CN205633054U - Fastening structure of trading with even load is torn fast open to multiaxis unmanned aerial vehicle horn - Google Patents
Fastening structure of trading with even load is torn fast open to multiaxis unmanned aerial vehicle horn Download PDFInfo
- Publication number
- CN205633054U CN205633054U CN201620380055.4U CN201620380055U CN205633054U CN 205633054 U CN205633054 U CN 205633054U CN 201620380055 U CN201620380055 U CN 201620380055U CN 205633054 U CN205633054 U CN 205633054U
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- horn
- unmanned plane
- quick release
- union joint
- fastening structure
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- 238000004891 communication Methods 0.000 claims description 3
- 230000008901 benefit Effects 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 7
- 230000007812 deficiency Effects 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 230000006872 improvement Effects 0.000 description 5
- 241000239290 Araneae Species 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/70—Constructional aspects of the UAV body
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/50—Transport or storage specially adapted for UAVs the UAVs being disassembled
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- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connections Effected By Soldering, Adhesion, Or Permanent Deformation (AREA)
- Pivots And Pivotal Connections (AREA)
Abstract
The utility model discloses a fastening structure of trading with even load is torn fast open to multiaxis unmanned aerial vehicle horn, the unmanned aerial vehicle main part is included and the horn subassembly can be dismantled, but the unmanned aerial vehicle main part is pull -plug type electric connection with dismantling the horn subassembly, is provided with the frame connector in the unmanned aerial vehicle main part, can dismantle is provided with the cooperation on the horn subassembly the horn connector of frame connector, the frame connector can with the horn connector detachable be connected and with the unmanned aerial vehicle main part with can dismantle the horn subassembly and connect into to a whole. This kind of fastening structure of trading with even load is torn fast open to multiaxis unmanned aerial vehicle horn has and dismantles high, the effective advantage that the existing product did not possess such as the volume can be reduced of simple to operate, joint strength.
Description
Technical field
This utility model relates to the mounting structure of a kind of unmanned plane application, and a kind of multiaxis unmanned plane horn quickly changes and the fastening structure of uniform load.
Background technology
In recent years, along with the popularization of unmanned plane application, application is constantly expanded, and different industries different field is different to unmanned plane dimensional requirement.In order to save cost of transportation, and packing cost, the detachability of unmanned plane and convenient for collecting become the measurement whether excellent important indicator of unmanned plane frame for movement.The most also the structure of some convenient dismountings, such as detachable horn, collapsible horn, detachable undercarriage etc. is occurred in that for this.Because determining that the topmost parts of unmanned plane size are the length of horn.So the structure break-through point that the detachability of horn Cheng Liaoge unmanned plane manufacturer again is pursued.
Although occurring in that such as thread bush fastening-type dismounting, the collapsible horn of hinge type in the market, but but not as people's will in convenience and robustness, the such as assembling of threaded cap fastening horn needs in advance by Screw assembly to horn bar, twisting thread bush multi-turn can be by relatively time-consuming for horn fix in position, and thread bush is limited by outward appearance and size it cannot be guaranteed that big twisting resistance, fastening effect is the best；Hinge type folds horn and can only conveniently fold, lack can not quick-detach soon, can not significantly reduce transportation volume.
In a word, there is the technological deficiencies such as dismounting is inconvenient, it is not enough to bear torsion, connect poor effect, the volume of product can not effectively reduce in existing product.
In view of this, the purpose of this utility model is to provide a kind of new technical scheme to solve existing technological deficiency.
Utility model content
In order to overcome the deficiencies in the prior art, this utility model provides a kind of multiaxis unmanned plane horn quickly to change and the fastening structure of uniform load, solves that the dismounting that existing unmanned plane exists is convenient not, disassembly and assembly structure bears the technological deficiencies such as torsion deficiency, volume-diminished poor effect.
This utility model solves its technical problem and be the technical scheme is that
A kind of multiaxis unmanned plane horn quickly changes and the fastening structure of uniform load, including unmanned plane main body and detachable horn assembly, described unmanned plane main body and detachable horn assembly are that plug type is electrically connected with, frame union joint it is provided with in unmanned plane main body, being provided with the horn union joint coordinating described frame union joint on described detachable horn assembly, described frame union joint detachable with horn union joint can be connected and unmanned plane main body and detachable horn assembly are connected to become an entirety.
Improvement as technique scheme, described frame union joint includes adapter body and quick dismountable cover, described quick dismountable cover is hinged in adapter body by rotating shaft, Quick Release stopper it is provided with on quick dismountable cover, being provided with the fastening recess coordinating described Quick Release stopper on described horn joint, described Quick Release stopper can buckle and buckle on recess.
Further improvement as technique scheme, described Quick Release stopper is a semiclosed U-shaped part, Quick Release stopper two ends are provided with hinged end, described quick dismountable cover medium position is provided with the hinge hole installing Quick Release stopper two hinged end, the hinged end of described Quick Release stopper inserts described hinge hole, and described Quick Release stopper can rotate around hinge hole.
As the further improvement of technique scheme, each frame union joint described is respectively provided with two groups of quick dismountable covers, rotating shaft and Quick Release stopper, and described horn joint arranges two groups of fastening recess of correspondence.
Further improvement as technique scheme, described frame union joint center is electrical slot, described horn union joint center is the plug coordinating described electrical slot, and described plug can be inserted in electrical slot and realizes unmanned plane main body and detachable horn assembly electrical communication.
As the further improvement of technique scheme, described detachable horn assembly is provided with motor and the propeller by described motor-driven rotation.
The beneficial effects of the utility model are: this utility model provides a kind of multiaxis unmanned plane horn and quickly changes and the fastening structure of uniform load, this kind of retention mechanism is detachably connected by frame joint and horn joint, have remove and install conveniently, bearing torque bearing capacity is high, the advantage that can effectively reduce whole unmanned plane volume, practical and convenient, Consumer's Experience is good.
Accompanying drawing explanation
With embodiment, this utility model is further illustrated below in conjunction with the accompanying drawings.
Fig. 1 is structure broken away view of the present utility model；
Fig. 2 is that this utility model is in the view installing detachable horn component mounting process；
Fig. 3 is the partial approach figure of A in Fig. 2；
Fig. 4 is this utility model structural representation after detachable horn assembly installation；
Fig. 5 is the partial enlarged drawing in Fig. 4.
Detailed description of the invention
Below with reference to embodiment and accompanying drawing, the technique effect of design of the present utility model, concrete structure and generation is clearly and completely described, to be completely understood by the purpose of this utility model, feature and effect.Obviously; described embodiment is a part of embodiment of the present utility model rather than whole embodiment, based on embodiment of the present utility model; other embodiments that those skilled in the art is obtained on the premise of not paying creative work, belong to the scope of this utility model protection.It addition, all connection/annexations related in patent, the most singly refer to that component directly connects, and refer to couple auxiliary according to being embodied as situation by adding or reducing, form more excellent draw bail.Each technical characteristic in this utility model creation, can be with combination of interactions on the premise of the most conflicting conflict, with reference to Fig. 1, Fig. 2,
A kind of multiaxis unmanned plane horn quickly changes and the fastening structure of uniform load, including unmanned plane main body 1 and detachable horn assembly 2, described unmanned plane main body 1 is electrically connected with for plug type with detachable horn assembly 2, frame union joint 3 it is provided with in unmanned plane main body 1, being provided with the horn union joint 4 coordinating described frame union joint 3 on described detachable horn assembly 2, described frame union joint 3 detachable with horn union joint 4 can be connected and unmanned plane main body 1 and detachable horn assembly 2 are connected to become an entirety.
Preferably, described frame union joint 3 includes adapter body 31 and quick dismountable cover 32, described quick dismountable cover 32 is hinged in adapter body 31 by rotating shaft 33, Quick Release stopper 34 it is provided with on quick dismountable cover 32, being provided with the fastening recess 41 coordinating described Quick Release stopper 34 on described horn joint 4, described Quick Release stopper 34 can buckle and buckle on recess 41.
Preferably, described Quick Release stopper 34 is a semiclosed U-shaped part, Quick Release stopper 34 two ends are provided with hinged end, described quick dismountable cover 32 medium position is provided with the hinge hole installing 34 liang of hinged ends of Quick Release stopper, the hinged end of described Quick Release stopper 34 inserts described hinge hole, and described Quick Release stopper 34 can rotate around hinge hole.
Preferably, each frame union joint 3 described is respectively provided with two groups of quick dismountable covers 32, rotating shaft 33 and Quick Release stopper 34, and described horn joint 4 arranges two groups of fastening recess 41 of correspondence.
Preferably, described frame union joint 3 center is electrical slot, and described horn union joint 4 center is the plug coordinating described electrical slot, and described plug can be inserted in electrical slot and realizes unmanned plane main body 1 and detachable horn assembly 2 electrical communication.
Preferably, described detachable horn assembly 2 it is provided with motor 5 and is driven the propeller 6 of rotation by described motor 5.
In use, the plug on horn joint 4 on described detachable horn assembly 2 is inserted the electrical slot on unmanned plane main body 1 upper spider joint 3, it is achieved the motor 5 on detachable horn assembly 3 electrically conducts with unmanned plane main body 1；Further Quick Release stopper 34 is rotated and snaps onto on the fastening recess 41 on horn joint 4, then pull quick dismountable cover 32 and make Quick Release stopper 34 buckle on horn joint 4, finally make whole detachable horn assembly 2 achieve a fixed connection with unmanned plane main body 1.
Combinations of the above structure realizes unmanned plane main body 1 and detachable horn assembly 2 Quick Release, fast-assembling function, and both attachment structures can provide enough bonding strengths, has the advantages such as resistance to torsion is good；It addition, by after fast quick-detach, whole unmanned plane can effectively reduce and be taken up space, convenient transport, storage etc..
It is above preferable enforcement of the present utility model is illustrated, but this utility model is created and is not limited to described embodiment, those of ordinary skill in the art it may also be made that all equivalent variations or replacement on the premise of this utility model spirit, and deformation or the replacement of these equivalents are all contained in the application claim limited range.
Claims (6)
1. a multiaxis unmanned plane horn quickly changes and the fastening structure of uniform load, it is characterized in that: include unmanned plane main body (1) and detachable horn assembly (2), described unmanned plane main body (1) and detachable horn assembly (2) are that plug type is electrically connected with, frame union joint (3) it is provided with in unmanned plane main body (1), the horn union joint (4) coordinating described frame union joint (3) it is provided with on described detachable horn assembly (2), described frame union joint (3) detachable with horn union joint (4) can be connected and unmanned plane main body (1) and detachable horn assembly (2) are connected to become an entirety.
A kind of multiaxis unmanned plane horn the most according to claim 1 quickly changes and the fastening structure of uniform load, it is characterized in that: described frame union joint (3) includes adapter body (31) and quick dismountable cover (32), described quick dismountable cover (32) is hinged in adapter body (31) by rotating shaft (33), Quick Release stopper (34) it is provided with on quick dismountable cover (32), being provided with the fastening recess (41) coordinating described Quick Release stopper (34) on described horn joint (4), described Quick Release stopper (34) can buckle and buckle on recess (41).
A kind of multiaxis unmanned plane horn the most according to claim 2 quickly changes and the fastening structure of uniform load, it is characterized in that: described Quick Release stopper (34) is a semiclosed U-shaped part, Quick Release stopper (34) two ends are provided with hinged end, described quick dismountable cover (32) medium position is provided with the hinge hole installing Quick Release stopper (34) two hinged end, the hinged end of described Quick Release stopper (34) inserts described hinge hole, and described Quick Release stopper (34) can rotate around hinge hole.
A kind of multiaxis unmanned plane horn the most according to claim 3 quickly changes and the fastening structure of uniform load, it is characterized in that: each frame union joint (3) described is respectively provided with two groups of quick dismountable covers (32), rotating shaft (33) and Quick Release stopper (34), described horn joint (4) arranges two groups of fastenings recess (41) of correspondence.
A kind of multiaxis unmanned plane horn the most according to claim 4 quickly changes and the fastening structure of uniform load, it is characterized in that: described frame union joint (3) center is electrical slot, described horn union joint (4) center is the plug coordinating described electrical slot, and described plug can be inserted in electrical slot and realizes unmanned plane main body (1) and detachable horn assembly (2) electrical communication.
A kind of multiaxis unmanned plane horn the most according to claim 5 quickly changes and the fastening structure of uniform load, it is characterised in that: it is provided with motor (5) on described detachable horn assembly (2) and is driven the propeller (6) rotated by described motor (5).
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620380055.4U CN205633054U (en) | 2016-04-28 | 2016-04-28 | Fastening structure of trading with even load is torn fast open to multiaxis unmanned aerial vehicle horn |
| PCT/CN2016/085808 WO2017185495A1 (en) | 2016-04-28 | 2016-06-15 | Fastening structure for fast dismounting and replacement of arm of multi-shaft unmanned aerial vehicle and for uniform force bearing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620380055.4U CN205633054U (en) | 2016-04-28 | 2016-04-28 | Fastening structure of trading with even load is torn fast open to multiaxis unmanned aerial vehicle horn |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205633054U true CN205633054U (en) | 2016-10-12 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620380055.4U Active CN205633054U (en) | 2016-04-28 | 2016-04-28 | Fastening structure of trading with even load is torn fast open to multiaxis unmanned aerial vehicle horn |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN205633054U (en) |
| WO (1) | WO2017185495A1 (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017185495A1 (en) * | 2016-04-28 | 2017-11-02 | 深圳市龙云创新航空科技有限公司 | Fastening structure for fast dismounting and replacement of arm of multi-shaft unmanned aerial vehicle and for uniform force bearing |
| CN108016601A (en) * | 2017-12-12 | 2018-05-11 | 余姚市荣事特电子有限公司 | A kind of dismountable unmanned plane of horn |
| WO2018107416A1 (en) * | 2016-12-15 | 2018-06-21 | XDynamics Limited | A manually operable mechanism for connecting parts of an unmanned aerial vehicle (uav) |
| WO2018113480A1 (en) * | 2016-12-21 | 2018-06-28 | 深圳市道通智能航空技术有限公司 | Detachable arm assembly and aircraft |
| WO2020119248A1 (en) * | 2018-12-13 | 2020-06-18 | 广州极飞科技有限公司 | Frame for aircraft and aircraft |
| CN112455648A (en) * | 2019-09-09 | 2021-03-09 | 苏州臻迪智能科技有限公司 | Unmanned aerial vehicle |
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| CN107672783B (en) * | 2017-11-08 | 2023-11-07 | 沈阳旋飞航空技术有限公司 | Cantilever quick-dismantling structure of oil-driven unmanned aerial vehicle |
| DE102019128202B4 (en) | 2019-10-18 | 2023-12-07 | Emqopter GmbH | System and method for ad-hoc configuration of a modular multicopter |
| CN114571438A (en) * | 2020-12-01 | 2022-06-03 | 苏州艾利特机器人有限公司 | Robot with body quick change function |
| CN112896497B (en) * | 2021-03-23 | 2023-03-28 | 珠海紫燕无人飞行器有限公司 | Unmanned helicopter |
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Family Cites Families (5)
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| DE102009001759B4 (en) * | 2009-03-23 | 2013-02-21 | Gregor Schnoell | locking system |
| CN204137319U (en) * | 2014-09-29 | 2015-02-04 | 深圳市大疆创新科技有限公司 | Unmanned vehicle and horn holding device and clamping device |
| CN204871580U (en) * | 2015-07-15 | 2015-12-16 | 零度智控（北京）智能科技有限公司 | Unmanned vehicles horn adjusting device |
| CN105523167A (en) * | 2016-02-01 | 2016-04-27 | 张琬彬 | Folding structure of unmanned aerial vehicle |
| CN205633054U (en) * | 2016-04-28 | 2016-10-12 | 深圳市龙云创新航空科技有限公司 | Fastening structure of trading with even load is torn fast open to multiaxis unmanned aerial vehicle horn |
-
2016
- 2016-04-28 CN CN201620380055.4U patent/CN205633054U/en active Active
- 2016-06-15 WO PCT/CN2016/085808 patent/WO2017185495A1/en active Application Filing
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017185495A1 (en) * | 2016-04-28 | 2017-11-02 | 深圳市龙云创新航空科技有限公司 | Fastening structure for fast dismounting and replacement of arm of multi-shaft unmanned aerial vehicle and for uniform force bearing |
| WO2018107416A1 (en) * | 2016-12-15 | 2018-06-21 | XDynamics Limited | A manually operable mechanism for connecting parts of an unmanned aerial vehicle (uav) |
| WO2018113480A1 (en) * | 2016-12-21 | 2018-06-28 | 深圳市道通智能航空技术有限公司 | Detachable arm assembly and aircraft |
| CN108016601A (en) * | 2017-12-12 | 2018-05-11 | 余姚市荣事特电子有限公司 | A kind of dismountable unmanned plane of horn |
| CN108016601B (en) * | 2017-12-12 | 2020-11-27 | 余姚市恒正金属制品有限公司 | Unmanned aerial vehicle with detachable arm |
| WO2020119248A1 (en) * | 2018-12-13 | 2020-06-18 | 广州极飞科技有限公司 | Frame for aircraft and aircraft |
| JP2021517092A (en) * | 2018-12-13 | 2021-07-15 | ▲広▼州▲極飛▼科技有限公司Ｇｕａｎｇｚｈｏｕ Ｘａｉｒｃｒａｆｔ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．， Ｌｔｄ． | Aircraft frame and air vehicle |
| AU2019399622B2 (en) * | 2018-12-13 | 2022-06-02 | Guangzhou Xaircraft Technology Co., Ltd. | Frame for aircraft and aircraft |
| JP7104801B2 (en) | 2018-12-13 | 2022-07-21 | 広州極飛科技股▲ふん▼有限公司 | Aircraft frame and air vehicle |
| CN112455648A (en) * | 2019-09-09 | 2021-03-09 | 苏州臻迪智能科技有限公司 | Unmanned aerial vehicle |
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| Publication number | Publication date |
|---|---|
| WO2017185495A1 (en) | 2017-11-02 |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |