Drone truss warehouse and drone with it

Abstract

The present invention discloses a UAV truss compartment and a UAV having the same, and relates to the technical field of UAVs. The UAV truss compartment includes: a bracket, a mounting portion, a buffer portion, a clamping portion, and a limiting portion. The UAV includes: a frame, a power system, a flight control system, a communication and data transmission system, an auxiliary system, and a landing gear. The present invention facilitates the rapid installation / disassembly of the bracket by providing an upper top cap and an upper annular cylinder. By rotating the upper top cap, the upper annular block is driven to disengage from the sleeve, so that the upper limit column and the upper slider are disengaged from the sleeve, thereby achieving rapid docking of the bracket and improving the efficiency of the working process. By providing a first elastic member and a second elastic member, when the lower limit column and the lower slider move to the first position, a first-level shock absorption is achieved. When the lower limit column and the lower slider move to the second position, a second-level shock absorption is achieved. Through double shock absorption, the UAV can achieve a better shock absorption effect when landing.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles, and particularly to an unmanned aerial vehicle truss bin and an unmanned aerial vehicle having the same. Background Art

[0002] In recent years, the technology of unmanned aerial vehicles has developed rapidly and is widely used in fields such as logistics transportation, agricultural plant protection, emergency rescue, and terrain survey. With the complication of application scenarios, unmanned aerial vehicles face higher requirements in terms of takeoff and landing stability, environmental adaptability, and maintenance efficiency. Especially when operating in the wild or complex terrains, unmanned aerial vehicles need to take off and land frequently, and the stability, shock absorption performance, and quick disassembly and assembly ability of their support structures directly affect the operation efficiency and equipment safety.

[0003] The patent with the publication number of CN119773969A discloses an unmanned aerial vehicle carrying structure and an unmanned aerial vehicle, including a box body and a connecting part for hanging at the bottom of the unmanned aerial vehicle body. The box body is used for storing materials, and the connecting part is used for connecting with the bottom of the unmanned aerial vehicle body; through the setting of the connecting part, when materials are placed, by means of the weight of the materials themselves, the wedge can be tightly pressed and fitted against the inclined surface of the fixing part, realizing a firm and reliable connection between the box body and the connecting part, strongly ensuring that during the entire flight process of the unmanned aerial vehicle, the box body will not easily become disengaged from the connecting part, improving the safety and reliability of the entire unmanned aerial vehicle carrying structure, and when the unmanned aerial vehicle is flying, even if affected by external forces such as shaking, the wedge and the fixing part will be further pressed due to relative movement, so that the connection strength between the two increases continuously during the flight process, and it can better cope with complex flight conditions and always maintain a stable connection state.

[0004] However, it is found in actual use that the above technical solution still has problems: using bolts for fixation has the problems of cumbersome disassembly and assembly steps and long time consumption, and it is difficult to meet the requirements of rapid deployment or emergency repair; at the same time, the landing gear is fixed under the unmanned aerial vehicle by bolts, and during the descent of the unmanned aerial vehicle, the landing gear impacts the ground, which is likely to damage the connection between the landing gear and the airframe.

[0005] Therefore, it is very necessary to invent an unmanned aerial vehicle truss bin and an unmanned aerial vehicle having the same to solve the above problems. Summary of the Invention

[0006] The purpose of the present invention is to provide an unmanned aerial vehicle truss bin and an unmanned aerial vehicle having the same to solve the problems raised in the above background art.

[0007] To achieve the above object, the present invention provides the following technical solutions: a drone truss warehouse, comprising: a bracket for carrying a box body; at least two mounting parts for fixing the bracket; a buffer part corresponding to the mounting part, when the bracket contacts the ground through the buffer part, the buffer part performs primary shock absorption and secondary shock absorption on the bracket to enhance the stability of the bracket when landing; a clamping part corresponding to the mounting part for clamping the box body on the outer side wall of the mounting part; a limiting part corresponding to the clamping part, which includes a first convex block and a second convex block, the first convex block is used to block the buffer part after secondary shock absorption to prevent the bracket from jumping up, and the second convex block is used to limit the limiting part, thereby achieving the limitation of the box body.

[0008] Preferably, the mounting part includes: a lower limit column rotatably arranged on the top of the bracket; a lower sliding block fixedly arranged on one side of the top of the lower limit column; a sleeve arranged on the outer wall of the lower limit column; a lower sliding groove opened inside the sleeve; a lower top cap threadedly arranged at the bottom of the sleeve; a lower annular block fixedly arranged inside the lower top cap; by rotating the lower top cap, the lower annular block is driven to move upward, so that the lower annular block pushes the lower sliding block and drives the lower limit column to move axially along the lower sliding groove, thereby driving the bracket to adjust its position.

[0009] Preferably, the mounting part further includes: an upper sliding groove opened inside the top of the sleeve; an upper limit column arranged inside the sleeve; an upper sliding block arranged on one side of the bottom of the upper limit column; an upper top cap threadedly arranged on the top of the sleeve; an upper annular block arranged inside the upper top cap; by rotating the upper top cap, the upper annular block is driven to move downward, so that the upper annular block pushes the upper sliding block and drives the upper limit column to move axially along the upper sliding groove until the upper limit column is fixed.

[0010] Preferably, the buffer part includes a first elastic member and a second elastic member arranged in the sleeve, the diameter of the first elastic member is larger than that of the second elastic member, and the elastic force of the first elastic member is larger than that of the second elastic member, which is used to improve the stability when the bracket contacts the ground; a jacking block arranged at the bottom of the first elastic member and corresponding to the first convex block.

[0011] Preferably, the clamping part includes: an arc-shaped groove arranged on the side wall of the sleeve; a support plate arranged on the side wall of the arc-shaped groove and flush with the arc-shaped groove; a limiting plate, one end of which is rotatably arranged on the top of the support plate and the other end extends into the arc-shaped groove; a receiving groove opened around the side of the limiting plate.

[0012] Preferably, the clamping part also includes: an elastic member 1, which is arranged at one end of the accommodating groove away from the axis of the sleeve; an adjusting plate 1, which is fixedly arranged at one end of the elastic member 1 and contacts with the inside of the accommodating groove; an elastic member 2, one end of which is fixedly arranged in the accommodating groove; an elastic member 3, one end of which is connected to the other end of the elastic member 2; an adjusting plate 2, one end of which is fixedly connected to the elastic member 3; the first protrusion is arranged at one end of the adjusting plate 2, and the second protrusion is arranged at one end of the adjusting plate 1; a clamping part is provided at the corresponding ends of the adjusting plate 1 and the adjusting plate 2; by controlling the adjusting plate 1 to drive the second protrusion to move into the interior of the accommodating groove, the elastic member 1 is deformed at this time, and the limit on the limiting part can be released, and by controlling the adjusting plate 2 to drive the first protrusion to move into the accommodating groove, the elastic member 2 and the elastic member 3 are deformed at this time, and the blocking of the buffer part can be released.

[0013] Preferably, the limiting portion includes a clamping plate fixedly provided on the box body, and a limiting groove opened on one side of the clamping plate. One end of the clamping plate is clamped on the outer wall of the sleeve, and the second protrusion is clamped into the limiting groove to limit the clamping plate, thereby achieving the limitation of the box body.

[0014] The present invention also discloses a UAV, comprising: a frame; a power system for providing power for the UAV; a flight control system for controlling the flight of the UAV; a communication and data transmission system for realizing real-time data interaction between the UAV and a ground station to ensure remote monitoring and scheduling; an auxiliary system for improving the environmental adaptability and safety of the UAV; a landing gear, which is fixedly arranged at the lower end of the frame, and the other end of the landing gear is rotatably arranged with the top of the upper limit column; the power system, flight control system, communication and data transmission system and auxiliary system are installed on the frame.

[0015] The technical effects and advantages of the present invention are as follows:

[0016] 1. The present invention facilitates the rapid installation / disassembly of the bracket by providing an upper cap and an upper annular cylinder. By rotating the upper cap, the upper annular block is driven to separate from the sleeve, so that the upper limit column and the upper slider are separated from the sleeve, thereby realizing the rapid docking of the bracket and improving the efficiency of the working process.

[0017] 2. The present invention provides a first elastic member and a second elastic member, so that when the lower limit column and the lower slider move to the first position, a first level of shock absorption is achieved, and when the lower limit column and the lower slider move to the second position, a second level of shock absorption is achieved. The double shock absorption can thereby improve the shock absorption effect of the drone during landing.

[0018] 3. The present invention provides a second elastic member. When the UAV lands on an uneven road surface, the elastic force of the second elastic member itself enables the bracket to better contact the ground, thereby increasing the overall stability of the UAV.

[0019] 4. Through the cooperation of components such as the second elastic member, the third elastic member, the second convex block, and the second adjusting plate, the present invention prevents the overall jump of the drone, thereby improving the stability of the drone during landing. By blocking the reset of the first elastic member with the second convex block, it is possible to prevent the damage of the drone caused by the excessive self-elastic force of the first elastic member. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 It is a schematic diagram of the overall structure of the present invention.

[0021] Figure 2 It is an exploded structural schematic diagram of the installation part of the present invention.

[0022] Figure 3 It is a schematic diagram of the sectional structure of the sleeve of the present invention.

[0023] Figure 4 It is a schematic diagram of the sectional structure of the clamping part of the present invention.

[0024] Figure 5 It is a schematic diagram of the structure for releasing the limit of the first adjusting plate and the second adjusting plate of the present invention.

[0025] Figure 6 It is a schematic diagram of the sectional structure of the second convex block and the limiting groove of the present invention.

[0026] Figure 7 It is a schematic diagram of the connection between the clamping plate and the box body of the present invention.

[0027] In the figure: 1, bracket; 2, installation part; 3, buffer part; 4, clamping part; 5, limiting part; 6, frame; 7, landing gear; 201, lower limiting column; 202, lower sliding block; 203, sleeve; 204, lower sliding groove; 205, lower top cap; 206, lower annular block; 207, upper sliding groove; 208, upper limiting column; 209, upper sliding block; 210, upper top cap; 211, upper annular block; 301, first elastic member; 302, second elastic member; 303, jacking block; 401, arc groove; 402, support plate; 403, limiting plate; 404, receiving groove; 405, first elastic member; 406, first adjusting plate; 407, second elastic member; 408, third elastic member; 409, second adjusting plate; 501, first convex block; 502, second convex block; 503, clamping plate; 504, limiting groove. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0028] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without creative efforts shall fall within the protection scope of the present invention.

[0029] Example 1, the present invention provides Figures 1 to 7 The drone truss cabin shown includes: a bracket 1, two brackets 1 are provided for supporting the box, and there is a certain distance between the bottom of the box and the upper part of the bracket 1 to prevent the bracket 1 from moving up and down when landing and causing damage to the bottom of the box.

[0030] The mounting portion 2 has at least two groups for fixing the bracket 1; a lower limit column 201, which is rotatably set at the top of the bracket 1; a lower slider 202, which is fixedly set on one side of the top of the lower limit column 201; a sleeve 203, the interior of the sleeve 203 is a circular cavity, which is set on the outer wall of the lower limit column 201; a lower sliding groove 204, which is opened inside the sleeve 203; a lower top cap 205, which is threaded and set at the bottom of the sleeve 203; and a lower annular block 206, which is fixedly set inside the lower top cap 205. By rotating the lower top cap 205, the lower annular block 206 is driven to move upward, so that the lower annular block 206 pushes the lower slider 202, and drives the lower limit column 201 to move axially along the lower slide groove 204, thereby driving the bracket 1 to adjust its position, so that it can better contact with the first elastic member 301, so that the first elastic member 301 can push the lower limit column 201 under the action of its own elastic force, so that the lower limit column 201 pushes the bracket 1 to contact the uneven ground, so that the drone as a whole maintains a balanced state; the upper slide groove 207 is opened at The inner side of the top of the sleeve 203; the upper limit post 208, which is arranged inside the sleeve 203; the upper slider 209, which is arranged on one side of the bottom of the upper limit post 208; the upper top cap 210, which is threadedly arranged on the top of the sleeve 203; the upper annular block 211, which is arranged inside the upper top cap 210; by rotating the upper top cap 210, the upper annular block 211 is driven to move downward, so that the upper annular block 211 pushes the upper slider 209, and drives the upper limit post 208 to move axially along the upper slide groove 207 until the upper limit post 208 is fixed.

[0031] The buffer portion 3 corresponds to the mounting portion 2. When the bracket 1 contacts the ground, the buffer portion 3 performs primary and secondary shock absorption on the bracket 1, so as to enhance the landing stability of the bracket 1; the buffer portion 3 includes a first elastic member 301 and a second elastic member 302 arranged in the sleeve 203. The first elastic member 301 has a larger diameter than the second elastic member 302, and the elastic force of the first elastic member 301 is greater than the elastic force of the second elastic member 302, so as to enhance the stability of the bracket 1 when in contact with the ground. The second elastic member 302 is longer than the first elastic member 301; the lifting block 303 is arranged at the bottom of the first elastic member 301 and corresponds to the first protrusion 501.

[0032] By removing the top cap 205 and separating it from the bottom of the sleeve 203, it is convenient to replace the buffer part 3 components in the sleeve 203.

[0033] The clamping part 4 corresponds to the installation part 2 and is used to clamp the box body on the outer side wall of the installation part 2; the arc-shaped groove 401 is arranged on the side wall of the sleeve 203; the support plate 402 is arranged on the side wall of the arc-shaped groove 401 and is flush with the arc-shaped groove 401; one end of the limiting plate 403 is rotatably arranged on the top of the support plate 402, and the other end extends into the arc-shaped groove 401. An arc-shaped surface is arranged at the end of the limiting plate 403 extending into the arc-shaped groove 401, and this arc-shaped surface coincides with the arc of the circular cavity part in the sleeve 203, as Figure 4 shown; the receiving groove 404 is opened around the side of the limiting plate 403; the first elastic member 405 is arranged at one end of the receiving groove 404 away from the axis of the sleeve 203; the first adjusting plate 406 is fixedly arranged at one end of the first elastic member 405 and contacts the inside of the receiving groove 404. The first convex block 501 is arranged at one end of the first adjusting plate 406. By controlling the first adjusting plate 406 to drive the second convex block 502 to move towards the inside of the receiving groove 404, at this time, the first elastic member 405 deforms, and the limit on the clamping part 4 can be released. By controlling the second adjusting plate 409 to drive the first convex block 501 to move into the receiving groove 404, at this time, the second elastic member 407 and the third elastic member 408 deform, and the blocking of the buffer part 3 can be released.

[0034] It should be noted that the height of the receiving groove 404 is higher than that of the first elastic member 405, the first adjusting plate 406, the second elastic member 407, the third elastic member 408, and the second adjusting plate 409 to facilitate movement inside the receiving groove 404.

[0035] The limiting part 5 corresponds to the clamping part 4 and includes a second convex block 502. The second convex block 502 is used to limit the clamping part 4, thereby achieving the limit on the box body; the limiting part 5 includes a clamping plate 503 fixedly arranged on the box body. The clamping plate 503 is of a C-shaped structure, and a limiting groove 504 is opened on one side of the clamping plate 503. One end of the clamping plate 503 is clamped on the outer wall of the sleeve 203, and the second convex block 502 is clamped into the limiting groove 504 to limit the clamping plate 503, thereby achieving the limit on the box body.

[0036] During use, by clamping the clamping plates 503 on both sides of the box body to the bottom of the sleeve 203, then lifting the box body upward, the box body drives the clamping plates 503 to slide on the outer wall of the sleeve 203 to a specified position, so that the second convex block 502 limits the clamping plate 503, and further limits the overall box body, improving the stability of the box body.

[0037] While the second convex block 502 is clamped into the limiting groove 504 to limit the clamping plate 503, the inner side wall of the clamping plate 503 also limits the limiting plate 403.

[0038] The present invention also provides a drone, including a frame 6; a power system for providing power to the drone; a flight control system for controlling the flight of the drone; a communication and data transmission system for realizing real-time data interaction between the drone and the ground station to ensure remote monitoring and scheduling; an auxiliary system for enhancing the environmental adaptability and safety of the drone; a landing gear 7, which is fixedly arranged at the lower end of the frame 6, and the other end of the landing gear 7 is rotatably arranged with the top of the upper limit post 208; the power system, the flight control system, the communication and data transmission system and the auxiliary system are installed on the frame 6.

[0039] The frame 6, the power system, the flight control system, the communication and data transmission system and the auxiliary system are prior arts and will not be elaborated herein.

[0040] In summary, when the drone transports goods to the designated location and contacts the ground during landing, the bracket 1 contacts the ground. The bracket 1 is impacted by the ground, and then drives the lower limit post 201 and the lower sliding block 202 to slide along the sliding groove 204 in the sleeve 203. When the lower limit post 201 slides upward in the sleeve 203 to the first position, the top of the lower limit post 201 first presses the second elastic member 302 for primary shock absorption. When the lower limit post 201 drives the lower sliding block 202 to move to the second position, the lower limit post 201 and the lower sliding block 202 press the first elastic member 301 for secondary shock absorption. At this time, through the primary shock absorption and the secondary shock absorption, the drone can achieve a better shock absorption effect during landing.

[0041] After the drone lands stably and it is necessary to disassemble the cargo box, by controlling the adjusting plate 406 to drive the second convex block 502 to move into the accommodating groove 404. At this time, the first elastic member 405 deforms, and the limit on the clamping plate 503 can be released. Then, push the box downward forcefully to drive the clamping plate 503 to disengage from the sleeve 203, and the box can be disassembled.

[0042] When using the drone to lift heavy objects, first use the support frame to support the drone. By rotating the upper top cap 210 to disengage from the top of the sleeve 203, the upper limit post 208 drives the upper sliding block 209 to disengage from the sleeve 203, so that the bracket 1 disengages from the landing gear 7, facilitating the fixing of the rope inside the frame 6 to lift the goods.

[0043] By providing the upper top cap 210 and the upper annular cylinder, it is convenient for the quick installation / dismantling of the bracket 1. By rotating the upper top cap 210 to move, the upper annular block 211 is driven to disengage from the sleeve 203, and the upper limit post 208 and the upper sliding block 209 disengage from the sleeve 203, thus realizing the quick docking of the bracket 1 and improving the efficiency during the working process.

[0044] By setting the first elastic member 301 and the second elastic member 302, primary shock absorption is achieved when the lower limit post 201 and the lower slider 202 move to the first position, and secondary shock absorption is achieved when the lower limit post 201 and the lower slider 202 move to the second position. Through double shock absorption, the shock absorption effect of the drone during landing can be improved better.

[0045] By setting the second elastic member 302, when the drone lands on an uneven road surface, the bracket 1 can better contact the ground under the action of the elastic force of the second elastic member 302 itself, increasing the overall stability of the drone.

[0046] Embodiment 2, on the basis of the above embodiment, since the elastic force of the first elastic member 301 is relatively large, after the first elastic member 301 is compressed, the whole drone will jump up during the reset process, resulting in the tipping of the drone and damage to the drone; for this reason, the following improvements are made.

[0047] As Figure 4 shown, the clamping portion 4 further includes a second elastic member 407, one end of which is fixedly arranged in the accommodating groove 404; a third elastic member 408, which is arranged in an arc structure, and one end of which is connected to the other end of the second elastic member 407; an adjusting plate 409, one end of which is fixedly connected to the third elastic member 408; a first convex block 501 is arranged at one end of the adjusting plate 409, and the buffer portion 3 after the second shock absorption is blocked by the first convex block 501 to prevent the bracket 1 from jumping up. A clamping member is arranged at the corresponding ends of the first adjusting plate 406 and the second adjusting plate 409, and a hook is arranged on each of the first adjusting plate 406 and the second adjusting plate 409, and the two are in a clamped state; the buffer portion 3 further includes a jacking block 303, which is arranged at the bottom of the first elastic member 301 and corresponds to the first convex block 501.

[0048] During the secondary shock absorption, the lower limit post 201 pushes the first elastic member 301 to be compressed upward. During the compression process of the first elastic member 301, the jacking block 303 is driven to rise, and the first convex block 501 is extruded, causing the first convex block 501 to tilt at an angle. At this time, the second elastic member 407 and the third elastic member 408 are deformed upward due to the influence of the first convex block 501.

[0049] While the first convex block 501 is tilting at an angle, the first convex block 501 drives the adjusting plate 409 to tilt at an angle accordingly. The tilted adjusting plate 409 is disengaged from the limit of the adjusting plate 406. As the first elastic member 301 continues to be compressed, the jacking block 303 jumps over the first convex block 501. At this time, due to the release of the limit of the adjusting plate 406 and the adjusting plate 409, the second elastic member 407 and the third elastic member 408 drive the first convex block 501 on the adjusting plate 409 to increase the blocking area of the first elastic member 301 under the action of the elastic force.

[0050] During the reset process of the first elastic member 301, since the bottom of the first elastic member 301 and the jacking block 303 are blocked and cannot be reset, the problem that the entire drone jumps up during the reset process due to the excessive elastic force of the first elastic member 301 is avoided, thereby improving the stability of the drone.

[0051] By manually controlling the adjusting plate two 409, the adjusting plate two 409 drives the first convex block 501 to move into the accommodating groove 404, releases the block of the first convex block 501 on the first elastic member 301, and makes the adjusting plate one 406 and the adjusting plate two 409 engage with each other.

[0052] By setting the cooperation of components such as the second elastic member 407, the third elastic member 408, the second convex block 502 and the adjusting plate two 409, the overall jump of the drone is prevented, thereby improving the stability of the drone during landing. By blocking the reset of the first elastic member 301 with the second convex block 502, the overall jump of the drone caused by the excessive elastic force of the first elastic member 301 can be prevented.

[0053] Finally, it should be noted that the above are only the preferred embodiments of the present invention and are not used to limit the present invention. Although the present invention has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments, or perform equivalent replacements for some of the technical features. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention shall be included in the protection scope of the present invention.

Claims

1. Drone truss warehouse, characterized in that, include: A bracket, used for supporting the box; A mounting portion, which has at least two groups and is used to fix the bracket; The buffer portion corresponds to the mounting portion and performs primary and secondary shock absorption on the bracket when the bracket contacts the ground, thereby enhancing the stability of the bracket landing; A clamping portion, corresponding to the mounting portion, for clamping the box body onto the outer side wall of the mounting portion; The limiting portion corresponds to the clamping portion and includes a first protrusion and a second protrusion. The first protrusion blocks the buffer portion after secondary shock absorption to prevent the bracket from jumping up. The second protrusion is used to limit the limiting portion, thereby limiting the position of the box body. The mounting portion includes: a lower limiting post rotatably disposed on the top of the bracket; a sleeve, which is arranged on the outer wall of the lower limit column; The clamping portion includes: an arc-shaped groove provided on the side wall of the sleeve; A support plate is provided on the side wall of the arc-shaped groove and is flush with the arc-shaped groove; A limiting plate, one end of which is rotatably arranged on the top of the supporting plate and the other end of which extends to the arc-shaped groove; The receiving groove is provided around the side of the limiting plate; Elastic member 1, which is arranged at one end of the accommodating groove away from the axis of the sleeve; an adjusting plate 1, which is fixedly disposed on one end of the elastic member 1 and contacts the interior of the accommodating groove; a second elastic member, one end of which is fixedly disposed in the receiving groove; an elastic member 3, one end of which is connected to the other end of the elastic member 2; an adjusting plate 2, one end of which is fixedly connected to the elastic member 3; The first protrusion is provided at one end of the second adjustment plate, and the second protrusion is provided at one end of the first adjustment plate; The corresponding ends of the adjusting plate 1 and the adjusting plate 2 are provided with a clamping piece; By controlling the adjustment plate 1 to drive the second protrusion to move into the accommodating groove, the elastic member 1 is deformed at this time, and the limit on the limiting part can be released. By controlling the adjustment plate 2 to drive the first protrusion to move into the accommodating groove, the elastic member 2 and the elastic member 3 are deformed at this time, and the obstruction on the buffer part can be released.

2. The drone truss warehouse according to claim 1, characterized in that The mounting portion further includes: a lower sliding block fixedly disposed on one side of the top of the lower limiting column; A lower sliding groove is provided inside the sleeve; a lower cap, the threads of which are set on the bottom of the sleeve; a lower annular block fixedly disposed inside the lower top cap; By rotating the lower top cap, the lower annular block is driven to move upward, so that the lower annular block pushes the lower slider and drives the lower limit column to move axially along the lower sliding groove, thereby driving the bracket to adjust its position.

3. The drone truss warehouse according to claim 1, characterized in that, The mounting portion further includes: an upper slide groove, which is opened on the inner side of the top of the sleeve; an upper limit post, which is arranged inside the sleeve; An upper slider, which is arranged on one side of the bottom of the upper limit column; an upper cap, the threads of which are arranged on the top of the sleeve; an upper annular block, which is arranged inside the upper top cap; By rotating the upper cap, the upper annular block is driven to move downward, so that the upper annular block pushes the upper slider and drives the upper limit column to move axially along the upper slide groove until it is fixed to the upper limit column.

4. The drone truss bin according to claim 2, characterized in that, The buffer portion includes a first elastic member and a second elastic member disposed in the sleeve, wherein the first elastic member has a larger diameter than the second elastic member and a greater elastic force than the second elastic member, and is used to improve the stability of the bracket when in contact with the ground; The lifting block is arranged at the bottom of the first elastic member and corresponds to the first protrusion.

5. The drone truss warehouse according to claim 1, wherein, The limiting part further includes a clamping plate fixedly arranged on the box body and a limiting groove opened on one side of the clamping plate. One end of the clamping plate is clamped on the outer wall of the sleeve, and the second convex block is inserted into the limiting groove to limit the clamping plate, thereby achieving the limitation of the box body.

6. A drone, having a drone truss bin as described in any one of claims 1-5, characterized in that, Comprising: A frame; A power system for providing power to the drone; A flight control system for controlling the flight of the drone; A communication and data transmission system for realizing real-time data interaction between the drone and the ground station to ensure remote monitoring and scheduling; An auxiliary system for enhancing the environmental adaptability and safety of the drone; A landing gear fixedly arranged at the lower end of the frame, and the other end of the landing gear is rotatably arranged with the top of the upper limiting column; The power system, flight control system, communication and data transmission system, and auxiliary system are installed on the frame.

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