CN105539857A - Battery clamping structure for unmanned aerial vehicle - Google Patents
Battery clamping structure for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN105539857A CN105539857A CN201610041180.7A CN201610041180A CN105539857A CN 105539857 A CN105539857 A CN 105539857A CN 201610041180 A CN201610041180 A CN 201610041180A CN 105539857 A CN105539857 A CN 105539857A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- container case
- casing
- battery
- interface arrangment
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000000994 depressogenic effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
The invention discloses a battery clamping structure for an unmanned aerial vehicle. The battery clamping structure comprises an unmanned aerial vehicle shell and a battery shell. The battery shell is plugged into the aerial vehicle shell in a matched mode. The battery shell is provided with an elastic clamping piece and movably connected with a flip cover. The unmanned aerial vehicle shell is provided with a block piece. The elastic clamping piece is in fit with the lower end of the block piece. The elastic clamping piece is provided with a protrusion. The protrusion and the block piece make contact to limit the battery shell. The flip cover rotates to press the elastic clamping piece downwards to enable the protrusion to move downwards to the position lower than the block piece to remove the limit of the battery shell. In this way, the battery clamping structure for the unmanned aerial vehicle can prevent a battery from falling off, and is simple, convenient to use, safe and reliable.
Description
Technical field
The present invention relates to unmanned plane field, particularly relate to a kind of unmanned plane battery interface arrangment.
Background technology
Robot airplane is called for short " unmanned plane ", and english abbreviation is " UAV ", is the non-manned aircraft utilizing radio robot to handle with the process controller provided for oneself.In order to simplify the project organization of unmanned plane, sometimes fuselage being separated setting with power supply, when needs use unmanned plane, power supply and fuselage being connected, when not needing to use unmanned plane, power supply dismounting being placed, is so also beneficial to the maintenance of fuselage and power supply.The present battery of unmanned plane is generally installed in body by polylith adapter plate or separate space, extremely inconvenient during placing battery, and battery case weight is large, affects the flight efficiency of unmanned plane.
Summary of the invention
The technical matters that the present invention mainly solves is to provide a kind of unmanned plane battery interface arrangment, can prevent battery from coming off, and interface arrangment is simple, easy to use, safe and reliable.
For solving the problems of the technologies described above, the technical scheme that the present invention adopts is: provide a kind of unmanned plane battery interface arrangment, comprise: unmanned plane casing and container case, described container case coordinates the inside being plugged in unmanned plane casing, described container case is provided with elastic card contact pin, described container case is connected with and renovates, described unmanned plane casing is provided with catch, the lower end of described elastic card contact pin and catch fits, described elastic card contact pin has a projection, described projection contacts with catch in order to spacing container case, described renovating rotates that to press down the position that elastic card contact pin makes projection be moved downward to lower than catch spacing to remove container case.
In a preferred embodiment of the present invention, the end of described elastic card contact pin has arc, described in renovate rotation press down arc remove spacing, pull to renovate and container case taken out in unmanned plane casing.
In a preferred embodiment of the present invention, described container case comprises upper casing, lower casing and end cap, and described upper casing is connected with end cap respectively with lower casing.
In a preferred embodiment of the present invention, described in the middle part of renovating be hinged on end cap by rotating shaft.
In a preferred embodiment of the present invention, be also provided with mounting groove in described unmanned plane casing, described container case coordinates cooperation to be arranged on mounting groove inside.
In a preferred embodiment of the present invention, in described container case, be provided with battery.
The invention has the beneficial effects as follows: unmanned plane battery interface arrangment of the present invention, can prevent battery from coming off, interface arrangment is simple, easy to use, safe and reliable.
Accompanying drawing explanation
In order to be illustrated more clearly in the technical scheme in the embodiment of the present invention, below the accompanying drawing used required in describing embodiment is briefly described, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings, wherein:
Fig. 1 is the structural representation of unmanned plane battery interface arrangment one of the present invention preferred embodiment;
Fig. 2 is the local structure enlarged diagram of the unmanned plane battery interface arrangment shown in Fig. 1;
Fig. 3 is the perspective view of the container case shown in Fig. 1;
In accompanying drawing, the mark of each parts is as follows: 1, unmanned plane casing, and 2, container case, 3, elastic card contact pin, 4, renovate, 5, catch, 6, protruding, 7, arc, 8, mounting groove, 9, battery, 10, upper casing, 11, lower casing, 12, end cap.
Detailed description of the invention
Be clearly and completely described to the technical scheme in the embodiment of the present invention below, obviously, described embodiment is only a part of embodiment of the present invention, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making other embodiments all obtained under creative work prerequisite, belong to the scope of protection of the invention.
Refer to Fig. 1, a kind of unmanned plane battery interface arrangment, comprise: unmanned plane casing 1 and container case 2, described container case 2 coordinates the inside being plugged in unmanned plane casing 1, described container case 2 is provided with elastic card contact pin 3, described container case 2 is connected with and renovates 4, described unmanned plane casing 1 is provided with catch 5, the lower end of described elastic card contact pin 3 and catch 5 fits, described elastic card contact pin 3 has a projection 6, described protruding 6 contact in order to spacing container case 2 with catch 5, describedly renovate 4 rotations and press down elastic card contact pin 3 and make protruding 6 positions be moved downward to lower than catch 5 spacing to remove container case 2.
In addition, the end of described elastic card contact pin 3 has arc 7, described in renovate 4 rotations and press down arc 7 and remove spacing, pull and renovate 4 container case 2 is taken out in unmanned plane casing 1.
In addition, described container case 2 comprises upper casing 10, lower casing 11 and end cap 12, and described upper casing 10 is connected with end cap 12 respectively with lower casing 11.
In addition, the middle part of renovating 4 described in is hinged on end cap 12 by rotating shaft.
In addition, be also provided with mounting groove 8 in described unmanned plane casing 1, it is inner that the cooperation of described container case 2 is arranged on mounting groove 8.
In addition, battery 9 is provided with in described container case 2.
Unmanned plane battery interface arrangment specific works principle of the present invention is as follows: the mounting groove 8 container case 2 that battery 9 is housed being inserted into unmanned plane casing 1 is inner, after inserting, elastic card contact pin 3 part and catch 5 are fitted, and projection 6 to be positioned on rear side of catch 5 thus to realize the effect that container case 2 clamping prevents container case from coming off.When needing to take out container case 2, rotary flip 4, renovate 4 turn an angle after, contact with the arc 7 of elastic card contact pin 2 end, and press down arc 7, protruding 5 positions are depressed to the position lower than catch 5 with elastic card contact pin 3, now pull to renovate 4 and just container case 2 can be taken out from mounting groove 8.
Be different from prior art, unmanned plane battery interface arrangment of the present invention, can prevent battery from coming off, and interface arrangment is simple, easy to use, safe and reliable.
The foregoing is only embodiments of the invention; not thereby the scope of the claims of the present invention is limited; every utilize description of the present invention to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical field, be all in like manner included in scope of patent protection of the present invention.
Claims (6)
1. a unmanned plane battery interface arrangment, it is characterized in that, comprise: unmanned plane casing and container case, described container case coordinates the inside being plugged in unmanned plane casing, described container case is provided with elastic card contact pin, described container case is connected with and renovates, described unmanned plane casing is provided with catch, the lower end of described elastic card contact pin and catch fits, described elastic card contact pin has a projection, described projection contacts with catch in order to spacing container case, described renovating rotates that to press down the position that elastic card contact pin makes projection be moved downward to lower than catch spacing to remove container case.
2. unmanned plane battery interface arrangment according to claim 1, is characterized in that, the end of described elastic card contact pin has arc, described in renovate rotation press down arc remove spacing, pull to renovate and container case taken out in unmanned plane casing.
3., according to the arbitrary described unmanned plane battery interface arrangment of claim 2, it is characterized in that, described container case comprises upper casing, lower casing and end cap, and described upper casing is connected with end cap respectively with lower casing.
4. unmanned plane battery interface arrangment according to claim 3, is characterized in that, described in the middle part of renovating be hinged on end cap by rotating shaft.
5. according to the arbitrary described unmanned plane battery interface arrangment of claim 1-4, it is characterized in that, be also provided with mounting groove in described unmanned plane casing, described container case coordinates cooperation to be arranged on mounting groove inside.
6. unmanned plane battery interface arrangment according to claim 5, is characterized in that, be provided with battery in described container case.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610041180.7A CN105539857B (en) | 2016-01-22 | 2016-01-22 | Unmanned plane battery interface arrangment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610041180.7A CN105539857B (en) | 2016-01-22 | 2016-01-22 | Unmanned plane battery interface arrangment |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105539857A true CN105539857A (en) | 2016-05-04 |
| CN105539857B CN105539857B (en) | 2017-09-12 |
Family
ID=55819514
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610041180.7A Expired - Fee Related CN105539857B (en) | 2016-01-22 | 2016-01-22 | Unmanned plane battery interface arrangment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105539857B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018032265A1 (en) * | 2016-08-15 | 2018-02-22 | 张琬彬 | Unmanned aerial vehicle battery mounting damping structure |
| WO2018058771A1 (en) * | 2016-09-27 | 2018-04-05 | 深圳市大疆创新科技有限公司 | Battery clamping mechanism, battery and unmanned aerial vehicle, and charging device |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101640258A (en) * | 2008-07-30 | 2010-02-03 | 深圳富泰宏精密工业有限公司 | Battery cover opening-closing mechanism |
| CN204223172U (en) * | 2014-10-27 | 2015-03-25 | 广州极飞电子科技有限公司 | Rotor craft battery fastening structure |
| CN204596856U (en) * | 2015-04-17 | 2015-08-26 | 深圳一电科技有限公司 | Power brick and unmanned plane |
| CN105226216A (en) * | 2015-11-06 | 2016-01-06 | 广州南方卫星导航仪器有限公司 | Battery cover clip structure |
| CN205525002U (en) * | 2016-01-22 | 2016-08-31 | 无锡觅睿恪科技有限公司 | Battery joint structure for unmanned aerial vehicle |
-
2016
- 2016-01-22 CN CN201610041180.7A patent/CN105539857B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101640258A (en) * | 2008-07-30 | 2010-02-03 | 深圳富泰宏精密工业有限公司 | Battery cover opening-closing mechanism |
| CN204223172U (en) * | 2014-10-27 | 2015-03-25 | 广州极飞电子科技有限公司 | Rotor craft battery fastening structure |
| CN204596856U (en) * | 2015-04-17 | 2015-08-26 | 深圳一电科技有限公司 | Power brick and unmanned plane |
| CN105226216A (en) * | 2015-11-06 | 2016-01-06 | 广州南方卫星导航仪器有限公司 | Battery cover clip structure |
| CN205525002U (en) * | 2016-01-22 | 2016-08-31 | 无锡觅睿恪科技有限公司 | Battery joint structure for unmanned aerial vehicle |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018032265A1 (en) * | 2016-08-15 | 2018-02-22 | 张琬彬 | Unmanned aerial vehicle battery mounting damping structure |
| WO2018058771A1 (en) * | 2016-09-27 | 2018-04-05 | 深圳市大疆创新科技有限公司 | Battery clamping mechanism, battery and unmanned aerial vehicle, and charging device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105539857B (en) | 2017-09-12 |
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| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
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Granted publication date: 20170912 Termination date: 20180122 |