CN205633053U - Unmanned aerial vehicle battery connection structure - Google Patents
Unmanned aerial vehicle battery connection structure Download PDFInfo
- Publication number
- CN205633053U CN205633053U CN201620378095.5U CN201620378095U CN205633053U CN 205633053 U CN205633053 U CN 205633053U CN 201620378095 U CN201620378095 U CN 201620378095U CN 205633053 U CN205633053 U CN 205633053U
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- China
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- battery
- unmanned plane
- cavity
- aerial vehicle
- unmanned aerial
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Abstract
The utility model discloses owing to be equipped with locking key, locking bolt, locking groove on unmanned aerial vehicle, realize the halving effect of unmanned aerial vehicle and battery, in addition the dual mode is equipped with joint spare and joint position in battery tray both sides, the looks clamping effect of realization unmanned aerial vehicle and battery, convenient effect of charging is realized to the interface that charges that still is equipped with on the battery tray in addition. Consequently the utility model discloses relative unmanned aerial vehicle battery connection structure has on the market improved the stability of being connected between unmanned aerial vehicle and the battery. Thereby reduce unmanned aerial vehicle and be connected to loosen with unmanned aerial vehicle because of the battery on the way in flight and take off, lead to unmanned aerial vehicle's the condition such as crash. Just because of the utility model discloses there is above advantage, increased unmanned aerial vehicle user's use satisfaction to play the effect that improves the market competition ability.
Description
Technical field
This utility model relates to unmanned plane, is specifically related to unmanned plane battery connecting construction.
Background technology
Existing unmanned plane, its battery and the connection of this unmanned plane, it is all by arranging battery case on unmanned plane mostly, then battery is installed in this battery case, the lid of battery case is fixed by screw interlocking, though battery is connected firmly with unmanned plane, but battery to be changed or when charging the battery, operate highly inconvenient；Also has the battery of some circumscribeds at present, on battery, i.e. it is provided with buckle, unmanned plane arranges cavity, screens is set on cavity, realizes battery be connected with unmanned plane by battery being inserted in cavity and make buckle and screens phase clamping, though so design facilitates dismounting and change, but connect insecure, it is easily caused battery and unmanned plane in unmanned plane flight course aloft to be disconnected or loose contact, so that unmanned plane falls because of power-off, causes unmanned plane to damage.
Summary of the invention
The purpose of this utility model is that providing a kind of not only facilitates dismounting and change but also ensure the unmanned plane battery connecting construction being connected firmly.
In order to reach above-mentioned purpose, this utility model be the technical scheme is that a kind of unmanned plane battery connecting construction, it is characterized in that: at least provided with the first interface arrangment and the second interface arrangment between interconnective unmanned plane and battery, described first interface arrangment is arranged on the bottom of unmanned plane and battery junction, and described second interface arrangment is arranged on the side of unmanned plane and battery junction.
In order to reach the connection effect of fixing unmanned plane and battery, cavity is had on described unmanned plane, described battery is plugged in described cavity by a battery holder, described first interface arrangment is positioned at the position of the lower section cavity wall of described cavity, and described second interface arrangment is positioned at the position of the both sides cavity wall of described cavity.
In order to reach manually lockable to improve the effect of connectivity robustness, described first interface arrangment, including locking switch, locking bolt, lock slots, described locking switch and locking bolt be fixing to be connected in bottom unmanned plane close at cavities open, described lock slots is correspondingly arranged on battery, realizes locking bolt and lock slots phase interlocking by stirring described locking switch.
Further, described cavity is provided with through hole in close opening part position and communicates with described cavity, and described locking switch is arranged at described through hole and is positioned at outside described cavity, and locking bolt extend in described cavity through described through hole accordingly.
Corresponding, the position of the corresponding described through hole of described battery holder is provided with a projection, and described lock slots is opened on described projection, and after described battery inserts in described cavity, described projection aligns with described through hole.
The effect fixing in order to reach dual connection, described second interface arrangment, including shackle member and clamping position, shackle member is arranged on described battery holder, and clamping position is arranged at cavity inside, realizes unmanned plane by shackle member and the phase clamping of clamping position and battery is connected.
In order to reach the effect of easy disassembly, described shackle member, including by compressing switch and buckle, by compressing switch and buckle is connected to one, realize buckle and the phase clamping of described clamping position by compressing switch by pressing is described.
Further, the both sides of described battery holder are respectively provided with a shackle member, described shackle member be positioned at battery holder two side position stretched out outside cavity by compressing switch, described buckle correspondence is positioned at battery holder two side position stretching into cavity.
Corresponding, described clamping position is corresponding is arranged at described cavity inner wall two side position, and described clamping position is in the groove-like matched with described buckle.
In order to realize the electrical contact that battery can be good with unmanned plane, described battery holder is provided with and can electrically connect with unmanned plane and be embodied as the electrical contact mouth that unmanned plane is powered.
This utility model due between interconnective unmanned plane and battery at least provided with two interface arrangments, by the associating clamping of the two interface arrangment, battery is effectively ensured firmly link into an integrated entity with unmanned function, improve the stability being connected between unmanned plane with battery, thus reduce unmanned plane and get loose because battery is connected with unmanned plane in flight way, the situation such as the crash of caused unmanned plane；And use snap fit to connect, therefore fixing without being connected by screw such that it is able to easy removal changes battery etc..Just there is above advantage because of this utility model, add the user satisfaction of unmanned plane user, thus play the effect improving the market competitiveness.
Accompanying drawing explanation
Fig. 1 is the overall structure schematic diagram that unmanned plane of the present utility model is connected with battery.
Fig. 2 is the perspective view of battery of the present utility model.
Fig. 3 is the overall structure schematic diagram of unmanned plane of the present utility model.
Fig. 4 is the overall structure schematic diagram of battery of the present utility model.
Fig. 5 is the sectional structure schematic diagram of unmanned plane of the present utility model.
Detailed description of the invention
Refer to Fig. 1 to Fig. 5, battery connecting construction of the present utility model, include unmanned plane 1, cavity 4, through hole 11, clamping position 32, battery 6, lock slots 23, battery holder 61, shackle member 31, by compressing switch 311 and buckle 312, its cavity 4 is arranged on the position by bottom, the inside of unmanned plane 1, and through hole 11 be arranged on unmanned plane cavity 4 get through toward the thinnest cavity wall formed as it is shown on figure 3, and at cavity 4 close to opening part cavity wall has clamping position 32 in half rectangular shape together.
Refer to Fig. 1, found out in the case of battery 6 and unmanned plane 1 connect by figure, 311 high-visible on the surface of unmanned plane 1 by compressing switch, the battery 6 structure in cuboid, and 311 be just arranged on two minor faces of battery case 61 by compressing switch, the singlehanded pressing of user is facilitated 311 to be taken out by battery 6 by compressing switch, it is achieved to facilitate battery 6 to change the effect of dismounting.
Refer to Fig. 2 and Fig. 3, found out that clamping position 32 is arranged in unmanned plane cavity 4 cavity wall by Fig. 3, and the opening part close to cavity 4, found out by Fig. 2 and on the minor face of battery 6, be provided with a projection 62, on projection 62, the position of the locking switch 21 of corresponding unmanned plane and shape are provided with a groove, and at the another side of projection 62, position and the shape of unmanned plane battery energising mouth are provided with an electrical contact mouth 63.
And can find out in fig. 2 by compress switch 311 and buckle 312 be solidified as a whole composition one shackle member 31, user 311 is made and the compression that certain angle occurs by 311 buckles 312 being connected that compress switch by compressing switch by pressing, realize buckle 312 to separate with clamping position 32, i.e. reach easily to unload the effect of battery 6.
Refer to Fig. 4,311 be that respectively assembly, in the minor face of battery case 61, by the surface compressed switch by be necessarily made up of patch angle, triangular prism angle, reaches anti-skidding effect by compressing switch as seen from Figure 4.Buckle 312, in hook, reaches and the effect of clamping position 32 phase clamping.
Refer again to Fig. 5, found out that locking switch 21 is solidified as a whole with locking bolt 22 by figure, locking switch 21 is set to the form of push button, when user promotes locking switch 21 to be the locking bolt 22 that band is automatically connected in locking switch, locking bolt 22 is allowed to inject the lock slots 23 that is arranged on battery 6, it is achieved the effect of locking bolt 22 and lock slots 23 phase interlocking.
The foregoing is only preferred embodiment of the present utility model, be not used to limit the scope of the claims of the present utility model, other uses the equivalence change of patent spirit of the present utility model, all should belong to the scope of the claims of the present utility model.
Claims (10)
1. a unmanned plane battery connecting construction, it is characterized in that: at least provided with the first interface arrangment (2) and the second interface arrangment (3) between interconnective unmanned plane (1) and battery (6), described first interface arrangment (2) is arranged on the bottom of unmanned plane (1) and battery (6) junction, and described second interface arrangment (3) is arranged on the side of unmanned plane (1) and battery (6) junction.
2. unmanned plane battery connecting construction as claimed in claim 1, it is characterized in that: on described unmanned plane (1), have cavity (4), described battery (6) is plugged in described cavity (4) by a battery holder (61), described first interface arrangment (2) is positioned at the position of the lower section cavity wall of described cavity (4), and described second interface arrangment (3) is positioned at the position of the both sides cavity wall of described cavity (4).
3. unmanned plane battery connecting construction as claimed in claim 2, it is characterized in that: described first interface arrangment (2), including locking switch (21), locking bolt (22), lock slots (23), described locking switch (21) and fixing unmanned plane (1) bottom that is connected in of locking bolt (22) are close to cavity (4) opening part, described lock slots (23) is correspondingly arranged on battery (6), realizes locking bolt (22) and lock slots (23) phase interlocking by stirring described locking switch (21).
4. unmanned plane battery connecting construction as claimed in claim 3, it is characterized in that: described cavity (4) is provided with through hole (11) in close opening part position and communicates with described cavity (4), described locking switch (21) is arranged at described through hole (11) place and is positioned at described cavity (4) outward, and locking bolt (22) extend in described cavity (4) through described through hole (11) accordingly.
5. unmanned plane battery connecting construction as claimed in claim 4, it is characterized in that: the position of the corresponding described through hole of described battery holder (61) (11) is provided with a projection (62), described lock slots (23) is opened on described projection (62), and described battery (6) inserts described projection (62) after in described cavity (4) and aligns with described through hole (11).
6. unmanned plane battery connecting construction as claimed in claim 2, it is characterized in that: described second interface arrangment (3), including shackle member (31) and clamping position (32), shackle member (31) is arranged on described battery holder (61), it is internal that clamping position (32) is arranged at cavity (4), realizes unmanned plane (1) by shackle member (31) and clamping position (32) phase clamping and battery (6) is connected.
7. unmanned plane battery connecting construction as claimed in claim 6, it is characterized in that: described shackle member (31), including by compressing switch (311) and buckle (312), by compressing switch (311) and buckle (312) is connected to one, described in pressing, realize buckle (312) and the phase clamping of described clamping position (32) by compress switch (311).
8. unmanned plane battery connecting construction as claimed in claim 7, it is characterized in that: the both sides of described battery holder (61) are respectively provided with a shackle member (31), described shackle member (31) be positioned at battery holder (61) two side position stretching out cavity (4) outward by compress switch (311), described buckle (312) correspondence is positioned at battery holder (61) two side position stretching into cavity (4).
9. unmanned plane battery connecting construction as claimed in claim 8, it is characterized in that: corresponding described cavity (4) inwall two side position that is arranged at of described clamping position (32), described clamping position (32) is in the groove-like matched with described buckle (312).
10. unmanned plane battery connecting construction as claimed in claim 2, it is characterised in that: described battery holder (61) is provided with and can be connected with unmanned plane energising interface and be embodied as the electrical contact mouth (63) that unmanned plane is powered.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620378095.5U CN205633053U (en) | 2016-04-29 | 2016-04-29 | Unmanned aerial vehicle battery connection structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620378095.5U CN205633053U (en) | 2016-04-29 | 2016-04-29 | Unmanned aerial vehicle battery connection structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205633053U true CN205633053U (en) | 2016-10-12 |
Family
ID=57061033
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620378095.5U Expired - Fee Related CN205633053U (en) | 2016-04-29 | 2016-04-29 | Unmanned aerial vehicle battery connection structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205633053U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11981226B2 (en) | 2017-07-19 | 2024-05-14 | Ford Global Technologies, Llc | Swappable battery system |
-
2016
- 2016-04-29 CN CN201620378095.5U patent/CN205633053U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11981226B2 (en) | 2017-07-19 | 2024-05-14 | Ford Global Technologies, Llc | Swappable battery system |
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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: 20161012 |