CN207303190U - Battery module and unmanned plane - Google Patents
Battery module and unmanned plane Download PDFInfo
- Publication number
- CN207303190U CN207303190U CN201721279705.7U CN201721279705U CN207303190U CN 207303190 U CN207303190 U CN 207303190U CN 201721279705 U CN201721279705 U CN 201721279705U CN 207303190 U CN207303190 U CN 207303190U
- Authority
- CN
- China
- Prior art keywords
- battery
- lock
- battery compartment
- unmanned plane
- battery body
- 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.)
- Expired - Fee Related
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Classifications
-
- 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
- H01M50/249—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders specially adapted for aircraft or vehicles, e.g. cars or trains
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/42—Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells
- H01M10/48—Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte
-
- 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
- H01M50/204—Racks, modules or packs for multiple batteries or multiple cells
-
- 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
Abstract
The utility model discloses a kind of battery module and unmanned plane, and battery module includes the battery body being detachably mounted in battery compartment, and battery body is equipped with least one latch components.Each latch components include lock pin and elastic component.Lock pin is slidingly disposed at the surface of battery body, and lock pin has connecting pin and lock end.Elastic component is resiliently attached between battery body and connecting pin.Wherein, when battery body is installed in battery compartment, resilient element urges lock is sold and lock end is caught in lock buckling groove.The utility model proposes battery module, using lock pin and the design of the cooperation of the lock buckling groove of battery compartment, can ensure the reliability of connection when battery module is installed in battery compartment.Meanwhile the utility model is slidably connected to the design of battery body using lock pin through elastic component, makes installing process more convenient laborsaving.
Description
Technical field
It the utility model is related to a kind of battery module and unmanned plane.
Background technology
In the field such as unmanned vehicle and its remote controler, the mounting design of currently used battery module is to utilize battery
Two elastic hooks in module catch on aircraft body.When aircraft shakes, elastic hook is impacted and due to existing
The component for disengaging elastic hook, elastic hook, which may disengage, causes the connection of battery module and aircraft to loosen, so as to cause
The reliability of existing battery module installation or buckle structure is relatively low.In order to overcome the component that this disengages hook, elastic hook
Elastic force can generally set very big, cause user installation or to apply larger operating force when taking out battery module to solve
Lock.In addition, user is when installing battery module, it is understood that there may be elastic hook does not have in existing design without the situation in place of fastening
There is the design being detected for such case, thus connect the risk loosened with aircraft there are larger battery module.
Utility model content
One main purpose of the utility model is at least one defect for overcoming the above-mentioned prior art, there is provided Yi Zhongan
Rapid operation and the battery module being connected firmly during dress.
Another main purpose of the utility model is at least one defect for overcoming the above-mentioned prior art, there is provided a kind of
The unmanned plane that rapid operation and battery are connected firmly when installing battery.
To achieve the above object, the utility model adopts the following technical solution：
One side according to the present utility model, there is provided a kind of battery module, for powering for unmanned plane.The unmanned plane
Including a battery compartment, the battery module is installed in the battery compartment, and the battery compartment offers lock buckling groove.Wherein, it is described
Battery module includes the battery body being detachably mounted in the battery compartment, and the battery body is equipped with least one lock
Component.Each latch components include lock pin and elastic component.The lock pin is slidingly disposed at the battery body
Surface, it is described lock pin have connecting pin and lock end.The elastic component is resiliently attached to the battery body and the company
Connect between end.Wherein, when the battery body is installed in the battery compartment, lock is sold and makes institute described in the resilient element urges
Lock end is stated to be caught in the lock buckling groove.
One of embodiment according to the present utility model, the battery module further include position detector.Institute's rheme
Put detector to be arranged on the battery body and be adjacent to the lock pin, compress the elastic component to detect the lock pin edge
Whether the distance that direction is slided exceedes predetermined threshold value.
One of embodiment according to the present utility model, the quantity of the position detector and the latch components phase
Together, and with the lock pin correspond, with detect respectively the lock pin be along compress that the elastic component direction slides away from
From whether exceeding the predetermined threshold value.
Other side according to the present utility model, there is provided a kind of unmanned plane, wherein, the unmanned plane includes fuselage, electricity
Chi Cang and battery module.The battery compartment is formed at the fuselage, and the battery compartment offers lock buckling groove.The battery module
For the battery module described in the above embodiment.
One of embodiment according to the present utility model, the battery compartment top is equipped with an opening, for the electricity
Pond body is arranged on the battery body side by loading the battery compartment, the latch components at the top of the battery compartment.
One of embodiment according to the present utility model, the lock end is in the wedge structure being downwardly inclined；With/
Or, the latch components are two, two latch components are respectively arranged on the both sides of the battery body.
One of embodiment according to the present utility model, the battery compartment have the tail end for being close in the connecting pin
With the front end for being close in the lock end；Wherein, the top member-retaining portion roof of the battery compartment tail end and form card slot, for
After the battery body tail end is caught in the card slot, its front end rotates and the battery body is installed in the battery still further below
Storehouse.
One of embodiment according to the present utility model, the position for corresponding to the lock pin of the battery compartment are opened
Equipped with opening, the lock pin part is exposed to the opening.
One of embodiment according to the present utility model, the battery compartment bottom are equipped with elastic parts, with to installing
Apply an elastic force in the battery body in the battery compartment；Wherein, the lock pin is in non-button with the lock buckling groove
During conjunction state, the elastic parts can eject the battery module.
One of embodiment according to the present utility model, the elastic parts include pedestal, bullet block and elastic component.
The seat is fixed on the battery compartment.The bullet block is arranged on the pedestal.The elastic component is connected to the pedestal and institute
State between bullet block.Wherein, when the battery body is installed in the battery compartment, the bullet block is resisted against the battery body.
As shown from the above technical solution, the utility model proposes battery module and unmanned plane the advantages of and good effect
It is：
The utility model proposes battery module and unmanned plane, utilize lock pin and the cooperation of the lock buckling groove of battery compartment
Design, can ensure the reliability of connection when battery module is installed in battery compartment.Meanwhile the utility model utilizes lock pin warp
Elastic component is slidably connected to the design of battery body, makes installing process more convenient laborsaving.
Brief description of the drawings
The detailed description of the following preferred embodiment to the utility model is considered in conjunction with the accompanying drawings, the utility model
Various targets, feature and advantage will become apparent.Attached drawing is only the exemplary diagram of the utility model, not necessarily
It is drawn to scale.In the accompanying drawings, same reference numeral represents same or similar component all the time.Wherein：
Fig. 1 is a kind of decomposition diagram of battery module according to an illustrative embodiments；
Fig. 2 is the assembling schematic diagram of the battery module shown in Fig. 1；
Fig. 3 is the sectional view (one) of the battery module shown in Fig. 1；
Fig. 4 is the sectional view (two) of the battery module shown in Fig. 1；
Fig. 5 is the sectional view (three) of the battery module shown in Fig. 1；
Fig. 6 is the sectional view (four) of the battery module shown in Fig. 1；
Fig. 7 is the assembling schematic diagram of another angle of the battery module shown in Fig. 1.
Wherein, the reference numerals are as follows：
100. battery compartment；
100 ', fuselage；
101. lock buckling groove；
102. card slot；
103. opening；
110. elastic parts；
111. pedestal；
112. bullet block；
113. elastic component；
200. battery body；
210. latch components；
211. lock pins；
212. elastic component；
300. detection switch；
400. connector.
Embodiment
Embodying the exemplary embodiments of the utility model features and advantages will describe in detail in the following description.It should be understood that
It is that the utility model can have various changes in different embodiments, it does not all depart from the scope of the utility model, and
Explanation therein and attached drawing are inherently illustrative, and are not used to limitation the utility model.
In being described below the different illustrative embodiments to the utility model, carry out referring to the drawings, the attached drawing
The part of the utility model is formed, and wherein shows many aspects of achievable the utility model by way of example not
Same example arrangement, system and step.It is to be understood that other of component, structure, exemplary means, system and step can be used
Specified scheme, and structural and functional modification can be carried out in the case of without departing from the scope of the utility model.Although moreover, originally
Can be used in specification term " upper end ", " bottom ", " between ", " side " etc. the different exemplary of the utility model is described
Feature and element, but these terms are with this article merely for convenient, for example, with reference to the accompanying drawings described in exemplary direction.This
Any content in specification is not necessarily to be construed that the specific three dimensional direction of Structure of need is just fallen into the scope of the utility model.
Battery module embodiment
Refering to Fig. 1, the decomposition that the battery module for the principle that can embody the utility model is representatively illustrated in Fig. 1 is shown
It is intended to.In the illustrative embodiments, the utility model proposes battery module be to be assemblied in the battery of unmanned vehicle
Further, illustrated by taking the battery module being assemblied on unmanned aerial vehicle body as an example exemplified by module.People in the art
Member is it is easily understood that be that the battery module is assemblied in other kinds of equipment, and following embodiments is done
Go out it is a variety of remodeling, addition, substitute, delete or other change, these change still the utility model proposes battery module original
In the range of reason.
As shown in Figure 1, in the present embodiment, the utility model proposes battery module mainly include removably installing
In the battery body 200 in battery compartment 100.Cooperation refers to Fig. 2 to Fig. 7, and the assembling of battery module is representatively illustrated in Fig. 2
Schematic diagram, the specific state represented when battery body 200 is installed in battery compartment 100；Fig. 3 to Fig. 6 is representatively shown respectively
Sectional view (one)~(four) of battery module different angle or position.Fig. 7 representatively illustrates the battery module shown in Fig. 1
Another angle assembling schematic diagram.Below in conjunction with above-mentioned attached drawing, to the utility model proposes each main group of battery module
Structure, connection mode and functional relationship into part are described in detail.
As depicted in figs. 1 and 2, in the present embodiment, battery compartment 100 is installed in the fuselage 100 ' of unmanned plane, with
In the lower explanation with reference to other accompanying drawings, only battery compartment 100 and battery body 200 are illustrated, repeat no more related battery compartment
100 with the structural relation of fuselage 100 ', specifically refer to the embodiment of existing unmanned plane and its battery compartment, but not as
Limit.Battery compartment 100 is in substantially the box structure with inner cavity and open top, so that battery body 200 loads battery by top
Storehouse 100 is simultaneously placed in the inner cavity of battery compartment 100.Wherein, the shape of 100 inner cavity of battery compartment and the shape of battery body 200 are big
Matching is caused, the phenomenon for producing and rocking is loaded after battery compartment 100 to avoid battery body 200.
As shown in Figure 3 and Figure 4, in the present embodiment, the both sides of battery body 200 are respectively equipped with latch components 210.Its
In, each latch components 210 mainly include lock pin 211 and elastic component.Specifically, lock pin 211 is slidingly disposed at electricity
The surface of pond body 200, lock pin 211 have connecting pin and lock end.Elastic component is resiliently attached to battery body 200 with being connected
Between end, and the elastic component is preferably a spring 212.
As shown in Figure 1, the position that 100 inner wall of battery compartment corresponds to lock end offers lock buckling groove 101, battery body 200
When being installed in the battery compartment 100 of unmanned plane, resilient element urges latch pin 211 and lock end is caught in lock buckling groove 101.Specifically
For, which can be by the way that 100 inner wall of battery compartment to be corresponded to the part at lock end towards the portion outside battery compartment 100
Divide and excavate and formed, and projection of the lock buckling groove 101 on 100 surface of battery compartment (being side in present embodiment) where it
Shape, can be preferably the form fit with latching end.In addition, the width of lock buckling groove 101 is greater than or equal to lock pin 211
Width, in present embodiment using lock buckling groove 101 width slightly larger than the width of lock pin 211 design.
It should be noted that in the present embodiment, due to 100 open top of battery compartment, so that battery body 200 is by battery
The top of storehouse 100 loads battery compartment 100, therefore is provided in battery body for the ease of the operation of operator, latch components 210
200 side.In other embodiments, when the opposite rigging position of battery body 200 and battery compartment 100, which is sent, to be changed,
The setting position of latch components 210 can also be adjusted flexibly, to meet the operation needs of operator.
As shown in figure 5, in the present embodiment, battery module further includes position detector.The position detector is arranged on
In battery body 200 and lock pin 211 is adjacent to, to detect whether lock pin 211 slides towards elastic component direction.
Specifically, as shown in figure 5, in the present embodiment, position detector can be preferably a detection switch 300,
And the detection switch 300 is set close to the connecting pin of lock pin 211.When lock pin 211 is located at latched position, detection switch
300 are in free state (as shown in Figure 5), and the circuit of detection switch 300 is in the conduction state at this time.When lock pin 211 backward
When (towards tail end direction) slides into certain position, detection trigger switchs 300 and disconnects the circuit of detection switch 300, battery
The relevant control mechanism of module responds according to this off-state, reminds the lock pin 211 of operator's battery body 200 and does not have
Fastening.
Further, in the present embodiment, the quantity of position detector is identical with latch components 210, and is sold with lock
211 correspond, to detect whether each lock pin 211 slides towards its elastic component direction connected respectively.
It should be noted here that the battery module for showing in attached drawing and describing in the present specification is only that can use this hair
An example in many kinds of battery modules of bright principle.It should be clearly understood that the principle of the present invention is only limitted to absolutely not attached drawing
In show or this specification described in any details of battery module or any part of battery module.
Unmanned aerial vehicle mode
In the illustrative embodiments, the utility model proposes unmanned plane be so that battery module is installed in fuselage
Structure exemplified by illustrate.It will be readily appreciated by those skilled in the art that for the design of the embodiment is applied to it
In the unmanned plane of his battery module rigging position, and following embodiments is made and a variety of retrofit, add, substituting, deleting
Remove or other change, these change still the utility model proposes unmanned plane principle in the range of.
In the present embodiment, the utility model proposes unmanned plane, it is mainly new including fuselage, battery compartment and this practicality
Battery module described in type the above embodiment.Specifically, battery compartment is formed at fuselage, its concrete structure design refers to
The explanation in battery module embodiment is stated, it will not be described here.Likewise, the structure of battery module and its latch components also may be used
With reference to the design of battery module and its latch components in above-mentioned battery module embodiment.In addition, in battery module embodiment
The design such as position detector be equally applicable for the utility model proposes unmanned plane structure design in, not with this reality
The mode of applying is limited.
Further, as depicted in figs. 1 and 2, in the present embodiment, battery compartment 100 correspond to two lock pins 211
Position (i.e. the both sides bulkhead of battery compartment 100) offer opening 103 respectively, two lock pins 211 are partly exposed to two respectively
A opening 103, so that operator operates.
Further, as shown in Figure 3 and Figure 4, in the present embodiment, the lock end for latching pin 211 is substantially in that court has a down dip
Oblique wedge structure.By above-mentioned design, the lock end of lock pin 211 can be made more swimmingly to be caught in lock buckling groove 101, reduced
The operating force that battery body 200 applies needed for operator during load battery compartment 100.Correspondingly, based on lock pin 211
The design of the wedge structure at end is latched, lock buckling groove 101 also can be substantially in downward in the shape of 100 side projection one end of battery compartment
Inclined wedge structure.
Further, as shown in figure 3, in the present embodiment, defining battery compartment 100 has tail end and front end, lock pin
211 connecting pin is close in the tail end of battery compartment 100, and the front end of battery compartment 100 is closed at the lock end of lock pin 211, similarly,
Battery body 200 also has tail end and front end, and the tail end of battery body 200, lock pin are closed in the connecting pin for latching pin 211
The front end of battery body 100 is closed at 211 lock end.Wherein, the top member-retaining portion roof of 100 tail end of battery compartment and form card
Groove 102, after being caught in card slot 102 for 200 tail end of battery body, its front end rotates and is installed in battery body 200 still further below
Battery compartment 100.
In the present embodiment, elastic parts 110 is additionally provided with battery compartment 100, with to the electricity being installed in battery compartment 100
Pond body 200 applies an elastic force, so that lock pin 211 does not fasten the battery body 200 of (non-buckling state) by battery compartment
100 pop-ups.Further, the structure design of the tail end formation card slot 102 based on battery compartment in present embodiment 100, elastic group
Part 110 is preferably arranged on the front end of battery compartment 100, i.e. elastic parts 110 is that the elastic force is applied to battery sheet
The front end of body 200.
As shown in Figure 6 and Figure 7, in the present embodiment, the elastic parts 110 mainly include pedestal 111, bullet block 112 with
And elastic component.Specifically, pedestal 111 is fixed on battery compartment 100, and bullet block 112 is arranged on the top of pedestal 111, elastic component connection
Between pedestal 111 and bullet block 112, and the elastic component can be preferably a spring 113.Based on above-mentioned design, work as battery body
During 200 loading battery compartment 100, bullet block 112 is resisted against the front end of battery body 200, and the elastic force that elastic component compression produces passes through
Bullet block 112 is delivered to battery body 200.At this time, as lock pin 211 does not fasten (non-buckling state) and operator does not apply electricity
Pond body 200 is pressed into the operating force of battery compartment 100, then under the action of above-mentioned elastic force, elastic parts 110 is by battery body
200 front end pop-up, so as to reach the effect of helping operator conveniently and efficiently to take out battery body 200.Furthermore such as lock pin
211 have fastened (buckling state), can not be by battery body 200 although then above-mentioned elastic force is still applied on battery body 200
Pop-up.
Based on it is above-mentioned to the utility model proposes battery module each chief component structure, connection mode and work(
Can relation exemplary illustration, in the present embodiment, by taking the battery module is applied to unmanned plane as an example, battery compartment 100 can be with
Be installed on the fuselage of unmanned plane, then the installation and removal process of the battery body 200 of the battery module approximately as：
When needing to load battery body 200, the tail end of battery body 200 is first loaded to the card slot of 100 tail end of battery compartment
In 102.Again by the front loaded battery compartment 100 of battery body 200, in this process, the lock end of lock pin 211 is subject to electricity
100 sidewall extrusion of pond storehouse, and the wedge structure being downwardly inclined by latching end designs, and sells lock in above-mentioned extrusion process
211 retract towards the tail end direction of battery body 200, and the spring 212 of latch components 210, which is pressurized, at this time gathers elastic potential energy.With
Battery body 200 loads downwards battery compartment 100, and the lock end of lock pin 211 corresponds to the lock buckling groove 101 of battery compartment 100, at this time
Extruding of the battery compartment 100 to lock pin 211 disappears, and the spring 212 of latch components 210 discharges the elastic potential energy of accumulation and will latch
Pin 211 is ejected towards extreme direction before battery body 200, so that the lock end of lock pin 211 is fastened in lock buckling groove 101, i.e., it is real
The installation of existing battery body 200 and battery compartment 100.In addition, in the installing process of above-mentioned battery body 200, elastic parts 110
Bullet block 112 by battery body 200 front end push and compress spring 113, at this time spring 113 gather elastic potential energy, and by
Buckling state is in lock buckling groove 101 in lock pin 211 and above-mentioned elastic potential energy is not discharged, i.e., elastic parts 110 can not
Battery body 200 is ejected.
When needing to dismantle battery body 200, operator slides pin 211 is latched towards 200 tail end of battery body, makes lock
The lock end of pin 211 in the lock buckling groove 101 of battery compartment 100 by skidding off, so that lock pin 211 is in non-button with lock buckling groove 101
Conjunction state.At this time, the spring 113 of elastic parts 110 discharges above-mentioned elastic potential energy and is converted into the kinetic energy of bullet block 112, leads to
Cross bullet block 112 to eject 200 front end of battery body, operator only needs the card slot by battery compartment 100 by the tail end of battery body 200
Taken out in 102, that is, complete the dismounting of battery body 200.
It should be noted here that the unmanned plane for showing in attached drawing and describing in the present specification is only that can use the present invention
An example in many kinds of unmanned planes of principle.It should be clearly understood that the principle of the present invention is only limitted to show in attached drawing absolutely not
Go out or this specification described in any details of unmanned plane or any part of unmanned plane.
For example, as shown in fig. 7, in the present embodiment, which further includes connector 400.Wherein, the connection
Device 400 mainly includes the battery compartment connector arranged on 100 front bottom end of battery compartment and the electricity arranged on 200 front bottom end of battery body
Pond connector, and battery compartment connector is corresponded with the position of battery connector.Specifically, when battery body 200 is installed
When battery compartment 100, battery connector is connected to battery compartment connector, so as to form the connector 400 of battery module, and with nothing
Man-machine connectivity port connection.
In conclusion the utility model proposes battery module and unmanned plane, utilize lock pin and the lock of battery compartment
The design of the cooperation of groove, can ensure the reliability of connection when battery body is installed in battery compartment.Meanwhile the utility model profit
The design of battery body is slidably connected to through elastic component with lock pin, makes installing process more convenient laborsaving.
It is described in detail above and/or illustrate the utility model proposes battery module and unmanned plane exemplary reality
Apply mode.But the embodiment of the utility model is not limited to particular implementation as described herein, on the contrary, each embodiment
Part and/or step can be independent with other parts as described herein and/or step and be used separately.One reality
The each part and/or each step for applying mode also can be with the other parts and/or step knot of other embodiment
Close and use.Introducing described here and/or diagram key element/part/when waiting, term "one", " one " and " above-mentioned "
Deng to represent there are one or more elements/part/etc..Term "comprising", " comprising " and " having " are representing out
Put formula be included look like and refer to the key element except listing/part/also may be present in addition to waiting other key element/
Part/etc..
Although according to different specific embodiments to the utility model proposes battery module and unmanned plane carry out
Description, but it will be recognized by those skilled in the art can in the spirit and scope of the claims the implementation to the utility model into
Row change.
Claims (10)
1. a kind of battery module, for powering for unmanned plane, the unmanned plane includes a battery compartment, and the battery module is installed in
In the battery compartment, the battery compartment offers lock buckling groove, it is characterised in that the battery module includes being detachably mounted on
Battery body in the battery compartment, the battery body are equipped with least one latch components, and each latch components include：
Lock pin, is slidingly disposed at the surface of the battery body, and the lock pin has connecting pin and lock end；And
Elastic component, is resiliently attached between the battery body and the connecting pin；
Wherein, when the battery body is installed in the battery compartment, lock is sold and makes the lock described in the resilient element urges
End of thread is caught in the lock buckling groove.
2. battery module according to claim 1, it is characterised in that the battery module further includes：
Position detector, arranged on the battery body and is adjacent to the lock pin, to detect the lock pin along compression institute
Whether the distance for stating the slip of elastic component direction exceedes predetermined threshold value.
3. battery module according to claim 2, it is characterised in that the quantity of the position detector and the lock group
Part is identical, and sells and correspond with the lock, is that the elastic component direction slip is compressed on edge to detect the lock pin respectively
Distance whether exceed the predetermined threshold value.
4. a kind of unmanned plane, it is characterised in that the unmanned plane includes：
Fuselage；
Battery compartment, is formed at the fuselage, and the battery compartment offers lock buckling groove；And
Such as claims 1 to 3 any one of them battery module.
5. unmanned plane according to claim 4 a, it is characterised in that opening is equipped with the top of the battery compartment, for described
Battery body is arranged on the battery body side by loading the battery compartment, the latch components at the top of the battery compartment.
6. unmanned plane according to claim 5, it is characterised in that the lock end is in the wedge structure being downwardly inclined；With/
Or, the latch components are two, two latch components are respectively arranged on the both sides of the battery body.
7. unmanned plane according to claim 4, it is characterised in that the battery compartment has the tail for being close in the connecting pin
Hold and be close in the front end at the lock end；Wherein, the top member-retaining portion roof of the battery compartment tail end and form card slot, with
After being caught in the card slot for the battery body tail end, its front end rotates and the battery body is installed in the electricity still further below
Chi Cang.
8. unmanned plane according to claim 4, it is characterised in that the position for corresponding to the lock pin of the battery compartment
Opening is offered, the lock pin part is exposed to the opening.
9. unmanned plane according to claim 4, it is characterised in that the battery compartment bottom is equipped with elastic parts, with to dress
The battery body in the battery compartment applies an elastic force；Wherein, the lock pin is in non-with the lock buckling groove
During buckling state, the elastic parts can eject the battery module.
10. unmanned plane according to claim 9, it is characterised in that the elastic parts includes：
Pedestal, is fixed on the battery compartment；
Bullet block, on the pedestal；And
Elastic component, is connected between the pedestal and the bullet block；
Wherein, when the battery body is installed in the battery compartment, the bullet block is resisted against the battery body.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721279705.7U CN207303190U (en) | 2017-09-30 | 2017-09-30 | Battery module and unmanned plane |
| CN201780087722.7A CN110383524B (en) | 2017-09-30 | 2017-11-24 | Battery module and unmanned aerial vehicle |
| PCT/CN2017/112932 WO2019061782A1 (en) | 2017-09-30 | 2017-11-24 | Battery module and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721279705.7U CN207303190U (en) | 2017-09-30 | 2017-09-30 | Battery module and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207303190U true CN207303190U (en) | 2018-05-01 |
Family
ID=62440547
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721279705.7U Expired - Fee Related CN207303190U (en) | 2017-09-30 | 2017-09-30 | Battery module and unmanned plane |
| CN201780087722.7A Expired - Fee Related CN110383524B (en) | 2017-09-30 | 2017-11-24 | Battery module and unmanned aerial vehicle |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201780087722.7A Expired - Fee Related CN110383524B (en) | 2017-09-30 | 2017-11-24 | Battery module and unmanned aerial vehicle |
Country Status (2)
| Country | Link |
|---|---|
| CN (2) | CN207303190U (en) |
| WO (1) | WO2019061782A1 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110383524A (en) * | 2017-09-30 | 2019-10-25 | 深圳市大疆创新科技有限公司 | Battery module and unmanned plane |
| WO2020041944A1 (en) * | 2018-08-27 | 2020-03-05 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle positioning system, handheld rtk positioning device, and sealing quick disassembling structure |
| CN111279514A (en) * | 2019-03-26 | 2020-06-12 | 深圳市大疆创新科技有限公司 | Battery loading structure, battery module and robot |
| CN112787031A (en) * | 2021-01-20 | 2021-05-11 | 东莞新能德科技有限公司 | Battery and electric device |
| CN113415407A (en) * | 2021-08-10 | 2021-09-21 | 珠海紫燕无人飞行器有限公司 | Collapsible unmanned aerial vehicle |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US11056746B2 (en) * | 2019-04-23 | 2021-07-06 | Xing Power Inc. | Battery cartridge for vehicle and locking mechanism |
| CN112996723A (en) * | 2020-08-06 | 2021-06-18 | 深圳市大疆创新科技有限公司 | Battery compartment structure, unmanned aerial vehicle, movable platform and external member thereof |
| CN111969154A (en) * | 2020-09-22 | 2020-11-20 | 东莞新能安科技有限公司 | Electrochemical device and unmanned aerial vehicle |
| CN114843695A (en) * | 2022-05-26 | 2022-08-02 | 博众精工科技股份有限公司 | Power supply unit and test equipment for electronic product test |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9748541B2 (en) * | 2009-11-20 | 2017-08-29 | Edmund David Burke | Advanced lithium polymer system (ALPS) |
| JP2011181347A (en) * | 2010-03-01 | 2011-09-15 | Fujitsu Toshiba Mobile Communications Ltd | Electronic equipment |
| JP6192509B2 (en) * | 2013-11-22 | 2017-09-06 | 日立オートモティブシステムズ株式会社 | Assembled battery |
| CN204424343U (en) * | 2015-02-12 | 2015-06-24 | 广州明美电子有限公司 | A kind of locker of external battery |
| WO2018053858A1 (en) * | 2016-09-26 | 2018-03-29 | 深圳市大疆创新科技有限公司 | Battery fixing assembly, unmanned aerial vehicle, and charger |
| CN106687374B (en) * | 2016-11-14 | 2020-04-24 | 深圳市大疆创新科技有限公司 | Detection device and unmanned aerial vehicle |
| CN206210895U (en) * | 2016-12-08 | 2017-05-31 | 国家电网公司 | Unmanned plane cell apparatus |
| CN207303190U (en) * | 2017-09-30 | 2018-05-01 | 深圳市大疆创新科技有限公司 | Battery module and unmanned plane |
-
2017
- 2017-09-30 CN CN201721279705.7U patent/CN207303190U/en not_active Expired - Fee Related
- 2017-11-24 CN CN201780087722.7A patent/CN110383524B/en not_active Expired - Fee Related
- 2017-11-24 WO PCT/CN2017/112932 patent/WO2019061782A1/en active Application Filing
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110383524A (en) * | 2017-09-30 | 2019-10-25 | 深圳市大疆创新科技有限公司 | Battery module and unmanned plane |
| CN110383524B (en) * | 2017-09-30 | 2022-03-15 | 深圳市大疆创新科技有限公司 | Battery module and unmanned aerial vehicle |
| WO2020041944A1 (en) * | 2018-08-27 | 2020-03-05 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle positioning system, handheld rtk positioning device, and sealing quick disassembling structure |
| CN110892234A (en) * | 2018-08-27 | 2020-03-17 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle positioning system, handheld RTK positioner, sealed rapid disassembly structure |
| CN111279514A (en) * | 2019-03-26 | 2020-06-12 | 深圳市大疆创新科技有限公司 | Battery loading structure, battery module and robot |
| CN112787031A (en) * | 2021-01-20 | 2021-05-11 | 东莞新能德科技有限公司 | Battery and electric device |
| CN112787031B (en) * | 2021-01-20 | 2023-08-11 | 东莞新能德科技有限公司 | Battery and electricity utilization device |
| CN113415407A (en) * | 2021-08-10 | 2021-09-21 | 珠海紫燕无人飞行器有限公司 | Collapsible unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2019061782A1 (en) | 2019-04-04 |
| CN110383524B (en) | 2022-03-15 |
| CN110383524A (en) | 2019-10-25 |
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
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