CN207015593U - Battery mounting box for unmanned plane - Google Patents
Battery mounting box for unmanned plane Download PDFInfo
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- CN207015593U CN207015593U CN201720631449.7U CN201720631449U CN207015593U CN 207015593 U CN207015593 U CN 207015593U CN 201720631449 U CN201720631449 U CN 201720631449U CN 207015593 U CN207015593 U CN 207015593U
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Abstract
The utility model discloses a kind of battery mounting box for unmanned plane, including bottom plate, two block length plates and three pieces of short slabs, the edge on four sides of bottom plate is provided with multiple first projections, the top and a left side of two block length plates, the edge of right two sides is designed with multiple second projections, jack is provided with long slab, the top of three pieces of short slabs, it is left, the edge of right two sides is designed with and cross one another the 3rd projection in dentation of the first projection and the second projection, bottom plate, two block length plates and three pieces of short slabs pass through the first projection, jack, second projection and the 3rd projection are mutually inserted and battery mounting box are separated into big chamber and small chamber by centrally located short slab, the bottom of two block length plates is provided with two pieces of connecting plates, the first slot is offered on connecting plate, the outwardly formation contiguous block in one end of long slab, the second slot is provided with contiguous block.Battery mounting box is connected in the fix bar of fuselage interior by the utility model by the first slot, the second slot, battery mounting box is fixed with fuselage.
Description
Technical field
It the utility model is related to the technical field for unmanned plane of taking photo by plane, especially a kind of battery mounting box for unmanned plane.
Background technology
Take photo by plane unmanned plane power supply source be usually battery is set in unmanned plane, battery is directly installed on fuselage
Interior, when unmanned plane carries out flight shooting, battery is likely to arbitrarily rock, and battery and airframe is sustained damage,
Also the aerial photography effect of unmanned plane can be influenceed, it is cumbersome and time consuming.
Utility model content
The technical problems to be solved in the utility model is：In order to solve to be asked existing for the prior art in above-mentioned background technology
A kind of topic, there is provided improved battery mounting box for unmanned plane.
Technical scheme is used by the utility model solves its technical problem：A kind of battery for unmanned plane is installed
Box, including bottom plate, two block length plates and three pieces of short slabs, three pieces of short slabs are set up in parallel, and the edge on four sides of described bottom plate is provided with
It is in dentation that multiple the first projections in dentation, the described top of two block length plates and the edge on arranged on left and right sides side, which are designed with multiple,
The second projection, be provided with the jack for the insertion of the first projection on long slab, the tops of described three pieces of short slabs, arranged on left and right sides side
Edge is designed with multiple and the first projection and cross one another the 3rd projection in dentation of the second projection, is provided with long slab for being located at
The middle socket of 3rd projection grafting of the short slab in centre position, described bottom plate, two block length plates and three pieces of short slabs pass through first
Projection, jack, the second projection and the 3rd being mutually inserted for projection and be fixedly connected and by centrally located short slab by electricity
Pond mounting box is separated into big chamber and small chamber, and the bottom of two described block length plates is provided with two pieces of connecting plates, opened on connecting plate
The first slot provided with connection external component, the outwardly formation contiguous block in one end of described long slab, the company of being provided with contiguous block
Connect the second slot of external component.
Described battery mounting box includes being used for the bundling belt for reinforcing battery mounting box.
The fixed plate of fixation binding band is provided between two pieces of described connecting plates.
The beneficial effects of the utility model are, of the present utility model simple in construction, simple operation, can be inserted by first
Battery mounting box is connected in the fix bar of fuselage interior by groove, the second slot, carries out consolidating for battery mounting box and airframe
Fixed connection, the influence to caused by battery, convenient disassembly, improves operating efficiency when avoiding unmanned plane during flying.
Brief description of the drawings
The utility model is further illustrated with reference to the accompanying drawings and examples.
Fig. 1 is structural representation of the present utility model.
Fig. 2 is front view of the present utility model.
Fig. 3 is Fig. 2 top view.
Fig. 4 is Fig. 2 upward view.
Fig. 5 is Fig. 2 left view.
In figure：1st, bottom plate, the 11, first projection, 2, long slab, the 21, second projection, 3, short slab, the 31, the 3rd projection, 4, connection
Plate, the 41, first slot, 5, contiguous block, the 51, second slot, 6, big chamber, 7, small chamber.
Embodiment
The utility model is described in further detail presently in connection with accompanying drawing.These accompanying drawings are simplified schematic diagram,
Only illustrate basic structure of the present utility model in a schematic way, therefore it only shows the composition relevant with the utility model.
As Figure 1-Figure 5, the battery mounting box for unmanned plane, including bottom plate 1, two block length plates 2 and three pieces of short slabs 3,
Three pieces of short slabs 3 are set up in parallel, and the edge on four sides of bottom plate 1 is provided with multiple the first projections 11 in dentation, two block length plates 2 it is upper
While and edge during arranged on left and right sides be designed with multiple the second projections 21 in dentation, be provided with long slab 2 and inserted for the first projection 11
Jack, top, the edge on arranged on left and right sides side of three pieces of short slabs 3 are designed with multiple with the first projection 11 and the phase of the second projection 21
The 3rd projection 31 in dentation mutually intersected, the grafting of the 3rd projection 31 for centrally located short slab 3 is provided with long slab 2
Middle socket, bottom plate 1, two block length plates 2 and three pieces of short slabs 3 pass through the first projection 11, jack, the second projection 21 and the 3rd projection 31
Be mutually inserted and be fixedly connected and battery mounting box is separated into by big chamber 6 and small chamber by centrally located short slab 3
Room 7, the bottom of two block length plates 2 are provided with two pieces of connecting plates 4, and the first slot 41 of connection external component is offered on connecting plate 4,
Outwardly the second slot 51 for forming contiguous block 5, connection external component being provided with contiguous block 5 in one end of long slab 2.
Battery mounting box includes being used for the bundling belt for fixing battery, after battery is put into big chamber 8 and small chamber 9,
After bundling belt is fastened, fixed battery.
The fixed plate 8 of fixation binding band is provided between two pieces of connecting plates 4.
Long slab 2, connecting plate 4 and contiguous block 5 are integrally formed.
In use, first passing through the first projection 11, the second projection 4, the 3rd projection 5 is mutually inserted the bottom plate for making battery mounting box
1st, two block length plates 2 and three pieces of short slabs 3 assemble, after battery is put into big chamber 8 and small chamber 9, by the both ends of bundling belt
Mutually fasten, then battery mounting box be put into the inner chamber of fuselage, fuselage inner chamber is provided with two fix bars, the first slot 61 with
Second slot 71 is plugged in two fix bars respectively, and this completes the fixation of battery mounting box.
Using it is above-mentioned according to desirable embodiment of the present utility model as enlightenment, pass through above-mentioned description, related work people
Member can carry out various changes and amendments in the range of without departing from this item utility model technological thought completely.This item is real
The content being not limited to new technical scope on specification, it is necessary to which its technology is determined according to right
Property scope.
Claims (3)
1. a kind of battery mounting box for unmanned plane, it is characterized in that：Including bottom plate (1), two block length plates (2) and three pieces of short slabs
(3), three pieces of short slabs (3) are set up in parallel, and the edge on four sides of described bottom plate (1) is provided with multiple the first projections in dentation
(11), the described top of two block length plates (2) and the edge on arranged on left and right sides side are designed with multiple the second projections in dentation
(21) jack for the first projection (11) insertion, the top of described three pieces of short slabs (3), arranged on left and right sides, are provided with long slab (2)
The edge on side is designed with multiple and the first projection (11) and cross one another the 3rd projection (31) in dentation of the second projection (21),
The middle socket of the 3rd projection (31) grafting for centrally located short slab (3), described bottom plate are provided with long slab (2)
(1), two block length plates (2) pass through the first projection (11), jack, the second projection (21) and the 3rd projection (31) with three pieces of short slabs (3)
Be mutually inserted and be fixedly connected and by centrally located short slab (3) by battery mounting box be separated into big chamber (6) and
Small chamber (7), the bottom of two described block length plates (2) are provided with two pieces of connecting plates (4), and it is outer that connection is offered on connecting plate (4)
The first slot (41) of portion's part, one end of described long slab (2) is outwardly to form contiguous block (5), and contiguous block is provided with (5)
Connect the second slot (51) of external component.
2. the battery mounting box according to claim 1 for unmanned plane, it is characterized in that：Described battery mounting box includes
For reinforcing the bundling belt of battery mounting box.
3. the battery mounting box according to claim 2 for unmanned plane, it is characterized in that：Two pieces of described connecting plates (4)
Between be provided with the fixed plate (8) of fixation binding band.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720631449.7U CN207015593U (en) | 2017-06-02 | 2017-06-02 | Battery mounting box for unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720631449.7U CN207015593U (en) | 2017-06-02 | 2017-06-02 | Battery mounting box for unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207015593U true CN207015593U (en) | 2018-02-16 |
Family
ID=61477092
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720631449.7U Active CN207015593U (en) | 2017-06-02 | 2017-06-02 | Battery mounting box for unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207015593U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110510101A (en) * | 2019-10-08 | 2019-11-29 | 漳州鹰航电子科技有限公司 | A kind of aircraft |
-
2017
- 2017-06-02 CN CN201720631449.7U patent/CN207015593U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110510101A (en) * | 2019-10-08 | 2019-11-29 | 漳州鹰航电子科技有限公司 | A kind of aircraft |
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| GR01 | Patent grant |