CN205376602U - Unmanned aerial vehicle's external battery securing device - Google Patents
Unmanned aerial vehicle's external battery securing device Download PDFInfo
- Publication number
- CN205376602U CN205376602U CN201620049438.3U CN201620049438U CN205376602U CN 205376602 U CN205376602 U CN 205376602U CN 201620049438 U CN201620049438 U CN 201620049438U CN 205376602 U CN205376602 U CN 205376602U
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- China
- Prior art keywords
- battery
- backing plate
- fixed block
- frame
- battery frame
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- 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 - Fee Related
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- 210000005056 cell body Anatomy 0.000 claims abstract description 20
- 210000004027 cell Anatomy 0.000 claims description 17
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- 239000004917 carbon fiber Substances 0.000 claims description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 3
- 238000009434 installation Methods 0.000 abstract description 5
- 238000012545 processing Methods 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 5
- 238000013461 design Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 238000011161 development Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000012857 repacking Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 238000012549 training Methods 0.000 description 1
Classifications
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Battery Mounting, Suspending (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle's external battery securing device, including bottom backing plate, top backing plate etc, a battery frame with the 2nd battery frame all has two, the top backing plate with the top backing plate is through two a battery frame and two the 2nd battery frame connects as an organic wholely, two a battery frame and two the 2nd battery frame symmetry respectively sets up two all be equipped with the panel fixed block on the battery frame, the installation of bottom backing plate the 2nd battery frame's one end is equipped with spacing fixed cell body, the bottom of battery quick detach backing plate be equipped with with the dop that spacing fixed cell body corresponds, the one end of battery quick detach board is passed through the panel fixed block is fixed, the other end of battery quick detach board passes through the dop with spacing fixed cell body is fixed. The utility model discloses used part structure is simple, and easily processing, and battery loading and unloading possess quick detach characteristic, convenient to use.
Description
Technical field
This utility model relates to unmanned plane auxiliary device field, particularly relates to the fixing device of externally hanging battery of a kind of unmanned plane.
Background technology
Progress along with automated control technology, many rotor wing unmanned aerial vehicles common on the market at present have become very easy left-hand seat, ordinary people only need to after simply training, just can handle it and realize smooth flight in simple environment, this has expanded the use scope of many rotor wing unmanned aerial vehicles to a certain extent, makes increasing people start to consider many rotor wing unmanned aerial vehicles are applied to all kinds of field.The miniaturization of sensor technology has been pushed further into this development especially, and by various sensor miniaturization, then carry becomes a main trend of present Development of UAV on many rotor wing unmanned aerial vehicles.
The fuselage of existing unmanned plane is smooth, it does not have three-dimension curved surface, and has reserved more screw and data transmission socket, facilitates user to carry the module oneself designed and produced and performs different tasks.Unmanned plane is to provide energy to carry out operating by battery mounted thereto, but the capacity of matched battery is less, it is impossible to support unmanned plane long-play.Existing four rotor wing unmanned aerial vehicles adopt two pieces of batteries to be powered, and one piece of battery is connected with flying control, it is provided that the electricity of this battery, voltage, life information, and powers for each control chip on fuselage and motor；And another block battery is only motor and powers, four rotor wing unmanned aerial vehicle flying platforms are after installing original-pack accessory, and the actual flying time using two pieces of batteries is shorter, when, after other equipment plug-in, its flight time can shorten further；Furthermore, if need to install bigger plug-in device on the platform, it is necessary to its power is replaced, this can cause its actual flying time to be difficult to meet actually used demand；Additionally, use two pieces of battery parallel power supplies, it is easy to one piece of battery situation to the charging of another block battery occurs, affects battery life, cause potential safety hazard during flight.
Therefore, how providing a kind of fixing device simple, easily detachable, it is possible to be fixed on fuselage by model airplane battery, facilitating battery repacking use is problem demanding prompt solution.
Utility model content
In view of this, this utility model provides the fixing device of externally hanging battery of a kind of unmanned plane, and the repacking facilitating battery uses, and has simple in construction, easily detachable feature.
This utility model solves the problems referred to above by techniques below means:
nullExternally hanging battery of the present utility model fixes device，It is characterized in that: include backing plate at bottom、Top backing plate、First battery frame、Second battery frame、Cell panel fixed block、Quick-detachable battery backing plate、Dop、Spacing fixing cell body，Described first battery frame and described second battery frame all have two，Described top backing plate and described top backing plate are connected as one by two described first battery frames and two described second battery frames，Two described first battery frames and two described second battery frames are respectively symmetrically setting，Two described first battery frames are equipped with cell panel fixed block，One end installing described second battery frame of described backing plate at bottom is provided with spacing fixing cell body，The bottom of described quick-detachable battery backing plate is provided with the dop corresponding with described spacing fixing cell body，One end of described quick-detachable battery plate is fixed by described cell panel fixed block，The other end of described quick-detachable battery plate is fixed by described dop and described spacing fixing cell body.
Further, described cell panel fixed block includes the first fixed block and the second fixed block that are fixed together, two the described semi-circular recesses offering semi-circular recesses, described first fixed block and described second fixed block on described first fixed block and described second fixed block respectively form the circular port being available for described first battery frame traverse.
Further, described backing plate at bottom and described top backing plate concretely carbon fiber board, described top backing plate offers the notch for installing avoidance module or sensor.
Further, described first battery frame and described second battery frame concretely aluminium alloy frame body.
Further, described quick-detachable battery backing plate offers the notch for installing magic strap or bundling belt.
Externally hanging battery of the present utility model fixes device, it is arranged on the original position installing secondary cell of unmanned plane, make the monoblock type Large Copacity power supply that four rotor wing unmanned aerial vehicles can change the outfit more reliable, battery after replacing and described quick-detachable battery backing plate are fixed, it is then inserted in the space reserved, described dop is snapped in described spacing fixing cell body and battery and fuselage can be fixed, increase service time of battery, compare original design, this utility model guarantees that this unmanned plane has had wider range of selection on battery selects, this machine is facilitated to carry out power-refitting, increase take-off weight, promote cruising time, this machine is made to be applicable to more association area；And design of part used by this utility model is simple, it is easy to processing, and battery handling possess Quick Release characteristic, easy to use, can in lift fuselage bulk strength and rigidity after installation.
Accompanying drawing explanation
Fig. 1 is the structural representation one of the fixing device of externally hanging battery of the present utility model；
Fig. 2 is the structural representation two of the fixing device of externally hanging battery of the present utility model.
As shown in Figure 1, Figure 2, backing plate at bottom-1, top backing plate the-2, first battery frame-3, the second battery frame-4, cell panel fixed block the-5, first fixed block-51, the second fixed block-52, quick-detachable battery backing plate-6, dop-7, spacing fixing cell body-8.
Detailed description of the invention
In description of the present utility model, it will be appreciated that, orientation or the position relationship of the instruction such as term " " center ", " on ", D score, "front", "rear", "left", "right", " vertically ", " level ", " top ", " end ", " interior ", " outward " be based on orientation shown in the drawings or position relationship; be for only for ease of description this utility model and simplifying and describe; rather than instruction or imply indication device or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that to restriction of the present utility model.
Term " first ", " second " only for descriptive purposes, and it is not intended that instruction or hint relative importance or the implicit quantity indicating indicated technical characteristic.Thus, define " first ", the feature of " second " can express or implicitly include one or more these features.In description of the present utility model, except as otherwise noted, " multiple " are meant that two or more.
nullBelow with reference to accompanying drawing, this utility model is described in detail，As shown in Figure 1 to Figure 2: the externally hanging battery described in the present embodiment fixes device，Including backing plate at bottom 1、Top backing plate 2、First battery frame 3、Second battery frame 4、Cell panel fixed block 5、Quick-detachable battery backing plate 6、Dop 7、Spacing fixing cell body 8，Described first battery frame 3 and described second battery frame 4 all have two，Described top backing plate 2 and described top backing plate 2 are connected as one by two described first battery frames 3 and two described second battery frames 4，Two described first battery frames 3 and two described second battery frames 4 are respectively symmetrically setting，Two described first battery frames 3 are equipped with cell panel fixed block 5，One end installing described second battery frame 4 of described backing plate at bottom 1 is provided with spacing fixing cell body 8，The bottom of described quick-detachable battery backing plate 6 is provided with the dop 7 corresponding with described spacing fixing cell body 8，One end of described quick-detachable battery plate is fixed by described cell panel fixed block 5，The other end of described quick-detachable battery plate is fixed with described spacing fixing cell body 8 by described dop 7.
nullExternally hanging battery described in the present embodiment fixes device，During assembling，First described first battery frame 3 and described second battery frame 4 are installed in the corresponding position, upper end of described backing plate at bottom 1，Wherein，Described first battery frame 3 is arranged close to one end of head，Described second battery frame 4 is arranged close to one end of tail，Then two described cell panel fixed blocks 5 are separately mounted on two described first battery frames 3，Make it need to guarantee that described quick-detachable battery backing plate 6 can normally insert in short transverse，Described top backing plate 2 is arranged on the upper end of described first battery frame 3 and described second battery frame 4 again，Constitute battery frame，Then described dop 7 is arranged on the bottom of described quick-detachable battery backing plate 6，The position that to be arranged on backing plate at bottom 1 by described spacing fixing cell body 8 corresponding with described dop 7，Battery utilize magic strap or bundling belt and quick-detachable battery backing plate 6 bundle again、Paste after connecting，Insert in described battery frame，Finally the dop 7 of described quick-detachable battery backing plate 6 is blocked with described spacing fixing cell body 8，Complete the installation of battery，Can use after battery lead is rationally connected.
Externally hanging battery described in the present embodiment fixes device, it is arranged on the original position installing secondary cell of unmanned plane, make the monoblock type Large Copacity power supply that four rotor wing unmanned aerial vehicles can change the outfit more reliable, battery after replacing and described quick-detachable battery backing plate 6 are fixed, it is then inserted in the space reserved, described dop 7 is snapped in described spacing fixing cell body 8 and battery and fuselage can be fixed, increase service time of battery, compare original design, this utility model guarantees that this unmanned plane has had wider range of selection on battery selects, this machine is facilitated to carry out power-refitting, increase take-off weight, promote cruising time, this machine is made to be applicable to more association area；And design of part used by this utility model is simple, it is easy to processing, and battery handling possess Quick Release characteristic, easy to use, can in lift fuselage bulk strength and rigidity after installation.
For the ease of installing and using, further improvement as technique scheme, described cell panel fixed block 5 includes the first fixed block 51 and the second fixed block 52 being fixed together, two the described semi-circular recesses offering semi-circular recesses (not shown), described first fixed block 51 and described second fixed block 52 on described first fixed block 51 and described second fixed block 52 respectively form the circular port being available for described first battery frame 3 traverse.
Further improvement as technique scheme, described backing plate at bottom 1 and described top backing plate 2 concretely carbon fiber board, described top backing plate 2 offers the notch (not shown) for installing avoidance module or sensor, the described backing plate at bottom 1 of carbon fibre materials and the feature that described top backing plate 2 has light weight, intensity is high, improve the overall intensity of fuselage and rigidity further, described notch can provide installation site for the avoidance module of unmanned plane or other sensor assemblies, uses more convenient.
As the further improvement of technique scheme, described first battery frame 3 and described second battery frame 4 concretely aluminium alloy frame body, improve the overall intensity of fuselage and rigidity further.
Fix with described quick-detachable battery backing plate 6 for the ease of battery, as the further improvement of technique scheme, described quick-detachable battery backing plate 6 offers the notch (not shown) for installing magic strap or bundling belt.
Wherein, the externally hanging battery described in the present embodiment fixes device, and the material of its each parts can be modified as required, and this utility model is not specifically limited；
Thickness and the position of opening of described backing plate at bottom 1, described top backing plate 2 and described quick-detachable battery backing plate 6 can be designed as required, and this utility model is not specifically limited；
Described first battery frame 3 and the height of described second battery frame 4, the width of described dop 7, described spacing fixing cell body 8 length can be designed as required, this utility model is not specifically limited.
What finally illustrate is, above example is only in order to illustrate the technical solution of the utility model and unrestricted, although this utility model being described in detail with reference to preferred embodiment, it will be understood by those within the art that, the technical solution of the utility model can be modified or equivalent replacement, without deviating from objective and the scope of technical solutions of the utility model, it all should be encompassed in the middle of right of the present utility model.
Claims (5)
- null1. the fixing device of the externally hanging battery of a unmanned plane，It is characterized in that: include backing plate at bottom、Top backing plate、First battery frame、Second battery frame、Cell panel fixed block、Quick-detachable battery backing plate、Dop、Spacing fixing cell body，Described first battery frame and described second battery frame all have two，Described top backing plate and described top backing plate are connected as one by two described first battery frames and two described second battery frames，Two described first battery frames and two described second battery frames are respectively symmetrically setting，Two described first battery frames are equipped with cell panel fixed block，One end installing described second battery frame of described backing plate at bottom is provided with spacing fixing cell body，The bottom of described quick-detachable battery backing plate is provided with the dop corresponding with described spacing fixing cell body，One end of described quick-detachable battery plate is fixed by described cell panel fixed block，The other end of described quick-detachable battery plate is fixed by described dop and described spacing fixing cell body.
- 2. the fixing device of the externally hanging battery of a kind of unmanned plane according to claim 1, it is characterized in that: described cell panel fixed block includes the first fixed block and the second fixed block that are fixed together, two the described semi-circular recesses offering semi-circular recesses, described first fixed block and described second fixed block on described first fixed block and described second fixed block respectively form the circular port being available for described first battery frame traverse.
- 3. the fixing device of the externally hanging battery of a kind of unmanned plane according to claim 1, it is characterised in that: described backing plate at bottom and described top backing plate concretely carbon fiber board, described top backing plate offers the notch for installing avoidance module or sensor.
- 4. the fixing device of the externally hanging battery of a kind of unmanned plane according to claim 1, it is characterised in that: described first battery frame and described second battery frame concretely aluminium alloy frame body.
- 5. the fixing device of the externally hanging battery of a kind of unmanned plane according to claim 1, it is characterised in that: described quick-detachable battery backing plate offers the notch for installing magic strap or bundling belt.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620049438.3U CN205376602U (en) | 2016-01-19 | 2016-01-19 | Unmanned aerial vehicle's external battery securing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620049438.3U CN205376602U (en) | 2016-01-19 | 2016-01-19 | Unmanned aerial vehicle's external battery securing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205376602U true CN205376602U (en) | 2016-07-06 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620049438.3U Expired - Fee Related CN205376602U (en) | 2016-01-19 | 2016-01-19 | Unmanned aerial vehicle's external battery securing device |
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| Country | Link |
|---|---|
| CN (1) | CN205376602U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106114879A (en) * | 2016-08-01 | 2016-11-16 | 武汉拓普新科无人机科技有限公司 | A kind of unmanned plane carry Quick-disassembling mechanism |
| CN106376208A (en) * | 2016-11-29 | 2017-02-01 | 北京博瑞空间科技发展有限公司 | Unmanned aerial vehicle with rack reinforced structure |
-
2016
- 2016-01-19 CN CN201620049438.3U patent/CN205376602U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106114879A (en) * | 2016-08-01 | 2016-11-16 | 武汉拓普新科无人机科技有限公司 | A kind of unmanned plane carry Quick-disassembling mechanism |
| CN106114879B (en) * | 2016-08-01 | 2018-01-19 | 武汉拓普新科无人机科技有限公司 | A kind of unmanned plane carry Quick-disassembling mechanism |
| CN106376208A (en) * | 2016-11-29 | 2017-02-01 | 北京博瑞空间科技发展有限公司 | Unmanned aerial vehicle with rack reinforced structure |
| CN106376208B (en) * | 2016-11-29 | 2021-12-03 | 北京博瑞空间科技发展有限公司 | Unmanned aerial vehicle with frame additional strengthening |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160706 |