CN209290704U - Battery fixing structure and unmanned plane - Google Patents

Battery fixing structure and unmanned plane Download PDF

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Publication number
CN209290704U
CN209290704U CN201822085189.5U CN201822085189U CN209290704U CN 209290704 U CN209290704 U CN 209290704U CN 201822085189 U CN201822085189 U CN 201822085189U CN 209290704 U CN209290704 U CN 209290704U
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CN
China
Prior art keywords
battery
fixing structure
unmanned plane
buckle slot
elastic component
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CN201822085189.5U
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Chinese (zh)
Inventor
梁杰
肖锭锋
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Guangzhou Xaircraft Technology Co Ltd
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Guangzhou Xaircraft Technology Co Ltd
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Priority to CN201822085189.5U priority Critical patent/CN209290704U/en
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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries

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  • Battery Mounting, Suspending (AREA)

Abstract

It includes: frame that the utility model, which discloses a kind of battery fixing structure and unmanned plane, battery fixing structure, is provided with the mounting groove of set battery, and the mounting groove has an open end and a front bulkhead, is provided with card slot via hole on the front bulkhead;It is set to the buckle slot of battery rear end face, after the battery is plugged in mounting groove from the open end, the battery rear end face is close to the front bulkhead and the card slot via hole exposes the buckle slot;Snap component is set to the front bulkhead backwards to the one side of the mounting groove, it is provided with mobilizable pressing piece, snap component and buckle slot are clamped to fix battery when the pressing piece is not pressed, and snap component is separated with buckle slot to dismantle battery when pressing piece is pressed.On the one hand, any side that battery can be held when user inserts battery improves user to the usage experience of unmanned plane, on the other hand, without reserving pressing space close to one end of battery front end face on unmanned plane, so that unmanned plane has good appearance.

Description

Battery fixing structure and unmanned plane
Technical field
The utility model relates to air vehicle technique field more particularly to a kind of battery fixing structures and unmanned plane.
Background technique
Unmanned plane be manipulated using radio robot (i.e. remote controler) and the presetting apparatus provided for oneself it is not manned Aircraft, and electronic unmanned plane is due to using clean energy resource to be widely used.
Unmanned plane is powered using battery on current electronic unmanned plane, on unmanned plane demand battery roll it is convenient, Sound construction is reliable.In existing battery fixing structure, generallys use Elastic buckle and by battery-disassembled be inserted into nobody In the casing of machine, for example, card slot is arranged in battery compartment roof, elastic card is set at battery front end face in battery upper surface Button, and in order to dismantle battery when can have sufficient space easily to press Elastic buckle, and Elastic buckle is arranged above battery Just it holds after the position of battery and installation from the appearance as it can be seen that have can for hand-held battery for convenience when one side user inserts battery Elastic buckle inserting battery can be pressed, causes user to there is query in place to whether battery inserts, reduces user to unmanned plane Usage experience, on the other hand, battery inserting after Elastic buckle be exposed to the overall appearance that appearance affects unmanned plane.
Utility model content
The utility model embodiment provides a kind of battery fixing structure and unmanned plane, to solve existing battery fixing structure User is reduced since design is unreasonable on the problem of the usage experience of unmanned plane and influence unmanned plane appearance.
In a first aspect, providing a kind of battery fixing structure, comprising:
Frame, is provided with the mounting groove of set battery, and the mounting groove has an open end and a front bulkhead, the front end Card slot via hole is provided on wall;
It is set to the buckle slot of battery rear end face, the battery is removably plugged in the mounting groove from the open end Afterwards, the battery rear end face is close to the front bulkhead and the card slot via hole exposes the buckle slot;
Snap component is set to the front bulkhead backwards to the one side of the mounting groove, and the snap component, which is provided with, to live Dynamic pressing piece, when the pressing piece is not pressed, the snap component and the buckle slot are clamped with the fixation battery, institute When stating pressing piece and being pressed, the snap component is separated with the buckle slot to dismantle the battery.
Optionally, the frame further includes bottom wall, roof and two side walls, and the bottom wall and the roof are oppositely arranged, Two side walls are oppositely arranged and are separately connected the left and right sides of the bottom wall and the roof, the side of the front bulkhead The bottom wall, institute's roof and two side walls are separately connected, described in the bottom wall, the roof, the front bulkhead and two Side wall forms the mounting groove.
Optionally, the activity direction of the pressing piece is perpendicular to one in two side walls, bottom wall and roofs.
Optionally, the snap component further includes articulated part, fastener, the first elastic component and drive-connecting shaft;
The articulated part is set to the front bulkhead backwards to the one side of the mounting groove;
The fastener includes clamping part, abutting part and the pivot joint between the clamping part and the abutting part Portion, the drive-connecting shaft are connect with the articulated part, and the fastener is sheathed on the drive-connecting shaft and institute by the articulated section It states articulated part to be rotatably connected, first elastic component is socketed on the drive-connecting shaft;
The pressing piece includes press section and the only top connecting with the press section, only top and the abutting part It abuts;
When the press section is not pressed, the fastener is under the action of the first elastic component, the clamping part and institute Buckle slot clamping is stated, when the press section is pressed, abutting part described in the only top drive is rotated around the drive-connecting shaft, institute Clamping part is stated to be detached from from the buckle slot.
Optionally, the articulated part setting is provided with accommodating first elasticity there are two lug, the articulated section is pivotally connected The accommodating space of part, the articulated section are embedded between two pivot joint lugs, and first elastic component is placed in the accommodating In space, the drive-connecting shaft is connect through the articulated section and first elastic component and with two pivot joint lugs.
Optionally, it is provided with first on the pivot joint lug and only supports protrusion, the abutting part two sides are provided with second and only support Protrusion, described second, which only supports protrusion, only only supports to protrusion under the action of first elastic component with described first.
Optionally, first elastic component is torsional spring.
Optionally, the frame is fixed in the shell of unmanned plane, and the battery fixing structure further includes locating piece;
The shell is provided with pressing hole, the locating piece and the cage connection, and the locating piece is provided with guide post, The press section is provided with pilot hole, and the pilot hole is sheathed in the guide post, and the press section is exposed to the pressing Outside hole.
It optionally, further include the second elastic component, second elastic component is sheathed in the guide post.
Optionally, second elastic component is pressure spring or elastic rubber sleeve.
Optionally, the buckle slot from the battery rear end face towards the battery outside extend or the buckle slot is from institute Battery rear end face is stated towards extending in the battery.
Second aspect, provides a kind of unmanned plane, and the unmanned plane includes battery described in the utility model any embodiment Fixed structure.
The battery fixing structure of the utility model embodiment, the mounting groove of set battery have open end and front bulkhead and Card slot via hole is provided on front bulkhead, battery rear end face is provided with buckle slot, and battery is removably plugged in installation from open end After slot, battery rear end face is close to front bulkhead and card slot via hole exposes buckle slot, and snap component is set to front bulkhead backwards to peace The one side of tankage, snap component and buckle slot are clamped to fix battery, pressing piece quilt when the pressing piece of snap component is not pressed Snap component is separated with buckle slot to dismantle battery when pressing, and in the utility model embodiment, buckle slot is arranged in battery rear end On face, snap component is located at front bulkhead backwards to the one side of mounting groove, i.e., in inserting, one end of hand-held battery front end face is not blocked The components such as button, on the one hand, user can hold any side of battery front end and will not be pressed into snap component when inserting battery, User is improved to the usage experience of unmanned plane, on the other hand, without reserved close to one end of battery front end face on unmanned plane Space is pressed, so that unmanned plane has good appearance.
Further, in snap component, since fastener can be rotated, when press section is not pressed, fastener is the The buckle slot of the clamping part and battery that make fastener under the action of one elastic component is clamped, when press section is pressed, press section The only abutting part of top drive fastener rotated around drive-connecting shaft, clamping part is detached from from buckle slot, i.e., blocks in the mounted state Buckle is clamped with buckle slot always under the action of the first elastic component, ensure that the fixed reliability of battery, and in press section After being pressed, clamping part is detached from from buckle slot, be can be convenient and is efficiently dismantled battery.
Detailed description of the invention
The utility model is described in further detail below according to drawings and examples.
Fig. 1 is the perspective view after the unmanned plane expansion of the utility model embodiment;
Fig. 2 is the position view of battery fixing structure in the unmanned plane of the utility model embodiment;
Fig. 3 is the structural schematic diagram of the battery of the utility model embodiment;
Fig. 4 is the structural schematic diagram of the frame of the utility model embodiment;
Fig. 5 is the fuselage cross-sectional view of the unmanned plane of the utility model embodiment;
Fig. 6 is the detailed construction schematic diagram of part A in Fig. 2;
Fig. 7 is the detailed construction schematic diagram of part B in Fig. 5;
Fig. 8 is the structural schematic diagram of the fastener of the utility model embodiment.
Fig. 9 is the structural schematic diagram of the pressing piece of the utility model embodiment;
Figure 10 is the structural schematic diagram of the articulated part of the utility model embodiment;
Figure 11 is the structural schematic diagram of the lower case of the utility model embodiment;
Figure 12 is the structural schematic diagram of the locating piece of the utility model embodiment.
In figure:
10, fuselage;13, frame;130, mounting groove;131, bottom wall;132, roof;133, front bulkhead;1331, card slot mistake Hole;1332, the first fixed column;134, side wall;14, snap component;141, articulated part;1411, it is pivotally connected lug;1412, first stops To protrusion;142, fastener;1421, articulated section;1422, clamping part;1423, abutting part;1424, second protrusion is only supported;1425, Accommodating space;143, the first elastic component;144, locating piece;1441, guide post;1442, fixation hole;145, pressing piece;1451, it presses Splenium;1452, at the top of only;1453, pilot hole;146, the second elastic component;162, lower case;1621, pressing hole;16211, hole Wall;1622, the second fixed column;105, battery;1051, buckle slot;20, horn;30, foot prop;40, Power Component.
Specific embodiment
The technical issues of to solve the utility model, the technical solution of use and the technical effect that reaches are clearer, It is described in further detail below in conjunction with technical solution of the attached drawing to the utility model embodiment, it is clear that described reality Applying example is only the utility model a part of the embodiment, instead of all the embodiments.Based on the embodiments of the present invention, It is practical new to belong to this for those skilled in the art's every other embodiment obtained without creative efforts The range of type protection.
Fig. 1 to Figure 12 is please referred to, unmanned plane provided by the embodiment of the utility model is described.Unmanned plane can be used for geographical mapping Equal activities.Certainly, unmanned plane is not limited to use in geographical mapping, it may also be used for photography of taking photo by plane, electric inspection process, environmental monitoring and The fields such as disaster inspection.
Referring to Fig.1 and 2, unmanned plane includes fuselage 10, horn 20, foot prop 30 and Power Component 40.This embodiment party In formula, unmanned plane is quadrotor drone, and 40 quantity of Power Component is four, and four Power Components 40 pass through the support of horn 20 And it is distributed in the rectangular area around fuselage 10, and each Power Component 40 is located on a vertex of rectangle.
Certainly, according to different demands, the quantity of Power Component 40 can do suitable variation, for example, Power Component 40 Quantity can be two, three, six etc., even, the quantity of Power Component 40 can be only one, correspondingly, horn 20 Quantity can also according to Power Component 40 quantity and be rationally arranged.
Application field according to unmanned plane is different, other can also be carried on fuselage 10 can be realized the negative of particular task It carries, for example, unmanned plane is for when taking photo by plane or surveying and drawing, fuselage 10 can be equipped with the capture apparatus for increasing steady holder;Unmanned plane is used for When competitive game, fuselage 10 can carry game station etc..
Referring to Figures 1 and 2, the unmanned plane of the utility model embodiment is electronic unmanned plane, i.e., is fitted with electricity on unmanned plane Pond 105 is provided with battery fixing structure so that battery 105 to be fixed on unmanned plane on unmanned plane, which makes 105 convenient disassembly of battery, the high reliablity of fixed battery 105.
Referring to Fig. 2-Fig. 4, the battery fixing structure of the utility model embodiment includes frame 13, is set to battery rear end Buckle slot 105 and snap component 14.
Referring to Fig. 3, the battery rear end face of battery 105 is provided with buckle slot 1051, wherein battery rear end face can be battery 105 along cartridge insertion direction C insert when with the opposite end face of front bulkhead 133, battery front end face can be along cartridge insertion direction C insert battery Battery user oriented end face when 105.Cooperate the fixation that battery 105 can be achieved with snap component 14 by buckle slot 1051 and tear open Unload, optionally, buckle slot 1051 can from the rear end face of battery 105 towards battery outside extend or buckle slot 1051 is from battery 105 Rear end face towards extending in battery 105, i.e., buckle slot 1051, which can be, is raised in 105 surface of battery or recessed in battery Groove body in 105, when implementing the utility model, those skilled in the art can select according to the actual situation buckle slot 1051 convex It rises or recessed in 105 surface of battery, the utility model embodiment is without restriction to this.
Referring to Fig. 4, frame 13 is in a frame structure and the mounting groove 130 for being provided with set battery 105, and mounting groove 130 has There are open end and front bulkhead 133, card slot via hole 1331 is provided on front bulkhead 133.Battery 105 can be inserted from open end into installation In slot 130, so that the exposure from card slot via hole 1331 of the buckle slot 1051 of battery 105.
Optionally, frame 13 includes bottom wall 131, roof 132, front bulkhead 133 and two side walls 134, bottom wall 131 and roof 132 are oppositely arranged, and two side walls 134 are oppositely arranged and are connected at the left and right sides of bottom wall 131 and roof 132, preceding Four sides of end wall 133 are separately connected bottom wall 131, roof 132 and two side walls 134, bottom wall 131, roof 132, front bulkhead 133 and two side walls 134 limit the mounting groove 130 of installation battery 105 jointly, battery 105 is removably plugged in mounting groove In 130, wherein the card slot via hole 1331 that can expose buckle slot 1051 is provided on front bulkhead 133, if buckle slot 1051 is convex 105 surface of battery is arised from, then card slot via hole 1331 is extend out in 1051 self installation slot 130 of buckle slot, to be exposed to front bulkhead Outside 133, if buckle slot 1051 is recessed in 105 surface of battery, battery in mounting groove 130 is exposed by card slot via hole 1331 Buckle slot 1051 on 105.
Referring to Fig. 2, in the utility model embodiment, snap component 14 is set to front bulkhead 133 backwards to the one of mounting groove 130 Face, snap component 14 is provided with mobilizable pressing piece, and when pressing piece is not pressed, snap component 14 and buckle slot 1051 are clamped To fix battery 105, when pressing piece is pressed, snap component 14 is separated with buckle slot 1051 to dismantle battery 105, wherein card The component that buckle assembly 14 can be realization and buckle slot 1051 is clamped, the component can be made of one or more component, this Utility model embodiment is without restriction to the specific structure of snap component 14.
In the utility model embodiment, buckle slot is arranged on battery rear end face, and snap component is located at front bulkhead backwards to peace The one side of tankage, i.e., in inserting, one end of hand-held battery front end face such as does not buckle at the components, on the one hand, when user inserts battery Any side that battery can be held improves user to the usage experience of unmanned plane, on the other hand, without leaning on unmanned plane The reserved pressing space in one end of nearly battery front end face, so that unmanned plane has good appearance.
Referring to Fig. 2 and Fig. 6, in the preferred embodiment of the utility model, snap component 14 further includes articulated part 141, card Fastener 142, the first elastic component 143 and drive-connecting shaft 140.
Referring to Fig. 2 and Fig. 4, articulated part 141 is located at one end that frame 13 is provided with card slot via hole 1331, and can pass through first Fixed column 1332 is detachably connected with frame 13, for example, the first fixed column 1332 is provided with threaded hole, articulated part 141 is provided with Articulated part 141 can be locked on frame 13 by fixation hole by screw.
Referring to figure 5-8, fastener 142 is including clamping part 1422, abutting part 1423 and positioned at clamping part 1422 and supports Articulated section 1421 between socket part 1423, drive-connecting shaft 140 are connect with articulated part 141, and fastener 142 is arranged by articulated section 1423 In being rotatably connected on drive-connecting shaft 140 with articulated part 141, the first elastic component 143 is socketed on drive-connecting shaft 140, wherein the first bullet Property part 143 can be torsional spring.
Referring to Fig. 9, pressing piece 145 includes press section 1451 and the only top 1452 connecting with press section 1451, only top 1452 abut with abutting part 1423, and pressing piece 145 is movably disposed in snap component 14, for example, pressing piece 145 can It is slideably positioned in snap component 14, so that the only top 1452 of pressing piece 145 can drive abutting part 1423 to unroll drive-connecting shaft 140 Rotation.
Referring to Fig. 7, the working principle of the snap component 14 of the utility model embodiment is as follows:
In snap component 14 shown in Fig. 7, pressing piece 145 can be slided up and down, and have preset sliding stroke, card Fastener 142 has first position and the second position when the drive-connecting shaft 140 that unrolls rotates.
Wherein, first position is 1422 locking clamp catching groove 1051 of clamping part with the position that battery 105 is fixed, at first When setting, fastener 142 has the rotation (counterclockwise in Fig. 7) counterclockwise of drive-connecting shaft 140 of unrolling under the action of the first elastic component 143 The trend turned, when battery 105 does not insert into mounting groove 130, rotation leads to clamping part to fastener 142 counterclockwise in order to prevent 1422 fail to be clamped with buckle slot 1051, and pressing piece 145 can be set when not being pressed, the only top 1452 of pressing piece 145 It is connected on the abutting part 1423 of fastener 142, to orient the extreme position that fastener 142 rotates counterclockwise, so that buckle For part 142 when pressing piece 145 is not pressed, fastener 142 is in first position, such as fastener 142 is in a horizontal position.When When battery 105 is inserted into mounting groove 130, under the thrust of inserting battery 130, buckle slot 1051 squeezes buckle slot 1051 Clamping part 1422, fastener 142 rotate clockwise, and after battery 105 is installed in place, buckle slot 1051 no longer squeezes clamping part 1422, rotation restores horizontal position to fastener 142 counterclockwise, and clamping part 1422 and buckle slot 1051 are clamped, and in the first bullet Property part 143 under the action of always with buckle slot 1051 be clamped, to realize the fixation of battery 105.
When dismantling battery 105, pressing piece 145 is depressed by the user, 145 upward sliding of pressing piece, and pressing piece 145 only pushes up Portion 1452 drives the drive-connecting shaft 140 that unrolls of abutting part 1423 to rotate clockwise, when press section 145 drives fastener 142 to revolve clockwise When going to the second position, clamping part 1422 is detached from from buckle slot 1051, can take out battery 105 from mounting groove 130 at this time.
In the utility model embodiment, since fastener can be rotated, when press section is not pressed, fastener is in the first bullet Property part under the action of make fastener clamping part and battery buckle slot be clamped, when press section is pressed, press section only The abutting part of top drive fastener is rotated around drive-connecting shaft, and clamping part is detached from from buckle slot, and clamping part exists in the mounted state It is clamped always with buckle slot under the action of first elastic component, ensure that the fixed reliability of battery, and be pressed in press section Afterwards, clamping part is detached from from buckle slot, be can be convenient and is efficiently dismantled battery.
As shown in Fig. 6, Fig. 8 and Figure 10, in the alternative embodiment of the utility model, there are two pivots for the setting of articulated part 141 Lug 1411 is connect, articulated section 1421 is provided with the accommodating space 1425 of the first elastic component 143 of accommodating, and articulated section 1421 is embedded in two It is pivotally connected between lug 1411, the first elastic component 143 is placed in accommodating space 1425, and drive-connecting shaft 140 runs through 1421 He of articulated section It first elastic component 143 and is connect with two pivot joint lugs 1411, so that fastener 142 can be under the action of the first elastic component 143 The drive-connecting shaft 140 that unrolls rotation.
Further, it is pivotally connected on lug 1411 and is provided with first and only supports protrusion 1412,1423 two sides of abutting part are provided with the Two only support raised 1424, and second, which only supports protrusion 1424, only only supports to protrusion 1412 under the action of the first elastic component 143 with first, To prevent fastener 142, rotation causes clamping part 1422 to fail to be clamped with buckle slot 1051 counterclockwise, so that fastener 142 is being pressed When casting die 145 is not pressed, fastener 142 is in first position.
Referring to Fig. 6, Fig. 7, Fig. 9, Figure 11 and Figure 12, in another alternative embodiment of the utility model, battery fixed knot Structure is additionally provided with locating piece 144.
Specifically, frame 13 can be fixed in the lower case 162 of unmanned plane, and lower case 162 is provided with pressing hole 1621, locating piece 144 is provided with guide post 1441 and fixation hole 1442, and lower case 162 is provided with the second fixed column 1622, and second Internal thread hole has can be set in fixed column 1622, can be locked at down locating piece 144 after passing through fixation hole 1422 by screw On shell 162.In addition, press section 1451 is provided with pilot hole 1453, pilot hole 1453 is sheathed in guide post 144, so that pressing Casting die 145 can be slided up and down along guide post 1441.
Optionally, the outer profile of pressing hole 1621 be less than press section 1451 outer profile, press section 1451 be placed in by Press hole 1621 in after, press section 1451 since the blocking of the hole wall 16211 of pressing hole 1621 can not deviate from from lower case 162, So that the press section 1451 of pressing piece 145 is exposed to that pressing hole 1621 is outer and pressing piece 145 refers in lower case 162 along guiding Column 144 slides up and down, it is of course also possible to by positioning being arranged in guide post 1441 to prevent pressing piece 145 from pressing hole Deviate from 1621.
Preferably, battery guide structure further includes the second elastic component 146, and the second elastic component is sheathed in guide post 144, makes Pressing piece 145 is obtained after pressing removes pressing force, pressing piece resets under the action of the second elastic component 146, optionally, the second bullet Property part be pressure spring or elastic rubber sleeve.
Certainly, in the utility model embodiment, unmanned plane further includes upper housing, is cooperatively formed by upper housing and lower case Unmanned plane shell, the shell are generally rectangular shaped, and when implementing the utility model, a left side for shell can also be arranged in pressing hole 1621 On side or right side or top surface, specifically, the axial direction of guide post 144 can be perpendicular to the two side walls of frame 13 With one in roof so that the activity direction of pressing piece 145 is perpendicular to one in two side walls and roof, i.e. pressing piece 145 press section 1451 can be exposed on a surface in top surface, left and right sides and the bottom surface of unmanned plane shell, such as be schemed Shown in 2, press section 1451 is exposed to the bottom surface of unmanned plane, naturally it is also possible to be exposed to the top surface of unmanned plane shell, such as nobody The mark of machine manufacturer marks on the outer surface of press section 1451, forms mark and press section 1451 is integrated, so that nothing Man-machine have a good appearance, and the utility model embodiment pressing piece 145 is arranged specifically a certain surface is not in unmanned plane shell It limits.
The utility model embodiment also provides a kind of unmanned plane, which includes the battery that any of the above-described embodiment provides Fixed structure.
In the description of the present invention, unless otherwise clearly defined and limited, term " connected ", " connection ", " Gu It is fixed " it shall be understood in a broad sense, for example, it may be being fixedly connected, it may be a detachable connection, or integral;It can be mechanical connect It connects, is also possible to be electrically connected;It can be directly connected, can also can be in two elements indirectly connected through an intermediary The interaction relationship of the connection in portion or two elements.For the ordinary skill in the art, it can be managed with concrete condition Solve the concrete meaning of above-mentioned term in the present invention.
In the present invention unless specifically defined or limited otherwise, fisrt feature the "upper" of second feature or it "lower" may include that the first and second features directly contact, and also may include that the first and second features are not direct contacts but lead to Cross the other characterisation contact between them.Moreover, fisrt feature includes above the second feature " above ", " above " and " above " One feature is right above second feature and oblique upper, or is merely representative of first feature horizontal height higher than second feature.First is special Sign is directly below and diagonally below the second feature including fisrt feature under the second feature " below ", " below " and " below ", or only Indicate that first feature horizontal height is less than second feature.
The position when nouns of locality such as the front, rear, left and right mentioned in following embodiment are according to unmanned plane normally travel is come Description, only as description reference.
In the description of this specification, the description of reference term " embodiment " etc. means the specific spy in conjunction with the embodiment Sign, structure, material or feature are contained at least one embodiment or example of the utility model.In the present specification, right The schematic representation of above-mentioned term is not necessarily referring to identical embodiment.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped Containing an independent technical solution, this narrating mode of specification be only be to understand device, those skilled in the art should It considers the specification as a whole, the technical solutions in the embodiments can also be appropriately combined, and forming those skilled in the art can With the other embodiments of understanding.
Technical principle of the utility model has been described above with reference to specific embodiments.These descriptions are intended merely to explain this reality With novel principle, and it cannot be construed to the limitation to scope of protection of the utility model in any way.Based on the explanation herein, Those skilled in the art, which does not need to pay for creative labor, can associate with other specific implementation modes of this utility model, These modes are fallen within the protection scope of the utility model.

Claims (12)

1. a kind of battery fixing structure characterized by comprising
Frame, is provided with the mounting groove of set battery, and the mounting groove has an open end and a front bulkhead, on the front bulkhead It is provided with card slot via hole;
It is set to the buckle slot of battery rear end face, after the battery is removably plugged in the mounting groove from the open end, The battery rear end face is close to the front bulkhead and the card slot via hole exposes the buckle slot;
Snap component is set to the front bulkhead backwards to the one side of the mounting groove, and the snap component is provided with mobilizable Pressing piece, when the pressing piece is not pressed, the snap component and the buckle slot are clamped with the fixation battery, described to press When casting die is pressed, the snap component is separated with the buckle slot to dismantle the battery.
2. battery fixing structure as described in claim 1, which is characterized in that the frame further includes bottom wall, roof and two Side wall, the bottom wall and the roof are oppositely arranged, and two side walls are oppositely arranged and are separately connected the bottom wall and described The left and right sides of roof, the side of the front bulkhead are separately connected the bottom wall, institute's roof and two side walls, the bottom Wall, the roof, the front bulkhead and two side walls form the mounting groove.
3. battery fixing structure as claimed in claim 2, which is characterized in that the activity direction of the pressing piece is perpendicular to two One in the side wall, bottom wall and roof.
4. battery fixing structure as described in claim 1, which is characterized in that the snap component further includes articulated part, buckle Part, the first elastic component and drive-connecting shaft;
The articulated part is set to the front bulkhead backwards to the one side of the mounting groove;
The fastener includes clamping part, abutting part and the articulated section between the clamping part and the abutting part, institute It states drive-connecting shaft to connect with the articulated part, the fastener is sheathed on the drive-connecting shaft and the pivot joint by the articulated section Part is rotatably connected, and first elastic component is socketed on the drive-connecting shaft;
The pressing piece includes press section and the only top connecting with the press section, and the only top is supported with the abutting part It connects;
When the press section is not pressed, the fastener is under the action of the first elastic component, the clamping part and the card Catching groove clamping, when the press section is pressed, abutting part described in the only top drive is rotated around the drive-connecting shaft, the card Buckle is detached from from the buckle slot.
5. battery fixing structure as claimed in claim 4, which is characterized in that
The articulated part setting is provided with the accommodating sky for accommodating first elastic component there are two lug, the articulated section is pivotally connected Between, the articulated section is embedded between two pivot joint lugs, and first elastic component is placed in the accommodating space, described Drive-connecting shaft is connect through the articulated section and first elastic component and with two pivot joint lugs.
6. battery fixing structure as claimed in claim 5, which is characterized in that be provided with first on the pivot joint lug only to convex It rises, the abutting part two sides are provided with second and only support protrusion, and described second only supports protrusion under the action of first elastic component Protrusion is only supported with described first only to support.
7. battery fixing structure as claimed in claim 4, which is characterized in that first elastic component is torsional spring.
8. battery fixing structure as claimed in claim 4, which is characterized in that the frame is set on the shell of unmanned plane, The battery fixing structure further includes locating piece;
The shell is provided with pressing hole, the locating piece and the cage connection, and the locating piece is provided with guide post, described Press section is provided with pilot hole, and the pilot hole is sheathed in the guide post, and the press section is exposed to outside the pressing hole.
9. battery fixing structure as claimed in claim 8, which is characterized in that it further include the second elastic component, second elasticity Part is sheathed in the guide post.
10. battery fixing structure as claimed in claim 9, which is characterized in that second elastic component is pressure spring or elasticity Rubber bush.
11. such as the described in any item battery fixing structures of claim 1-10, which is characterized in that the buckle slot is from the battery Rear end face towards extend outside the battery or the buckle slot from the battery rear end face towards the battery in extend.
12. a kind of unmanned plane, which is characterized in that the unmanned plane includes that battery as described in any one of claim 1 to 11 is solid Determine structure.
CN201822085189.5U 2018-12-12 2018-12-12 Battery fixing structure and unmanned plane Active CN209290704U (en)

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