CN203601572U - Unmanned aerial vehicle battery and aerial vehicle with unmanned aerial vehicle battery - Google Patents
Unmanned aerial vehicle battery and aerial vehicle with unmanned aerial vehicle battery Download PDFInfo
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- CN203601572U CN203601572U CN201320701225.0U CN201320701225U CN203601572U CN 203601572 U CN203601572 U CN 203601572U CN 201320701225 U CN201320701225 U CN 201320701225U CN 203601572 U CN203601572 U CN 203601572U
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- battery
- unmanned vehicle
- vehicle battery
- power supply
- wire port
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Abstract
The utility model discloses an unmanned aerial vehicle battery and an aerial vehicle with the unmanned aerial vehicle battery. The aerial vehicle comprises a vehicle body and the unmanned aerial vehicle battery. The vehicle body is provided with a battery bin, the battery bin comprises a bin body and containing space located in the bin body, the containing space is matched with the unmanned aerial vehicle battery, the unmanned aerial vehicle battery is installed in the battery bin of the aerial vehicle through a battery connecting piece and comprises a battery body and a power source wiring part, the power source wiring part is installed at one end of the battery body, serial ports, negative electrode lead ports and positive electrode lead ports are formed in the power source wiring part, the negative electrode lead ports and the positive electrode lead ports are formed corresponding to power source wiring terminals of the vehicle body of the unmanned aerial vehicle respectively, and the power source wiring terminals of the vehicle body are arranged in the battery bin and correspondingly connected into the negative electrode lead ports and the positive electrode lead ports in an inserted mode.
Description
Technical field
The utility model relates to vehicle technology field, and particularly a kind of assembling and disassembling is easily for the battery on unmanned vehicle and have the aircraft of this battery.
Background technology
Carry-on battery, as the important Primary Component of aircraft, it is for providing the power of aircraft.Aircraft of the prior art, in particular for the aircraft of taking photo by plane, rescuing or spray insecticide etc., the structure of its battery all needs other accessories to be fixed, and need to take other fixed partss apart just can take out, in addition, after battery installation, also need the manual positive and negative power supply terminal that connects separately.The battery structure of prior art aircraft, in installation and demolishing process, all needs to consume more man-hour, has reduced efficiency, makes its production and use to be all under some influence.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of deficiency that can overcome battery structure in prior art, assembling and disassembling unmanned vehicle battery and have the aircraft of this battery easily.
To achieve these goals, the utility model provides a kind of unmanned vehicle battery, be arranged in the battery compartment of aircraft, wherein, described unmanned vehicle battery is arranged on by battery connecting piece in the battery compartment of described aircraft, described unmanned vehicle battery comprises battery body and power supply wiring portion, described power supply wiring portion is arranged on one end of described battery body, in described power supply wiring portion, be provided with serial ports, negative wire port and positive wire port, described negative wire port and positive wire port respectively with the corresponding setting of fuselage power supply terminal of described unmanned vehicle, described fuselage power supply terminal is arranged in described battery compartment and can correspondence be plugged in described negative wire port and positive wire port.
Above-mentioned unmanned vehicle battery, wherein, described battery connecting piece comprises the battery adapter plate being arranged in described battery compartment, on described battery adapter plate, be provided with at least one for guiding the guide rail of described unmanned vehicle battery installation, on described battery body, be provided with sliver corresponding to described guide rail, described sliver and described guide rail adaptation.
Above-mentioned unmanned vehicle battery, wherein, described battery adapter plate is a pair of adapter plate being symmetricly set in described battery compartment, on each described adapter plate, be provided with at least one described in guide rail.
Above-mentioned unmanned vehicle battery, wherein, described a pair of adapter plate is symmetricly set on respectively on the both sides inwall of described battery compartment, and described sliver is corresponding to described guide rail symmetrical being arranged on the both sides outer wall of described battery body respectively.
Above-mentioned unmanned vehicle battery, wherein, described guide rail arranges near the bottom of described battery compartment, and described sliver is arranged on the both sides outer wall of described battery body the one end near described power supply wiring portion.
Above-mentioned unmanned vehicle battery, wherein, also comprises handle, and described handle is arranged on described battery body and is positioned at one end relative with described power supply wiring portion.
Above-mentioned unmanned vehicle battery, wherein, described serial ports, negative wire port and positive wire port are in pairs and are symmetrical arranged.
In order to realize better above-mentioned purpose, the utility model also provides a kind of aircraft, comprise fuselage and unmanned vehicle battery, described fuselage is provided with battery compartment, described battery compartment comprises warehouse and is positioned at an accommodation space of described warehouse, described accommodation space and described unmanned vehicle battery adaptation, wherein, described unmanned vehicle battery is above-mentioned unmanned vehicle battery.
Above-mentioned aircraft, wherein, described battery compartment also comprises the battery door for sealing described accommodation space, and one end of described battery door is articulated on described warehouse corresponding to described accommodation space, and the other end of described battery door is provided with the bindiny mechanism for fastening with described warehouse.
Above-mentioned aircraft, wherein, the setting that overlaps with the vertical centre axis of described fuselage of the vertical centre axis of described unmanned vehicle battery.
Beneficial functional of the present utility model is:
1. unmanned vehicle battery can take out separately and fix without other any accessory;
2. the both sides of unmanned vehicle battery adopt two aluminium section bars to do guide rail, install to take out easily consuming time shortly, and that handle is installed is easy to carry for battery itself in addition;
3. the battery structure of prior art all needs to take apart other fixed parts and just can take out battery, unmanned vehicle battery of the present utility model is to extract out from fuselage side, any parts that do not need to dismantle can take out, and it is very convenient to install with dismounting, and can reduce and install and removal time;
4. when unmanned vehicle battery inserts fuselage, power supply wiring both positive and negative polarity also connects simultaneously, does not need to connect by hand separately positive and negative power supply terminal again, has saved the set-up time, and the comfort feature of installation effectiveness and installation is provided.
Below in conjunction with the drawings and specific embodiments, the utility model is described in detail, but not as to restriction of the present utility model.
Accompanying drawing explanation
Fig. 1 is the aircraft perspective view of the utility model one embodiment;
Fig. 2 is the unmanned vehicle battery perspective view of the utility model one embodiment;
Fig. 3 is the unmanned vehicle battery structure schematic diagram shown in Fig. 2;
Fig. 4 is the left view of Fig. 3;
Fig. 5 is the birds-eye view of Fig. 3;
Fig. 6 A is the battery adapter plate installation site schematic diagram of the utility model one embodiment;
Fig. 6 B is the perspective view of Fig. 6 A;
Fig. 7 is the A-A cutaway view of Fig. 6 A;
Fig. 8 is the battery scheme of installation of the utility model one embodiment;
Fig. 9 is the B-B cutaway view of Fig. 8;
Figure 10 A-10D is the utility model installation process schematic diagram;
Figure 11 A-11B is the utility model demolishing process schematic diagram.
Wherein, Reference numeral
1 fuselage
11 battery compartments
111 warehouses
112 accommodation spaces
113 battery doors
114 bindiny mechanisms
12 fuselage power patch panels
13 power supply terminals
2 unmanned vehicle batteries
21 battery bodies
211 slivers
22 power supply wiring portions
221 serial ports
222 negative wire ports
223 positive wire ports
23 handles
3 battery connecting pieces
31 battery adapter plates
32 guide rails
4 drive and control setup
5 screw propellers
The specific embodiment
Below in conjunction with accompanying drawing, structural principle of the present invention and principle of work are described in detail:
Referring to Fig. 1, Fig. 1 is the aircraft perspective view of the utility model one embodiment.Aircraft of the present utility model, be mainly used in taking photo by plane, rescue or spray insecticide, its load-carrying capacity and flying speed to aircraft is had relatively high expectations, therefore adopt unmanned vehicle battery as propulsion source, specifically comprise fuselage 1 and unmanned vehicle battery 2, described fuselage 1 is provided with battery compartment 11, above battery compartment 11, be provided with and drive and control setup 4, battery compartment 11 in the present embodiment is preferably set to quadrilateral structure, its each limit is made up of inner concave curve, on tetragonal four angles, be formed as four outstanding ends, be separately installed with rotation in these four ends to produce the screw propeller 5 of lift, this screw propeller 5, installation and annexation between driving and control setup 4 and unmanned vehicle battery 2 are more ripe prior art, therefore do not repeat at this.Only described in detail with regard to unmanned vehicle battery 2 of the present utility model and battery compartment correspondingly below.
Referring to Fig. 2-Fig. 5, Fig. 2 is the unmanned vehicle battery perspective view of the utility model one embodiment, wherein, power supply wiring portion 22 is detached position, Fig. 3 is the unmanned vehicle battery structure schematic diagram shown in Fig. 2, the left view that Fig. 4 is Fig. 3, the birds-eye view that Fig. 5 is Fig. 3.Unmanned vehicle battery 2 of the present utility model, be arranged on by battery connecting piece 3 in the battery compartment 11 of described aircraft, described unmanned vehicle battery 2 comprises battery body 21 and power supply wiring portion 22, described power supply wiring portion 22 is arranged on one end of described battery body 21, in described power supply wiring portion 22, be provided with serial ports 221, negative wire port 222 and positive wire port 223, described negative wire port 222 and positive wire port 223 respectively with the corresponding setting of power supply terminal 13 being arranged on the fuselage power patch panel 12 of described aircraft, described power supply terminal 13 is arranged in described battery compartment 11 and in the time that this unmanned vehicle battery 2 is installed, correspondence is plugged in described negative wire port 222 and positive wire port 223.Described serial ports 221, negative wire port 222 and positive wire port 223 are all preferably in pairs and are symmetrical arranged.
Wherein, described battery connecting piece 3 comprises the battery adapter plate 31 being arranged in described battery compartment 11, on described battery adapter plate 31, be provided with at least one guide rail 32 for guiding described unmanned vehicle battery 2 to install, on described battery body 21, be provided with sliver 211 corresponding to described guide rail 32, described sliver 211 and described guide rail 32 adaptations.When installation, this sliver 211 is in the interior slip of guide rail 32, this battery body 21 is under the common guiding of sliver 211 and guide rail 32, pack into smoothly in the accommodation space 112 of battery compartment 11, this guide rail 32 can be for example the U-shaped groove of aluminium alloy extrusions, this sliver 211 can be for example and the rectangular structure of the square-section of this U-shaped groove adaptation, structure and the quantity of this guide rail 32 and sliver 211 are all not particularly limited, as long as can complete the guiding to unmanned vehicle battery 2 while installation, this sliver 211 and guide rail 32 are after installation, can play the spacing and fixation to unmanned vehicle battery 2 simultaneously.
In the present embodiment, described battery adapter plate 31 is preferably a pair of adapter plate in the accommodation space 112 that is symmetricly set on described battery compartment 11, on each described adapter plate, be provided with at least one described in guide rail 32(accompanying drawing all take a guide rail as example).In addition, described a pair of adapter plate can be separately positioned on the Huo Liang top and bottom, inwall both sides of accommodation space 112 of battery compartment 11, consider the comfort feature of installation and save material and space, preferably be symmetricly set on the both sides inwall of described accommodation space 112, described sliver 211 is corresponding to described guide rail 32 symmetrical being arranged on the both sides outer wall of described battery body 21 respectively.Wherein, described guide rail 32 preferably arranges near the bottom of the accommodation space 112 of described battery compartments 11, and described sliver 211 is arranged on the both sides outer wall of described battery body 21 one end near described power supply wiring portion 22.
Convenient for Assembly &Disassembly, in the present embodiment, this unmanned vehicle battery 2 also can comprise handle 23, and described handle 23 is arranged on described battery body 21 and is positioned at one end relative with described power supply wiring portion 22.
Referring to Fig. 6 A-Fig. 9, Fig. 6 A is the battery adapter plate installation site schematic diagram of the utility model one embodiment, and Fig. 6 B is the perspective view of Fig. 6 A, and Fig. 7 is the A-A cutaway view of Fig. 6 A, Fig. 8 is the battery scheme of installation of the utility model one embodiment, the B-B cutaway view that Fig. 9 is Fig. 8.In the present embodiment, described battery compartment 11 comprises warehouse 111 and is positioned at an accommodation space 112 of described warehouse 111, described accommodation space 112 and described unmanned vehicle battery 2 adaptations.Described battery compartment 11 also can comprise the battery door 113 for sealing described accommodation space 112, one end of described battery door 113 is articulated on described warehouse 111 corresponding to described accommodation space 112, the other end of described battery door 113 is provided with the bindiny mechanism 114 for fastening with described warehouse 111, this connection structure 114 firmly fastens as long as can realize with warehouse 111, and can open easily and locking, can be for example hasp structure, latch structure or Spring lock catch structure etc., to this, there is no particular restriction.After fastening, the two ends of described unmanned vehicle battery 2 can be resisted against respectively on the bottom and described battery door 113 of described battery compartment 11, the both sides of this unmanned vehicle battery 2 plug together in guide rail 32 by sliver 211 respectively, described power supply terminal 13 correspondences are plugged in described negative wire port 222 and positive wire port 223, therefore unmanned vehicle battery 2 of the present utility model is fixing separately without other parts.Wherein, stable in order to turn round, the setting that overlaps with the vertical centre axis of described fuselage 1 of the vertical centre axis of preferred described unmanned vehicle battery 2.
Referring to Figure 10 A-10D, Figure 10 A-10D is the utility model installation process schematic diagram.When installation, first open battery door 113(Figure 10 A), how holding handle 23 inserts unmanned vehicle battery 2 in accommodation space 112, be arranged on sliver 211 on battery body 21 in the interior slip of guide rail 32, under the guiding of this sliver 211, unmanned vehicle battery 2 is in place smoothly, and described power supply terminal 13 correspondences are plugged in described negative wire port 222 and positive wire port 223 (Figure 10 B), then close and this battery door 113(Figure 10 C that is fastened), so far, the installation of unmanned vehicle battery 2 (Figure 10 D).
Referring to Figure 11 A-11B, Figure 11 A-11B is the utility model demolishing process schematic diagram.The process of dismantling this unmanned vehicle battery 2 is contrary with above-mentioned installation process, first open battery door 113(Figure 11 A), then hold handle 23 and pull it (Figure 11 B), after battery body 21 departs from battery compartment 11 completely, again battery door 113 is closed, or change another unmanned vehicle battery 2.The unmanned vehicle battery 2 disassembling can charge or other work such as maintenance.
Unmanned vehicle battery of the present utility model can take out separately and fix without other any accessory; Preferably adopt two aluminium section bars to do guide rail, install and take out easily consuming time shortly, that handle is installed is easy to carry for battery itself in addition; The battery structure that is different from prior art all needs to take apart other fixed parts just can take out battery, unmanned vehicle battery of the present utility model is to extract out from fuselage side, any parts that do not need to dismantle can take out, and it is very convenient to install with dismounting, and can reduce and install and removal time; When unmanned vehicle battery inserts fuselage, power supply wiring both positive and negative polarity also connects simultaneously, does not need to connect by hand separately positive and negative power supply terminal again, has saved the set-up time, and the comfort feature of installation effectiveness and installation is provided.
Certainly; the utility model also can have other various embodiments; in the situation that not deviating from the utility model spirit and essence thereof; those of ordinary skill in the art are when making various corresponding changes and distortion according to the utility model, but these corresponding changes and distortion all should belong to the protection domain of the appended claim of the utility model.
Claims (10)
1. a unmanned vehicle battery, be arranged in the battery compartment of aircraft, it is characterized in that, described unmanned vehicle battery is arranged on by battery connecting piece in the battery compartment of described aircraft, described unmanned vehicle battery comprises battery body and power supply wiring portion, described power supply wiring portion is arranged on one end of described battery body, in described power supply wiring portion, be provided with serial ports, negative wire port and positive wire port, described negative wire port and positive wire port respectively with the corresponding setting of fuselage power supply terminal of described unmanned vehicle, described fuselage power supply terminal is arranged in described battery compartment and can correspondence be plugged in described negative wire port and positive wire port.
2. unmanned vehicle battery as claimed in claim 1, it is characterized in that, described battery connecting piece comprises the battery adapter plate being arranged in described battery compartment, on described battery adapter plate, be provided with at least one for guiding the guide rail of described unmanned vehicle battery installation, on described battery body, be provided with sliver corresponding to described guide rail, described sliver and described guide rail adaptation.
3. unmanned vehicle battery as claimed in claim 2, is characterized in that, described battery adapter plate is a pair of adapter plate being symmetricly set in described battery compartment, on each described adapter plate, be provided with at least one described in guide rail.
4. unmanned vehicle battery as claimed in claim 3, is characterized in that, described a pair of adapter plate is symmetricly set on respectively on the both sides inwall of described battery compartment, and described sliver is corresponding to described guide rail symmetrical being arranged on the both sides outer wall of described battery body respectively.
5. unmanned vehicle battery as claimed in claim 4, is characterized in that, described guide rail arranges near the bottom of described battery compartment, and described sliver is arranged on the both sides outer wall of described battery body the one end near described power supply wiring portion.
6. the unmanned vehicle battery as described in claim 1,2,3,4 or 5, is characterized in that, also comprises handle, and described handle is arranged on described battery body and is positioned at one end relative with described power supply wiring portion.
7. the unmanned vehicle battery as described in claim 1,2,3,4 or 5, is characterized in that, described serial ports, negative wire port and positive wire port are in pairs and are symmetrical arranged.
8. an aircraft, comprise fuselage and unmanned vehicle battery, described fuselage is provided with battery compartment, described battery compartment comprises warehouse and is positioned at an accommodation space of described warehouse, described accommodation space and described unmanned vehicle battery adaptation, it is characterized in that, described unmanned vehicle battery is the unmanned vehicle battery described in any one in the claims 1-7.
9. aircraft as claimed in claim 8, it is characterized in that, described battery compartment also comprises the battery door for sealing described accommodation space, one end of described battery door is articulated on described warehouse corresponding to described accommodation space, and the other end of described battery door is provided with the bindiny mechanism for fastening with described warehouse.
10. aircraft as claimed in claim 8, is characterized in that, the setting that overlaps with the vertical centre axis of described fuselage of the vertical centre axis of described unmanned vehicle battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320701225.0U CN203601572U (en) | 2013-11-07 | 2013-11-07 | Unmanned aerial vehicle battery and aerial vehicle with unmanned aerial vehicle battery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320701225.0U CN203601572U (en) | 2013-11-07 | 2013-11-07 | Unmanned aerial vehicle battery and aerial vehicle with unmanned aerial vehicle battery |
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| Publication Number | Publication Date |
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| CN203601572U true CN203601572U (en) | 2014-05-21 |
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| CN201320701225.0U Expired - Fee Related CN203601572U (en) | 2013-11-07 | 2013-11-07 | Unmanned aerial vehicle battery and aerial vehicle with unmanned aerial vehicle battery |
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Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106516073A (en) * | 2016-11-30 | 2017-03-22 | 厦门汉航精密科技有限公司 | Fuselage conductive structure of unmanned aerial vehicle and manufacturing method of fuselage frames |
| CN106628105A (en) * | 2017-02-28 | 2017-05-10 | 天峋（常州）智能科技有限公司 | Unmanned aerial vehicle with rod-shaped plug batteries |
| CN106741891A (en) * | 2016-11-30 | 2017-05-31 | 厦门汉航精密科技有限公司 | A kind of unmanned plane structure |
| WO2017107170A1 (en) * | 2015-12-25 | 2017-06-29 | 深圳市大疆创新科技有限公司 | Battery and unmanned aerial vehicle comprising same |
| CN107108042A (en) * | 2016-09-21 | 2017-08-29 | 深圳市大疆创新科技有限公司 | Lock uint, unmanned plane and electronic equipment |
| KR101807368B1 (en) * | 2015-12-09 | 2017-12-08 | 한국항공우주연구원 | drone equipped with one touch battery pack |
| CN107807662A (en) * | 2017-11-25 | 2018-03-16 | 东莞市众前电子有限公司 | A kind of interactive four-axle aircraft and its gesture control interactive approach |
| CN107972854A (en) * | 2017-10-27 | 2018-05-01 | 成都睿翼无人机科技有限公司 | A kind of power patrol unmanned machine |
| WO2018086202A1 (en) * | 2016-11-11 | 2018-05-17 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle battery compartment, and unmanned aerial vehicle |
| CN108146404A (en) * | 2016-12-02 | 2018-06-12 | 成都天府新区光启未来技术研究院 | The replacement system and method and unmanned plane of unmanned machine battery |
| CN109562837A (en) * | 2016-10-25 | 2019-04-02 | 深圳市大疆创新科技有限公司 | Unmanned vehicle and battery warehouse component and battery compartment |
| CN109562838A (en) * | 2016-11-09 | 2019-04-02 | 深圳市大疆创新科技有限公司 | Unmanned plane |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101807368B1 (en) * | 2015-12-09 | 2017-12-08 | 한국항공우주연구원 | drone equipped with one touch battery pack |
| WO2017107170A1 (en) * | 2015-12-25 | 2017-06-29 | 深圳市大疆创新科技有限公司 | Battery and unmanned aerial vehicle comprising same |
| CN107108042A (en) * | 2016-09-21 | 2017-08-29 | 深圳市大疆创新科技有限公司 | Lock uint, unmanned plane and electronic equipment |
| CN107108042B (en) * | 2016-09-21 | 2019-03-29 | 深圳市大疆创新科技有限公司 | Lock uint, unmanned plane and electronic equipment |
| CN109562837A (en) * | 2016-10-25 | 2019-04-02 | 深圳市大疆创新科技有限公司 | Unmanned vehicle and battery warehouse component and battery compartment |
| CN109562837B (en) * | 2016-10-25 | 2022-03-22 | 深圳市大疆创新科技有限公司 | Unmanned vehicles and battery compartment subassembly and battery compartment |
| CN109562838A (en) * | 2016-11-09 | 2019-04-02 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| CN109562838B (en) * | 2016-11-09 | 2021-12-21 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| WO2018086202A1 (en) * | 2016-11-11 | 2018-05-17 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle battery compartment, and unmanned aerial vehicle |
| CN109562839A (en) * | 2016-11-11 | 2019-04-02 | 深圳市大疆创新科技有限公司 | Unmanned plane battery compartment and unmanned plane |
| CN106516073B (en) * | 2016-11-30 | 2019-03-15 | 福建汉航精密科技有限公司 | The production method of the fuselage conductive structure and its fuselage ring of unmanned plane |
| CN106516073A (en) * | 2016-11-30 | 2017-03-22 | 厦门汉航精密科技有限公司 | Fuselage conductive structure of unmanned aerial vehicle and manufacturing method of fuselage frames |
| CN106741891A (en) * | 2016-11-30 | 2017-05-31 | 厦门汉航精密科技有限公司 | A kind of unmanned plane structure |
| CN106741891B (en) * | 2016-11-30 | 2023-06-16 | 厦门汉航精密科技有限公司 | Unmanned aerial vehicle structure |
| CN108146404A (en) * | 2016-12-02 | 2018-06-12 | 成都天府新区光启未来技术研究院 | The replacement system and method and unmanned plane of unmanned machine battery |
| CN108146404B (en) * | 2016-12-02 | 2024-04-02 | 成都天府新区光启未来技术研究院 | Unmanned aerial vehicle battery replacement system and method and unmanned aerial vehicle |
| CN106628105A (en) * | 2017-02-28 | 2017-05-10 | 天峋（常州）智能科技有限公司 | Unmanned aerial vehicle with rod-shaped plug batteries |
| CN107972854A (en) * | 2017-10-27 | 2018-05-01 | 成都睿翼无人机科技有限公司 | A kind of power patrol unmanned machine |
| CN107807662A (en) * | 2017-11-25 | 2018-03-16 | 东莞市众前电子有限公司 | A kind of interactive four-axle aircraft and its gesture control interactive approach |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140521 Termination date: 20151107 |
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| EXPY | Termination of patent right or utility model |