Utility model content
The purpose of this utility model is to provide a kind of battery-mounting devices, and structure is simple, and can facilitate battery
Installation.
The another object of the utility model is to provide a kind of unmanned plane, and battery provided by the utility model is used to install
Device can be realized the Fast Installation of battery, practical.
It is that it is realized by adopting the following technical scheme that the utility model, which solves its technical problem:
A kind of battery-mounting device provided by the utility model, including locked component and battery accommodating structure, the battery
Accommodating structure is for accommodating battery, and the battery accommodating structure is detachably arranged on the locked component, the locking group
Part includes base assembly and elastic locking structure, and the locked component is connect by the base assembly with a carrier, the bullet
Property locking structure is connected on the base assembly.
Lock pin is provided in the elastic locking structure, the battery accommodating structure offers lock hole, pushes the electricity
Pond accommodating structure makes the relatively described base assembly sliding of the elastic locking structure, until the lock pin is caught in the lock hole.
Further, the base assembly includes fixed plate and pressing plate, and the fixed plate with the carrier for connecting, institute
It states pressing plate and the fixed plate is detachably connected and is formed between sliding groove, offered on the pressing plate and the sliding
The opening of slot connection, the elastic locking structure are slidingly arranged in the sliding groove, and the lock pin is revealed by the opening
Out.
Further, the elastic locking structure includes elastic component and lock tongue, one end of the elastic component and the lock tongue
Connection, the other end are connect with the fixed plate, and the lock pin is set on the lock tongue for driving the lock tongue relatively described
Sliding groove sliding.
Further, the lock tongue includes interior sliding part and the outer sliding part that is set on the interior sliding part, it is described in
Sliding part is slidingly arranged in the sliding groove, and the outer sliding part and the inner wall of the opening are slidably matched, the lock pin
It is set on the outer sliding part.
Further, the battery accommodating structure is also provided with guide runner, and the guide runner is connected to the lock hole, institute
An inner wall for stating guide runner is obliquely installed, for being slidably matched with the lock pin.
Further, the battery accommodating structure further includes unlock piece, is provided with solution closing piece in the elastic locking structure,
The unlock piece is pushed to support it with solution closing piece to drive solution closing piece sliding, the solution closing piece slip band moves the elastic locking
The relatively described battery accommodating structure sliding of structure.
Further, the solution closing piece has the slide guide face being obliquely installed.
Further, the battery accommodating structure is also provided with accommodation groove reconciliation lockhole, the solution lockhole and the accommodating
Slot connection, the accommodation groove are passed through for accommodating the solution closing piece, the solution lockhole for the unlock piece.
Further, the solution lockhole is connected to the accommodation groove bias.
The utility model also provides a kind of unmanned plane, including fuselage and the battery-mounting device.
The battery-mounting device includes locked component and battery accommodating structure, and the battery accommodating structure is for accommodating electricity
Pond, the battery accommodating structure are detachably arranged on the locked component, and the locked component includes base assembly and bullet
Property locking structure, the locked component connect by the base assembly with a carrier, and the elastic locking structure is slidably connected
On the base assembly.
Lock pin is provided in the elastic locking structure, the battery accommodating structure offers lock hole, pushes the electricity
Pond accommodating structure makes the relatively described base assembly sliding of the elastic locking structure, until the lock pin is caught in the lock hole.
The fuselage bottom offers mounting groove, and the locked component is mounted on the inner wall of the mounting groove.
The beneficial effect of the utility model embodiment is:
Its battery accommodating structure of a kind of battery-mounting device disclosed by the utility model can be used for accommodating battery, locking group
Part can be used for being fixed on the carriers such as fuselage, and push the battery accommodating structure towards locked component, enable to elasticity
Lock pin on locking structure is caught in the lock hole of battery accommodating structure, conveniently and efficiently realizes the installation of battery, practical.
A kind of unmanned plane disclosed by the utility model, uses battery-mounting device disclosed by the utility model, Neng Goufang
Just the installation of battery is quickly realized, it is easy to operate, it is practical.
Specific embodiment
It is practical new below in conjunction with this to keep the objectives, technical solutions, and advantages of the embodiments of the present invention clearer
Attached drawing in type embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that is retouched
The embodiment stated is the utility model a part of the embodiment, instead of all the embodiments.Usually here in attached drawing description and
The component of the utility model embodiment shown can be arranged and be designed with a variety of different configurations.
Therefore, requirement is not intended to limit to the detailed description of the embodiments of the present invention provided in the accompanying drawings below
The scope of the utility model of protection, but it is merely representative of the selected embodiment of the utility model.Based in the utility model
Embodiment, every other embodiment obtained by those of ordinary skill in the art without making creative efforts, all
Belong to the range of the utility model protection.
It should also be noted that similar label and letter indicate similar terms in following attached drawing, therefore, once a certain Xiang Yi
It is defined in a attached drawing, does not then need that it is further defined and explained in subsequent attached drawing.
In the description of the present invention, it should be noted that the orientation or positional relationship of the instructions such as term " on " is base
In orientation or positional relationship shown in the drawings or the utility model product using when the orientation usually put or position close
System, is merely for convenience of describing the present invention and simplifying the description, rather than the device or element of indication or suggestion meaning are necessary
It with specific orientation, is constructed and operated in a specific orientation, therefore should not be understood as limiting the present invention.
In addition, term " first ", " second ", " third " and " the 4th " etc. are only used for distinguishing description, and should not be understood as referring to
Show or imply relative importance.
In the description of the present invention, it should also be noted that, unless in addition having more specific regulation and limiting, term
" setting ", " connection " should do more broadly understanding, for example, " connection " may be a fixed connection, may be a detachable connection, or
It is integrally connected;It can be mechanical connection, be also possible to be electrically connected;It can be directly connected, it can also be by between intermediary
It connects connected, can be the connection inside two elements.For the ordinary skill in the art, can be understood with concrete condition
The concrete meaning of above-mentioned term in the present invention.
Battery-mounting device provided by the utility model can be applied on the carriers such as unmanned plane, automobile, and following the application is real
Example is applied only to be illustrated for being applied to unmanned plane.
With reference to the accompanying drawing, it elaborates to an embodiment of the utility model, in the absence of conflict, under
The feature in embodiment stated can be combined with each other.
Fig. 1 is the decomposition texture schematic diagram of unmanned plane 100 provided in this embodiment.Fig. 1 is please referred to, present embodiment discloses
A kind of unmanned plane 100 comprising fuselage 110, battery 120 and battery-mounting device 200.Battery 120 is installed on battery installation dress
It sets in 200, battery-mounting device 200 and fuselage 110 are detachably connected.
Due to using the battery-mounting device 200, unmanned plane 100 disclosed in the present embodiment can be realized the fast of battery 120
Speed dismounting, it is easy to operate, it is practical.
Battery-mounting device 200 described in the present embodiment includes locked component 210 and battery accommodating structure 220, and Fig. 2 is this
The mounting structure schematic diagram of the locked component 210 for the unmanned plane 100 that embodiment provides.Incorporated by reference to referring to Figures 1 and 2, this implementation
In example, 110 bottom of fuselage offers mounting groove 112, and mounting groove 112 is used for fixedly locked component 210.The locked component 210 peace
Inner wall loaded on mounting groove 112, battery accommodating structure 220 are used for detachable with locked component 210 for accommodating battery 120
Connection.
Optionally, the battery-mounting device 200 can also include unlock piece 230, and the unlock piece 230 is for unlocking electricity
The locking of pond accommodating structure 220 and locked component 210.Under 210 lock state of battery accommodating structure 220 and locked component, lead to
Crossing the unlock piece 230 can unlock, and realize the disassembly of battery 120.
It should be appreciated that battery accommodating structure 220 is for accommodating battery 120, but in the battery accommodating structure 220 regardless of whether
Accommodating battery 120 can realize locking with the locked component 210.
Fig. 3 is the enlarged drawing in Fig. 2 at A.Locked component 210 includes base assembly 211 and elastic locking structure 212.
Wherein, locked component 210 is used to connect by base assembly 211 with the inner wall of mounting groove 112 on fuselage 110, bullet
Property locking structure 212 be slidably connected on base assembly 211, and for and battery accommodating structure 220 be detachably connected.
Fig. 4 is the exploded structural schematic diagram of the locked component 210 of unmanned plane 100 provided in this embodiment.Fig. 5 is figure
Enlarged drawing in 4 at B.Incorporated by reference to referring to Fig. 3-Fig. 5, base assembly 211 includes fixed plate 2112 and pressing plate 2113.
Fixed plate 2112 is used to connect with the inner wall of mounting groove 112, such as can be connected by modes such as screws, fixed plate
2112 have hollow accommodating cavity 201, for accommodating elastic locking structure 212.And the bottom wall of fixed plate 2112 also projection
There is the first fixed ear 202, for connecting elastic locking structure 212.
Pressing plate 2113 and fixed plate 2112 are detachably connected and form sliding groove (figure is not marked) between, so that elastic
Locking structure 212 can be slidingly arranged in sliding groove.
Optionally, pressing plate 2113 is fixed with fixed plate 2112 by screw.Pressing plate 2113 can also lead to fixed plate 2112
The modes such as clamping are crossed to fix.
The opening 203 being connected to sliding groove is offered on pressing plate 2113.It is open 203 in long strip, and is open and 203 has
Two inner walls being oppositely arranged, for being slidably matched with elastic locking structure 212.
Continuing with combining referring to Fig. 3 and Fig. 5, elastic locking structure 212 includes elastic component 2122 and lock tongue 2123.Wherein,
Lock tongue 2123 is connected by elastic component 2122 and fixed plate 2112, and lock tongue 2123 is for locking battery accommodating structure 220.
Fig. 6 is a kind of structural schematic diagram at visual angle of the lock tongue 2123 of unmanned plane 100 provided in this embodiment.Please refer to figure
6, as an implementation, in the present embodiment, lock tongue 2123 is in long strip, and lock tongue 2123 includes interior sliding part 204 and setting
Outer sliding part 205 on interior sliding part 204, interior sliding part 204 are slidingly arranged in sliding groove, outer sliding part 205 with open
The inner wall of mouth 203 is slidably matched.
It is understood that lock tongue 2123 can reciprocatingly slide in sliding groove, and the inner wall of opening 203 has slide guide
And position-limiting action.
Lock pin 206 and solution closing piece 207 are convexly equipped on outer sliding part 205.Lock pin 206 conciliates the setting of the interval of closing piece 207, lock pin
206 reconciliation closing pieces 207 are exposed by opening 203.Also, lock pin 206 is used to that lock tongue 2123 to be driven to slide with respect to sliding groove, with
Battery accommodating structure 220 is locked, solution closing piece 207 is used for and the cooperation of unlock piece 230 is to unlock battery accommodating structure 220 and locking group
Part 210.
Optionally, there are two lock pins 206, two settings of lock pin 206 to solve 207 two sides of closing piece for the setting of lock tongue 2123, wherein
Preferably, which is arranged equally spaced at solution 207 two sides of closing piece, may be implemented to connect with battery accommodating structure 220
When structural stability.
Closing piece 207 is solved in bulk, and there is the slide guide face 208 being obliquely installed, slide guide face 208 is used for and unlock piece 230 is sliding
Dynamic cooperation.
It should be noted that inclined surface is directed away from the side inclination of the first fixed ear 202.
Fig. 7 is the structural schematic diagram at another visual angle of the lock tongue 2123 for the unmanned plane 100 that embodiment provides.Please refer to figure
7, lock tongue 2123 is also convexly equipped with the second fixed ear 2101 towards the side of fixed plate 2112, and the second fixed ear 2101 is used for and first
Fixed ear 202 cooperates, to connect elastic component 2122.
Fig. 8 is the enlarged drawing in Fig. 5 at C.Incorporated by reference to referring to Fig. 5 and Fig. 8, optionally, elastic component 2122 is both ends setting
Have a spring of connection ring 209, also, two connection rings 209 respectively with 2101 clamping of the first fixed ear 202 and the second fixed ear.
Fig. 9 is the partial profile structure of unmanned plane 100 provided in this embodiment.Figure 10 is the enlarged drawing in Fig. 9.
Incorporated by reference to referring to Fig. 9 and Figure 10, it is to be understood that when locked component 210 assembles, by fixed plate 2112 and mounting groove 112
Inner wall is fixed by screw, then that the connection ring 209 at 2122 both ends of elastic component is fixed with the first fixed ear 202 and second respectively
Pressing plate 2113 and fixed plate 2112, are further connected by screw to by 2101 clamping of ear, wherein the interior sliding part of lock tongue 2123
204 are slidingly arranged in the sliding groove formed between pressing plate 2113 and fixed plate 2112, the outer sliding part 205 of lock tongue 2123 with
The inner wall of opening 203 is slidably matched, and the lock pin 206 and solution closing piece 207 of lock tongue 2123 are exposed by opening 203.
It should be appreciated that in other preferred embodiments, elastic component 2122 it is also an option that the modes one end such as welding, clamping with
Lock tongue 2123 connects, and the other end is connect with fixed plate 2112.
In other preferred embodiments, elastic locking structure 212, which can also be selected, conciliates closing piece 207 with lock pin 206
Elastic sliding vane, as long as being able to achieve elastic locking structure 212 can connect with base assembly 211, and opposite base component 211 is sliding
Dynamic, base assembly 211 may be set to be the matrix with sliding part.
In order to guarantee the stability of 210 assembling structure of battery accommodating structure 220 and locked component, two lockings can be selected
Component 210, and two locked components 210 are relatively arranged on the inner wall of mounting groove 112.
It is understood that the present embodiment does not limit the quantity of the locked component 210 and battery accommodating structure 220, it is right
In a battery-mounting device 200, it contains at least one locked component 210 and a battery accommodating structure 220 (referred to as one
It is right), such as can be two pairs, it can also be with four pairs etc..
It should be appreciated that in other preferred embodiments, the side of battery accommodating structure 220 and 112 inner wall of mounting groove can be with
It is locked by locked component 210, the other side can also complete to connect by modes such as clampings.
It should be appreciated that in other preferred embodiments, battery-mounting device 200 disclosed in the present embodiment can also pass through by
The base assembly 211 of locked component 210 is installed on such as automobile carrier, to be applied to the machine that other need to install battery 120
Tool construction applications, and it is not limited to unmanned plane 100.
And, it is understood that in the battery-mounting device 200 between battery accommodating structure 220 and locked component 210
The mode that is connected and fixed can also be applied to the installation of other equipment.
Figure 11 is that the structure of the battery accommodating structure 220 for being equipped with battery 120 of unmanned plane 100 provided in this embodiment is shown
It is intended to.Figure 11 is please referred to, the top of battery accommodating structure 220 is provided with accommodating cavity (figure is not marked), and battery 120 is installed on the accommodating
It is intracavitary.
It should be noted that top is side of the battery accommodating structure 220 close to 110 bottom of fuselage in the present embodiment.
The two sides of battery accommodating structure 220 are respectively arranged with locking plate 221, and locking plate 221 is used for and the lock pin of locked component 210
206 lockings.
The structure of locking plate 221 of the Figure 12 to be arranged on the battery accommodating structure 220 of unmanned plane 100 provided in this embodiment is shown
It is intended to.Incorporated by reference to referring to Fig.1 1 and Figure 12, lock hole 2212 is offered on locking plate 221, lock hole 2212 is used to push battery
When accommodating structure 220 slides 212 opposite base component 211 of elastic locking structure, under the restoring force effect of elastic component 2122,
Cooperate with lock pin 206, lock pin 206 is made to be caught in lock hole 2212, realizes locking.
Push battery accommodating structure 220 that can synchronously drive 212 opposite base of elastic locking structure in order to facilitate realizing
Component 211 slides, and is also provided with guide runner 2213 on locking plate 221, guide runner 2213 is connected to lock hole 2212, also, slide guide
One inner wall of slot 2213 is obliquely installed, and for being slidably matched with lock pin 206.
It should be noted that guide runner 2213 is prejudicially connected to the top of lock hole 2212, and with 2212 shape of lock hole
At angle, when battery accommodating structure 220 and locked component 210 assemble, the inclined inner wall of guide runner 2213 is directed away from lock pin
206 side inclination.
It is understood that pushing up battery accommodating structure 220 can since the inner wall of guide runner 2213 is obliquely installed
So that the inner wall of lock pin 206 and guide runner 2213 slides, and synchronously drive 212 opposite base component 211 of elastic locking structure
Sliding, until lock pin 206 is caught in lock hole 2212 under the restoring force effect of elastic component 2122.
It should be noted that the quantity of locking plate 221 and the quantity of lock pin 206 are correspondingly arranged, and guide runner 2213 and lock
Pin 206 is correspondingly arranged.Locking plate 221 and battery accommodating structure 220 pass through the fastening such as screw.
It should be appreciated that directly guide runner can also be opened up on battery accommodating structure 220 in other preferred embodiments
2213 and lock hole 2212.
Please continue to refer to Figure 11, battery accommodating structure 220 is also provided with accommodation groove 223 and conciliates lockhole 224, solves lockhole 224
It is connected to accommodation groove 223.Wherein, accommodation groove 223 for accommodate solution closing piece 207, solution lockhole 224 for unlock piece 230 pass through with
It supports, and is slidably matched with the slide guide face 208 of solution closing piece 207, to unlock battery accommodating structure 220 and locked component 210.
It is understood that accommodation groove 223 with solution closing piece 207 be correspondingly arranged, and be set to two adjacent locking plates 221 it
Between.
Optionally, solution lockhole 224 is connected to 223 bias of accommodation groove, so that solution closing piece 207 is being placed in accommodation groove 223
Under state, the bottom wall of one end and accommodation groove 223 for solving closing piece 207 is supported, and the other end is oppositely arranged with solution lockhole 224 interval.
It is understood that this structure can facilitate unlock piece 230 to protrude into, and facilitate drive solution closing piece 207 to act, with
Elastic locking structure 212 is driven to slide with respect to battery accommodating structure 220.
As long as it should be appreciated that unlock piece 230 can be facilitated to pass through battery accommodating structure 220, and supporting with slide guide face 208 with band
Dynamic solution closing piece 207 slides, and in other preferred embodiments, battery accommodating structure 220 can also only open up solution lockhole 224 etc..
Figure 13 is the structural schematic diagram of the unlock piece 230 of unmanned plane 100 provided in this embodiment.Please refer to Figure 13, this reality
It applies in example, unlock piece 230 includes key 231 and two unlock pins 232 being arranged on key 231, and two unlock pins 232 are parallel
Interval setting, and for protrude into two solution lockholes 224 and further with two solve closing pieces 207 slide guide face 208 support, with solution
Lock battery accommodating structure 220 and locked component 210.
It should be appreciated that the structures such as the structure of unlock piece 230 and the solution lockhole 224 of battery accommodating structure 220 are correspondingly arranged, only
It is able to achieve unlock piece 230 and passes through solution lockhole 224 to support with the slide guide face 208 for solving closing piece 207, and drive solution 207 phase of closing piece
Battery accommodating structure 220 is slided to unlock, in other preferred embodiments, the structure of unlock piece 230 can have different variations,
Such as a unlock pin 232 is only set, or four unlock pins 232 etc. are arranged simultaneously.
To sum up, when unmanned plane 100 disclosed in the present embodiment assembles, fixed plate 2112 is fixed by screws in mounting groove
Two connection rings 209 of elastic component 2122 are respectively clamped into the first fixed ear 202 and the second fixed ear 2101 by 112 inner wall, then
Pressing plate 2113 is connect by screw with fixed plate 2112, and lock tongue 2123 is made to be slidingly arranged at pressing plate 2113 and fixed plate
In the sliding groove formed between 2112, lock pin 206 is conciliate closing piece 207 and is exposed by the opening 203 on pressing plate 2113.It again will installation
There is the inner wall of the guide runner 2213 of the battery accommodating structure 220 of battery 120 to support with lock pin 206, further battery is pushed to hold
Structure 220 is set, so that the inner wall of guide runner 2213 is slidably matched with lock pin 206, until lock pin 206 is caught in lock hole 2212, it is complete
At locking.
When needing replacing battery 120, the unlock pin 232 of unlock piece 230 is protruded into solution lockhole 224, and with solution closing piece 207
Slide guide face 208 supports, and further pushes up unlock piece 230 so that unlock pin 232 and slide guide face 208 be slidably matched until
Lock pin 206 is popped up from lock hole 2212, completes unlock.
A kind of its battery accommodating structure 220 of battery-mounting device 200 disclosed in the present embodiment can be used for accommodating battery
120, locked component 210 can be used for being fixed on the carriers such as fuselage 110, and push the battery to hold towards locked component 210
Structure 220 is set, the lock pin 206 in elastic locking structure 212 is enabled to be caught in the lock hole 2212 of battery accommodating structure 220
It is interior, conveniently and efficiently realize the installation of battery 120, it is practical.
A kind of unmanned plane 100, uses battery-mounting device 200 disclosed in the present embodiment disclosed in the present embodiment, can
Conveniently and efficiently realize the installation and disassembly of battery 120, it is easy to operate, it is practical.
The above descriptions are merely preferred embodiments of the present invention, is not intended to limit the utility model, for this
For the technical staff in field, various modifications and changes may be made to the present invention.It is all in the spirit and principles of the utility model
Within, any modification, equivalent replacement, improvement and so on should be included within the scope of protection of this utility model.