CN209650555U - A kind of adjustable unmanned plane of number of batteries - Google Patents
A kind of adjustable unmanned plane of number of batteries Download PDFInfo
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- CN209650555U CN209650555U CN201822128351.7U CN201822128351U CN209650555U CN 209650555 U CN209650555 U CN 209650555U CN 201822128351 U CN201822128351 U CN 201822128351U CN 209650555 U CN209650555 U CN 209650555U
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Abstract
The utility model relates to unmanned plane fields, disclose a kind of adjustable unmanned plane of number of batteries, including battery and fuselage, and fuselage roof is equipped with cavity, and battery is fixed in cavity, and the quantity for the battery installed in cavity is adjustable, in parallel between multiple batteries.The unmanned plane can change the carry ability of unmanned plane by adjusting the quantity for the battery wherein installed, and improve the adaptability of unmanned plane.
Description
Technical field
The utility model relates to unmanned plane field more particularly to a kind of adjustable unmanned planes of number of batteries.
Background technique
In recent years, with the development of science and technology unmanned plane has in the fields such as military, civilian is more and more widely used.
Lithium battery has the advantages that energy density is high, good cycle, memory-less effect, and unmanned plane mainly uses lithium battery conduct at present
Lithium battery is integrated on unmanned plane by power.But since battery is integrated on unmanned plane, so charging is inconvenient, and
And the constant number of battery, it both can not extend the cruise duration of unmanned plane by increasing number of batteries, and can not also pass through reduction
Number of batteries improves the load-carrying upper limit of unmanned plane.Therefore, the adaptability to changes of unmanned plane in the prior art is insufficient, can not basis
The quantity of battery is adjusted in the weight size of unmanned plane institute carry object.
Utility model content
For overcome the deficiencies in the prior art, the utility model provides a kind of adjustable unmanned plane of number of batteries, this nobody
Machine can be adjusted the quantity of battery according to the weight size of institute's carry object.
The technical scheme adopted by the utility model to solve the technical problem is as follows:
A kind of adjustable unmanned plane of number of batteries, including battery and fuselage are provided, the fuselage roof is equipped with cavity, institute
It is fixed in the cavity to state battery, the quantity of the battery of installation is adjustable in the cavity, between multiple batteries
It is in parallel.
As a further improvement of the above technical scheme, the quantity of the battery is odd number.
As a further improvement of the above technical scheme, battery described in odd number is fixed in the cavity in parallel, is in
The most intermediate battery is located on the center of gravity line of the fuselage, remaining described battery be located at the front and rear sides of the center of gravity line and
It is symmetrically placed about the center of gravity line.
As a further improvement of the above technical scheme, the quantity of the battery is even number.
As a further improvement of the above technical scheme, battery described in even number is fixed in the cavity in parallel, is located at
The battery of the front and rear sides of the center of gravity line is symmetrically placed about the center of gravity line.
As a further improvement of the above technical scheme, the fuselage bottom is equipped with hook, hangs with needs on the hook
The cargo of delivery, the hook are located on the center of gravity line.
As a further improvement of the above technical scheme, the cavity bottom is equipped with groove, and the battery bottom is equipped with convex
Block, the convex block are caught in the groove.
As a further improvement of the above technical scheme, handle is fixed at the top of the battery.
The beneficial effects of the utility model are: changing unmanned plane by the quantity for adjusting the battery installed in unmanned plane
Carry ability improves the adaptability of unmanned plane.
Detailed description of the invention
The present invention will be further described with reference to the accompanying drawings and examples:
Fig. 1 is the stereoscopic schematic diagram of the utility model one embodiment；
Fig. 2 is the stereoscopic schematic diagram of the battery of the utility model one embodiment；
Fig. 3 is the side view of the battery of the utility model one embodiment.
Specific embodiment
It is carried out below with reference to technical effect of the embodiment and attached drawing to the design of the utility model, specific structure and generation
Clear, complete description, to be completely understood by the purpose of this utility model, scheme and effect.It should be noted that not conflicting
In the case where, the features in the embodiments and the embodiments of the present application can be combined with each other.
It should be noted that unless otherwise specified, when a certain feature referred to as " fixation ", " connection " are in another feature,
It can directly fix, be connected to another feature, and can also fix, be connected to another feature indirectly.In addition, this
The descriptions such as up, down, left, right, before and after used in utility model are only relative to each composition portion of the utility model in attached drawing
For the mutual alignment relation divided.
In addition, unless otherwise defined, the technology of all technical and scientific terms used herein and the art
The normally understood meaning of personnel is identical.Term used in the description is intended merely to description specific embodiment herein, without
It is to limit the utility model.Term " and or " used herein includes appointing for one or more relevant listed items
The combination of meaning.
Referring to Fig.1-3, the stereoscopic schematic diagram of the utility model one embodiment and the battery of one embodiment are shown
Stereoscopic schematic diagram, unmanned plane include fuselage 1 and battery 2, have the cavity of a placing battery 2 at the top of fuselage 1, battery 2 is side by side
It is placed in cavity.Fluted in cavity bottom, the bottom of battery 2 is equipped with convex block 21, and convex block 21 is caught in the recessed of cavity bottom
In slot.The top of battery 2 is fixed with handle, is removed or placed into battery 2 out of groove with facilitating.
It is equipped with hook in the bottom of fuselage 1, the object delivered can will be needed to hang on hook and transported.Hook is located at machine
On the center of gravity line of body, it can guarantee that hung object is located on body nodal point line in this way, facilitate unmanned plane in flight course
Balance is kept, avoids flying shakiness due to hung object, which deviates body nodal point line, leads to unmanned plane inclination.
Multiple batteries 2 can be placed in the cavity of fuselage roof, the quantity of the battery 2 of placement can be according to the weight of carry object
And it is adjusted.If the weight for the object for needing to transport is smaller, then it can increase the installation number of battery 2, to improve nobody
The cruising ability of machine；If the weight for the object for needing to transport is larger, and the distance for needing to transport is shorter, then appropriate can reduce
The installation number of battery 2, thus increase unmanned plane can object carrier upper weight limit.
When the quantity for the battery installed is odd number, the battery in most middle position is in a column battery placed side by side
Center of gravity line be overlapped with the center of gravity line of fuselage, remaining battery is distributed in the front and rear sides of body nodal point line, before and after body nodal point line
Two sides distribution number of batteries it is equal, and be distributed in body nodal point line front and rear sides battery position about body nodal point line pair
Claim.If need the object of carry heavier, then the battery at the symmetric position of body nodal point line front and rear sides can be removed in pairs,
When needing the object of carry overweight, and when the distance that needs to transport is shorter, it might even be possible to only leave at body nodal point line
One piece of battery.
When the quantity of the battery of installation is even number, the number of batteries positioned at body nodal point line front and rear sides is equal, and point
The position for being distributed in the battery of body nodal point line front and rear sides is symmetrical about body nodal point line.If needing the object of carry heavier
When, then can remove the battery at the symmetric position of body nodal point line front and rear sides in pairs, when need carry object it is overweight when, very
It extremely can only leave the front and rear sides for being located at body nodal point line and the two piece batteries symmetrically placed about body nodal point line.
It is in parallel between multiple lithium batteries to be connect with external circuit.It is logical that each individually lithium battery can form one with external circuit
Road, therefore, even if wherein there is one piece of battery failure, remaining battery still can continue to be powered unmanned plane.And if
The series connection of muti-piece battery is connect with external circuit, and one of battery failure then will lead to open circuit, can not work normally unmanned plane.
And the whole power supply that muti-piece battery parallel connection is formed has more electricity compared with monoblock battery, can extend nothing
Allow to execute remote task man-machine cruise duration.
It is illustrating for progress to be implemented to the preferable of the utility model, but the invention is not limited to the reality above
Example is applied, those skilled in the art can also make various equivalent variations without departing from the spirit of the present invention
Or replacement, these equivalent deformations or replacement are all included in the scope defined by the claims of the present application.
Claims (8)
1. a kind of adjustable unmanned plane of number of batteries, including battery and fuselage, which is characterized in that the fuselage roof is equipped with sky
Chamber, the battery is fixed in the cavity, and the quantity for the battery installed in the cavity is adjustable, multiple batteries
Between it is in parallel.
2. the adjustable unmanned plane of number of batteries according to claim 1, which is characterized in that the quantity of the battery is surprise
Number.
3. the adjustable unmanned plane of number of batteries according to claim 2, which is characterized in that battery described in odd number is solid in parallel
Determine in the cavity, on the center of gravity line that the most intermediate battery is located at the fuselage, remaining described battery is located at institute
State front and rear sides of center of gravity line and symmetrically placed about the center of gravity line.
4. the adjustable unmanned plane of number of batteries according to claim 1, which is characterized in that the quantity of the battery is even
Number.
5. the adjustable unmanned plane of number of batteries according to claim 4, which is characterized in that battery described in even number is solid in parallel
Determine in the cavity, the battery positioned at the front and rear sides of the center of gravity line of the fuselage is symmetrically placed about the center of gravity line.
6. the adjustable unmanned plane of the number of batteries according to claim 3 or 5, which is characterized in that the fuselage bottom is equipped with
It links up with, the cargo for needing to deliver is hung on the hook, the hook is located on the center of gravity line.
7. the adjustable unmanned plane of number of batteries according to claim 6, which is characterized in that the cavity bottom is equipped with recessed
Slot, the battery bottom are equipped with convex block, and the convex block is caught in the groove.
8. the adjustable unmanned plane of number of batteries according to claim 7, which is characterized in that be fixed at the top of the battery
Handle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822128351.7U CN209650555U (en) | 2018-12-18 | 2018-12-18 | A kind of adjustable unmanned plane of number of batteries |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822128351.7U CN209650555U (en) | 2018-12-18 | 2018-12-18 | A kind of adjustable unmanned plane of number of batteries |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209650555U true CN209650555U (en) | 2019-11-19 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822128351.7U Active CN209650555U (en) | 2018-12-18 | 2018-12-18 | A kind of adjustable unmanned plane of number of batteries |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113955067A (en) * | 2021-11-17 | 2022-01-21 | 青岛科技大学 | Modular battery power supply system of container ship |
-
2018
- 2018-12-18 CN CN201822128351.7U patent/CN209650555U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113955067A (en) * | 2021-11-17 | 2022-01-21 | 青岛科技大学 | Modular battery power supply system of container ship |
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