105644769A (en) * | 2016-02-29 | 2016-06-08 | 无锡觅睿恪科技有限公司 | Folding arm assembly for unmanned aerial vehicle |
| CN105857589A (en) * | 2016-04-22 | 2016-08-17 | 平玉兰 | Multi-rotor-wing unmanned aerial vehicle |
| WO2016192021A1 (en) * | 2015-06-01 | 2016-12-08 | SZ DJI Technology Co., Ltd. | Systems and methods for foldable arms |
| CN106915434A (en) * | 2015-12-25 | 2017-07-04 | 北京臻迪机器人有限公司 | The horn of aircraft |
| WO2017143644A1 (en) * | 2016-02-22 | 2017-08-31 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and frame thereof, kit, assembly method, and operation method |
| EP3272652A4 (en) * | 2016-05-27 | 2018-05-23 | Uvify Co., Ltd. | Unmanned aerial vehicle |
| US10093418B2 (en) | 2016-05-27 | 2018-10-09 | Uvify Co., Ltd. | Unmanned aerial vehicle |
| US10118697B2 (en) | 2015-06-25 | 2018-11-06 | Riderless Technologies Inc. | Unmanned aerial vehicle |
| WO2018025122A3 (en) * | 2016-08-01 | 2018-11-08 | Heaney Jonathan Michael | Damage mitigating, modular system for multirotor airframes |
| CN108928470A (en) * | 2018-06-28 | 2018-12-04 | 中国直升机设计研究所 | One kind having cable multi-rotor aerocraft |
| CN113415407A (en) * | 2021-08-10 | 2021-09-21 | 珠海紫燕无人飞行器有限公司 | Collapsible unmanned aerial vehicle |
| US11226064B2 (en) * | 2020-03-13 | 2022-01-18 | Asia Link Co., Ltd. | Foldable display stand |
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2014
- 2014-10-21 CN CN201420608793.0U patent/CN204223178U/en not_active Expired - Fee Related
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| CN104859837B (en) * | 2015-04-30 | 2018-03-20 | 深圳一电航空技术有限公司 | Foldable paddle arm component and unmanned plane |
| CN104859837A (en) * | 2015-04-30 | 2015-08-26 | 深圳一电科技有限公司 | Foldable propeller arm assembly and unmanned aerial vehicle |
| US10202191B2 (en) | 2015-06-01 | 2019-02-12 | SZ DJI Technology Co., Ltd. | Systems and methods for foldable arms |
| US9914537B2 (en) | 2015-06-01 | 2018-03-13 | SZ DJI Technology Co., Ltd | Systems and methods for foldable arms |
| US11091262B2 (en) | 2015-06-01 | 2021-08-17 | SZ DJI Technology Co., Ltd. | Systems and methods for foldable arms |
| US10472063B2 (en) | 2015-06-01 | 2019-11-12 | SZ DJI Technology Co., Ltd. | Systems and methods for foldable arms |
| WO2016192021A1 (en) * | 2015-06-01 | 2016-12-08 | SZ DJI Technology Co., Ltd. | Systems and methods for foldable arms |
| US10118697B2 (en) | 2015-06-25 | 2018-11-06 | Riderless Technologies Inc. | Unmanned aerial vehicle |
| CN104986324A (en) * | 2015-07-15 | 2015-10-21 | 广州天翔航空科技有限公司 | Rotary locking mechanism and plant protection unmanned aerial vehicle with the same |
| CN104986324B (en) * | 2015-07-15 | 2017-03-08 | 广州天翔航空科技有限公司 | A kind of rotary locking mechanism and the plant protection unmanned plane with which |
| CN105035318B (en) * | 2015-09-01 | 2017-03-29 | 湖南云顶智能科技有限公司 | A kind of multi-rotor unmanned aerial vehicle |
| CN105035318A (en) * | 2015-09-01 | 2015-11-11 | 湖南云顶智能科技有限公司 | Multi-rotor unmanned aerial vehicle |
| CN106915434A (en) * | 2015-12-25 | 2017-07-04 | 北京臻迪机器人有限公司 | The horn of aircraft |
| CN105599895A (en) * | 2016-01-29 | 2016-05-25 | 浙江智天科技有限公司 | Multi-axis aircraft |
| CN105539810A (en) * | 2016-02-01 | 2016-05-04 | 张琬彬 | Irregularly-shaped arm folding device for unmanned aerial vehicle |
| CN105539810B (en) * | 2016-02-01 | 2018-04-17 | 深圳市盛禾农业科技有限公司 | A kind of unmanned plane abnormity horn folding device |
| WO2017143644A1 (en) * | 2016-02-22 | 2017-08-31 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and frame thereof, kit, assembly method, and operation method |
| US11427319B2 (en) | 2016-02-22 | 2022-08-30 | SZ DJI Technology Co., Ltd. | Foldable multi-rotor aerial vehicle |
| US10625855B2 (en) | 2016-02-22 | 2020-04-21 | SZ DJI Technology Co., Ltd. | Foldable multi-rotor aerial vehicle |
| CN112937836A (en) * | 2016-02-22 | 2021-06-11 | 深圳市大疆创新科技有限公司 | Use unmanned aerial vehicle of frame |
| CN105644769A (en) * | 2016-02-29 | 2016-06-08 | 无锡觅睿恪科技有限公司 | Folding arm assembly for unmanned aerial vehicle |
| CN105857589B (en) * | 2016-04-22 | 2018-05-11 | 安徽天鹰兄弟无人机科技创新有限公司 | A kind of multi-rotor unmanned aerial vehicle |
| CN105857589A (en) * | 2016-04-22 | 2016-08-17 | 平玉兰 | Multi-rotor-wing unmanned aerial vehicle |
| EP3272652A4 (en) * | 2016-05-27 | 2018-05-23 | Uvify Co., Ltd. | Unmanned aerial vehicle |
| US10093418B2 (en) | 2016-05-27 | 2018-10-09 | Uvify Co., Ltd. | Unmanned aerial vehicle |
| WO2018025122A3 (en) * | 2016-08-01 | 2018-11-08 | Heaney Jonathan Michael | Damage mitigating, modular system for multirotor airframes |
| CN108928470A (en) * | 2018-06-28 | 2018-12-04 | 中国直升机设计研究所 | One kind having cable multi-rotor aerocraft |
| US11226064B2 (en) * | 2020-03-13 | 2022-01-18 | Asia Link Co., Ltd. | Foldable display stand |
| CN113415407A (en) * | 2021-08-10 | 2021-09-21 | 珠海紫燕无人飞行器有限公司 | Collapsible unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C53 | Correction of patent of invention or patent application | ||
| CB03 | Change of inventor or designer information |
Inventor after: Cao Cao Inventor after: Wang Chengbo Inventor after: He Yong Inventor before: Yang Debin |
|
| COR | Change of bibliographic data |
Free format text: CORRECT: INVENTOR; FROM: YANG DEBIN TO: CAO CAO WANG CHENGBO HE YONG |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160429 Address after: 16 Wuhan, Jianghan District, Xinhua Road, No. 29 building, court building, No. 430022, Patentee after: Hubei Tianyu cruise Polytron Technologies Inc. Address before: 430070 Hubei Province, Wuhan city Wuchang District Shipai Ling Road No. 118 Patentee before: HUBEI MECHANICAL AND ELECTRICAL RESEARCH AND DESIGN INSTITUTE CO.,LTD. |
|
| TR01 | Transfer of patent right |
Effective date of registration: 20170414 Address after: 18 Wuhan, Jianghan District, Xinhua Road, No. 29 building, court building, No. 430000, Patentee after: BEIJING TODAY INNOVATION TECHNOLOGY Co.,Ltd. Address before: 16 Wuhan, Jianghan District, Xinhua Road, No. 29 building, court building, No. 430022, Patentee before: Hubei Tianyu cruise Polytron Technologies Inc. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150325 Termination date: 20211021 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |