High-integration-level intelligent vehicle-mounted device for receiving, transmitting, storing and transporting large unmanned aerial vehicle cluster

Abstract

The utility model relates to the technical field of unmanned aerial vehicle cluster receiving and transmitting, and particularly discloses a high-integration-level intelligent vehicle-mounted device for receiving, transmitting, storing and transporting a large unmanned aerial vehicle cluster. Comprising a vehicle body, a square cabin installed on the vehicle body and capable of achieving opening and closing of the top face and the side faces, a second lifting device installed in the square cabin and moving in the Z-axis direction, and a first lifting device installed in the square cabin and in sliding fit with the square cabin in the Y-axis direction. A partition plate for dividing the interior of the square cabin into a first space and a second space is arranged in the square cabin; the second space is arranged on one side close to the top surface; the first space is arranged on one side far away from the top surface; the first lifting devices are located in the first spaces and are in sliding fit in the Y-axis direction, and two first lifting devices are arranged in each first space. The second lifting device is located in the second space. According to the utility model, all unmanned aerial vehicles in an unmanned aerial vehicle cluster can be effectively transmitted and received at one time, the working efficiency is greatly improved, the space utilization rate is improved, and more unmanned aerial vehicles can be accommodated.

Description

Technical Field

[0001] The utility model relates to the technical field of sending and receiving of unmanned aerial vehicle clusters, and more specifically, to a highly integrated intelligent vehicle-mounted device for sending, receiving, storing and transporting a large-scale unmanned aerial vehicle cluster. Background Art

[0002] The vehicle-mounted device for sending, receiving, storing and transporting drone clusters in the prior art has the following problems when used:

[0003] The drone takes off and lands only on the top of the device, or only on one side of the device. The device can accommodate a relatively small number of drones, and the space utilization rate of the device is low;

[0004] The device has low compactness. Due to the low space utilization of the above-mentioned device, when facing the needs of drone clusters, the device space is relatively large and the device structure is low in compactness, which cannot meet the needs of sending and receiving drones of different models;

[0005] The deployment time is long and the implementation efficiency is low; when cluster drones need to be launched, landed, stored and transported at the same time, a multi-batch processing method is adopted, that is, the needs of a single drone are met at a time, which leads to a long deployment time and low implementation efficiency. Utility Model Content

[0006] The technical problem to be solved by the utility model is to provide a highly integrated intelligent vehicle-mounted device for receiving, sending, storing and transporting a large-scale UAV cluster;

[0007] The solution adopted by the utility model to solve the technical problem is:

[0008] A highly integrated intelligent vehicle-mounted device for receiving, sending, storing and transporting a large-scale UAV cluster, comprising a vehicle body, a cabin installed on the vehicle body and capable of opening and closing the top and sides, a second take-off and landing device installed in the cabin and moving along the Z-axis direction, and a first take-off and landing device installed in the cabin and slidingly cooperating with the cabin along the Y-axis direction;

[0009] A partition is arranged in the square cabin to vertically divide the square cabin into a first space and a second space; the second space is arranged on a side close to the top surface; and the first space is arranged below the second space;

[0010] The first lifting and landing device is located in the first space and slides along the Y-axis direction. There are two groups of first lifting and landing devices in each first space. The second lifting and landing device is located in the second space.

[0011] In some possible embodiments, the partitions are in two groups and are arranged in parallel along the X-axis direction, and a second space for installing a second take-off and landing device is formed between the plane where the top of the partition is located and the top cover; three groups of first spaces for installing a first take-off and landing device are formed between the two groups of partitions and between the partitions and the inner side surfaces of the cabin.

[0012] In some possible implementations, the second take-off and landing device includes a support platform installed in the second space, a second homing device installed on the support platform and controlling the homing of the UAV, a lifting platform installed on the support platform and slidingly cooperating with the support platform along the Z-axis direction, and a second locking device used in conjunction with the lifting platform and used to lock and fix the UAV on the lifting platform;

[0013] A cavity is arranged on the supporting platform, and the lifting platform is located in the cavity.

[0014] In some possible implementations, the second homing device includes two groups of X-axis linear modules installed on the support platform and arranged in parallel along the X-axis, two groups of Y-axis linear modules arranged in parallel along the Y-axis direction and installed on the two groups of X-axis modules, and push rods respectively installed on the two groups of Y-axis linear modules and moving along the Y-axis direction;

[0015] Two groups of X-axis linear modules and two groups of Y-axis linear modules form a mounting cavity; the long directions of the two groups of push rods are arranged along the X-axis direction and are located above the mounting cavity.

[0016] In some possible embodiments, the lifting platform includes a support plate located in the cavity and slidingly matched with the support platform along the Z-axis direction, and a vertical lifting device installed at the bottom of the support platform and used to control the movement of the support plate along the Z-axis direction.

[0017] In some possible embodiments, the second locking device is composed of two groups and is symmetrically arranged, including a second locking motor installed under the support plate, a second rotating shaft connected to the output shaft of the second locking motor, a second claw mounted on the outside of the second rotating shaft and rotating around the axis of the second rotating shaft under the drive of the second locking motor, and a second through groove arranged on the support plate and used for one end of the second claw to pass through; one side of the second claw passing through the second through groove cooperates with the support plate to form a second clamping cavity.

[0018] In some possible embodiments, the first take-off and landing device includes a support platform located in the first space and slidingly cooperating with a support platform located in the first space along the Y-axis direction, a first homing device installed on the support platform and used to realize the homing action of the UAV, a first locking device installed on the support platform and used to lock and fix the UAV after the UAV is homed, and a Y-sliding mechanism located at the bottom of the mounting platform and used to control the sliding of the support platform along the Y-axis direction.

[0019] In some possible embodiments, the first homing device includes two groups of first clamping plates arranged on the support platform and slidingly cooperate with the support platform along the Y-axis direction, two groups of second clamping plates arranged on the support platform and slidingly cooperate with the support platform along the X-axis direction, a Y-axis driving device for driving the two groups of first clamping plates to move closer to or away from each other, and an X-axis driving device for driving the two groups of second clamping plates to move closer to or away from each other; the two groups of first clamping plates and the two groups of second clamping plates cooperate with each other to form a clamping cavity for parking the drone; the two groups of first clamping plates are located between the two groups of second clamping plates.

[0020] In some possible implementations, the first locking device is located in the clamping cavity, and includes two sets of locking members respectively matched with the two sets of first clamping plates; the locking members are arranged in a one-to-one correspondence with the first clamping plates and form a locking cavity for locking the landing gear of the UAV;

[0021] The locking member includes a first locking motor installed at the bottom of the support platform, a first rotating shaft connected to the output shaft of the first locking motor, a first claw which is sleeved on the outside of the first rotating shaft and rotates around the axis of the first rotating shaft when driven by the first locking motor, and a first through groove which is arranged on the first support platform and is used for one end of the first claw to pass through.

[0022] In some possible embodiments, the square cabin includes a cabin body with an inner cavity, two groups of top covers symmetrically arranged on the cabin body along the Y-axis direction and sliding along the X-axis direction, two groups of side panels symmetrically arranged on the cabin body along the X-axis direction and hinged to the cabin body, a cabin top opening and closing mechanism that is transmission-connected to the top cover and used to control the sliding of the top cover on the cabin body, and a cabin side opening and closing mechanism that is transmission-connected to the side panels and installed on the cabin body; the partition is located in the inner cavity and is perpendicular to the side panels and the top cover.

[0023] Compared with the prior art, the utility model has the following beneficial effects:

[0024] Compared with the prior art, the utility model opens the top and side surfaces of the cabin at the same time, so that the first take-off and landing device slides out from the side, and all drones can be sent and received at the same time; the first take-off and landing device is stacked in the first space, and the second take-off and landing device slides vertically; thus, the utilization rate of the space is greatly improved, so that the number of drones that can be accommodated is greatly increased;

[0025] The utility model provides a return device on the first take-off and landing device and the second take-off and landing device respectively, so that the UAV can effectively adjust its position after landing, avoiding mutual interference between UAVs or between UAVs and the cabin after parking; the locking device is used to lock and fix the UAV after it returns to its position, so as to avoid sliding during transportation, thereby causing collision and damage to the UAV;

[0026] The utility model greatly improves the accommodation of larger drones under the same cabin volume by moving the first take-off and landing device along the Y-axis direction after sending and receiving the drone and the second take-off and landing device along the vertical direction when retrieving the drone. BRIEF DESCRIPTION OF THE DRAWINGS

[0027] Figure 1 It is a schematic diagram of the structure of the utility model;

[0028] Figure 2 It is a structural schematic diagram of the first space, the second space, the partition and the cabin in the utility model;

[0029] Figure 3 It is a structural schematic diagram of the second take-off and landing device in the utility model;

[0030] Figure 4 It is a structural schematic diagram of the entire second lifting and lowering device after the lifting platform in the utility model moves downward along the Z axis;

[0031] Figure 5 This is a schematic diagram of the top view of the lifting platform in the utility model;

[0032] Figure 6 It is a side schematic diagram of the lifting platform in the utility model;

[0033] Figure 7 It is a schematic diagram of the structure of the drone in the utility model being retracted into the second take-off and landing device;

[0034] Figure 8 It is a structural schematic diagram of the first take-off and landing device in the utility model;

[0035] Fig. 9 It is a structural schematic diagram of the first homing device in the utility model;

[0036] Fig.10 It is a structural schematic diagram of the first locking device in the utility model;

[0037] Fig.11 It is a structural schematic diagram of the UAV in the utility model being stored on the first take-off and landing device;

[0038] Fig.12 A schematic diagram of the structure for the drone cluster to be recovered in the shelter;

[0039] Among them: 1. Car body; 2. Cabin; 21. Second space; 22. First space; 23. Top cover; 24. Side plate; 25. Cabin top opening and closing mechanism; 26. Cabin side opening and closing mechanism; 3. Second lifting and lowering device; 31. Support platform; 32. Second homing device; 321. X-axis linear module; 322. Y-axis linear module; 323. Push rod; 324. Push plate; 33. Lifting platform; 331. Support plate; 332. Vertical lifting device; 34. Second locking device; 341. Second locking motor; 342. Second rotating axis; 3 43. Second clamping claw; 344. Second through slot; 4. First lifting and lowering device; 41. Support platform; 42. First homing device; 421. First clamping plate; 422. Second clamping plate; 423. Y-axis driving device; 4231. Y-axis linear driving device; 4232. Y-axis slide slot; 4233. Y-axis transmission member; 424. X-axis driving device; 4242. X-axis slide slot; 43. First locking device; 431. First locking motor; 432. First rotating shaft; 433. First clamping claw; 434. First through slot; 5. Partition. DETAILED DESCRIPTION

[0040] In the present utility model, unless otherwise clearly specified and limited, the terms "installed", "connected", "connected", "fixed" and the like should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral body; it can be directly connected, or indirectly connected through an intermediate medium, it can be the internal connection of two elements or the interaction relationship between two elements. The "first", "second" and similar words mentioned in this application do not indicate any order, quantity or importance, but are only used to distinguish different components. Similarly, "one" or "one" and other similar words do not indicate a quantity limit, but indicate the existence of at least one. In the implementation of this application, "and / or" describes the association relationship of the associated objects, indicating that there can be three relationships, for example, A and / or B can indicate: A exists alone, A and B exist at the same time, and B exists alone. In the description of the embodiments of the present application, unless otherwise specified, the meaning of "multiple" refers to two or more. For example, multiple positioning columns refer to two or more positioning columns. For ordinary technicians in this field, the specific meanings of the above terms in the utility model can be understood according to the specific circumstances.

[0041] The utility model is described in detail below.

[0042] like Figure 1-Figure 12 As shown:

[0043] A highly integrated intelligent vehicle-mounted device for receiving, sending, storing and transporting a large-scale UAV cluster, comprising a vehicle body 1, a square cabin 2 installed on the vehicle body 1 and capable of opening and closing the top and sides, a second take-off and landing device 3 installed in the square cabin 2 and moving along the Z-axis direction, and a first take-off and landing device 4 installed in the square cabin 2 and slidingly cooperating with the square cabin 2 along the Y-axis direction; a partition 5 is arranged in the square cabin 2 to vertically divide the square cabin 2 into a first space 22 and a second space 21; the second space 21 is arranged on a side close to the top surface; the first space 22 is arranged on a side away from the top surface;

[0044] The partitions 5 are in two groups and are arranged in parallel along the X-axis direction. A second space 21 for installing the second landing device 3 is formed between the plane where the top of the partition 5 is located and the top cover 23; three groups of first spaces 22 for installing the first landing device 4 are formed between the two groups of partitions 5 and between the partitions 5 and the inner side of the cabin; the second space 21 is used for installing the second landing device 3, and the second landing device 3 can be one group, two groups or more groups. The first space 22 is three groups and is on the same plane; the first landing device 4 is located in the first space 22 and slides along the Y-axis direction. There are two groups of first landing devices 4 in each group of the first space 22 and they are arranged at equal intervals along the Z-axis direction; the second landing device 3 is located in the second space 21;

[0045] like Figure 1 , Fig.12 As shown, the second take-off and landing devices 3 in a group of second spaces 21 can be arranged according to the specifications of the drone, generally in two groups; in this way, a drone with a size larger than the maximum size of the drone that can be retracted by the first take-off and landing device 4 can be retracted on the second take-off and landing device 3;

[0046] In the utility model, two groups of partitions 5 are arranged in the square cabin 2 to divide the inner cavity of the square cabin 2 into a second space 21 and three groups of first spaces 22. The top of one group of second spaces 21 is connected to the top opening of the square cabin 2, and the side openings of the square cabin 2 of the three groups of first spaces 22 are connected. There are two groups of first take-off and landing devices 4 in each group of first spaces 22 and they are arranged vertically, and the distance between them is greater than the height of the drone along the Z-axis direction.

[0047] When retrieving the drone, first, the side and top surfaces of the cabin 2 are all opened; then, the first take-off and landing devices 4 are controlled to move along the Y-axis direction to expose all the first take-off and landing devices 4, and the two groups of first take-off and landing devices 4 in the same second space 21 slide in opposite directions along the Y-axis direction; for large drones, they are directly landed on the second take-off and landing devices 3 from the top surface, and then returned to their original positions and locked; for small drones, they are landed on the first take-off and landing devices 4, and then the drones are returned to their original positions and locked;

[0048] After the large drone is locked, the second take-off and landing device 3 moves downward along the Z-axis direction, thereby preventing the top of the large drone from being unable to enter the second space 21, resulting in the situation that the top surface cannot be closed after the large drone is retracted;

[0049] After the small drone is locked, the first take-off and landing device 4 is moved along the Y-axis direction so that the small drone is located in the first space 22;

[0050] In the utility model, by setting up the second space 21 and the first space 22, it can be suitable for the transmission and reception of drones with more specifications and sizes; by controlling the simultaneous unfolding of the top surface and the side surface, all drones can transmit and receive at the same time, and the efficiency will be greatly improved.

[0051] In some possible implementations, in order to effectively realize the sending and receiving of large drones, and to ensure that after the drone is retracted, there is no interference between the top of the drone and the top surface of the cabin 2, causing the top surface to be unable to close;

[0052] like Figure 3-Figure 7 As shown, the second take-off and landing device 3 includes a support platform 31 installed in the second space 21, a second homing device 32 installed on the support platform 31 and controlling the drone landing on the support platform 31 to return to a specified position, a lifting platform 33 installed on the support platform 31 and slidingly cooperated with the support platform 31 along the Z-axis direction, and a second locking device 34 used in cooperation with the lifting platform 33 and used to lock and fix the drone located on the lifting platform 33;

[0053] A cavity is provided on the support platform 31, and the lifting platform 33 is located in the cavity and moves along the Z-axis direction. After the landing gear of the large UAV is returned to the lifting platform 33, the landing gear is locked by the second locking device 34 to achieve the locking and fixing of the UAV. Then, the lifting platform 33 is controlled to move downward along the Z-axis direction so that the top of the UAV falls into the second space 21, and will not interfere with the closing when the top surface of the cabin 2 is closed; on the contrary, before the UAV takes off, the top surface of the cabin 2 is opened, the lifting platform 33 is raised along the Z-axis direction, and then the lock is released, and the UAV can take off.

[0054] In some possible implementations, when the drone lands on the support platform 31, its landing position is arbitrary, and for this purpose, it is necessary to control the drone to move in the X-axis and Y-axis directions through a second homing device 32 to return it to the lifting platform 33; this can be achieved through a device capable of linear movement in the prior art, such as an electric push rod, a screw and motor matching structure, and a hydraulic cylinder / cylinder linear telescopic drive structure.

[0055] Specifically, the second homing device 32 includes two groups of X-axis linear modules 321 installed on the support platform 31 and arranged in parallel along the X-axis, two groups of Y-axis linear modules 322 arranged in parallel along the Y-axis direction and installed on the two groups of X-axis modules, and push rods 323 respectively installed on the two groups of Y-axis linear modules 322 and moving along the Y-axis direction;

[0056] The two groups of X-axis linear modules 321 and the two groups of Y-axis linear modules 322 form a mounting cavity; the long directions of the two groups of push rods 323 are arranged along the X-axis direction and are located above the mounting cavity.

[0057] Two sets of X-axis linear modules 321 are installed on the support platform 31, and two sets of Y-axis linear modules 322 are installed on the two sets of X-axis linear modules 321. The two sets of X-axis linear modules 321 drive the two sets of Y-axis linear modules 322 to move closer to or farther from each other along the X-axis direction, so as to adjust the landing position of the UAV in the X-axis direction. Furthermore, push plates 324 are provided on the two sets of linear modules. When the Y-axis linear module 322 moves along the X-axis direction, it drives it to move and contact and abut against the landing gear of the UAV, so as to control it to return to its position in the X-axis direction.

[0058] Two sets of push rods 323 are arranged on two sets of Y-axis linear modules 322 and move respectively along the Y-axis direction under the control of the Y-axis linear modules 322; the long direction of the two sets of push rods 323 is arranged along the X-axis direction and cooperates with the two sets of push plates 324 to form a second chamber with a rectangular structure, and the two sets of push rods 323 are located on different sides; the landing gear of the UAV passes through the second chamber and is located on the supporting platform 31; the UAV is returned to the lifting platform 33 by the cooperation of the two sets of push plates 324 and the two sets of push rods 323;

[0059] In some possible implementations, in order to effectively realize the lifting and lowering of the lifting platform 33, thereby driving the drone to rise and fall, and preventing the top surface of the cabin 2 from being unable to close;

[0060] like Figure 5 As shown, the lifting platform 33 includes a support plate 331 located in the cavity and slidingly matched with the support platform 31 along the Z-axis direction, and a vertical lifting device 332 installed at the bottom of the support platform 31 and used to control the movement of the support plate 331 along the Z-axis direction;

[0061] The vertical lifting device 332 is composed of two groups and is symmetrically installed at the bottom of the support plate 331. The vertical lifting device 332 is provided with a transmission block connected to the bottom of the lifting platform 33. The transmission block will rise and fall vertically, thereby driving the lifting platform 33 to rise and fall vertically.

[0062] The vertical lifting device 332 is implemented by a device capable of realizing linear movement in the prior art, for example, it can be realized by using a linear module, an electric push rod 323, a hydraulic cylinder / cylinder linear telescopic mechanism, a lead screw and a motor; further, the vertical lifting device 332 is a linear module.

[0063] In some possible implementations, in order to effectively lock and fix the drone after it is returned to its original position;

[0064] like Figure 1 , Figure 5 , Figure 6 As shown, the second locking device 34 is composed of two groups and is symmetrically arranged, which includes a second locking motor 341 installed under the support plate 331, a second rotating shaft 342 connected to the output shaft of the second locking motor 341, and a second clamping claw 343 which is sleeved on the outside of the second rotating shaft 342 and rotates around the axis of the second rotating shaft 342 under the drive of the second locking motor 341; a second through groove 344 for one end of the second clamping claw 343 to pass through is provided on the support plate 331; one side of the second clamping claw 343 passing through the second through groove 344 cooperates with the support plate 331 to form a second clamping cavity.

[0065] The second through slot 344 is a U-shaped slot with its opening facing outward; the second locking motor 341 is installed at the bottom of the support plate 331, and the second rotating shaft 342 is arranged along the X-axis direction. The second clamping claw 343 is fixed on the second and under the rotation control of the second rotating shaft 342, one end of the second clamping claw 343 can pass through the second through slot 344 and be located above the support plate 331. At this time, it will cooperate with the support plate 331 to form a second clamping cavity to lock the landing gear located on the support plate 331.

[0066] In some possible implementations, such as Figure 1 , Figure 8-Figure 11 As shown, the first take-off and landing device 4 includes a support platform 41 located in the first space 22 and slidingly cooperating with the first space 22 along the Y-axis direction, a first homing device 42 installed on the support platform 41 and used to realize the homing action of the UAV, a first locking device 43 installed on the support platform 41 and locking and fixing the UAV after the UAV is returned to its position, and a Y-direction sliding mechanism located at the bottom of the mounting platform and used to control the support platform 41 to slide along the Y-axis direction.

[0067] When the UAV is being retrieved, the top and sides of the cabin 2 are opened, and the support platform 41 is extended from the side along the Y-axis direction under the drive of the Y-direction sliding mechanism; after reaching the designated position, the UAV lands on the support platform 41 after receiving the command, and the UAV is moved to the designated position by the first homing device 42, and then the landing gear of the UAV is locked and fixed to the support platform 41 by the first locking device 43, and then the support platform 41 returns to the initial position; the retrieval is completed; otherwise, the release is achieved.

[0068] The Y-direction sliding mechanism is mainly used to drive the support table 41 to slide along the Y-axis direction, and can adopt a mechanism capable of realizing linear drive in the prior art, such as a gear, a rack and a motor matching structure, a synchronous belt driving structure, etc.;

[0069] The utility model can effectively move the drone to a designated position through the first homing device 42 and the second homing device 32 to avoid interference with other drones, and then use the first locking device 43 and the second locking device 34 to lock and fix the drone to prevent it from moving without anyone in the transportation process.

[0070] In some possible implementations, in order to enable the drone located on the first take-off and landing device to be parked at a designated position of the support platform 41 as required;

[0071] The first homing device 42 includes two groups of first clamping plates 421 arranged on the support platform 41 and slidingly cooperated with the support platform 41 along the Y-axis direction, two groups of second clamping plates 422 arranged on the support platform 41 and slidingly cooperated with the support platform 41 along the X-axis direction, a Y-direction driving device 423 for driving the two groups of first clamping plates 421 to move closer to or away from each other, and an X-direction driving device 424 for driving the two groups of second clamping plates 422 to move closer to or away from each other; the two groups of first clamping plates 421 and the two groups of second clamping plates 422 cooperate with each other to form a clamping cavity for parking the drone; the two groups of first clamping plates 421 are located between the two groups of second clamping plates 422.

[0072] The two groups of first clamping plates 421 are parallel to each other, the two groups of second clamping plates 422 are parallel to each other, and the first clamping plates 421 and the second clamping plates 422 are perpendicular to each other; after the UAV lands on the support platform 41, the first clamping plates 421 are driven by the Y-axis driving device 423 to approach each other and abut against the landing gear of the UAV, and then the second clamping plates 422 are driven by the X-axis driving device 424 to approach each other, so that the area of ​​the clamping cavity formed is reduced, and when the first clamping plates 421 and the second clamping plates 422 are respectively in contact with the landing gear and move them to the specified position, the Y-axis driving device 423 and the X-axis driving device 424 stop driving; then the first locking device 43 is started to lock and fix the landing gear;

[0073] It should be noted that before the drone is retrieved, the distance between the two sets of first clamping plates 421 and the distance between the two sets of second clamping plates 422 are at the maximum, and the first clamping plates 421 and the second clamping plates 422 will be located at the edge of the support platform 41; in this way, no matter where the drone lands on the support platform 41, it can be returned to the designated position through the cooperation of the first clamping plates 421 and the second clamping plates 422;

[0074] The Y-direction driving device 423 comprises a Y-direction linear driving device 4231 installed at the bottom of the support platform 41 and connected to the first clamping plate 421, a Y-direction sliding groove 4232 arranged on the support platform 41 and slidably matched with the first clamping plate 421, and a Y-direction transmission member 4233 located in the Y-direction sliding groove 4232 and slidably matched with the Y-direction sliding groove 4232; the long direction of the Y-direction sliding groove 4232 is parallel to the long direction of the second clamping plate 422 and is located between the two groups of second clamping plates 422; the Y-direction transmission member 4233 is respectively connected to the bottom of the first clamping plate 421 and the Y-direction linear driving device 4231;

[0075] Specifically, the Y-direction linear drive device 4231 is installed at the bottom of the support platform 41, and is connected to the first clamping plate 421 through the Y-direction transmission member 4233 located in the Y-direction slide groove 4232; the Y-direction linear drive device 4231 controls the Y-direction transmission member 4233 to perform linear motion in the Y-direction slide groove 4232, thereby driving the first clamping plate 421 to perform linear motion along the long direction of the Y-direction slide groove 4232;

[0076] The X-direction drive device 424 has the same structure as the Y-direction drive device 423. The X-direction drive device 424 includes an X-direction linear drive device, an X-direction slide groove 4242 disposed on the support table 41 and slidably matched with the second clamping plate 422, and an X-direction transmission member disposed in the X-direction slide groove 4242 and slidably matched with the X-direction slide groove 4242; the long direction of the X-direction slide groove 4242 is parallel to the long direction of the first clamping plate 421; the X-direction transmission member is respectively connected to the bottom of the second clamping plate 422 and the X-direction linear drive device; the X-direction drive device 424 and the Y-direction drive device 423 are only different in the setting direction, and their working principles are not described in detail here;

[0077] The Y-axis linear drive device 4231 and the X-axis linear drive device can be implemented as linear drive mechanisms by the electric push rod 323, a linear module, a hydraulic cylinder / cylinder linear telescopic mechanism, a lead screw and a motor; when the Y-axis linear drive device 4231 adopts the cooperation of a lead screw and a drive motor, the Y-axis transmission member 4233 is a lead screw nut; a slideway is also provided at the bottom of the support platform 41, and a slider is provided on the slideway, which will be connected to the lead screw nut, and the cooperation between the slideway and the slider is used to limit the rotation of the lead screw nut along the axial direction of the lead screw, so that it can only make linear motion.

[0078] In some possible implementations, such as Figure 8 As shown, the first locking device 43 is located in the clamping cavity, and includes two sets of locking members respectively matched with the two sets of first clamping plates 421; the locking members are arranged in a one-to-one correspondence with the first clamping plates 421 and form a locking cavity for locking the landing gear of the UAV;

[0079] After the UAV returns to the specified position, the locking piece is activated and contacts and abuts against the side of the landing gear away from the first clamping plate 421. Since the other side of the landing gear is also in contact and abuts against the first clamping plate 421, with the cooperation of the first clamping plate 421 and the locking piece, the landing gear will be unable to move on the support platform 41, thereby achieving locking and fixation.

[0080] like Fig.10 As shown, the locking member includes a first locking motor 431 installed at the bottom of the support platform 41, a first rotating shaft 432 connected to the output shaft of the first locking motor 431, and a first claw 433 which is sleeved on the outside of the first rotating shaft 432 and rotates around the axis of the first rotating shaft 432 under the drive of the first locking motor 431; a first through groove 434 is provided on the support platform 41 for one end of the first claw 433 to pass through.

[0081] There are two groups of first claws 433 arranged on each group of first rotating shafts 432. When there are two groups of first claws 433, there will also be two groups of first through slots 434 for the two groups of claws to move respectively. Specifically, the first rotating shaft 432 drives the first claws 433 around the axis of the first rotating shaft 432 under the drive of the first locking motor 431, and one end of the first claws 433 passes through the first through slot 434 and rotates from the side of the support platform 41 close to the landing gear, and contacts with the landing gear to cooperate with the corresponding first clamping plate 421 to achieve locking and fixing of the landing gear. The locking member has the same structure as the second homing device 32.

[0082] like Fig.11 As shown, there are two sets of landing gears and they are parallel to the first clamping plate 421 after returning to their original positions. At this time, the two sets of locking members are used to cooperate with the two sets of landing gears.

[0083] In some possible implementations, such as Figure 1 , Fig.12 As shown, the square cabin 2 includes a cabin body with an inner cavity, two groups of top covers 23 symmetrically arranged on the cabin body along the Y-axis direction and sliding along the X-axis direction, two groups of side panels 24 symmetrically arranged on the cabin body along the X-axis direction and hinged to the cabin body, a cabin top opening and closing mechanism 25 transmission-connected to the top cover 23 and used to control the sliding of the top cover 23 on the cabin body, and a cabin side opening and closing mechanism 26 transmission-connected to the side panels 24 and installed on the cabin body; the partition 5 is located in the inner cavity and is perpendicular to the side panels 24 and the top cover 23.

[0084] The top cover 23 is provided in two groups and slides with the cabin body along the X-axis direction; the cabin top opening and closing mechanism 25 is provided in two groups and corresponds to the top cover 23 one by one; the side panels 24 are provided in two groups and are symmetrically provided along the X-axis direction, and the two groups of side panels 24 are provided on both sides of the cabin body along the X-axis direction and are hingedly provided with the cabin body; the cabin side opening and closing mechanism 26 is provided in one-to-one correspondence with the two groups of side panels 24;

[0085] Specifically, the cabin body includes a bottom plate, two groups of end plates installed on the bottom plate and arranged along the X-axis direction, and two groups of enclosure plates arranged between the two groups of end plates and respectively connected to the two groups of end plates; the two groups of end plates, the two groups of enclosure plates, and the bottom plate cooperate with each other to form an inner cavity; the top surface of the cabin body is formed by the enclosure plate and the top of the bottom plate to form a top opening connected to the inner cavity, and the top cover 23 can open or close the top opening at the cabin top opening and closing mechanism 25; the bottom of each group of enclosure plates, the bottom plate, and the two groups of end plates cooperate to form a side opening connected to the inner cavity, and the length of the side plate 24 along the X-axis direction is consistent with the length of the enclosure plate and is located below the enclosure plate, which is used to open or close the side opening; the drone lifting device will be installed in the inner cavity to realize the sending and receiving of the drone cluster;

[0086] Specifically, Figure 1 As shown, the bottom of the side panel 24 can be hinged with the bottom panel through a hinge, so that under the drive of the cabin side opening and closing mechanism 26, the side panel 24 rotates around the X-axis direction and outwards to open the side of the cabin, and vice versa to close it;

[0087] Compared with the prior art, the top cover 23 of the utility model is divided into two groups and is arranged to slide in a split manner. The two groups of top covers 23 are controlled to move away from each other along the X-axis direction by two groups of cabin top opening and closing mechanisms 25, so that the cabin top can be opened as much as possible, so that the use of the cabin space can be effectively improved, and the lifting and lowering of the drone is convenient; when closing, the two groups of top covers 23 are controlled to move closer to each other by the cabin top opening and closing mechanisms 25, and the two sides approaching each other are in contact with each other;

[0088] By controlling the opening and closing of the side panels 24 and the top cover 23, and cooperating with the drone lifting device disposed in the safety chamber, the drone can take off and land at the top and the side at the same time; the utilization rate of the internal space of the cabin is greatly improved, so that the cabin with the same space can accommodate more drones;

[0089] By controlling the top cover 23 to slide in an open manner along the X-axis direction, the floor space occupied when the top opening is opened can be reduced, making it applicable to a wider range of scenarios.

[0090] The present invention is not limited to the above-mentioned specific implementation modes, but extends to any new features or any new combination disclosed in this specification, as well as any new method or process steps or any new combination disclosed.

Claims

1. A highly integrated intelligent vehicle-mounted device for sending, receiving, storing and transporting large drone clusters, characterized in that: The vehicle comprises a vehicle body (1), a cabin (2) installed on the vehicle body (1) and capable of opening and closing the top and sides, a second lift-off and landing device (3) installed in the cabin (2) and movable along the Z-axis direction, and a first lift-off and landing device (4) installed in the cabin (2) and slidingly cooperating with the cabin (2) along the Y-axis direction; A partition (5) is arranged in the square cabin (2) to vertically divide the square cabin (2) into a first space (22) and a second space (21); the second space (21) is arranged on a side close to the top surface; and the first space (22) is arranged on a side away from the top surface; The first lifting and lowering device (4) is located in the first space (22) and is slidably matched along the Y-axis direction. There are two groups of first lifting and lowering devices (4) in each group of the first space (22) and they are arranged at intervals in the vertical direction. The second lifting and lowering device (3) is located in the second space (21).

2. According to claim 1, a highly integrated intelligent vehicle-mounted device for sending, receiving, storing and transporting a large-scale UAV cluster is characterized in that: The partitions (5) are in two groups and are arranged in parallel along the X-axis direction; a second space (21) for installing a second take-off and landing device (3) is formed between the plane where the top of the partition (5) is located and the top cover (23); three groups of first spaces (22) for installing a first take-off and landing device (4) are formed between the two groups of partitions (5) and between the partitions (5) and the same cabin.

3. According to claim 1, a highly integrated intelligent vehicle-mounted device for sending, receiving, storing and transporting a large-scale UAV cluster is characterized in that: The second take-off and landing device (3) comprises a support platform (31) installed in the second space (21), a second homing device (32) installed on the support platform (31) and controlling the homing of the UAV, a lifting platform (33) installed on the support platform (31) and slidingly cooperating with the support platform (31) along the Z-axis direction, and a second locking device (34) used in conjunction with the lifting platform (33) and used to lock and fix the UAV located on the lifting platform (33); A cavity is provided on the supporting platform (31), and the lifting platform (33) is located in the cavity.

4. According to claim 3, a highly integrated intelligent vehicle-mounted device for sending, receiving, storing and transporting a large-scale UAV cluster is characterized in that: The second homing device (32) comprises two groups of X-axis linear modules (321) installed on the support platform (31) and arranged in parallel along the X-axis, two groups of Y-axis linear modules (322) arranged in parallel along the Y-axis direction and installed on the two groups of X-axis modules, and push rods (323) respectively installed on the two groups of Y-axis linear modules (322) and moving along the Y-axis direction; Two groups of X-axis linear modules (321) and two groups of Y-axis linear modules (322) form a mounting cavity; the long directions of the two groups of push rods (323) are arranged along the X-axis direction and are located above the mounting cavity.

5. According to claim 3, a highly integrated intelligent vehicle-mounted device for sending, receiving, storing and transporting a large-scale UAV cluster is characterized in that: The lifting platform (33) comprises a support plate (331) located in the cavity and slidably matched with the support platform (31) along the Z-axis direction, and a vertical lifting device (332) installed at the bottom of the support platform (31) and used to control the movement of the support plate (331) along the Z-axis direction.

6. A highly integrated intelligent vehicle-mounted device for sending, receiving, storing and transporting a large-scale UAV cluster according to claim 5, characterized in that: The second locking device (34) is composed of two groups and is symmetrically arranged, and includes a second locking motor (341) installed below the support plate (331), a second rotating shaft (342) connected to the output shaft of the second locking motor (341), a second clamping claw (343) sleeved on the outside of the second rotating shaft (342) and rotating around the axis of the second rotating shaft (342) under the drive of the second locking motor (341), and a second through groove (344) arranged on the support plate (331) and used for one end of the second clamping claw (343) to pass through; one side of the second clamping claw (343) passing through the second through groove (344) cooperates with the support plate (331) to form a second clamping cavity.

7. A highly integrated intelligent vehicle-mounted device for sending, receiving, storing and transporting a large-scale UAV cluster according to claim 6, characterized in that: The first take-off and landing device (4) comprises a support platform (41) located in the first space (22) and slidably matched with the support platform (41) located in the first space (22) along the Y-axis direction, a first homing device (42) installed on the support platform (41) and used to realize a homing action for the drone, a first locking device (43) installed on the support platform (41) and used to lock and fix the drone after the drone has been returned to its position, and a Y-direction sliding mechanism located at the bottom of the mounting platform and used to control the support platform (41) to slide along the Y-axis direction.

8. A highly integrated intelligent vehicle-mounted device for sending, receiving, storing and transporting a large-scale UAV cluster according to claim 7, characterized in that: The first homing device (42) comprises two groups of first clamping plates (421) arranged on the support platform (41) and slidingly matched with the support platform (41) along the Y-axis direction, two groups of second clamping plates (422) arranged on the support platform (41) and slidingly matched with the support platform (41) along the X-axis direction, a Y-direction driving device (423) for driving the two groups of first clamping plates (421) to move closer to or away from each other, and an X-direction driving device (424) for driving the two groups of second clamping plates (422) to move closer to or away from each other; the two groups of first clamping plates (421) and the two groups of second clamping plates (422) cooperate with each other to form a clamping cavity for parking the drone; the two groups of first clamping plates (421) are located between the two groups of second clamping plates (422).

9. A highly integrated intelligent vehicle-mounted device for sending, receiving, storing and transporting a large-scale UAV cluster according to claim 7, characterized in that: The first locking device (43) is located in the clamping cavity and comprises two groups of locking members respectively matched with the two groups of first clamping plates (421); the locking members and the first clamping plates (421) are arranged in a one-to-one correspondence and form a locking cavity for locking the landing gear of the UAV; The locking member comprises a first locking motor (431) mounted on the bottom of the support platform (41), a first rotating shaft (432) connected to the output shaft of the first locking motor (431), a first clamping claw (433) sleeved on the outside of the first rotating shaft (432) and driven by the first locking motor (431) to rotate around the axis of the first rotating shaft (432), and a first through slot (434) arranged on the first support platform (41) and used for one end of the first clamping claw (433) to pass through.

10. A highly integrated intelligent vehicle-mounted device for sending, receiving, storing and transporting a large-scale UAV cluster according to any one of claims 1 to 9, characterized in that: The square cabin (2) comprises a cabin body with an inner cavity, two sets of top covers (23) symmetrically arranged on the cabin body along the Y-axis direction and sliding along the X-axis direction, two sets of side panels (24) symmetrically arranged on the cabin body along the X-axis direction and hingedly matched with the cabin body, a cabin top opening and closing mechanism that is transmission-connected to the top cover (23) and used to control the top cover (23) to slide on the cabin body, and a cabin side opening and closing mechanism that is transmission-connected to the side panels (24) and installed on the cabin body; the partition plate (5) is located in the inner cavity and is perpendicular to the side panels (24) and the top cover (23).

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