Anti-vibration solid-state battery module and agricultural unmanned aerial vehicle adaptive equalization management device

Abstract

The application relates to the technical field of batteries, in particular to an anti-vibration solid-state battery module and an agricultural unmanned aerial vehicle self-adaptive equalization management device. The anti-vibration solid-state battery module comprises a battery body, the battery body is installed on an unmanned aerial vehicle, and a supporting convex ring is symmetrically arranged on the battery body; an operation assembly is installed on the supporting convex ring, and the operation assembly is matched with the supporting convex ring to realize self-locking; a plug-in fixing assembly preliminarily fixes the battery body; and an adsorption fixing assembly adsorptively fixes the battery body. The application also relates to the agricultural unmanned aerial vehicle self-adaptive equalization management device, which comprises a fixing reinforcing assembly, the fixing reinforcing assembly reinforces and fixes the battery body; a control assembly controls the fixing reinforcing assembly to move; and the fixing reinforcing assembly and the control assembly are both installed on the unmanned aerial vehicle.

Description

TECHNICAL FIELD

[0001] The application relates to the technical field of batteries, in particular to an anti-vibration solid-state battery module and an agricultural unmanned aerial vehicle self-adaptive equalization management device. BACKGROUND

[0002] A battery is a power source for normal work of an agricultural unmanned aerial vehicle. The agricultural unmanned aerial vehicle can spray pesticide on crops, and has high work efficiency, thereby greatly reducing the work intensity of workers. During the flight work of the agricultural unmanned aerial vehicle, various complex environments and unexpected conditions may be encountered, such as air flow changes and terrain undulations, which can cause the unmanned aerial vehicle to vibrate. In order to facilitate the mounting and dismounting of the battery, the battery of the existing agricultural unmanned aerial vehicle is generally fixed in a buckle form. Although such a fixing mode is simple and convenient, the anti-vibration effect is poor. During long-term use, the battery and the unmanned aerial vehicle may be electrically connected unsteadily due to vibration, and the phenomenon of poor contact may occur. In addition, the battery is prone to being damaged in vibration for a long time, thereby causing certain economic losses. SUMMARY

[0003] The application aims to provide an anti-vibration solid-state battery module and an agricultural unmanned aerial vehicle self-adaptive equalization management device to solve the problems in the background.

[0004] To achieve the above-mentioned purpose, the application provides the following technical scheme.

[0005] The anti-vibration solid-state battery module comprises a battery body, the battery body is installed on an unmanned aerial vehicle, and a supporting convex ring is symmetrically arranged on the battery body;

[0006] An operating assembly is installed on the supporting convex ring, and the operating assembly and the supporting convex ring are matched to realize self-locking;

[0007] A plug-in fixing assembly is installed on the supporting convex ring to fix the battery body;

[0008] An adsorption fixing assembly is also installed on the supporting convex ring to adsorb and fix the battery body;

[0009] The operating assembly is connected with the adsorption fixing assembly and the plug-in fixing assembly respectively to drive the two assemblies to move.

[0010] Preferably, the operating assembly comprises an operating ring plate, and the operating ring plate is movably installed on the supporting convex ring.

[0011] Self-locking matching plates are symmetrically installed on the operating ring plate.

[0012] Preferably, the self-locking matching plate is connected with the operation ring plate through an elastic member and can move relative to the self-locking matching plate.

[0013] Preferably, the plug-in fixing assembly is a moving block body, the moving block body is movably connected with the operation ring plate to drive the moving block body to move and fix the battery body in cooperation with the unmanned aerial vehicle.

[0014] Preferably, the adsorption fixing assembly is a connecting carrier disc, the connecting carrier disc is movably connected with the operation ring plate to drive the connecting carrier disc to move and adsorb and fix the battery body in cooperation with the unmanned aerial vehicle.

[0015] The agricultural unmanned aerial vehicle self-adaptive balanced management device comprises a fixed reinforcing assembly which reinforces and fixes the battery body.

[0016] A control assembly is arranged to control the fixed reinforcing assembly to move.

[0017] The fixed reinforcing assembly and the control assembly are both installed on the unmanned aerial vehicle.

[0018] Preferably, the fixed reinforcing assembly comprises a driving ring plate which is sleeved on the outside of the battery body.

[0019] A reinforcing carrier is movably connected with the driving ring plate.

[0020] A movable carrier strip is movably connected with the driving ring plate.

[0021] Preferably, the driving ring plate drives the reinforcing carrier to move, so that the reinforcing carrier supports and fixes the battery body in cooperation with the battery body.

[0022] Preferably, the driving ring plate drives the movable carrier strip to move, so that the movable carrier strip cooperates with the self-locking matching plate to ensure the stability of the self-locking matching plate.

[0023] Preferably, the control assembly comprises an electric telescopic rod which is fixedly installed on the unmanned aerial vehicle.

[0024] A controller is fixedly installed on the unmanned aerial vehicle to control the electric telescopic rod.

[0025] A vibration sensor is also fixedly installed on the unmanned aerial vehicle.

[0026] Preferably, the electric telescopic rod is fixedly connected with the driving ring plate to drive the driving ring plate to move up and down.

[0027] Compared with the prior art, the present application has the following advantages:

[0028] 1. Through the double locking of negative pressure adsorption and moving lock rod to the battery body, it can be stably installed on the unmanned aerial vehicle, and it is firmly connected with the unmanned aerial vehicle. Through the double locking, the vibration resistance of the battery body can be improved, and through the operation of the ring plate, the movement of the negative pressure adsorption and the moving lock rod is synchronized, so that the battery body is convenient and fast to disassemble, and the vibration resistance is improved without losing the convenience of disassembly.

[0029] 2. When the vibration sensor detects that the unmanned aerial vehicle vibrates during flight, the controller will control the electric telescopic rod to elongate, and then drive the driving ring plate to move up under the action of the electric telescopic rod. With the upward movement of the driving ring plate, it will drive the movable load strip to move, and with the movement of the movable load strip, the gear convex plate will be in contact with the self-locking support strip, which will limit the self-locking support strip. In this way, the self-locking cooperation plate cannot move even under the action of external force, which fully guarantees the firmness and reliability of the battery body installation.

[0030] 3. In addition, with the upward movement of the driving ring plate, it will also drive the reinforced carrier to move, and with the movement of the reinforced carrier, the reinforced cooperation column on the reinforced carrier will be inserted into the auxiliary cavity on the battery body. In this way, the battery body can be further fixed and supported, and its vibration resistance is improved again, which can better cope with vibration. BRIEF DESCRIPTION OF DRAWINGS

[0031] Figure 1 The first perspective view of the battery body assembly.

[0032] Figure 2 The second perspective view of the battery body assembly.

[0033] Figure 3 The structure diagram of the battery body.

[0034] Figure 4 The assembly diagram of the operation ring plate.

[0035] Figure 5 The assembly diagram of the unmanned aerial vehicle.

[0036] Figure 6 The assembly diagram of the unmanned aerial vehicle and the battery body.

[0037] Figure 7 The structure diagram of the unmanned aerial vehicle.

[0038] Figure 8 The assembly diagram of the unmanned aerial vehicle.

[0039] Figure 9 The cooperation diagram of the bearing plate and the driving ring plate.

[0040] In the figure: 1, battery body; 11, support convex ring; 12, lower insertion hole; 13, matching cavity; 14, rubber carrier pad; 15, moving hole; 16, support channel; 17, limiting baffle; 18, auxiliary cavity; 2, operating ring plate; 21, lower insertion connecting rod; 22, connecting plate; 23, lower vertical connecting plate; 24, connecting movable strip; 25, connecting rod holder; 26, bearing channel; 3, connecting carrier disc; 31, moving carrier rod; 32, cavity plug plate; 4, moving block; 41, moving lock rod; 5, self-locking matching plate; 51, bearing strip rod; 52, elastic strip; 53, self-locking bearing strip; 54, self-locking bearing block; 6, unmanned aerial vehicle; 60, protective cover; 61, battery cavity; 62, lock rod insertion hole; 63, bearing plate; 64, limiting channel; 65, vertical plate carrier; 66, matching plate cavity; 67, support plate; 68, stabilizing carrier rod; 7, driving ring plate; 71, stabilizing channel; 72, connecting groove; 73, driving column; 74, push-pull rod; 8, reinforced carrier; 81, reinforced carrier rod; 82, reinforced matching column; 9, movable carrier strip; 91, driving matching slide; 92, matching bearing rod; 93, matching block; 94, gear convex plate; 10, electric telescopic rod; 101, controller; 102, vibration sensor. DETAILED DESCRIPTION

[0041] The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without creative labor fall within the scope of protection of the present application.

[0042] The present application provides a technical solution:

[0043] As shown in Figure 1 , Figure 2 and Figure 6 , the anti-vibration solid-state battery module comprises: a battery body 1: the battery body 1 is installed on an unmanned aerial vehicle 6, and a support convex ring 11 is integrally formed on the battery body 1.

[0044] An operating assembly: the operating assembly is installed on the support convex ring 11, and the operating assembly and the support convex ring 11 cooperate to realize self-locking.

[0045] A plug-in fixing assembly: the plug-in fixing assembly preliminarily fixes the battery body 1.

[0046] An adsorption fixing assembly: the adsorption fixing assembly adsorbs and fixes the battery body 1, and the operating assembly is connected with the adsorption fixing assembly and the plug-in fixing assembly respectively, thereby driving the two to move.

[0047] AsFigure 3 As shown in the drawings, the support convex ring 11 is provided with a lower insertion hole 12, and two symmetrical matching cavities 13 are provided on the two sides of the support convex ring 11. A rubber pad 14 is attached to the end face of the port of the matching cavity 13, and a moving hole 15 is provided at the bottom of the matching cavity 13. In addition, two symmetrical support channels 16 are provided on the two sides of the support convex ring 11, and the support channels 16 are located below the matching cavities 13. A limiting baffle 17 is integrally formed on the support convex ring 11. Two symmetrical auxiliary cavities 18 are provided on the battery body 1.

[0048] As shown in the drawings, Figure 1 and Figure 4 The operation assembly includes an operation ring plate 2, which is movably mounted on the support convex ring 11. The operation ring plate 2 is symmetrically welded and fixed with a lower insertion connecting rod 21. The lower insertion connecting rod 21 is inserted into the lower insertion hole 12, and the lower end of the lower insertion connecting rod 21 is welded and fixed with a connecting plate strip 22. The lower end of the connecting plate strip 22 is symmetrically integrally formed with a downward connecting plate 23, and the upper end of the connecting plate strip 22 is symmetrically hinged with a connecting movable strip 24. The downward connecting plate 23 is hinged with a connecting rod holder 25. In addition, the operation ring plate 2 is also provided with a bearing channel 26.

[0049] As shown in the drawings, Figure 2 and Figure 4 The self-locking matching plate 5 is two, symmetrically mounted on the operation ring plate 2, connected with the operation ring plate 2 through the elastic piece, and can move relative to the self-locking matching plate 5. The self-locking matching plate 5 is integrally formed with a bearing strip 51 on the upper end. The bearing strip 51 is inserted into the bearing channel 26. The elastic piece is an elastic strip 52, and the two ends of the elastic strip 52 are respectively welded on the self-locking matching plate 5 and the operation ring plate 2. The self-locking matching plate 5 is also integrally formed with a self-locking bearing strip 53. The lower end of the self-locking bearing strip 53 is integrally formed with a self-locking bearing block 54. When the self-locking bearing block 54 locks the operation ring plate 2, it is clamped at the lower end face of the limiting baffle 17, and the surface of the self-locking bearing block 54 is smooth without burr.

[0050] As shown in the drawings, Figure 2 and Figure 4 The insertion fixing assembly is a moving block body 4, which is movably connected with the operation ring plate 2 to drive the moving block body 4 to move and cooperate with the unmanned aerial vehicle 6 to fix the battery body 1. The lower end of the connecting rod holder 25 is hinged with the moving block body 4. The moving block body 4 is integrally formed with a moving lock rod 41, and the moving lock rod 41 is partially inserted into the support channel 16.

[0051] The adsorption fixing assembly is a connecting carrier plate 3, which is movably connected with the operation ring plate 2 to drive the connecting carrier plate 3 to move and cooperate with the unmanned aerial vehicle 6 to adsorb and fix the battery body 1. The connecting carrier plate 3 is hingedly connected with the upper end of the connecting movable strip 24, and a movable carrier rod 31 is welded and fixed on the connecting carrier plate 3. The movable carrier rod 31 is partially inserted into the matching cavity 13 through the movable through hole 15, and a cavity plug plate 32 is welded and fixed at the end of the movable carrier rod 31 away from the connecting carrier plate 3. The cavity plug plate 32 is in the matching cavity 13 and tightly matches with the inner wall of the matching cavity 13. In addition, when the cavity plug plate 32 does not adsorb and fix the battery body 1, the end face of the cavity plug plate 32 is flush with the end face where the cavity opening of the matching cavity 13 is located.

[0052] As shown in Figure 5 , Figure 6 , Figure 7 , Figure 8 and Figure 9 , the protective cover 60 is fixedly installed on the unmanned aerial vehicle 6 by bolts. The battery cavity 61 is formed in the unmanned aerial vehicle 6, and the battery body 1 is partially inserted into the battery cavity 61 when the battery body 1 is installed on the unmanned aerial vehicle 6. The inside of the battery cavity 61 is provided with a lock rod insertion hole 62. In addition, the bearing plate 63 is symmetrically welded and fixed on the unmanned aerial vehicle 6. The limiting channel 64 is symmetrically formed in the bearing plate 63. The vertical plate bearing 65 is also symmetrically and integrally formed on the bearing plate 63. The matching plate cavity 66 is formed in the vertical plate bearing 65. The support plate 67 is integrally formed at the upper end of the vertical plate bearing 65. The stable carrier rod 68 is welded and fixed on the support plate 67.

[0053] As shown in Figure 8 , the agricultural unmanned aerial vehicle self-adaptive balanced management device comprises a fixed reinforcing assembly which reinforces and fixes the battery body 1.

[0054] The control assembly controls the movement of the fixed reinforcing assembly. The fixed reinforcing assembly and the control assembly are both installed on the unmanned aerial vehicle 6.

[0055] As shown in Figure 9 , the fixed reinforcing assembly comprises a drive ring plate 7 which is sleeved on the outside of the battery body 1.

[0056] The reinforcing carrier 8 is movably connected with the drive ring plate 7.

[0057] The movable carrier strip 9 is movably connected with the driving ring plate 7, the driving ring plate 7 is provided with a stable channel 71, the stable channel 71 is inserted with a stable carrier rod 68, and the driving ring plate 7 is also provided with an adapter groove 72, the adapter groove 72 is symmetrically welded with a driving column 73, the driving column 73 is connected with the movable carrier strip 9, and in addition, the lower side of the driving ring plate 7 is also hinged with a push-pull rod 74, and the lower end of the push-pull rod 74 is hinged with the reinforced carrier 8.

[0058] The driving ring plate 7 drives the reinforced carrier 8 to move, so that the reinforced carrier 8 cooperates with the battery body 1 to support and fix the battery body 1, the reinforced carrier 8 is two, which are respectively installed on two carrier plate members 63, the reinforced carrier 8 is symmetrically welded with a reinforced carrier rod 81, the reinforced carrier rod 81 is inserted in the limiting channel 64, and the reinforced carrier 8 is limited through the limiting channel 64, the reinforced carrier rod 81 can move along the limiting channel 64, and the reinforced carrier rod 81 is welded with a reinforced cooperation column 82 at the head away from the reinforced carrier 8.

[0059] The driving ring plate 7 drives the movable carrier strip 9 to move, so that it cooperates with the self-locking cooperation plate 5 to ensure the stability of the self-locking cooperation plate 5, the movable carrier strip 9 is partially inserted in the adapter groove 72, and the movable carrier strip 9 is symmetrically provided with a driving cooperation slide 91, the inner wall of the driving cooperation slide 91 is smooth without burrs, and the driving cooperation slide 91 is inserted with the driving column 73, the driving column 73 is in contact with the inner wall of the driving cooperation slide 91, and the movable carrier strip 9 is also integrally provided with a cooperation carrier rod 92, the cooperation carrier rod 92 is inserted in the cooperation plate cavity 66, and the movable carrier strip 9 is supported through the cooperation of the cooperation plate cavity 66 and the cooperation carrier rod 92, and the cooperation carrier rod 92 is welded with a cooperation block 93 at the head away from the movable carrier strip 9, and the cooperation block 93 is integrally provided with a gear protruding plate 94, and the surface of the gear protruding plate 94 is smooth without burrs.

[0060] The control assembly comprises an electric telescopic rod 10: the electric telescopic rod 10 is fixedly installed on the unmanned aerial vehicle 6;

[0061] A controller 101: the controller 101 is fixedly installed on the unmanned aerial vehicle 6, and controls the electric telescopic rod 10;

[0062] A vibration sensor 102: the vibration sensor 102 is also fixedly installed on the unmanned aerial vehicle 6, detects vibration when the unmanned aerial vehicle 6 vibrates, and the controller 101 controls the electric telescopic rod 10 to elongate.

[0063] The electric telescopic rod 10 is fixedly connected with the driving ring plate 7, drives the driving ring plate 7 to move up and down, and the electric telescopic rod 10 and the driving ring plate 7 can be connected and fixed through bolts.

[0064] By multiple fixing of the battery body 1, the firmness and stability of the battery body 1 installation can be fully ensured, and then a good anti-vibration effect can be achieved, the safety of the battery body 1 in the working process is ensured, and the stability of the electrical connection between the battery body 1 and the unmanned aerial vehicle 6 is ensured, the normal flight work of the unmanned aerial vehicle 6 is ensured, when installing the battery body 1, it is inserted into the battery cavity 61, and the cavity plug plate 32 is pulled upward during the insertion process to be located at the cavity opening of the cavity 13, at this time, the self-locking block 54 is in contact with the inner end face of the limiting baffle 17, and the elastic strip 52 is in a compressed state at this time, when the battery body 1 is inserted into the battery cavity 61, the moving lock rod 41 is aligned with the lock rod insertion hole 62, at this time, the rubber pad 14 is in contact with the end face of the vertical plate carrier 65, and the rubber pad 14 is in a certain compression state, so that the sealing performance of the cavity opening of the cavity 13 can be ensured, after the battery body 1 is inserted, the operating ring plate 2 is pushed downward, and the engaging carrier plate 3 is driven to move under the action of the engaging movable strip 24, so that the cavity plug plate 32 is further moved into the cavity 13, and a negative pressure is generated in the cavity 13, so that the battery body 1 can be adsorbed and fixed under the action of the negative pressure, in addition, the moving block 4 is driven to move under the action of the engaging rod frame 25 when the operating ring plate 2 moves downward, so that the moving lock rod 41 is inserted into the lock rod insertion hole 62, so that the battery body 1 can be further fixed under the cooperation of the moving lock rod 41 and the lock rod insertion hole 62, the multi-point fixing of the battery body 1 is ensured, and the stable installation is ensured, when the operating ring plate 2 moves downward, the self-locking block 54 on the self-locking block 54 moves to the lower side of the limiting baffle 17, so that the self-locking block 54 loses the limitation, the self-locking block 54 is moved under the action of the elastic strip 52, and the self-locking block 54 is clamped at the lower end of the limiting baffle 17, so that the operating ring plate 2 cannot be moved upward, and the stable installation of the battery body 1 is ensured, when the unmanned aerial vehicle 6 vibrates during flight, the vibration sensor 102 detects the vibration, and the controller 101 controls the electric telescopic rod 10 to be elongated, so that the driving ring plate 7 can be moved upward, the reinforced carrier 8 is moved to the direction of the battery body 1 under the action of the push-pull rod 74 when the driving ring plate 7 moves upward, the reinforced fitting column 82 is inserted into the auxiliary cavity 18 on the battery body 1 when the reinforced carrier 8 moves, so that the battery body 1 can be further supported and fixed under the cooperation of the reinforced fitting column 82 and the auxiliary cavity 18, in addition, the movable carrier strip 9 is moved under the cooperation of the driving column 73 and the driving fitting slide 91 when the driving ring plate 7 moves upward, so that the blocking convex plate 94 on the fitting block 93 is in contact with the self-locking block 53,In this way, the self-locking block 53 is positioned between the blocking cam 94 and the limiting stop 17, and is in contact with both, so that the self-locking block 53 is well fixed and cannot move, thereby achieving the fixing of the self-locking cooperation plate 5, and the fixing of the moving block 4 and the connecting carrier 3 through the fixing of the self-locking cooperation plate 5, thereby fully ensuring the stability of the battery body 1 in vibration, that is, the fixing and support of the battery body 1 can be further strengthened when vibration occurs, thereby ensuring the safe use of the battery body 1. When the vibration is eliminated, the electric telescopic rod 10 drives the driving ring plate 7 to move downward, and when the battery body 1 needs to be disassembled, the two self-locking cooperation plates 5 are pulled to make the self-locking block 54 no longer clamped at the lower end of the limiting stop 17, so that the battery body 1 can be quickly disassembled, which is very convenient and fast.

[0065] Although embodiments of the present application have been shown and described, it is to be understood that various modifications, substitutions, replacements and changes can be made to these embodiments without departing from the principles and spirit of the present application, and the scope of the present application is defined by the appended claims and their equivalents.

Claims

1. Vibration-resistant solid-state battery module, characterized by: include: A battery body, the battery body being mounted on the drone, and having supporting protruding rings symmetrically fixedly provided on the battery body; An operating assembly is mounted on the supporting convex ring, and the operating assembly cooperates with the supporting convex ring to achieve self-locking; The operating assembly includes an operating ring plate and a self-locking matching plate, and the operating ring plate is movably mounted on the supporting convex ring; There are two self-locking matching plates, which are symmetrically mounted on the operating ring plate, and the self-locking matching plates are connected to the operating ring plate through elastic members and can move relative to the self-locking matching plates; A plug-in fixing assembly is installed on the supporting convex ring to fix the battery body, and the plug-in fixing assembly is a movable block. The movable block is movably connected to the operating ring plate to drive the movable block to move and cooperate with the drone to fix the battery body. A movable locking rod is integrally formed on the movable block; An adsorption and fixing component is also installed on the supporting convex ring to adsorb and fix the battery body, and the adsorption and fixing component is a connecting carrier, which is movably connected to the operating ring plate to drive the connecting carrier to move and cooperate with the drone to adsorb and fix the battery body; The operating component is connected to the adsorption fixing component and the plug-in fixing component respectively, driving the two to move.

2. The vibration-resistant solid-state battery module according to claim 1, characterized in that: A lower insertion hole is provided on the supporting convex ring, and matching cavities are symmetrically provided on both sides of the supporting convex ring. A rubber pad is pasted on the end face where the matching cavity port is located, and a movable through hole is provided at the bottom of the matching cavity. In addition, support channels are symmetrically provided on both sides of the supporting convex ring. The support channels are located on the lower side of the matching cavity. A limiting baffle is also provided on the supporting convex ring, and auxiliary cavities are symmetrically provided on the battery body.

3. The vibration-resistant solid-state battery module according to claim 2, characterized in that: The operating ring plate is movably installed on the supporting convex ring, and the operating ring plate is symmetrically fixed with lower plug-in connecting rods, which are inserted into the lower plug-in through holes, and the lower ends of the lower plug-in connecting rods are fixed with connecting strips, and the lower ends of the connecting strips are symmetrically provided with hanging connecting plates, and the upper ends of the connecting strips are symmetrically hinged with connecting movable strips, and the hanging connecting plates are hinged with connecting rod frames, and the operating ring plate is also symmetrically provided with bearing channels.

4. The vibration-resistant solid-state battery module according to claim 3, characterized in that: The self-locking mating plate is connected to the operating ring plate through an elastic part. The self-locking mating plate is symmetrically provided with bearing bars, which are inserted into the bearing channel. The self-locking mating plate is also symmetrically provided with self-locking bearing strips, and the lower end of the self-locking bearing strip is provided with a self-locking bearing block.

5. The vibration-resistant solid-state battery module according to claim 4, characterized in that: The moving block is movably connected to the operating ring plate to drive the moving block to move and cooperate with the drone to fix the battery body. The lower end of the connecting rod frame is hinged to the moving block, and the moving locking rod part is inserted into the support channel.

6. The vibration-resistant solid-state battery module according to claim 5, characterized in that: The connecting carrier is movably connected to the operating ring plate to drive the connecting carrier to move and cooperate with the drone to adsorb and fix the battery body. The connecting carrier is hinged to the upper end of the connecting movable bar, and a movable carrier rod is fixedly provided on the connecting carrier. The movable carrier rod passes through the movable through-hole part and is inserted into the matching cavity. A cavity plug plate is fixed on the end of the movable carrier rod away from the connecting carrier, and the cavity plug plate is in the matching cavity.

7. The vibration-resistant solid-state battery module according to claim 6, characterized in that: A battery cavity is provided on the drone, and a locking rod socket is provided inside the battery cavity. The drone is symmetrically fixed with load-bearing plates, and limited position channels are symmetrically provided on the load-bearing plates. Vertical plate carriers are symmetrically provided on the load-bearing plates, and a matching plate cavity is provided on the vertical plate carrier. A supporting plate is also provided at the upper end of the vertical plate carrier, and a stabilizing load rod is fixed on the supporting plate.

8. Agricultural UAV adaptive balancing management device, characterized by: The adaptive equalization management device is used to strengthen and fix the battery module according to any one of claims 1 to 7, comprising: a fixing and strengthening component, wherein the fixing and strengthening component strengthens and fixes the battery body; The fixed reinforcement assembly includes a driving ring plate, a reinforcement carrier, and a movable carrier bar. The driving ring plate is sleeved on the outer side of the battery body. The reinforcement carrier is movably connected to the driving ring plate, and the movable carrier bar is movably connected to the driving ring plate. The driving ring plate drives the reinforcement carrier to move, so that the reinforcement carrier cooperates with the battery body to support and fix the battery body, and the driving ring plate drives the movable carrier bar to move so that it cooperates with the self-locking matching plate to ensure the stability of the self-locking matching plate. a control component, wherein the control component controls the fixed reinforcement component to move; The fixed reinforcement component and the control component are both installed on the UAV.

9. The agricultural UAV adaptive balancing management device according to claim 8, characterized in that: The driving ring plate is sleeved on the outside of the battery body, the reinforcing carrier is movably connected to the driving ring plate, and the movable carrier bar is movably connected to the driving ring plate. A stabilizing channel is provided on the driving ring plate, and a stabilizing carrier rod is inserted into the stabilizing channel. The driving ring plate is also provided with a connecting groove, and a driving column is symmetrically fixed in the connecting groove. The driving column is connected to the movable carrier bar. A push-pull rod is also hinged on the lower side of the driving ring plate, and the lower end of the push-pull rod is hinged to the reinforcing carrier.

10. The agricultural UAV adaptive balancing management device according to claim 9, characterized in that: The driving ring plate drives the reinforcement carrier to move. There are two reinforcement carriers, which are respectively installed on two bearing plates. The reinforcement carriers are welded and fixed with reinforcement rods. The reinforcement rods are inserted into the limiting channels. A reinforcement matching column is fixed on the end of the reinforcement rod away from the reinforcement carrier. The movable carrier bar is partially inserted in the connecting groove, and a driving matching slideway is symmetrically provided on the movable carrier bar, a driving column is inserted in the driving matching slideway, and the driving column contacts the inner wall of the driving matching slideway. A matching bearing rod is also provided on the movable carrier bar, and the matching bearing rod is inserted in the matching plate cavity, and a matching block is fixed on the end of the matching bearing rod away from the movable carrier bar, and a shift convex plate is provided on the matching block.

11. The agricultural UAV adaptive balancing management device according to claim 10, characterized in that: The control assembly includes: an electric telescopic rod, which is fixedly mounted on the drone; A controller, which is fixedly mounted on the drone and controls the electric telescopic rod; The vibration sensor is also fixedly installed on the drone, and the electric telescopic rod is fixedly connected to the drive ring plate to drive the drive ring plate to move up and down.

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