Vertical lifting unmanned aerial vehicle parking clamping device

Abstract

The utility model discloses a vertical lifting unmanned aerial vehicle parking and clamping device, and relates to the technical field of vertical lifting unmanned aerial vehicles, the vertical lifting unmanned aerial vehicle parking and clamping device comprises a partition plate and a plurality of locking mechanisms, the partition plate is provided with a plurality of locking mechanisms at intervals, and each locking mechanism comprises a base and a clamping assembly; during use, a supporting piece of the unmanned aerial vehicle is firstly placed between the two clamping parts, an unmanned aerial vehicle body or a specific part is pressed to enable the unmanned aerial vehicle to trigger the triggering part to move downwards, so that the two clamping parts are driven to move oppositely, after the two clamping parts are clamped, the two clamping parts and the base define the limiting space, and the limiting space is used for limiting the unmanned aerial vehicle. According to the unmanned aerial vehicle clamping and releasing device, the limiting space is formed in the clamping part, the unmanned aerial vehicle part located in the limiting space is limited, locking can be achieved through matching of the multiple locking mechanisms, the operation process is greatly simplified, the clamping and releasing process can be achieved through the action of the triggering part, the working efficiency is greatly improved, and the universality is improved.

Description

TECHNICAL FIELD

[0001] The utility model relates to vertical lift unmanned plane technical field, especially vertical lift unmanned plane parking clamping device. BACKGROUND

[0002] In the unmanned plane application field, the scene of needing large-scale deployment unmanned plane often appears, how to guarantee the stability of unmanned plane in the transportation process becomes a technical challenge.

[0003] The vertical lift unmanned plane is supported by the support piece when parking, and the support piece of the existing vertical lift unmanned plane is usually a support rod structure, the support rod is arranged in parallel with the support surface to support the body of the unmanned plane, and because the unmanned plane is expensive, it is usually necessary to fix or limit the unmanned plane to avoid bumping and damaging in the transportation process, which reduces the operation efficiency and the fixing quality.

[0004] In the patent file with publication number CN212243871U, a kind of unmanned plane launcher can be installed on car and used, for carrying unmanned plane, the unmanned plane launcher includes installation base, stabilizing mechanism, receiving platform and fastening mechanism;Fastening mechanism includes electromagnet, electromagnet is installed on receiving platform, the fastening mechanism is suitable for unmanned plane with ferrous unmanned plane landing gear;The unmanned plane launcher can only fasten unmanned plane with magnetic attraction piece, and in order to reduce the dead weight of unmanned plane, most of them are made of non-metallic material, so the use scene of the unmanned plane launcher is limited, unmanned plane without magnetic attraction piece cannot be fastened, and the versatility is low. UTILITY MODEL CONTENT

[0005] The main purpose of the utility model is to provide a kind of vertical lift unmanned plane parking clamping device, to solve the problem that fastening device operation step is complex, and unmanned plane needs to be equipped with corresponding components.

[0006] To achieve the above-mentioned purpose, the vertical lift unmanned plane parking clamping device provided by the utility model comprises:

[0007] Partition plate;

[0008] Locking mechanism, a plurality of locking mechanisms are arranged on the partition plate, the locking mechanism comprises a base and a clamping assembly;

[0009] The clamping assembly comprises a clamping part and a trigger part, the clamping part and the trigger part are both two and oppositely arranged, the two clamping parts are rotatably connected to the base, the clamping part is fixedly connected to the trigger part, the trigger part is located between the two clamping parts, to drive the two clamping parts to move towards each other, the two clamping parts and the base form a limiting space.

[0010] In an embodiment, the two trigger portions are staggered, one of the trigger portions is provided with a clamping protrusion, and the clamping protrusion is in interference fit with the other trigger portion.

[0011] The other trigger portion is provided with a receiving groove for receiving the clamping protrusion.

[0012] In an embodiment, the locking mechanism further comprises a control member, the control member is located on the side of the trigger portion away from the limiting space, and the control member is slidingly connected to the base for driving the trigger portion to move.

[0013] In an embodiment, the locking mechanism further comprises a connecting member, one end of the connecting member is rotatably connected to the trigger portion, and the other end of the connecting member is rotatably connected to the control member.

[0014] In an embodiment, the locking mechanism further comprises a first driving member, the first driving member is fixedly connected to the base, and an output end of the first driving member is connected to the control member for driving the control member to slide.

[0015] In an embodiment, the vertical lifting unmanned aerial vehicle parking clamping device further comprises an unlocking push plate, the unlocking push plate is arranged between the locking mechanism and the partition plate.

[0016] The control member partially protrudes from the base and extends towards the unlocking push plate, and the unlocking push plate is slidingly connected to the partition plate for abutting and pushing the control member to move towards the side of the trigger portion.

[0017] In an embodiment, the partition plate is fixedly connected with a second driving member, and an output end of the second driving member is connected to the unlocking push plate for driving the unlocking push plate to lift.

[0018] In an embodiment, the vertical lifting unmanned aerial vehicle parking clamping device further comprises a sliding assembly, the sliding assembly comprises a sliding block and a mounting rod connected to each other, the sliding block is slidingly connected to the partition plate, and the mounting rod is connected to the locking mechanism.

[0019] In an embodiment, the base is provided with a first sliding channel, and the locking mechanism is slidingly connected to the mounting rod through the first sliding channel.

[0020] In an embodiment, the sliding assembly further comprises a positioning member, the positioning member comprises an abutting portion and a rotating portion connected to each other, the rotating portion is threadedly connected to the sliding block, and the abutting portion and the sliding block clamp the partition plate in cooperation.

[0021] The utility model discloses a technical scheme is locked to unmanned aerial vehicle through adopting locking mechanism, when using, first the support piece of unmanned aerial vehicle is placed between two clamping parts, presses unmanned aerial vehicle body or specific position to make unmanned aerial vehicle trigger trigger portion downward movement, to drive two clamping parts opposite movement, two clamping parts are clamped, and two clamping parts and base enclose and form the spacing of limiting space, and the unmanned aerial vehicle component in the spacing of limiting space is positioned, and through a plurality of locking mechanism collocation can realize locking, greatly simplifies the operation process, and clamping and releasing process can be realized through the action of trigger portion, does not need complicated binding or unbundling step, greatly improves work efficiency, and whether the unmanned aerial vehicle can be magnetically attracted does not have special requirement, improves the versatility. BRIEF DESCRIPTION OF DRAWINGS

[0022] In order to more clearly illustrate the technical scheme in the embodiments of the utility model or prior art, below will be to the embodiment or prior art description needed to use the drawing briefly introduced, obviously, the drawing in the following description only some embodiments of the utility model, for those skilled in the art, under the premise of not paying creative labor, still can obtain other drawings according to the structure shown in these drawings.

[0023] Figure 1 The structure schematic diagram of one embodiment of the vertical lifting unmanned aerial vehicle parking clamping device provided by the utility model is provided.

[0024] Figure 2 The structure schematic diagram of the locking mechanism is provided.

[0025] Figure 3 The assembly relationship schematic diagram of trigger portion and control piece is provided.

[0026] Figure 4 The structure schematic diagram of another embodiment of the vertical lifting unmanned aerial vehicle parking clamping device provided by the utility model is provided.

[0027] Figure 5 The side view of the vertical lifting unmanned aerial vehicle parking clamping device provided by the utility model is provided.

[0028] Explanation of the attached drawings:

[0029] 100, vertical lifting unmanned aerial vehicle parking clamping device, 1, partition, 11, guide column, 2, locking mechanism, 21, base, 211, first slide, 212, second slide, 22, clamping assembly, 221, clamping part, 222, trigger portion, 2221, detent protrusion, 2222, containing groove, 23, control piece, 24, connecting piece, 25, first driving piece, 26, rack, 3, unlocking push plate, 31, second driving piece, 4, sliding assembly, 41, sliding block, 42, mounting rod, 5, positioning piece, 51, abutment, 52, rotating part.

[0030] The purposes, functional features and advantages of the utility model will be further explained in combination with embodiments with reference to the drawings. DETAILED DESCRIPTION

[0031] The technical solutions in the embodiments of the utility model will be clearly and completely described below in combination with the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor belong to the protection scope of the utility model.

[0032] It should be noted that if the embodiments of the utility model involve directional indications (such as up, down, left, right, front, back, etc.), the directional indications are only used to explain the relative position relationship, movement condition, etc. between components in a certain posture, and if the certain posture changes, the directional indications also change accordingly.

[0033] In addition, if the embodiments of the utility model involve descriptions such as "first", "second", etc., the descriptions of "first", "second", etc. are only for description purposes, and cannot be understood as indicating or implying the relative importance or implicitly indicating the number of indicated technical features. Therefore, the features limited by "first", "second" can explicitly or implicitly include at least one feature. In addition, "and / or" or "and / or" appearing throughout the text means that the three parallel schemes are included, for example, "A and / or B" includes A scheme, or B scheme, or A and B simultaneously satisfy the scheme. In addition, the technical solutions of each embodiment can be combined with each other, but it must be based on the realization of ordinary skilled in the art, when the combination of technical solutions appears contradictory or unachievable, it should be considered that the combination of technical solutions does not exist, and is not within the protection scope required by the utility model.

[0034] In the field of unmanned aerial vehicle application, there are often scenes that need to deploy unmanned aerial vehicles on a large scale, and how to ensure the stability of unmanned aerial vehicles during transportation has become a technical challenge.

[0035] The vertical take-off and landing unmanned aerial vehicle is supported by the support piece when parking, and the support piece of the existing vertical take-off and landing unmanned aerial vehicle is usually a support rod structure, the support rod is arranged in parallel with the support surface to support the body of the unmanned aerial vehicle, and since the unmanned aerial vehicle is expensive, it is usually necessary to fix or limit the unmanned aerial vehicle to avoid bumping and damaging it during transportation, and the unmanned aerial vehicle is limited by a rope, which is low in operation efficiency and low in fixing quality.

[0036] A kind of unmanned aerial vehicle launching rack is disclosed in the patent document with publication number CN212243871U, which can be installed on a vehicle for use and used to carry an unmanned aerial vehicle.The unmanned aerial vehicle launching rack includes a mounting base, a stabilizing mechanism, a receiving platform, and a fastening mechanism.The fastening mechanism includes an electromagnet mounted on the receiving platform and is suitable for unmanned aerial vehicles with ferrous unmanned aerial vehicle landing gear.The unmanned aerial vehicle launching rack can only fasten unmanned aerial vehicles equipped with magnetic attractable components, and in order to reduce the weight of the unmanned aerial vehicle, non-metallic materials are often used, so the use scenarios of the unmanned aerial vehicle launching rack are limited, and it cannot fasten unmanned aerial vehicles without magnetic attractable components, so the versatility is low.

[0037] The utility model provides a vertical lift unmanned aerial vehicle parking clamping device 100.

[0038] Please refer to Figures 1 to 5 In an embodiment of the utility model, the vertical lift unmanned aerial vehicle parking clamping device 100 has a partition 1.

[0039] The partition 1 is provided with a plurality of locking mechanisms 2 at intervals, and the locking mechanism 2 includes a base 21 and a clamping assembly 22.

[0040] The clamping assembly 22 includes a clamping part 221 and a trigger part 222, and both the clamping part 221 and the trigger part 222 are oppositely arranged, both the clamping part 221 are rotationally connected to the base 21, the clamping part 221 is fixedly connected to the trigger part 222, the trigger part 222 is located between the two clamping parts 221 to drive the two clamping parts 221 to move towards each other, and the two clamping parts 221 and the base 21 form a limiting space.

[0041] The utility model discloses a technical scheme that locks the unmanned aerial vehicle by using the locking mechanism 2.When in use, first place the support of the unmanned aerial vehicle between the two clamping parts 221, press the unmanned aerial vehicle body or a specific part to make the unmanned aerial vehicle trigger the trigger part 222 to move downwards, thereby driving the two clamping parts 221 to move towards each other.After the two clamping parts 221 are clamped, the two clamping parts 221 and the base 21 form the limiting space, which limits the unmanned aerial vehicle components in the limiting space. By matching multiple locking mechanisms 2, the locking can be realized, the operation process is greatly simplified, the clamping and releasing process can be realized by the action of the trigger part 222, without complex binding or unbinding steps, the work efficiency is greatly improved, and there is no special requirement for whether the unmanned aerial vehicle can be magnetically attracted, improving the versatility.

[0042] Optionally, the two trigger parts 222 are staggered, one trigger part 222 is provided with a clamping protrusion 2221, and the clamping protrusion 2221 is in interference fit with the other trigger part 222.

[0043] Another said trigger part 222 is provided with a containing groove 2222 for containing the clamping protrusion 2221.

[0044] As Figure 2 and Figure 3 It should be noted that the two trigger parts 222 are staggered to avoid mutual interference, and the clamping protrusion 2221 is in interference fit with another trigger part 222.

[0045] It can be understood that the clamping part 221 is rotationally connected to the base 21, the trigger part 222 is fixedly connected to the clamping part 221, and the trigger part 222 can also rotate relative to the base 21. When the trigger part 222 is rotated to a certain angle, the clamping protrusion 2221 abuts against another trigger part 222, and the friction between the two trigger parts 222 increases.

[0046] When the two clamping parts 221 move towards each other to clamp the unmanned aerial vehicle, the clamping protrusion 2221 is located in the containing groove 2222, the containing groove 2222 limits the movement of the clamping protrusion 2221, and the two trigger parts 222 are relatively fixed. Therefore, the two clamping parts 221 are also relatively fixed, ensuring the clamping and fixing of the unmanned aerial vehicle, so that the clamping part 221 is not easy to move away from each other to release the clamping due to the bumping during transportation, and the stability of clamping is improved.

[0047] Optionally, as Figure 3 shown, the side surface of the clamping protrusion 2221 is inclined, and the clamping protrusion 2221 can be brought into abutment with another trigger part 222 by directly rotating the trigger part 222.

[0048] In addition, the inclined arrangement also facilitates the movement of the clamping protrusion 2221 out of the containing groove 2222 by directly rotating the trigger part 222, which is convenient to operate and improves work efficiency.

[0049] Optionally, the side surface of the clamping protrusion 2221 can be an arc surface or an inclined surface, which is not limited in the embodiment.

[0050] Optionally, as Figure 3 shown, the locking mechanism 2 further includes a control member 23 located on the side of the trigger part 222 away from the limiting space, and the control member 23 is slidingly connected to the base 21 to drive the movement of the trigger part 222.

[0051] It should be noted that when the clamping part 221 needs to be unlocked after clamping the unmanned aerial vehicle and moving towards, the unmanned aerial vehicle needs to be lifted, or forces moving away from each other are applied to the two clamping parts 221, so that the clamping parts 221 release the restriction on the unmanned aerial vehicle.

[0052] The base 21 is provided with a second sliding channel 212, and the control member 23 is slidingly connected to the base 21 through the second sliding channel 212. By lifting the control member 23, the control member 23 abuts against the trigger part 222 and pushes the trigger part 222 to rotate, thereby driving the two clamping parts 221 to move away from each other and release the restriction on the unmanned aerial vehicle. By lifting the control member 23, the unmanned aerial vehicle can be unlocked without directly applying an external force to the two clamping parts 221, avoiding the inconvenience caused by the blocking of the unmanned aerial vehicle. Moreover, the control member 23 can be lifted to unlock, which is simple, efficient, and improves the unlocking efficiency.

[0053] In some embodiments, the control member 23 partially protrudes from the base 21. The protruding part of the control member 23 facilitates the control of the lifting of the control member 23.

[0054] Optionally, the second sliding channel 212 communicates the inside and outside of the base 21, and the control member 23 partially protrudes from the base 21 through the second sliding channel 212. The protruding part drives the lifting of the control member 23.

[0055] Optionally, the locking mechanism 2 further comprises a connecting member 24, one end of the connecting member 24 being rotationally connected to the trigger part 222, and the other end of the connecting member 24 being rotationally connected to the control member 23.

[0056] It should be noted that the control member 23 abutting against the trigger part 222 can push the trigger part 222 to rotate to achieve unlocking, but cannot drive the trigger part 222 to rotate to achieve locking.

[0057] As shown in Figure 3 The number of the connecting members 24 is two, and the two connecting members 24 are respectively connected to the two trigger parts 222. The other ends of the two connecting members 24 are connected to the control member 23. The connecting members 24 connect the trigger parts 222 and the control member 23, so that the control member 23 can not only push the trigger parts 222 to rotate to achieve unlocking, but also pull the trigger parts 222 to rotate to achieve locking. The control member 23 can achieve bidirectional control of the trigger parts 222, providing higher flexibility and convenience and meeting the use requirements in different scenarios.

[0058] It should be noted that the connecting piece 24 can also make the rotation angles of the two clamping parts 221 relative to the base 21 the same, and rotating one clamping part 221 can drive the other clamping part 221 to rotate. Since the rotation angles of the two clamping parts 221 are the same and interlock, when one clamping part 221 is operated to clamp or unlock, the other clamping part 221 will synchronously perform the same action. This synchronization ensures that the UAV receives uniform and stable force during the clamping and unlocking processes, thereby ensuring the stability of clamping the UAV.

[0059] Optionally, the locking mechanism 2 further comprises a first driving piece 25 fixedly connected to the base 21, and an output end of the first driving piece 25 is connected to the control piece 23 to drive the control piece 23 to slide.

[0060] It can be understood that the first driving piece 25 can control the control piece 23, and then the control piece 23 drives the clamping part 221 to rotate to clamp the UAV. The first driving piece 25 can automatically control the clamping and unlocking of the locking mechanism 2, which greatly improves the operation efficiency and reduces the need for manual intervention.

[0061] In some embodiments, the support of the UAV is placed on the trigger position. Due to the arrangement of the clamping protrusion 2221, an external force needs to be applied to the trigger part 222 or the clamping part 221 to make the clamping protrusion 2221 located in the accommodating groove 2222 to achieve locking. The weight of the UAV cannot make the clamping protrusion located in the accommodating groove 2222, so it is often necessary to manually press the UAV or manually adjust the locking mechanism 2, which is relatively inconvenient.

[0062] In some embodiments, the support of the UAV is placed on the trigger position. The first driving piece 25 drives the control piece 23 to descend, drives the trigger part 222 to rotate, and makes the clamping protrusion 2221 located in the accommodating groove 2222 to achieve locking.

[0063] And the first driving piece 25 drives the control piece 23 to ascend, drives the trigger part 222 to rotate, and makes the clamping protrusion 2221 disengage from the accommodating groove 2222 to achieve unlocking. This greatly improves the operation efficiency and reduces the need for manual intervention.

[0064] As shown in the drawings, Figure 4 In an embodiment, the first driving piece 25 comprises a motor, the control piece 23 is fixedly connected with a rack 26, and the rack 26 is meshingly connected with an output shaft of the motor to drive the control piece 23 to ascend and descend.

[0065] It should be noted that the vertical take-off and landing unmanned aerial vehicle parking clamping device 100 further comprises a central control assembly, and the first driving member 25 is electrically connected with the central control assembly. It can be understood that the number of the locking mechanisms 2 is multiple, one of the locking mechanisms 2 comprises one first driving assembly, and the central control assembly can control multiple first driving members 25, so that the clamping and unlocking of multiple locking mechanisms 2 are synchronously operated.

[0066] Optionally, the vertical take-off and landing unmanned aerial vehicle parking clamping device 100 further comprises an unlocking push plate 3, which is arranged between the locking mechanism 2 and the partition plate 1.

[0067] The control member 23 partially protrudes from the base 21 and extends towards the unlocking push plate 3, and the unlocking push plate 3 is slidably connected with the partition plate 1, so as to abut and push the control member 23 to move to one side of the trigger part 222.

[0068] It should be noted that when the unmanned aerial vehicle needs to take off, multiple locking mechanisms 2 clamping the unmanned aerial vehicle need to be unlocked, and the unmanned aerial vehicle can take off without obstacles.

[0069] In some embodiments, multiple locking mechanisms 2 need to be manually unlocked, which is low in unlocking efficiency and inconvenient to operate.

[0070] In another embodiment, the central control assembly can be used to synchronously control multiple first driving members 25, thereby improving the unlocking efficiency, but the first driving member 25 needs to be arranged in each locking mechanism 2, which is high in manufacturing cost.

[0071] It should be noted that by lifting the unlocking push plate 3, the unlocking push plate 3 abuts against the protruding part of multiple control members 23 protruding from the base 21 and extending towards the unlocking push plate 3, and simultaneously drives multiple control members 23 to lift, thereby achieving the unlocking of multiple locking mechanisms 2, reducing the manufacturing cost, and improving the unlocking efficiency.

[0072] As shown in FIG. 1, Figure 5 In an embodiment, the partition plate 1 is provided with multiple guide columns 11, which guide the partition plate 1, and the unlocking push plate 3 is slidably connected with the partition plate 1 through the guide columns 11.

[0073] In some embodiments, the partition plate 1 is provided with a sliding groove corresponding to the unlocking push plate 3, which guides the sliding direction of the unlocking push plate 3, and the unlocking push plate 3 is slidably connected with the partition plate 1 through the sliding groove.

[0074] Optionally, the partition 1 is fixedly connected with a second driving member 31, an output end of the second driving member 31 is connected with the unlocking push plate 3, so as to drive the unlocking push plate 3 to lift.

[0075] It can be understood that the second driving member 31 can realize automatic control of the unlocking push plate 3, which greatly improves the operation efficiency and reduces the need for manual intervention.

[0076] In some embodiments, the second driving member 31 includes a pneumatic pump, the pneumatic pump is fixedly connected with the partition 1, an output shaft of the pneumatic pump is fixedly connected with the unlocking push plate 3, the pneumatic pump can drive the unlocking push plate 3 to lift, realize automatic control of the unlocking push plate 3, and improve the unlocking efficiency.

[0077] As shown in the drawings, Figure 5 In other embodiments, the second driving member 31 includes a hydraulic pump, the hydraulic pump is fixedly connected with the partition 1, an output shaft of the hydraulic pump is fixedly connected with the unlocking push plate 3, the hydraulic pump can drive the unlocking push plate 3 to lift, realize automatic control of the unlocking push plate 3, and improve the unlocking efficiency.

[0078] Optionally, the number of the second driving assembly is two, which is respectively located on the opposite sides of the unlocking push plate 3, so as to ensure that the unlocking push plate 3 is evenly stressed, and the stability of the lifting of the unlocking push plate 3 is ensured.

[0079] Optionally, the number of the second driving assembly is four, for example, the cross section of the unlocking push plate 3 is rectangular, the second driving assembly is respectively located at four corners of the unlocking push plate 3, which further improves the stability of the lifting of the unlocking push plate 3, and improves the pushing force and pulling force of the unlocking push plate 3.

[0080] In some embodiments, the second driving member 31 is electrically connected with the central control assembly, and the second driving assembly controlled by the central control assembly can realize simultaneous unlocking of a plurality of locking mechanisms 2.

[0081] Optionally, the vertical lifting unmanned aerial vehicle parking clamping device 100 further includes a sliding assembly 4, the sliding assembly 4 includes sliding blocks 41 and mounting rods 42 connected with each other, the sliding blocks 41 are slidingly connected with the partition 1, and the mounting rods 42 are connected with the locking mechanisms 2.

[0082] It can be understood that the existing vertical lifting unmanned aerial vehicle support is often a support rod structure, and the support rods are arranged in parallel with the support surface to support the unmanned aerial vehicle body. Due to the different sizes of the unmanned aerial vehicles, the sizes of the support rods are also different, and the distance between the support rods is also adjusted. The distance between different locking mechanisms 2 is fixed when the locking mechanisms 2 are fixedly connected to the partition plate 1, which is inconvenient for adapting to unmanned aerial vehicles of different sizes.

[0083] It should be noted that the number of the sliding assemblies 4 is multiple, and the sliding blocks 41 are slidably connected to the partition plate 1, so that the relative distance between different sliding assemblies 4 can be changed. The locking mechanisms 2 are installed on the mounting rods 42, so that the distance between the locking mechanisms 2 located on different mounting rods 42 can also be changed, thereby adapting to unmanned aerial vehicles of different sizes and improving the versatility.

[0084] Alternatively, as shown in Figure 2 The base 21 is provided with a first sliding groove 211, and the locking mechanisms 2 are slidably connected to the mounting rods 42 through the first sliding groove 211.

[0085] It can be understood that, due to the different sizes of the unmanned aerial vehicles, the sizes of the support rods are also different, and not only the distance between the support rods is adjusted, but also the length of the support rods is changed. In order to ensure the stability of the unmanned aerial vehicle during clamping, one support rod is usually clamped by two locking mechanisms 2, and the greater the distance between the two locking mechanisms 2, the higher the stability of the unmanned aerial vehicle.

[0086] It should be noted that the locking mechanisms 2 can slide relative to the mounting rods 42 through the first sliding groove 211, so that the positions of the locking mechanisms 2 can be adjusted, thereby adapting to unmanned aerial vehicles of different sizes and improving the versatility.

[0087] It can be understood that, according to the different relative directions of the locking mechanisms 2 and the mounting rods 42, in other embodiments, the sliding blocks 41 slidably connect the partition plate 1, and the distance between different mounting rods 42 is adjusted to adapt to support rods of different lengths.

[0088] The positions of the locking mechanisms 2 relative to the support rods are adjusted to adapt to the case that the distance between the support rods of different unmanned aerial vehicles is different.

[0089] Alternatively, the sliding assembly 4 further comprises a positioning member 5, the positioning member 5 comprises an abutting portion 51 and a rotating portion 52 connected to each other, the rotating portion 52 is threadedly connected to the sliding block 41, and the abutting portion 51 and the sliding block 41 clamp the partition plate 1 in cooperation.

[0090] It should be noted that since the sliding assembly 4 is slidably connected to the partition 1, during transportation, the sliding assembly 4 may slide relative to the partition 1, and the clamped drone may also slide relatively, which is not conducive to the stability of the drone during transportation.

[0091] To this end, the distance between the abutting portion 51 and the sliding block 41 is adjusted by rotating the rotating portion 52. Figure 1 As shown, the sliding block 41 partially protrudes and cooperates with the ground connection part to clamp the partition 1, thereby increasing the friction between the sliding block 41 and the partition 1, thereby achieving tight clamping of the partition 1, effectively preventing the sliding component 4 from sliding relative to the partition 1 due to external factors such as road bumps and vibrations, and improving the safety and reliability of the overall transportation.

[0092] In addition, the positioning member 5 also allows the operator to adjust the clamping force of the positioning member 5 by rotating the rotating part 52 at any time according to actual needs, which can not only provide sufficient clamping force during transportation, but also easily release the sliding assembly 4 when needed, making it convenient to adjust the sliding block 41 when adapting to different drones.

[0093] Optionally, the contact surface between the abutting portion 51 and the partition 1 is provided with anti-slip grooves to increase friction.

[0094] The above description is merely an exemplary embodiment of the present invention and does not limit the patent scope of the present invention. All equivalent structural transformations made using the contents of the present invention specification and drawings under the technical concept of the present invention, or direct / indirect application in other related technical fields are included in the patent protection scope of the present invention.

Claims

1. A vertical lift drone parking clamping device, characterized in that, The utility model relates to a vertical lifting unmanned plane parking clamping device, including: A partition plate is arranged on the partition plate, and a plurality of locking mechanisms are arranged at intervals on the partition plate. The locking mechanism includes a base and a clamping assembly. The clamping assembly includes a clamping part and a trigger part, both of which are oppositely arranged, both of which are rotatably connected to the base, and the clamping part is fixedly connected to the trigger part.

2. The vertical lift drone parking clamp apparatus of claim 1, wherein, The trigger part is located between the two clamping parts and drives the two clamping parts to move towards each other, and the two clamping parts and the base form a limiting space. The two trigger parts are staggered, one of the trigger parts is provided with a clamping protrusion, and the clamping protrusion is in interference fit with the other trigger part.

3. The vertical lift drone parking clamp of claim 2, wherein, The other trigger part is provided with a receiving groove for accommodating the clamping protrusion.

4. The vertical lift drone parking clamp of claim 3, wherein, The locking mechanism further includes a control member, which is located on the side of the trigger part away from the limiting space, and is slidably connected to the base to drive the trigger part to move.

5. The vertical lift drone parking clamp apparatus of claim 4, wherein, The locking mechanism further includes a connecting member, one end of which is rotatably connected to the trigger part, and the other end is rotatably connected to the control member.

6. The vertical lift drone parking clamp apparatus of claim 4, wherein, The locking mechanism further includes a first drive member fixedly connected to the base, and the output end of the first drive member is connected to the control member to drive the control member to slide. The vertical lifting unmanned plane parking clamping device further includes an unlocking push plate arranged between the locking mechanism and the partition plate.

7. The vertical lift drone parking clamp apparatus of claim 6, wherein, The control member partially protrudes from the base and extends towards the unlocking push plate, and the unlocking push plate is slidably connected to the partition plate to abut and push the control member to move towards the side of the trigger part.

8. The vertical lift drone parking clamp apparatus of any one of claims 1 to 7, wherein, The partition plate is fixedly connected with a second drive member, and the output end of the second drive member is connected with the unlocking push plate to drive the unlocking push plate to lift.

9. The vertical lift drone parking clamp apparatus of claim 8, wherein, The vertical lifting unmanned plane parking clamping device further includes a sliding assembly, which includes a sliding block and a mounting rod connected with each other.

10. The vertical lift drone parking clamp apparatus of claim 8, wherein, The base is provided with a first sliding channel, and the locking mechanism is slidably connected with the mounting rod through the first sliding channel. The sliding assembly further includes a positioning member, which includes an abutting part and a rotating part connected with each other. The rotating part is threadedly connected with the sliding block, and the abutting part and the sliding block clamp the partition plate.

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