CN218887408U

CN218887408U - Battery fast-assembling structure

Info

Publication number: CN218887408U
Application number: CN202223414294.1U
Authority: CN
Inventors: 林圣展
Original assignee: Taicang Zhongruishi Technology Co ltd
Current assignee: Taicang Zhongruishi Technology Co ltd
Priority date: 2022-12-20
Filing date: 2022-12-20
Publication date: 2023-04-18
Anticipated expiration: 2032-12-20

Abstract

The utility model discloses a battery fast-assembling structure, which relates to the technical field of battery fast-assembling, comprising an unmanned aerial vehicle body, a first groove is arranged in the unmanned aerial vehicle body, the inner side wall of the first groove is symmetrically provided with a socket, a second groove is arranged on the bottom surface in the first groove, a lifting seat is movably arranged in the second groove, the end part of the lifting seat is provided with a battery, the two sides of the lifting seat are symmetrically provided with clamping plates, the lifting seat descends vertically to drive the two clamping plates to rotate synchronously and in different directions for clamping the battery, the bottom surface in the second groove is also provided with an inclined plane block, the inclined plane block reciprocates linearly along the horizontal direction for locking and unlocking the position of the lifting seat; the utility model discloses a press the realization to the battery fast-assembling, pull the slide bar again and realize the battery quick detach, simple and convenient efficient.

Description

Battery fast-assembling structure

Technical Field

The utility model relates to a battery fast-assembling technical field specifically is a battery fast-assembling structure.

Background

The airplane structural battery is a high-energy-ratio battery which is based on the existing graphene material technology and the nanometer battery technology, breaks through the novel battery structure stacking, carries out brand-new aircraft battery structural design, reduces the weight of an aircraft body, realizes the preparation of a high-conductivity solid electrolyte and has enough structural strength and fatigue strength for the aircraft.

Most of batteries installed in the existing unmanned aerial vehicle are lithium batteries, the lithium batteries are placed in a battery box, and then the batteries are fixed in position through a fixing structure, so that the operation steps are relatively more during installation and disassembly of the batteries, and a quick-assembly and quick-disassembly technology for the batteries is needed.

To the problem, the utility model provides a battery fast-assembling structure.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a battery fast-assembling structure, the utility model discloses a press the realization to the battery fast-assembling, pull the slide bar again and realize the battery quick detach, simple and convenient efficient to the problem in the background art has been solved.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a battery fast-assembling structure, including the unmanned aerial vehicle body, first groove has been seted up in the unmanned aerial vehicle body, first inslot lateral wall symmetry is provided with the socket, the second groove has been seted up on the first inslot bottom surface, the activity of second inslot portion is provided with the lift seat, the tip of lift seat is provided with the battery, the bilateral symmetry of lift seat is provided with the clamp plate, the perpendicular decline of lift seat drives two synchronous incorgruous rotations of clamp plate, a be used for pressing from both sides tightly the battery, still be provided with the sloping piece on the second inslot bottom surface, the reciprocating linear motion of horizontal direction is followed to the sloping piece, a position lock and the unblock for the lift seat.

Further, the holding tank has been seted up to second inslot lateral wall symmetry, L type hole has been seted up to the inside of inclined plane piece, inclined plane piece side middle part fixedly connected with slide bar, the slide bar other end passes the holding tank and extends to the unmanned aerial vehicle body outside, slide bar and holding tank inside wall sliding connection, holding tank inside wall fixedly connected with second spring, second spring other end fixed connection is on inclined plane piece side, the cladding of second spring is in the slide bar outside, inclined plane piece and second inslot ground sliding connection.

Further, fixedly connected with L template on the lift seat bottom, L template bottom and inclined plane piece inclined plane sliding connection, L template and the downthehole surface sliding connection of L type, the first spring of the mutual symmetry of second inslot bottom surface both sides fixedly connected with, the first spring other end fixed connection is on the lift seat bottom, lift seat and second inslot lateral wall sliding connection.

Furthermore, the clamping plate is fixedly connected to the periphery of the gear, the gear is rotatably connected to the inner side wall of the accommodating groove through the positioning pin, the gear is meshed with the connecting rack, the rack is fixedly connected to the middle of the outer side wall of the lifting seat, and the positioning groove is formed in the end face of the lifting seat.

Furthermore, a fixed plate is fixedly connected to the bottom surface of the first groove, a line arranging groove is symmetrically formed in the side surface of the fixed plate, and a sliding cover is arranged at the end of the first groove.

Compared with the prior art, the beneficial effects of the utility model are as follows:

the utility model provides a battery fast-assembling structure, open the sliding closure, place the battery in the constant head tank, then press the battery downwards, the lift seat descends and drives L template decline, and then promote the sloping block to slide to the outside, when the L template descends to L shaped hole, under the effort of second spring, the sloping block slides to the inside, L template block is in L shaped hole this moment, and the position of lift seat locks, in the lift seat descending process, the rack drives the gear rotation, and then drives the pinch-off blades rotation and presss from both sides tightly the battery both sides, make the battery position fix, then insert the data line plug on the battery in the socket, accomplish the fast-assembling; if the quick release is needed, the sliding rod is pulled outwards, the lifting seat is unlocked and ascended under the action of the first spring, the clamping plate rotates reversely, and the battery can be directly taken out. The purpose of design like this presses the realization and realizes the fast-assembling to the battery, pulls the slide bar again and realizes the quick detach to the battery, and is simple and convenient efficient.

Drawings

FIG. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a schematic view of the internal structure of the first groove of the present invention;

FIG. 3 is a schematic view of the inner structure of the second groove of the present invention;

fig. 4 is the external structure diagram of the middle lifting seat of the present invention.

In the figure: 1. an unmanned aerial vehicle body; 2. a sliding cover; 3. a first groove; 4. a fixing plate; 5. arranging wire grooves; 6. a socket; 7. a battery; 8. a second groove; 9. a first spring; 10. a lifting seat; 11. positioning a groove; 12. a rack; 13. an L-shaped plate; 14. a gear; 15. a clamping plate; 16. a bevel block; 17. an L-shaped hole; 18. a slide bar; 19. a second spring; 20. and (6) accommodating the tank.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

In order to solve the technical problem of how to realize quick assembly and disassembly of the battery 7, as shown in fig. 1 to 4, the following preferred technical solutions are provided:

the utility model provides a battery fast-assembling structure, including unmanned aerial vehicle body 1, first groove 3 has been seted up in unmanned aerial vehicle body 1, 3 inside wall symmetries in first groove are provided with socket 6, second groove 8 has been seted up on the bottom surface in first groove 3, the inside activity of second groove 8 is provided with lift seat 10, the tip of lift seat 10 is provided with battery 7, the bilateral symmetry of lift seat 10 is provided with clamp plate 15, lift seat 10 descends perpendicularly and drives two synchronous incorgruous rotations of clamp plate 15, be used for pressing from both sides tightly battery 7, still be provided with bevel block 16 on the bottom surface in second groove 8, bevel block 16 is along the reciprocal linear motion of horizontal direction, be used for the position locking and the unblock of lift seat 10.

Specifically, the sliding cover 2 is opened, the battery 7 is placed in the positioning groove 11, then the battery 7 is pressed downwards, the lifting seat 10 descends to drive the L-shaped plate 13 to descend, and further the inclined plate 16 is pushed to slide outwards, when the L-shaped plate 13 descends into the L-shaped hole 17, under the action of the second spring 19, the inclined plate 16 slides inwards, at the moment, the L-shaped plate 13 is clamped in the L-shaped hole 17, the position of the lifting seat 10 is locked, in the descending process of the lifting seat 10, the rack 12 drives the gear 14 to rotate, and further the clamping plate 15 is driven to rotate to clamp two sides of the battery 7, so that the position of the battery 7 is fixed, then a data line plug on the battery 7 is inserted into the socket 6, and fast assembly is completed; if the quick release is needed, the sliding rod 18 is pulled outwards, the lifting seat 10 is unlocked and ascended under the action of the first spring 9, the clamping plate 15 rotates reversely, and the battery 7 can be directly taken out. The purpose of the design is to press the battery 7 to be quickly assembled, pull the sliding rod 18 to quickly disassemble the battery 7, and the design is simple, convenient and efficient.

Further, as shown in fig. 2-4, the following preferred technical solutions are provided:

holding tank 20 has been seted up to 8 inside wall symmetries in second groove, L type hole 17 has been seted up to inclined plane piece 16 inside, 16 side middle part fixedly connected with slide bar 18 in inclined plane piece, the slide bar 18 other end passes holding tank 20 and extends to unmanned aerial vehicle body 1 outside,

slide bar

18 and 20 inside wall sliding connection in holding tank, 20 inside wall fixedly connected with second springs 19 in holding tank, 19 other end fixed connection of second springs is on 16 sides in inclined plane piece, 19 cladding of second springs are in the slide bar 18 outside,

inclined plane piece

16 and 8 ground sliding connection in the second groove, but the purpose of design like this guarantees 16 horizontal direction reciprocating motion of inclined plane piece.

fixedly connected with L template 13 on the lift seat 10 bottom, L template 13 bottom and the 16 inclined plane sliding connection of inclined plane piece, L template 13 and the internal surface sliding connection in L type hole 17, the first spring 9 of bottom surface both sides fixedly connected with mutual symmetry in second groove 8, first spring 9 other end fixed connection is on lift seat 10 bottom, lift seat 10 and the 8 inside wall sliding connection in second groove, the purpose of design like this is to guarantee that lift seat 10 descends and drives L template 13 and descend and utilize inclined plane piece 16 to fix the position of lift seat 10, utilize inclined plane piece 16 to remove simultaneously, carry out the unblock to lift seat 10 position under the effect of first spring 9.

15 fixed connection of clamp plate is in gear 14 periphery, gear 14 rotates through the locating pin to be connected on the 20 inside walls of holding tank, gear 14 meshes connecting rack 12, rack 12 fixed connection is at 10 lateral wall middle parts of lift seat, constant head tank 11 has been seted up to lift seat 10 terminal surfaces, the purpose of design like this utilizes constant head tank 11 to fix a position battery 7, utilize lift seat 10 to descend to drive clamp plate 15 and rotate and press from both sides tightly battery 7, utilize lift seat 10 to rise to drive clamp plate 15 antiport and loosen battery 7.

Further, as shown in fig. 1 and fig. 2, the following preferred technical solutions are provided:

fixedly connected with fixed plate 4 on the bottom surface in first groove 3, reason wire casing 5 has been seted up to fixed plate 4 side symmetry, and 3 tip in first groove are provided with sliding closure 2, and the purpose of design like this is that the data line plug on the battery 7 of being convenient for is inserted on socket 6, avoids the data line winding together through reason wire casing 5, opens and shuts first groove 3 through sliding closure 2.

In summary, the following steps: the sliding cover 2 is opened, the battery 7 is placed in the positioning groove 11, then the battery 7 is pressed downwards, the lifting seat 10 descends to drive the L-shaped plate 13 to descend, the inclined surface block 16 is further pushed to slide outwards, when the L-shaped plate 13 descends into the L-shaped hole 17, under the action of the second spring 19, the inclined surface block 16 slides inwards, the L-shaped plate 13 is clamped in the L-shaped hole 17 at the moment, the position of the lifting seat 10 is locked, in the descending process of the lifting seat 10, the rack 12 drives the gear 14 to rotate, the clamping plate 15 is further driven to rotate to clamp two sides of the battery 7, the position of the battery 7 is fixed, then a data line plug on the battery 7 is inserted into the socket 6, and fast assembly is completed; if the quick release is needed, the sliding rod 18 is pulled outwards, the lifting seat 10 is unlocked and ascended under the action of the first spring 9, the clamping plate 15 rotates reversely, and the battery 7 can be directly taken out. The purpose of the design is to press the battery 7 to be quickly assembled, pull the sliding rod 18 to quickly disassemble the battery 7, and the design is simple, convenient and efficient.

It should be noted that, in this document, relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a battery fast-assembling structure, includes unmanned aerial vehicle body (1), its characterized in that: first groove (3) have been seted up in unmanned aerial vehicle body (1), first groove (3) inside wall symmetry is provided with socket (6), second groove (8) have been seted up on first groove (3) bottom surface, second groove (8) inside activity is provided with lift seat (10), the tip of lift seat (10) is provided with battery (7), the bilateral symmetry of lift seat (10) is provided with clamp plate (15), lift seat (10) descend perpendicularly to drive two clamp plate (15) synchronous incorgruous rotations for press from both sides tightly battery (7), still be provided with bevel block (16) on second groove (8) bottom surface, bevel block (16) are along the reciprocal linear motion of horizontal direction, a position locking and the unblock of lift seat (10).

2. The battery quick-mounting structure as claimed in claim 1, wherein: holding tank (20) have been seted up to second groove (8) inside wall symmetry, L type hole (17) have been seted up to inclined plane piece (16) inside, inclined plane piece (16) side middle part fixedly connected with slide bar (18), slide bar (18) other end passes holding tank (20) and extends to unmanned aerial vehicle body (1) outside, slide bar (18) and holding tank (20) inside wall sliding connection, holding tank (20) inside wall fixedly connected with second spring (19), second spring (19) other end fixed connection is on inclined plane piece (16) side, the cladding of second spring (19) is in the slide bar (18) outside, ground sliding connection in inclined plane piece (16) and second groove (8).

3. The battery quick-assembly structure as claimed in claim 1, wherein: fixedly connected with L template (13) on lift seat (10) bottom, L template (13) bottom and sloping block (16) inclined plane sliding connection, L template (13) and L type hole (17) internal surface sliding connection, first spring (9) of bottom surface both sides fixedly connected with mutual symmetry in second groove (8), first spring (9) other end fixed connection is on lift seat (10) bottom, lift seat (10) and second groove (8) inside wall sliding connection.

4. The battery quick-mounting structure as claimed in claim 1, wherein: clamping plate (15) fixed connection is in gear (14) periphery, and gear (14) rotate through the locating pin and connect on holding tank (20) inside wall, and rack (12) are connected in gear (14) meshing, and rack (12) fixed connection has seted up constant head tank (11) at lift seat (10) lateral wall middle part, lift seat (10) terminal surface.

5. The battery quick-mounting structure as claimed in claim 1, wherein: the fixed plate (4) is fixedly connected to the inner bottom surface of the first groove (3), the wire arranging groove (5) is symmetrically formed in the side surface of the fixed plate (4), and the sliding cover (2) is arranged at the end of the first groove (3).