A vibration-proof mounting structure of an unmanned aerial vehicle intelligent battery

Abstract

The application provides a vibration-proof mounting structure of an unmanned aerial vehicle intelligent battery, which comprises a bottom mounting mechanism, a battery pack, two radial vibration-proof mechanisms, two first axial vibration-proof mechanisms and a second axial vibration-proof mechanism. The bottom mounting mechanism comprises a vibration-proof base, a bottom plate and a plurality of first adjusting assemblies, the vibration-proof base is mounted on an unmanned aerial vehicle, the bottom plate is mounted on the vibration-proof base, and the plurality of first adjusting assemblies are mounted on the bottom plate. The battery pack is arranged between the plurality of first adjusting assemblies. The two radial vibration-proof mechanisms are both mounted on the plurality of first adjusting assemblies. The two first axial vibration-proof mechanisms are both mounted on the plurality of first adjusting assemblies. The second axial vibration-proof mechanism is mounted between the two first axial vibration-proof mechanisms. The vibration-proof mounting structure of the unmanned aerial vehicle intelligent battery provided by the application has wide buffering directions and good buffering effects under the joint action of the two radial vibration-proof mechanisms, the two first axial vibration-proof mechanisms and the second axial vibration-proof mechanism.

Description

Technical Field

[0001] This application relates to the field of drone battery equipment technology, and in particular to a vibration-proof mounting structure for a drone smart battery. Background Technology

[0002] Currently, drones typically consist of seven main modules: flight platform, power system, flight control and navigation system, sensing system, mission payload, ground terminal, and power system. The power system usually uses lithium batteries to power the entire drone. Utilizing the high energy density and strong discharge capacity of lithium batteries, drones can achieve lightweight design, thus improving flight endurance. However, lithium batteries are also chemically reactive, meaning they are prone to catching fire due to external factors such as compression or puncture during use. During drone operation, vibrations act on the lithium batteries. Under the impact of these vibrations, lithium batteries are prone to bulging and even catching fire. Summary of the Invention

[0003] The purpose of this application is to provide a vibration-proof mounting structure for a drone smart battery, so as to solve the technical problems of lithium batteries bulging and catching fire due to vibration in the prior art.

[0004] To achieve the above objectives, the technical solution adopted in this application is: to provide a vibration-damping mounting structure for a drone smart battery, comprising: The bottom mounting mechanism includes a vibration-damping base, a base plate, and multiple first adjustment components. The vibration-damping base is mounted on the drone, the base plate is mounted on the vibration-damping base, and the multiple first adjustment components are mounted on the base plate. A battery pack is disposed among a plurality of the first regulating components; Two radial vibration damping mechanisms are installed on multiple first adjustment components and are capable of radially damping the battery pack. One of the radial vibration damping mechanisms is fixed to one end of the first adjustment component near the base plate, and the other radial vibration damping mechanism is configured to move along a first direction under the drive of the first adjustment component. Two first axial vibration damping mechanisms are installed on multiple first adjustment components and move along the first direction under the drive of the first adjustment components. They can also dampen vibration at one end of the battery pack along the axial direction. The second axial vibration damping mechanism is installed between the two first axial vibration damping mechanisms and is capable of damping the other end of the battery pack along the axial direction.

[0005] Optionally, the radial vibration damping mechanism includes a mounting frame, a second adjusting component, two adjusting rods, and multiple rolling vibration damping components. The mounting frame is mounted on multiple first adjusting components, the second adjusting component is mounted on the mounting frame, and both adjusting rods are mounted on the second adjusting component and move towards each other or away from each other along a second direction under the drive of the second adjusting component. Multiple rolling vibration damping components are mounted on each adjusting rod and can dampen vibration between the adjusting rod and the battery pack.

[0006] Optionally, the rolling vibration damping assembly includes a mounting cylinder, a vibration damping rod, an elastic element, and a flexible roller. The mounting cylinder is mounted on the adjusting rod, the vibration damping rod passes through the mounting cylinder, the elastic element abuts between the mounting cylinder and the vibration damping rod, and the flexible roller is mounted on one end of the vibration damping rod near the battery pack.

[0007] Optionally, the mounting cylinder includes an arm body, a cylinder body, a first limiting boss and a second limiting boss. The arm body is mounted on the adjusting rod, and the cylinder body is connected to the end of the arm body away from the adjusting rod. The first limiting boss is formed at one end of the cylinder body, and the second limiting boss is formed at the end of the cylinder body away from the first limiting boss. The vibration damping rod includes a rod body and a third limiting boss. The rod body passes through the cylinder, and the third limiting boss is formed on the outer periphery of the rod body and located inside the cylinder. The elastic element includes a first elastic structure and a second elastic structure. The first elastic structure is sleeved on the rod body and abuts against the first limiting boss and the third limiting boss. The second elastic structure is sleeved on the rod body and abuts against the second limiting boss and the third limiting boss.

[0008] Optionally, the second adjusting assembly includes a second adjusting screw, a first threaded segment, a second threaded segment, and at least one guide rod. The second adjusting screw passes through the mounting frame and the two adjusting rods and is rotatable relative to the mounting frame about a second direction. The first threaded segment is formed on the second adjusting screw and screwed to one of the adjusting rods. The second threaded segment is formed on the second adjusting screw and screwed to the other adjusting rod. At least one guide rod is mounted on the mounting frame and passes through the two adjusting rods. The first threaded segment and the second threaded segment have opposite thread directions.

[0009] Optionally, the first axial vibration damping mechanism includes a first mounting rod, a third adjusting component, and an axial vibration damping component. The first mounting rod is mounted on a plurality of the first adjusting components, the third adjusting component is mounted on the first mounting rod, and the axial vibration damping component is mounted on the third adjusting component and moves axially under the drive of the third adjusting component.

[0010] Optionally, the third adjustment component includes two mounting seats, a guide rail, a slider, and a third adjustment screw. Both mounting seats are mounted on the first mounting rod, the guide rail is mounted between the two mounting seats, the slider is engaged with the guide rail and can move axially, and the third adjustment screw passes through the two mounting seats and the slider, is screwed to the slider, and can rotate about the axial direction. The axial vibration damping assembly includes multiple movable rods, a movable block, multiple first slide rods, a first limiting plate, multiple first limiting blocks, and multiple first axial elastic structures. The multiple movable rods are all inserted through the slider. The movable block is connected to one end of each of the multiple movable rods near the battery pack. The multiple first slide rods are all inserted through the movable block. The first limiting plate is connected to one end of each of the multiple first slide rods near the battery pack. The multiple first limiting blocks are connected to one end of each of the multiple first slide rods away from the battery pack and are respectively configured to correspond one-to-one with each of the multiple first slide rods. The multiple first axial elastic structures are sleeved on the multiple first slide rods and abut against the movable block and the first limiting plate, and are respectively configured to correspond one-to-one with each of the multiple first slide rods.

[0011] Optionally, the second axial vibration damping mechanism includes a second mounting rod, a plurality of second sliding rods, a second limiting plate, a plurality of second limiting blocks, and a plurality of second axial elastic structures. The second mounting rod is installed between two first axial vibration damping mechanisms. The plurality of second sliding rods are all inserted through the second mounting rod. The second limiting plate is installed at one end of the plurality of second sliding rods near the battery pack. The plurality of second limiting blocks are connected to the ends of the plurality of second sliding rods away from the second limiting plate and are respectively arranged in a one-to-one correspondence with the plurality of second sliding rods. The plurality of second axial elastic structures are sleeved on the plurality of second sliding rods and abut against the second mounting rod and the second limiting plate, and are respectively arranged in a one-to-one correspondence with the plurality of second sliding rods.

[0012] Optionally, the first adjusting assembly includes a first adjusting screw, a lower fixing nut, and two upper fixing nuts. The first adjusting screw is mounted on the base plate and passes through the two mounting frames. The lower fixing nut is sleeved on the first adjusting screw and screwed to it, and is located between the two mounting frames. The two upper fixing nuts are both sleeved on the first adjusting screw and screwed to it, and are respectively located on both sides of the mounting frame away from the base plate along the first direction.

[0013] Optionally, the first adjusting assembly includes a first adjusting screw and two central fixing nuts. The first adjusting screw is mounted on the base plate and passes through the first mounting rod. The two central fixing nuts are sleeved on the first adjusting screw and screwed to the first adjusting screw, and are respectively located on both sides of the first mounting rod along the first direction.

[0014] The beneficial effects of the vibration-damping mounting structure for a drone smart battery provided in this application are as follows: This application provides a vibration-damping mounting structure for a drone's intelligent battery. Through the combined action of two radial vibration-damping mechanisms, two first axial vibration-damping mechanisms, and a second axial vibration-damping mechanism, the battery pack can be completely secured, preventing it from easily loosening. It also provides secondary vibration damping along the radial and axial directions, preventing vibration from being directly transmitted to the battery pack. This secondary vibration damping provides a wide range of damping directions and excellent damping effect, effectively protecting the battery pack and preventing it from bulging or catching fire due to vibration. With the action of multiple first adjustment components, the two radial vibration-damping mechanisms can be used to fix battery packs of different sizes, and the first and second axial vibration-damping mechanisms can always be aligned with battery packs of different sizes, making it widely applicable. Attached Figure Description

[0015] To more clearly illustrate the technical solutions in the embodiments of this application, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0016] Figure 1 A first-view perspective perspective view of a vibration-damping mounting structure for a drone smart battery provided in this application; Figure 2 A second-view perspective perspective view of a vibration-damping mounting structure for a drone smart battery provided in this application; Figure 3 A plan view of a vibration-damping mounting structure for a drone smart battery provided in this application; Figure 4A perspective view of a radial vibration damping mechanism for a vibration damping mounting structure of a drone smart battery provided in this application; Figure 5 for Figure 4 A magnified view of a section at point A in the middle; Figure 6 A perspective view of a rolling vibration damping component of a vibration damping mounting structure for a drone smart battery provided in this application; Figure 7 A perspective view of the first axial vibration damping component and the second axial vibration damping component of a vibration damping mounting structure for a drone smart battery provided in this application; Figure 8 for Figure 7 A magnified view of a section at point B in the middle; Figure 9 for Figure 7 A magnified view of a section at point C; Figure 10 for Figure 7 A magnified view of a section at point D.

[0017] The following are the labeling elements in the figure: 1. Bottom mounting mechanism; 11. Base plate; 12. First adjusting component; 121. First adjusting screw; 122. Lower fixing nut; 123. Upper fixing nut; 124. Middle fixing nut; 2. Battery pack; 3. Radial vibration damping mechanism; 31. Mounting frame; 32. Second adjustment component; 321. Second adjustment screw; 322. First threaded section; 323. Second threaded section; 324. Guide rod; 33. Adjusting rod; 34. Rolling vibration damping component; 341. Mounting cylinder; 3411. Arm body; 3412. Cylinder body; 3413. First limiting boss; 3414. Second limiting boss; 342. Vibration damping rod; 3421. Rod body; 3422. Third limiting boss; 343. Elastic element; 3431. First elastic structure; 3432. Second elastic structure; 344. Flexible roller; 345. Groove; 4. First axial vibration damping mechanism; 41. First mounting rod; 42. Third adjusting assembly; 421. Mounting base; 422. Guide rail; 423. Slider; 424. Third adjusting screw; 43. Axial vibration damping assembly; 431. Moving rod; 432. Moving block; 433. First sliding rod; 434. First limiting plate; 435. First limiting block; 436. First axial elastic structure; 5. Second axial vibration damping mechanism; 51. Second mounting rod; 52. Second sliding rod; 53. Second limiting plate; 54. Second limiting block; 55. Second axial elastic structure. Detailed Implementation

[0018] To make the technical problems, technical solutions, and beneficial effects to be solved by this application clearer, the following detailed description is provided in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative and are not intended to limit the scope of this application.

[0019] It should be noted that when a component is referred to as being "mounted to," "fixed to," or "set on" another component, it can be directly on or indirectly on that other component. When a component is referred to as being "connected to" another component, it can be directly connected to or indirectly connected to that other component.

[0020] It should be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this application and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this application.

[0021] Furthermore, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of this application, "multiple" means two or more, unless otherwise explicitly specified.

[0022] like Figures 1 to 10As shown, this application provides a vibration-damping mounting structure for a drone smart battery, including a bottom mounting mechanism 1, a battery pack 2, two radial vibration-damping mechanisms 3, two first axial vibration-damping mechanisms 4, and a second axial vibration-damping mechanism 5. The bottom mounting mechanism 1 includes a vibration-damping base (not shown), a base plate 11, and multiple first adjustment components 12. The vibration-damping base is mounted on the drone, the base plate 11 is mounted on the vibration-damping base, and the multiple first adjustment components 12 are mounted on the base plate 11. The battery pack 2 is disposed between the multiple first adjustment components 12. Both radial vibration-damping mechanisms 3 are mounted on the multiple first adjustment components 12 and are capable of radially damping the battery pack 2. One radial vibration-damping mechanism 3 is fixed to one end of the first adjustment component 12 near the base plate 11, and the other radial vibration-damping mechanism 3 is configured to move along a first direction under the drive of the first adjustment component 12. Both first axial vibration-damping mechanisms 4 are mounted on the multiple first adjustment components 12 and move along the first direction under the drive of the first adjustment component 12, and are also capable of axially damping one end of the battery pack 2. The second axial vibration damping mechanism 5 is installed between the two first axial vibration damping mechanisms 4 and can dampen the other end of the battery pack 2 along the axial direction.

[0023] It should be noted that the "above" and "below" directions refer to the bidirectional direction of the shortest line connecting the base plate 11 and the radial vibration damping mechanism 3, as detailed below. Figure 1 The X-axis is shown in the diagram. The second direction, above and below, refers to the bidirectional direction of the shortest line connecting the two first axial vibration damping mechanisms 4, specifically as follows: Figure 1 The Y-axis is shown in the diagram. The "above" and "below" axes refer to the bidirectional direction of the shortest connection between the battery pack 2 and the second axial anti-vibration mechanism 5, specifically as follows: Figure 1 The Z-axis is shown in the diagram. The radial directions above and below refer to any direction within the plane containing the first and second directions.

[0024] This application provides a vibration-damping mounting structure for a drone's smart battery. The vibration-damping base provides primary vibration damping. Two radial vibration damping mechanisms 3 limit the battery pack 2 along a first and second direction, preventing it from detaching. Furthermore, the two radial vibration damping mechanisms 3 provide secondary vibration damping along the radial direction. The combined action of two first axial vibration damping mechanisms 4 and a second axial vibration damping mechanism 5 limits the battery pack 2 along the axial direction, preventing it from detaching. Furthermore, the two first axial vibration damping mechanisms 4 and the second axial vibration damping mechanism 5 provide secondary vibration damping along the axial direction. In summary, the combined action of the two radial vibration damping mechanisms 3, the two first axial vibration damping mechanisms 4, and the second axial vibration damping mechanism 5 can completely fix the battery pack 2, making it difficult for it to loosen. Furthermore, it can provide secondary vibration damping along the radial and axial directions, preventing vibration from being directly transmitted to the battery pack 2. This secondary vibration damping provides a wide range of damping directions and a good damping effect, effectively protecting the battery pack 2 and preventing it from bulging or catching fire due to vibration. With the action of multiple first adjustment components 12, the two radial vibration damping mechanisms 3 can be used to fix battery packs 2 of different sizes, and the first axial vibration damping mechanisms 4 and the second axial vibration damping mechanism 5 can always be aligned with battery packs 2 of different sizes, making it widely applicable.

[0025] In one embodiment of this application, please refer to Figures 1 to 10 The radial vibration damping mechanism 3 includes a mounting frame 31, a second adjustment component 32, two adjustment rods 33, and multiple rolling vibration damping components 34. The mounting frame 31 is mounted on multiple first adjustment components 32, the second adjustment component 32 is mounted on the mounting frame 31, and the two adjustment rods 33 are both mounted on the second adjustment component 32 and move towards each other or away from each other along the second direction under the drive of the second adjustment component 32. Multiple rolling vibration damping components 34 are mounted on each adjustment rod 33 and can dampen vibration between the adjustment rod 33 and the battery pack 2.

[0026] With this configuration, under the action of the second adjusting component 32, the two adjusting rods 33 can move simultaneously towards each other or simultaneously away from each other along the second direction to adjust the distance between the rolling anti-vibration components 34 in the second direction. This allows for limiting the movement of battery packs 2 of different sizes, making it widely applicable. When disassembling and installing the battery pack 2, the multiple rolling anti-vibration components 34, compared to the buffer strips used in existing technologies, convert sliding into rolling, greatly reducing the difficulty of disassembly and installation and improving ease of use. Furthermore, the multiple rolling anti-vibration components 34 can provide radial vibration protection, effectively protecting the battery pack 2.

[0027] In one embodiment of this application, please refer to the following: Figures 1 to 10The rolling vibration damping assembly 34 includes a mounting cylinder 341, a vibration damping rod 342, an elastic element 343, and a flexible roller 344. The mounting cylinder 341 is mounted on the adjusting rod 33, the vibration damping rod 342 passes through the mounting cylinder 341, the elastic element 343 abuts between the mounting cylinder 341 and the vibration damping rod 342, and the flexible roller 344 is mounted on the end of the vibration damping rod 342 near the battery pack 2.

[0028] This configuration, under the action of the elastic element 343, creates a buffer between the mounting cylinder 341 and the anti-vibration rod 342, thereby preventing vibration from being directly transmitted to the battery pack 2. Furthermore, under the action of the elastic element 343, the flexible roller 344 has elastic adjustment space through the anti-vibration rod 342, preventing the flexible roller 344 from squeezing the battery pack 2, thus protecting the battery pack 2 and further improving safety performance. The mounting cylinder 341 can be used to mount the anti-vibration rod 342, the elastic element 343, and the flexible roller 344.

[0029] Optionally, the flexible roller 344 has an annular groove.

[0030] This design, under the action of the annular groove, can limit the side of the battery pack 2, which helps to improve the structural stability between the battery pack 2 and the flexible roller 344. During vibration damping, the side of the battery pack 2 can move slightly within the annular groove, and the four rolling vibration damping components 34 located in the plane formed by the first and second directions can dampen the battery pack 2 in any radial direction, resulting in good vibration damping effect.

[0031] In one embodiment of this application, see [reference] Figures 1 to 10 The mounting cylinder 341 includes an arm 3411, a cylinder 3412, a first limiting boss 3413, and a second limiting boss 3414. The arm 3411 is mounted on the adjusting rod 33. The cylinder 3412 is connected to the end of the arm 3411 away from the adjusting rod 33. The first limiting boss 3413 is formed at one end of the cylinder 3412, and the second limiting boss 3414 is formed at the end of the cylinder 3412 away from the first limiting boss 3413. The vibration damping rod 342 includes a rod 3421 and a third limiting boss 3422. The rod 3421 passes through the cylinder 3412, and the third limiting boss 3422 is formed on the outer periphery of the rod 3421 and located inside the cylinder 3412. The elastic element 343 includes a first elastic structure 3431 and a second elastic structure 3432. The first elastic structure 3431 is sleeved on the rod body 3421 and abuts between the first limiting boss 3413 and the third limiting boss 3422. The second elastic structure 3432 is sleeved on the rod body 3421 and abuts between the second limiting boss 3414 and the third limiting boss 3422.

[0032] This configuration, with the first limiting boss 3413 and the second limiting boss 3414 acting as a limit, and through the third limiting boss 3422, can create a limit, preventing the first elastic structure 3431, the second elastic structure 3432, and the rod 3421 from detaching from the cylinder 3412, thus improving structural stability. The first elastic structure 3431 acts as a buffer between the first limiting boss 3413 and the third limiting boss 3422. Similarly, the second elastic structure 3432 acts as a buffer between the second limiting boss 3414 and the third limiting boss 3422. In summary, the first elastic structure 3431 and the second elastic structure 3432 can create buffers on both sides of the third limiting boss 3422, resulting in a better buffering effect compared to a single-sided buffer.

[0033] Optionally, both the first elastic structure 3431 and the second elastic structure 3432 are configured as springs or sheet springs.

[0034] In one embodiment of this application, please refer to Figures 1 to 10 The second adjusting assembly 32 includes a second adjusting screw 321, a first threaded section 322, a second threaded section 323, and at least one guide rod 324. The second adjusting screw 321 passes through the mounting frame 31 and the two adjusting rods 33, and is rotatable relative to the mounting frame 31 in a second direction. The first threaded section 322 is formed on the second adjusting screw 321 and screwed to one of the adjusting rods 33. The second threaded section 323 is formed on the second adjusting screw 321 and screwed to the other adjusting rod 33. At least one guide rod 324 is mounted on the mounting frame 31 and passes through the two adjusting rods 33. The threads of the first threaded section 322 and the second threaded section 323 have opposite directions of rotation.

[0035] With this configuration, the rotation of the second adjusting screw 321, through the first threaded section 322 and the second threaded section 323, can simultaneously drive the two adjusting rods 33 to move towards each other or away from each other along the second direction, so as to adjust the distance between the two flexible rollers 344 arranged along the second direction, which is convenient for adjustment.

[0036] In one embodiment of this application, please refer to the following: Figures 1 to 10 The first axial vibration damping mechanism 4 includes a first mounting rod 41, a third adjusting component 42, and an axial vibration damping component 43. The first mounting rod 41 is mounted on a plurality of first adjusting components 12, the third adjusting component 42 is mounted on the first mounting rod 41, and the axial vibration damping component 43 is mounted on the third adjusting component 42 and moves axially under the drive of the third adjusting component 42.

[0037] With this configuration, the position of the axial vibration damping component 43 in the axial direction can be adjusted under the action of the third adjustment component 42, so that the axial vibration damping component 43 can always be in contact with the battery pack 2, which can limit and buffer battery packs 2 of different sizes, has a wide range of applications and good buffering effect.

[0038] In one embodiment of this application, see [reference] Figures 1 to 10 The third adjustment component 42 includes two mounting seats 421, a guide rail 422, a slider 423, and a third adjustment screw 424. Both mounting seats 421 are mounted on the first mounting rod 41. The guide rail 422 is mounted between the two mounting seats 421. The slider 423 is engaged with the guide rail 422 and can move axially. The third adjustment screw 424 passes through the two mounting seats 421 and the slider 423, and is screwed to the slider 423 and can rotate around the axis. The axial vibration damping assembly 43 includes multiple movable rods 431, movable blocks 432, multiple first slide rods 433, a first limiting plate 434, multiple first limiting blocks 435, and multiple first axial elastic structures 436. The multiple movable rods 431 are all inserted through the slider 423. The movable blocks 432 are connected to the ends of the multiple movable rods 431 near the battery pack 2. The multiple first slide rods 433 are all inserted through the movable blocks 432. The first limiting plate 434 is connected to the ends of the multiple first slide rods 433 near the battery pack 2. The multiple first limiting blocks 435 are connected to the ends of the multiple first slide rods 433 away from the battery pack 2 and are respectively arranged in a one-to-one correspondence with the multiple first slide rods 433. The multiple first axial elastic structures 436 are sleeved on the multiple first slide rods 433 and abut against the movable blocks 432 and the first limiting plates 434, and are respectively arranged in a one-to-one correspondence with the multiple first slide rods 433.

[0039] This configuration, with the two mounting bases 421 acting as limiters, restricts the third adjusting screw 424, allowing it to rotate only axially. The rotation of the third adjusting screw 424 drives the slider 423 to move axially, thus adjusting the axial position of the axial vibration damping component 43. The guide rail 422 guides the movement of the slider 423, ensuring it moves only axially and improving its axial stability. Multiple moving rods 431 drive the moving block 432 to move in the second direction, adjusting its position. During battery pack 2 installation and removal, the moving block 432 avoids interfering with its movement. The first axial elastic structure 436 creates a buffer between the first limiting plate 434 and the moving block 432, preventing vibration from being directly transmitted to the end of the battery pack 2 furthest from the second axial vibration damping mechanism 5, effectively protecting the battery pack 2. Under the action of the first sliding rod 433 and the first limiting plate 434, the first axial elastic structure 436 can be limited, preventing it from detaching and ensuring stable vibration damping along the axial direction. Under the action of the first limiting block 435, the first sliding rod 433 can be prevented from detaching from the moving block 432, thus improving the structural stability between the first sliding rod 433 and the moving block 432. During buffering, the supporting action of the first axial elastic structure 436 limits the moving block 432, preventing it from moving in the second direction and causing the first axial elastic structure 436 to misalign with the battery pack 2, thus achieving stable buffering.

[0040] Optionally, the first axial elastic structure 436 is configured as a spring or a sheet.

[0041] Optionally, a first buffer pad (not shown in the figure) is installed on the side of the first limiting plate 434 facing the battery pack 2.

[0042] With this configuration, the first buffer pad can prevent the first limiting plate 434 from directly contacting the battery pack 2, and can form a buffer between the first limiting plate 434 and the battery pack 2, effectively protecting the battery pack 2.

[0043] In one embodiment of this application, please refer to Figures 1 to 10The second axial vibration damping mechanism 5 includes a second mounting rod 51, a plurality of second sliding rods 52, a second limiting plate 53, a plurality of second limiting blocks 54, and a plurality of second axial elastic structures 55. The second mounting rod 51 is installed between the two first axial vibration damping mechanisms 4. The plurality of second sliding rods 52 are all inserted through the second mounting rod 51. The second limiting plate 53 is installed at one end of the plurality of second sliding rods 52 near the battery pack 2. The plurality of second limiting blocks 54 are connected to the ends of the plurality of second sliding rods 52 away from the second limiting plate 53 and are respectively arranged in a one-to-one correspondence with the plurality of second sliding rods 52. The plurality of second axial elastic structures 55 are sleeved on the plurality of second sliding rods 52 and abut against the second mounting rod 51 and the second limiting plate 53, and are respectively arranged in a one-to-one correspondence with the plurality of second sliding rods 52.

[0044] This configuration, under the action of the second axial elastic structure 55, forms a buffer between the second limiting plate 53 and the second mounting rod 51, preventing vibration from being transmitted axially to the end of the battery pack 2 away from the moving block 432. Under the action of the second sliding rod 52, the second axial elastic structure 55 is limited, preventing it from detaching from the second limiting plate 53 and the second mounting rod 51, thus ensuring stable vibration damping of the battery pack 2. Under the action of the second limiting block 54, the second sliding rod 52 is prevented from detaching from the second mounting rod 51, contributing to improved structural stability between the second sliding rod 52 and the second mounting rod 51.

[0045] Optionally, the second axial elastic structure 55 is configured as a spring or a sheet.

[0046] Optionally, a second buffer pad (not shown in the figure) is installed on the side of the second limiting plate 53 facing the battery pack 2.

[0047] With this configuration, the second buffer pad can prevent the second limiting plate 53 from directly contacting the battery pack 2, and can form a buffer between the second limiting plate 53 and the battery pack 2, effectively protecting the battery pack 2.

[0048] In one embodiment of this application, please refer to the following: Figures 1 to 10 The first adjustment assembly 12 includes a first adjustment screw 121, a lower fixing nut 122, and two upper fixing nuts 123. The first adjustment screw 121 is mounted on the base plate 11 and passes through two mounting frames 31. The lower fixing nut 122 is sleeved on the first adjustment screw 121 and screwed to the first adjustment screw 121, and is located between the two mounting frames 31. The two upper fixing nuts 123 are both sleeved on the first adjustment screw 121 and screwed to the first adjustment screw 121, and are respectively located on both sides of the mounting frame 31 away from the base plate 11 along the first direction.

[0049] With this configuration, the lower fixing nut 122 can secure the mounting frame 31 near the floor end of the first adjusting screw 121, resulting in good fixation. The two upper fixing nuts 123 can also secure the mounting frame 31 furthest from the base plate 11 to the first adjusting screw 121, and adjust the position of the mounting frame 31 furthest from the base plate 11 on the first adjusting screw 121, thereby adjusting the distance between the two mounting frames 31.

[0050] In one embodiment of this application, see [reference] Figures 1 to 10 The first adjustment assembly 12 includes a first adjustment screw 121 and two central fixing nuts 124. The first adjustment screw 121 is mounted on the base plate 11 and passes through the first mounting rod 41. The two central fixing nuts 124 are sleeved on the first adjustment screw 121 and screwed to the first adjustment screw 121, and are respectively located on both sides of the first mounting rod 41 along the first direction.

[0051] With this configuration, the first mounting rod 41 can be fixed to the first adjusting screw 121 by the two central fixing nuts 124, and the position of the first mounting rod 41 on the first adjusting screw 121 can also be adjusted so that the first axial elastic structure 436 and the second axial elastic structure 55 are always facing the battery pack 2.

[0052] The working principle of the anti-vibration mounting structure for a drone smart battery provided in this application is as follows: Before use, adjust the spacing between the two mounting frames 31 in the first direction according to the dimensions of the battery pack 2 in the first direction, the second direction, and the axial direction, and then adjust the position of the flexible roller 344 in the second direction.

[0053] When installing the battery pack 2, pull the first slide bar 433 to move the two moving blocks 432 in opposite directions along the second direction. Place the battery pack 2 between the two mounting frames 31 and push it in, so that the battery pack 2 contacts the flexible roller 344. Under the rolling action of the flexible roller 344, the battery pack 2 moves axially toward the second limiting plate 53 until the battery pack 2 and the second limiting plate 53 contact each other. Push the first slide bar 433 to move the two moving blocks 432 toward each other along the second direction. Rotate the two third adjusting screws 424, and the two sliders 423 drive the two moving blocks 432 to move axially toward the battery pack 2 through the first slide bar 433 until the first limiting plate 434 contacts the battery pack 2.

[0054] When disassembling battery pack 2, rotate the two third adjusting screws 424. The two sliders 423 drive the two moving blocks 432 to move axially away from battery pack 2 via the first sliding rod 433 until the first limiting plate 434 separates from battery pack 2. Pull the first sliding rod 433 to make the two moving blocks 432 move in opposite directions in the second direction, and finally remove battery pack 2 from between the two mounting frames 31.

[0055] One or more embodiments in this application are intended to cover all such substitutions, modifications, and variations that fall within the broad scope of this application. Therefore, any omissions, modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of one or more embodiments in this application should be included within the protection scope of this application.

Claims

1. A vibration-damping mounting structure for a drone smart battery, characterized in that, include: The bottom mounting mechanism includes a vibration-damping base, a base plate, and multiple first adjustment components. The vibration-damping base is mounted on the drone, the base plate is mounted on the vibration-damping base, and the multiple first adjustment components are mounted on the base plate. A battery pack is disposed among a plurality of the first regulating components; Two radial vibration damping mechanisms are installed on multiple first adjustment components and are capable of radially damping the battery pack. One of the radial vibration damping mechanisms is fixed to one end of the first adjustment component near the base plate, and the other radial vibration damping mechanism is configured to move along a first direction under the drive of the first adjustment component. Two first axial vibration damping mechanisms are installed on multiple first adjustment components and move along the first direction under the drive of the first adjustment components. They can also dampen vibration at one end of the battery pack along the axial direction. The second axial vibration damping mechanism is installed between the two first axial vibration damping mechanisms and is capable of damping the other end of the battery pack along the axial direction.

2. The vibration-damping mounting structure for a drone smart battery as described in claim 1, characterized in that, The radial vibration damping mechanism includes a mounting frame, a second adjustment component, two adjustment rods, and multiple rolling vibration damping components. The mounting frame is mounted on multiple first adjustment components, and the second adjustment component is mounted on the mounting frame. Both adjustment rods are mounted on the second adjustment component and move towards each other or away from each other along a second direction under the drive of the second adjustment component. Multiple rolling vibration damping components are mounted on each adjustment rod and can dampen vibration between the adjustment rod and the battery pack.

3. The vibration-damping mounting structure for a drone smart battery as described in claim 2, characterized in that, The rolling vibration damping assembly includes a mounting cylinder, a vibration damping rod, an elastic element, and a flexible roller. The mounting cylinder is mounted on the adjusting rod, the vibration damping rod passes through the mounting cylinder, the elastic element abuts between the mounting cylinder and the vibration damping rod, and the flexible roller is mounted on the end of the vibration damping rod near the battery pack.

4. The vibration-damping mounting structure for a drone smart battery as described in claim 3, characterized in that, The mounting cylinder includes an arm body, a cylinder body, a first limiting boss, and a second limiting boss. The arm body is mounted on the adjusting rod, and the cylinder body is connected to the end of the arm body away from the adjusting rod. The first limiting boss is formed at one end of the cylinder body, and the second limiting boss is formed at the end of the cylinder body away from the first limiting boss. The vibration damping rod includes a rod body and a third limiting boss. The rod body passes through the cylinder, and the third limiting boss is formed on the outer periphery of the rod body and located inside the cylinder. The elastic element includes a first elastic structure and a second elastic structure. The first elastic structure is sleeved on the rod body and abuts against the first limiting boss and the third limiting boss. The second elastic structure is sleeved on the rod body and abuts against the second limiting boss and the third limiting boss.

5. The vibration-damping mounting structure for a drone smart battery as described in claim 2, characterized in that, The second adjustment assembly includes a second adjustment screw, a first threaded section, a second threaded section, and at least one guide rod. The second adjustment screw passes through the mounting frame and the two adjustment rods and is rotatable relative to the mounting frame about a second direction. The first threaded section is formed on the second adjustment screw and screwed to one of the adjustment rods. The second threaded section is formed on the second adjustment screw and screwed to the other adjustment rod. At least one guide rod is mounted on the mounting frame and passes through the two adjustment rods. The first threaded segment and the second threaded segment have opposite thread directions.

6. The vibration-damping mounting structure for a drone smart battery as described in claim 1, characterized in that, The first axial vibration damping mechanism includes a first mounting rod, a third adjusting component, and an axial vibration damping component. The first mounting rod is mounted on a plurality of the first adjusting components, the third adjusting component is mounted on the first mounting rod, and the axial vibration damping component is mounted on the third adjusting component and moves axially under the drive of the third adjusting component.

7. The vibration-damping mounting structure for a drone smart battery as described in claim 6, characterized in that, The third adjustment component includes two mounting seats, a guide rail, a slider, and a third adjustment screw. Both mounting seats are mounted on the first mounting rod. The guide rail is mounted between the two mounting seats. The slider is engaged with the guide rail and can move axially. The third adjustment screw passes through the two mounting seats and the slider, is screwed to the slider, and can rotate about the axial direction. The axial vibration damping assembly includes multiple movable rods, a movable block, multiple first slide rods, a first limiting plate, multiple first limiting blocks, and multiple first axial elastic structures. The multiple movable rods are all inserted through the slider. The movable block is connected to one end of each of the multiple movable rods near the battery pack. The multiple first slide rods are all inserted through the movable block. The first limiting plate is connected to one end of each of the multiple first slide rods near the battery pack. The multiple first limiting blocks are connected to one end of each of the multiple first slide rods away from the battery pack and are respectively configured to correspond one-to-one with each of the multiple first slide rods. The multiple first axial elastic structures are sleeved on the multiple first slide rods and abut against the movable block and the first limiting plate, and are respectively configured to correspond one-to-one with each of the multiple first slide rods.

8. The vibration-damping mounting structure for a drone smart battery as described in claim 1, characterized in that, The second axial vibration damping mechanism includes a second mounting rod, a plurality of second sliding rods, a second limiting plate, a plurality of second limiting blocks, and a plurality of second axial elastic structures. The second mounting rod is installed between two first axial vibration damping mechanisms. The plurality of second sliding rods are all inserted through the second mounting rod. The second limiting plate is installed at one end of the plurality of second sliding rods near the battery pack. The plurality of second limiting blocks are connected to the ends of the plurality of second sliding rods away from the second limiting plate and are respectively arranged in a one-to-one correspondence with the plurality of second sliding rods. The plurality of second axial elastic structures are sleeved on the plurality of second sliding rods and abut against the second mounting rod and the second limiting plate, and are respectively arranged in a one-to-one correspondence with the plurality of second sliding rods.

9. The vibration-damping mounting structure for a drone smart battery as described in claim 2, characterized in that, The first adjustment assembly includes a first adjustment screw, a lower fixing nut, and two upper fixing nuts. The first adjustment screw is mounted on the base plate and passes through the two mounting frames. The lower fixing nut is sleeved on the first adjustment screw and screwed to it, and is located between the two mounting frames. The two upper fixing nuts are both sleeved on the first adjustment screw and screwed to it, and are respectively located on both sides of the mounting frame away from the base plate along the first direction.

10. The vibration-damping mounting structure for a drone smart battery as described in claim 6, characterized in that, The first adjustment assembly includes a first adjustment screw and two central fixing nuts. The first adjustment screw is mounted on the base plate and passes through the first mounting rod. The two central fixing nuts are sleeved on the first adjustment screw and screwed to the first adjustment screw, and are respectively located on both sides of the first mounting rod along the first direction.

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