Unmanned aerial vehicle take-off and landing device and unmanned aerial vehicle cluster transmitting and receiving device

Abstract

The utility model relates to the technical field of unmanned aerial vehicle recovery, and particularly discloses an unmanned aerial vehicle take-off and landing device and an unmanned aerial vehicle cluster receiving and transmitting device. Comprising a supporting table which is mounted in a vehicle-mounted square cabin and is in sliding fit with the vehicle-mounted square cabin, a homing device which is mounted on the supporting table and is used for realizing homing action on the unmanned aerial vehicle, and a locking device which is mounted on the supporting table and is used for locking and fixing the unmanned aerial vehicle after the unmanned aerial vehicle is homed. According to the unmanned aerial vehicle take-off and landing device, the unmanned aerial vehicle can be effectively returned according to a designated position after being parked and is locked and fixed after being returned, and the unmanned aerial vehicle is prevented from being damaged due to sliding collision in the transportation process; according to the unmanned aerial vehicle cluster receiving and transmitting device, the side face and the top face of the vehicle-mounted square cabin are opened, so that the supporting platform can move towards the side face of the vehicle-mounted square cabin; therefore, all the unmanned aerial vehicles can take off or stop at one time; through movement of the unmanned aerial vehicle take-off and landing device in the vehicle-mounted square cabin, the utilization rate of the space in the vehicle-mounted square cabin is greatly increased.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle (UAV) recovery, and more specifically, to an unmanned aerial vehicle (UAV) take-off and landing device and a UAV cluster transceiver device. Background Art

[0002] The UAV cluster transceiver device in the prior art has the following problems when used:

[0003] Drone take-off and landing are only carried out in the space above the transceiver device, or only one side of the device is used for drone take-off and landing. The device can accommodate a relatively small number of drones, and the space utilization rate of the device is relatively low.

[0004] The compactness of the device is low. Due to the low space utilization of the above-mentioned device, when facing the demand of drone clusters, the device space is relatively large and the compactness of the device structure is low. The maximum number of drones taking off and landing in a single batch is relatively small. Utility Model Content

[0005] The technical problem to be solved by the utility model is to provide a UAV take-off and landing device and a UAV cluster transceiver device;

[0006] The solution adopted by the utility model to solve the technical problem is:

[0007] A UAV take-off and landing device comprises a support platform installed in a vehicle-mounted cabin and slidingly matched with the vehicle-mounted cabin, a homing device installed on the support platform and used to realize the homing action of the UAV, and a locking device installed on the support platform and locking and fixing the UAV after the UAV is returned to its position.

[0008] In some possible implementations,

[0009] The homing device includes two groups of first clamping plates arranged on the support platform and slidingly matched with the support platform, two groups of second clamping plates arranged on the support platform and slidingly matched with the support platform, a transverse driving device for driving the two groups of first clamping plates to move closer to or away from each other, and a longitudinal 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.

[0010] In some possible implementations,

[0011] The transverse drive device has the same mechanism as the longitudinal drive device;

[0012] The transverse driving device comprises a transverse linear driving device installed on the bottom of the support platform and connected to the first clamping plate, a transverse slide groove arranged on the support platform and slidably matched with the first clamping plate, and a transverse transmission member located in the transverse slide groove and slidably matched with the transverse slide groove; the long direction of the transverse slide groove is parallel to the long direction of the second clamping plate and is located between the two groups of second clamping plates; the transverse transmission member is respectively connected to the bottom of the first clamping plate and the transverse linear driving device;

[0013] The longitudinal drive device includes a longitudinal linear drive device installed on the bottom of the support platform and connected to the second clamping plate, a longitudinal slide groove arranged on the support platform and slidingly matched with the second clamping plate, and a longitudinal transmission member located in the longitudinal slide groove and slidingly matched with the longitudinal slide groove; the long direction of the longitudinal slide groove is parallel to the long direction of the first clamping plate; the longitudinal transmission member is respectively connected to the bottom of the second clamping plate and the longitudinal linear drive device.

[0014] In some possible implementations,

[0015] The transverse driving device also includes a first movable plate connected to the bottom of the transverse transmission member and sliding along the long direction of the second clamping plate, a first telescopic scissors frame installed at the bottom of the first movable plate and connected to the first clamping plate at one end and telescopic along the long direction of the transverse slide groove, and the other end of the first telescopic scissors frame is connected to the bottom of the support platform;

[0016] The longitudinal driving device also includes a second movable plate connected to the bottom of the longitudinal transmission member and sliding along the long direction of the first clamping plate, a second telescopic scissors frame installed at the bottom of the second movable plate and connected to the second clamping plate at one end and telescopic along the long direction of the longitudinal slide groove, and the other end of the second telescopic scissors frame is connected to the bottom of the support platform.

[0017] In some possible implementations,

[0018] The locking device is located in the clamping cavity and includes two groups of locking pieces respectively matched with two groups of first clamping plates; the locking pieces 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.

[0019] In some possible implementations,

[0020] The locking member includes a locking motor installed at the bottom of the support platform, a rotating shaft connected to the output shaft of the locking motor and arranged along the long direction of the longitudinal slide groove, a claw sleeved on the outside of the rotating shaft and rotating around the axis of the rotating shaft under the drive of the locking motor, and a through groove arranged on the support platform for one end of the claw to pass through.

[0021] In some possible implementations,

[0022] A sliding mechanism is provided at the bottom of the support platform to control the support platform to slide along the longitudinal direction of the transverse slide groove and to cooperate with the vehicle-mounted shelter;

[0023] The sliding mechanism includes a rack arranged along the long direction of the transverse slide groove and installed at the bottom of the support platform, a gear matched with the rack, a sliding drive motor for driving the gear transmission, a guide rail arranged on the vehicle-mounted cabin and used to guide the moving direction of the support platform, and a guide groove arranged on the outside of the support platform and slidably matched with the guide rail.

[0024] A drone cluster transceiver comprises a vehicle body, a vehicle-mounted cabin installed on the vehicle body, a plurality of drone take-off and landing devices installed in the vehicle-mounted cabin and as described above; a plurality of partitions arranged in the vehicle-mounted cabin at equal intervals along the length direction of the vehicle body; and an installation space for installing the drone take-off and landing device is formed between two adjacent sets of partitions.

[0025] In some possible implementations,

[0026] Multiple sets of drone take-off and landing devices are arranged vertically in each installation space, and the vertical distance between two adjacent sets of drone take-off and landing devices is greater than the vertical height of the drone;

[0027] A mounting frame for mounting on the sliding mechanism and corresponding to the sliding mechanism is arranged between the two groups of partitions; the guide rails are in two groups and are arranged on the side where the partitions are close to each other.

[0028] In some possible implementations,

[0029] The vehicle-mounted square cabin includes a bottom plate, end plates arranged on the bottom plate and at both ends along the length direction of the vehicle body, two groups of doors symmetrically arranged along the length direction of the vehicle body and cooperating with the bottom plate and the end plates to form a sending and receiving compartment, and a multi-link drive mechanism hinged to the end plates and the doors at both ends and used for opening and closing the sending and receiving compartment; when the door is fully opened, the bottom plate is exposed and the top surface of the door is located below the partition; the partition is installed on the bottom plate.

[0030] Compared with the prior art, the utility model has the following beneficial effects:

[0031] The drone take-off and landing device of the utility model can effectively realize the return of the drone to the designated position after docking, and lock and fix it after returning to the position, so as to avoid the drone from slipping and colliding and being damaged during transportation;

[0032] The UAV cluster transceiver device in the utility model opens the side and top surfaces of the vehicle-mounted cabin so that the devices installed on the support platform can move toward the side of the vehicle-mounted cabin; thereby, all the UAVs can complete takeoff or docking at one time; and through the movement of the UAV take-off and landing device in the vehicle-mounted cabin, the utilization rate of the space in the vehicle-mounted cabin is greatly improved, and the number of UAVs accommodated is greatly increased. BRIEF DESCRIPTION OF THE DRAWINGS

[0033] Figure 1 This is a schematic diagram of the three-dimensional structure of the UAV cluster transceiver in the utility model;

[0034] Figure 2 This is a schematic diagram of the structure of the UAV cluster transceiver device in the utility model during the UAV transportation process;

[0035] Figure 3 This is a schematic diagram of the structure of the take-off and landing device of the UAV in the utility model;

[0036] Figure 4 It is a structural schematic diagram of the transverse driving device and the first clamping plate in the utility model;

[0037] Figure 5 It is a structural schematic diagram of a transverse driving device with a first telescopic scissor frame in the utility model;

[0038] Figure 6 It is a structural schematic diagram of a longitudinal drive device with a second telescopic scissor frame in the utility model;

[0039] Figure 7 It is a structural schematic diagram of the locking device in the utility model;

[0040] Figure 8 This is a structural schematic diagram of the locking device and the first clamping plate in the utility model cooperating to lock the landing gear of the UAV;

[0041] Fig. 9 For this utility model Figure 3 The enlarged view of point A in the middle;

[0042] Among them: 1, support platform; 2, homing device; 21, first clamping plate; 22, second clamping plate; 23, horizontal driving device; 231, horizontal linear driving device; 232, horizontal slide; 233, horizontal transmission member; 234, first moving plate; 235, first telescopic scissors frame; 24, longitudinal driving device; 241, longitudinal linear driving device; 242, longitudinal slide; 243, longitudinal transmission member; 244, second moving plate; 245, first telescopic scissors frame; 246, longitudinal driving device; 247, longitudinal linear driving device; 248, longitudinal slide; 249, longitudinal transmission member; 250, second moving plate; 251, first telescopic scissors frame; 252, longitudinal driving device; 253, longitudinal transmission member; 254, second moving plate; 255, first telescopic scissors frame; 256, longitudinal driving device; 257, longitudinal linear driving device; 258, longitudinal slide; 259, longitudinal transmission member; 260, second moving plate; 261, longitudinal linear driving device; 262, longitudinal slide; 263, longitudinal transmission member; 264, second moving plate; 265, first telescopic scissors frame; 266, longitudinal driving device; 267, longitudinal linear driving device; 268, longitudinal slide; 269, longitudinal transmission member; 270, second moving plate; 271, first telescopic scissors frame; 272, longitudinal 2. Telescopic scissor frames; 3. Locking device; 31. Locking motor; 32. Rotating shaft; 33. Clamping claw; 34. Through slot; 4. Sliding mechanism; 41. Rack; 42. Sliding drive motor; 43. Gear; 44. Guide rail; 45. Transmission shaft; 46. Commutator; 5. Vehicle-mounted cabin; 50. Partition; 51. Bottom plate; 52. End plate; 53. Hatch door; 531. Top plate; 532. Side plate; 533. End mold; 54. Multi-link drive mechanism. DETAILED DESCRIPTION

[0043] 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.

[0044] The utility model is described in detail below.

[0045] Embodiment 1:

[0046] like Figure 1-Figure 8 As shown, a UAV take-off and landing device includes a support platform 1 installed in a vehicle-mounted cabin 5 and slidingly matched with the vehicle-mounted cabin 5, a homing device 2 installed on the support platform 1 and used to realize the homing action of the UAV, and a locking device 3 installed on the support platform 1 and used to lock and fix the UAV after the UAV is returned to its position.

[0047] When the UAV is to be recovered, the vehicle-mounted cabin 5 is opened and the support platform 1 is extended; after receiving the command, the UAV lands on the support platform 1, the UAV is moved to the designated position by the homing device 2, and then the landing gear of the UAV is locked and fixed to the support platform 1 by the locking device 3, and then the support platform 1 returns to the initial position; the recovery is completed; otherwise, the release is achieved.

[0048] The homing device 2 can effectively move the drone to a designated location to avoid interference with other drones, and then the locking device 3 is used to lock and fix it to prevent it from moving when no one is there during transportation.

[0049] In some possible implementations, in order to enable the drone to be parked at a designated position of the support platform 1 as required;

[0050] The homing device 2 includes two groups of first clamps 21 arranged on the support platform 1 and slidingly matched with the support platform 1, two groups of second clamps 22 arranged on the support platform 1 and slidingly matched with the support platform 1, a transverse driving device 23 for driving the two groups of first clamps 21 to move closer to or away from each other, and a longitudinal driving device 24 for driving the two groups of second clamps 22 to move closer to or away from each other; the two groups of first clamps 21 and the two groups of second clamps 22 cooperate with each other to form a clamping cavity for parking the drone; the two groups of first clamps 21 are located between the two groups of second clamps 22.

[0051] The two groups of first clamping plates 21 are parallel to each other, the two groups of second clamping plates 22 are parallel to each other, and the first clamping plates 21 and the second clamping plates 22 are perpendicular to each other; after the UAV lands on the support platform 1, the first clamping plates 21 are driven by the transverse driving device 23 to approach each other and abut against the landing gear of the UAV, and then the second clamping plates 22 are driven by the longitudinal driving device 24 to approach each other, so that the area of ​​the formed clamping cavity is reduced, and when the first clamping plates 21 and the second clamping plates 22 are respectively in contact with the landing gear and move them to the specified position, the transverse driving device 23 and the longitudinal driving device 24 stop driving; then the locking device 3 is started to lock and fix the landing gear;

[0052] It should be noted that before the drone is retracted, the distance between the two sets of first clamping plates 21 and the distance between the two sets of second clamping plates 22 are at the maximum, and the first clamping plates 21 and the second clamping plates 22 will be located at the edge of the support platform 1; in this way, no matter where the drone lands on the support platform 1, it can be returned to the designated position through the cooperation of the first clamping plates 21 and the second clamping plates 22;

[0053] In some possible implementations, in order to effectively realize the movement of the first clamping plate 21 and the second clamping plate 22, and then realize the return of the drone;

[0054] The transverse drive device 23 has the same structure as the longitudinal drive device 24, but differs in the direction of setting;

[0055] The transverse driving device 23 includes a transverse linear driving device 231 installed at the bottom of the support platform 1 and connected to the first clamping plate 21, a transverse sliding groove 232 arranged on the support platform 1 and slidably matched with the first clamping plate 21, and a transverse transmission member 233 located in the transverse sliding groove 232 and slidably matched with the transverse sliding groove 232; the long direction of the transverse sliding groove 232 is parallel to the long direction of the second clamping plate 22 and is located between the two groups of second clamping plates 22; the transverse transmission member 233 is respectively connected to the bottom of the first clamping plate 21 and the transverse linear driving device 231;

[0056] Specifically, the transverse linear drive device 231 is installed at the bottom of the support platform 1, and is connected to the first clamping plate 21 through a transverse transmission member 233 located in the transverse slide groove 232; the transverse linear drive device 231 controls the transverse transmission member 233 to perform linear motion in the transverse slide groove 232, thereby driving the first clamping plate 21 to perform linear motion along the long direction of the transverse slide groove 232;

[0057] The two groups of first clamping plates 21 cooperate with each other through two groups of transverse linear driving devices 231, so as to move closer to or farther from each other;

[0058] The longitudinal drive device 24 comprises a longitudinal linear drive device 241 installed at the bottom of the support platform 1 and connected to the second clamping plate 22, a longitudinal slide groove 242 provided on the support platform 1 and slidably matched with the second clamping plate 22, and a longitudinal transmission member 243 located in the longitudinal slide groove 242 and slidably matched with the longitudinal slide groove 242; the long direction of the longitudinal slide groove 242 is parallel to the long direction of the first clamping plate 21; the longitudinal transmission member 243 is respectively connected to the bottom of the second clamping plate 22 and the longitudinal linear drive device 241;

[0059] Specifically, the longitudinal linear drive device 241 is also installed at the bottom of the support platform 1, and is connected to the second clamping plate 22 through a longitudinal transmission member 243 located in the longitudinal slide groove 242; the longitudinal linear drive device 241 controls the longitudinal transmission member 243 to perform linear motion in the longitudinal slide groove 242, thereby driving the second clamping plate 22 to perform linear motion along the long direction of the longitudinal slide groove 242;

[0060] Preferably, the length of the second clamping plate 22 is greater than the length of the second clamping plate 22; after the drone lands on the support platform 1, the second clamping plate 22 is first started, and the two groups of second clamping plates 22 approach each other, driving the drone in contact with a certain group of second clamping plates 22 to move along the length direction of the transverse slide groove 232. When the two ends of the drone landing gear are respectively in contact with the two groups of second clamping plates 22, the first clamping plate 21 is started, and the two groups of first clamping plates 21 approach each other and control the drone to move along the length direction of the transverse slide groove 232. When the two sides of the landing gear are respectively in contact with the two groups of first clamping plates 21, the drone returns to the designated position.

[0061] It should be noted that: the horizontal linear drive device 231 and the longitudinal linear drive device 241 can realize linear motion through the cooperation of the electric push rod, cylinder, hydraulic cylinder, screw and drive motor in the prior art; when the horizontal linear drive device 231 and the longitudinal linear drive device 241 both adopt the cooperation of the screw and the drive motor, the horizontal transmission member 233 and the longitudinal transmission member 243 will be the screw nut; a slideway is also provided at the bottom of the support platform 1, and a slider is provided on the slideway, and the slider will be connected to the screw nut, and the cooperation between the slideway and the slider is used to limit the rotation of the screw nut along the axial direction of the screw, so that it can only make linear motion.

[0062] In some possible implementations, in order to effectively increase the moving stroke of the transverse driving device 23 and the longitudinal driving device 24, the first clamping plate 21 and the second clamping plate 22 can have a larger stroke;

[0063] The transverse driving device 23 also includes a first movable plate 234 connected to the bottom of the transverse transmission member 233 and sliding along the long direction of the second clamping plate 22, a first telescopic scissor frame 235 installed at the bottom of the first movable plate 234 and connected to the first clamping plate 21 at one end and telescopic along the long direction of the transverse slide 232, and the other end of the first telescopic scissor frame 235 is hinged to the bottom of the support platform 1; the first movable plate 234 and the transverse transmission member 233 are integrally formed;

[0064] The first movable plate 234 is connected to the connection point of the two sets of hinged arms of the first telescopic scissor frame 235 and rotates together. Driven by the transverse transmission member 233, the first movable plate 234 moves along the long direction of the second clamping plate 22, so that the angle formed between the hinged arms of the first telescopic scissor frame 235 is deformed, so that the first telescopic scissor frame 235 is extended or shortened, so that the first clamping plates 21 are moved closer or farther away from each other;

[0065] Specifically, Figure 5 As shown, the matching structure of the lead screw and the motor of the transverse linear drive device 231 includes a linear drive motor, a lead screw connected to the output shaft of the linear drive motor and arranged along the long direction of the transverse slide groove 232, and a transverse transmission member 233 sleeved on the outside of the lead screw and screwed to the lead screw; the first movable plate 234 is installed under the transverse transmission member 233 and is rotatably connected to the first telescopic scissor frame 235;

[0066] When the transverse transmission member 233 moves away from the first clamping plate 21, the first telescopic scissor frame 235 is shortened, and the two sets of first clamping plates 21 move away from each other.

[0067] The longitudinal driving device 24 also includes a second movable plate 244 connected to the bottom of the longitudinal transmission member 243 and sliding along the long direction of the first clamping plate 21, a second telescopic scissor frame 245 installed at the bottom of the second movable plate 244 and connected to the second clamping plate 22 at one end and telescopic along the long direction of the longitudinal slide 242, and the other end of the second telescopic scissor frame 245 is hinged to the bottom of the support platform 1;

[0068] The longitudinal drive device 24 is the same as the transverse drive device 23, and its specific working principle will not be described in detail here; Figure 6 As shown, since the second clamping plate 22 is relatively long, the second telescopic scissor frame 245 can be arranged in multiple groups along the length of the second clamping plate 22 and respectively connected and matched with the second movable plate 244, so that the movement of the second clamping plate 22 is more stable;

[0069] The first telescopic scissors frame 235 and the second telescopic scissors frame 245 are prior art, and their specific structures are not described in detail here.

[0070] In some possible implementations, in order to effectively lock the landing gear through the cooperation between the first clamping plate 21 and the locking device 3, the UAV is locked and fixed;

[0071] like Figure 7 , Figure 8 As shown, the locking device 3 is located in the clamping cavity, and includes two sets of locking members respectively matched with two sets of first clamping plates 21; the locking members are arranged in a one-to-one correspondence with the first clamping plates 21 and form a locking cavity for locking the landing gear of the UAV;

[0072] After the UAV returns to the specified position, the locking member is activated and contacts and abuts against the side of the landing gear away from the first clamping plate 21. Since the other side of the landing gear is also in contact and abuts against the first clamping plate 21, with the cooperation of the first clamping plate 21 and the locking member, the landing gear will be unable to move on the support platform 1, thereby achieving locking and fixation.

[0073] In some possible implementations, in order to effectively control the locking member, the landing gear is used to lock and fix the UAV only after the UAV is returned to the designated position;

[0074] The locking member includes a locking motor 31 installed at the bottom of the support platform 1, a rotating shaft 32 connected to the output shaft of the locking motor 31 and arranged along the long direction of the longitudinal slide groove 242, a claw 33 which is sleeved on the outside of the rotating shaft 32 and rotates around the axis of the rotating shaft 32 under the drive of the locking motor 31, and a through groove 34 arranged on the support platform 1 and used for one end of the claw 33 to pass through.

[0075] Furthermore, there are two groups of claws 33 provided on each group of rotating shafts 32. When there are two groups of claws 33, there will also be two groups of through slots 34 for the two groups of claws 33 to move respectively. Specifically, the rotating shaft 32 drives the claws 33 around the axis of the rotating shaft 32 under the drive of the locking motor 31, and one end of the claws 33 passes through the through slot 34 and rotates from the side of the support platform 1 close to the landing gear, and contacts with the corresponding first clamping plate 21 of the landing gear to achieve locking and fixing of the landing gear.

[0076] like Figure 8 As shown, there are two sets of landing gears and they are parallel to the first clamping plate 21 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.

[0077] In some possible implementations, in order to effectively achieve the sliding cooperation between the support platform 1 and the vehicle-mounted shelter 5;

[0078] A sliding mechanism 4 is provided at the bottom of the support platform 1 for controlling the support platform 1 to slide along the longitudinal direction of the transverse slide groove 232 and to cooperate with the vehicle-mounted shelter 5;

[0079] The sliding mechanism 4 includes a rack 41 arranged along the length direction of the transverse slide groove 232 and installed at the bottom of the support platform 1, a gear 43 matched with the rack 41, a sliding drive motor 42 for driving the gear 43, a guide rail 44 arranged on the vehicle-mounted cabin 5 and used to guide the moving direction of the support platform 1, and a guide groove arranged on the outside of the support platform 1 and slidingly matched with the guide rail 44;

[0080] When the support platform 1 moves, the sliding drive motor 42 drives the gear 43 to rotate, and the gear 43 drives the rack 41 to move, so that the support platform 1 moves; further, in order to ensure that the movement of the support platform 1 is more stable, the gear 43 and the rack 41 are both two groups, and the two groups of gears 43 are coaxially arranged and respectively provided with a transmission shaft 45, and a commutator 46 is arranged on the output shaft of the sliding drive motor 42, and the commutator 46 is connected to the two groups of transmission shafts 45, so that one group of sliding drive motors 42 drives the two groups of gears 43 to rotate, so that they cooperate with the two groups of racks 41 arranged at the bottom of the support platform 1, and control the support platform 1 to move along the long direction of the guide rail 44; specifically, the guide rail 44 is arranged parallel to the rack 41;

[0081] The utility model provides a sliding mechanism 4 so that the support platform 1 can be moved in the vehicle-mounted cabin 5. After the drone is locked, the positional relationship between the multiple groups of support platforms 1 arranged in the vehicle-mounted cabin 5 can be adjusted by moving the support platform 1 to ensure that the vehicle-mounted cabin 5 can accommodate more drones in the same space.

[0082] Embodiment 2:

[0083] In this embodiment, the axis arranged vertically is the Z axis, the axis along the length direction of the vehicle body is the Y axis, and the axis perpendicular to the Y axis on the same horizontal plane is the X axis;

[0084] like Figure 1-Figure 9 As shown, a UAV cluster transceiver includes a vehicle body, a vehicle-mounted cabin 5 installed on the vehicle body, and multiple sets of UAV take-off and landing devices installed in the vehicle-mounted cabin 5 and as described in Example 1; multiple sets of partitions 50 are arranged in the vehicle-mounted cabin 5 and at equal intervals along the length direction of the vehicle body; an installation space for installing the UAV take-off and landing device is formed between two adjacent sets of partitions 50; the UAV take-off and landing device is slidably installed in the installation space and moves along the X-axis direction.

[0085] The vehicle body is mainly used for controlled transportation. The vehicle-mounted cabin 5 is installed on the vehicle body. Multiple partitions 50 arranged along the length direction of the vehicle body form the vehicle-mounted cabin 5 into multiple installation spaces of uniform volume; the UAV take-off and landing device is located in the installation space and slidably cooperates with the partition 50, and the guide rail 44 is installed on the partition 50 and cooperates with the slide groove arranged on the support platform 1; the long direction of the slide groove is perpendicular to the moving direction of the vehicle body, so that the support platform 1 can move from the installation space to the side of the vehicle-mounted cabin 5, that is, move along the X-axis direction.

[0086] In some possible implementations,

[0087] Multiple groups of drone take-off and landing devices are arranged vertically in each installation space, and the vertical distance between two adjacent groups of drone cluster transceiver devices is greater than the vertical height of the drones; the number of drones is consistent with the number of drone take-off and landing devices;

[0088] There are multiple groups of drone take-off and landing devices in each installation space, which are stacked vertically and slidably matched with two groups of partitions 50; when all the drones are parked on the support platform 1, the support platform 1 in each installation space will be stacked vertically; for example, when there are three groups of drones in each installation space, when the drones need to fly, the vehicle-mounted cabin 5 opens the side and top surface, and the support platform 1 at the top of the installation space does not move, so the sliding mechanism 4 is not required; the other two groups of support platforms 1 are driven by the sliding mechanism 4 along the long direction (X-axis direction) of the guide rail 44 to the side away from each other until they move to the specified position; the three drones corresponding to the installation space will all be extended, and their upper parts will not be disturbed, so they can take off. Before take-off, the locking device 3 and the homing device 2 are activated, and the drone is no longer restricted;

[0089] In order to facilitate the installation of the sliding mechanism 4, a mounting frame for mounting on the sliding mechanism 4 and corresponding to the sliding mechanism 4 is provided between the two groups of partitions 50; the guide rails 44 are in two groups and are provided on the side where the partitions 50 are close to each other.

[0090] In some possible implementations, in order to enable the vehicle-mounted shelter 5 to effectively adapt to the sliding of the support platform so as not to interfere with the take-off and landing of the drone;

[0091] The vehicle-mounted cabin 5 includes a bottom plate 51, end plates 52 arranged on the bottom plate 51 and at both ends along the length direction of the vehicle body, two groups of hatches 53 that are symmetrically arranged along the length direction of the vehicle body and cooperate with the bottom plate 51 and the end plates 52 to form a sending and receiving compartment, and a multi-link drive mechanism 54 that is hinged to the end plates 52 and the hatches 53 at both ends and is used for opening and closing the sending and receiving compartment; when the hatches 53 are fully opened, the bottom plate 51 is exposed to the outside and the top surface of the hatches 53 is located below the partition 50; the partition 50 is installed on the bottom plate 51.

[0092] The hatch 53 includes a mounting plate with a 7-shaped cross section, and end molds 533 arranged at both ends of the mounting plate and used in conjunction with the end plate 52; the outer side of the end mold 533 and the multi-link driving mechanism 54; the mounting plate includes a top plate 531 and a side plate 532; the top plate 531 of the two sets of hatches 53 is used to close the top surface of the vehicle-mounted cabin 5, and the side plate 532 is used to close the two side surfaces of the vehicle-mounted cabin 5 along the length direction of the vehicle body, and the end mold 533 on the same side cooperates with the end plate 52 to close the two end surfaces of the vehicle-mounted cabin 5, thereby forming a receiving and sending warehouse, and after all are closed, drone transportation can be carried out; when the drone is transported to the designated location, the two sets of multi-link driving mechanisms 54 control the two sets of hatches 53 to open, so that the top and side surfaces of the receiving and sending warehouse are fully exposed, and at the same time, the top surface of the top plate 531 will be located below the partition 50 so as not to affect the extension of the lowest support platform 1, and finally the support platform 1 is controlled to slide toward the side of the receiving and sending warehouse to expose the drone, and after moving to the designated position, the flight action can be performed;

[0093] Compared with the prior art, the drone cluster transceiver in the utility model can realize simultaneous take-off and landing from the top and two sides of the vehicle-mounted cabin 5, and can complete the take-off and landing of all drones in a single batch; the drone cluster take-off and landing efficiency is high and the deployment time is short.

[0094] 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 drone take-off and landing device, characterized in that: The invention comprises a support platform (1) installed in a vehicle-mounted cabin (5) and slidably matched with the vehicle-mounted cabin (5), a homing device (2) installed on the support platform (1) and used for homing a drone, and a locking device (3) installed on the support platform (1) and used for locking and fixing the drone after the drone has been returned to its position.

2. The UAV take-off and landing device according to claim 1, characterized in that: The homing device (2) comprises two groups of first clamping plates (21) arranged on the support platform (1) and slidingly matched with the support platform (1), two groups of second clamping plates (22) arranged on the support platform (1) and slidingly matched with the support platform (1), a transverse driving device (23) for driving the two groups of first clamping plates (21) to move closer to or away from each other, and a longitudinal driving device (24) for driving the two groups of second clamping plates (22) to move closer to or away from each other; the two groups of first clamping plates (21) and the two groups of second clamping plates (22) cooperate with each other to form a clamping cavity for parking the drone; the two groups of first clamping plates (21) are located between the two groups of second clamping plates (22).

3. The UAV take-off and landing device according to claim 2, characterized in that: The transverse driving device (23) and the longitudinal driving device (24) have the same structure; The transverse driving device (23) comprises a transverse linear driving device (231) installed at the bottom of the support platform (1) and connected to the first clamping plate (21), a transverse sliding groove (232) arranged on the support platform (1) and slidably matched with the first clamping plate (21), and a transverse transmission member (233) located in the transverse sliding groove (232) and slidably matched with the transverse sliding groove (232); the long direction of the transverse sliding groove (232) is parallel to the long direction of the second clamping plate (22) and is located between the two groups of second clamping plates (22); the transverse transmission member (233) is respectively connected to the bottom of the first clamping plate (21) and the transverse linear driving device (231); The longitudinal drive device (24) comprises a longitudinal linear drive device (241) installed at the bottom of the support platform (1) and connected to the second clamping plate (22), a longitudinal slide groove (242) arranged on the support platform (1) and slidably matched with the second clamping plate (22), and a longitudinal transmission member (243) located in the longitudinal slide groove (242) and slidably matched with the longitudinal slide groove (242); the long direction of the longitudinal slide groove (242) is parallel to the long direction of the first clamping plate (21); the longitudinal transmission member (243) is respectively connected to the bottom of the second clamping plate (22) and the longitudinal linear drive device (241).

4. The UAV take-off and landing device according to claim 3, characterized in that: The transverse driving device (23) further comprises a first movable plate (234) connected to the bottom of the transverse transmission member (233) and sliding along the length direction of the second clamping plate (22), a first telescopic scissors frame (235) installed at the bottom of the first movable plate (234) and connected to the first clamping plate (21) at one end and telescopic along the length direction of the transverse sliding groove (232), and the other end of the first telescopic scissors frame (235) is connected to the bottom of the support platform (1); The longitudinal drive device (24) further comprises a second movable plate (244) connected to the bottom of the longitudinal transmission member (243) and sliding along the length direction of the first clamping plate (21), a second telescopic scissors frame (245) installed at the bottom of the second movable plate (244) and connected to the second clamping plate (22) at one end and telescopic along the length direction of the longitudinal slide groove (242), and the other end of the second telescopic scissors frame (245) is connected to the bottom of the support platform (1).

5. The UAV take-off and landing device according to claim 2, characterized in that: The locking device (3) is located in the clamping cavity and comprises two groups of locking members respectively matched with two groups of first clamping plates (21); the locking members and the first clamping plates (21) are arranged in a one-to-one correspondence and form a locking cavity for locking the landing gear of the UAV.

6. The UAV take-off and landing device according to claim 5, characterized in that: The locking member comprises a locking motor (31) mounted on the bottom of the support platform (1), a rotating shaft (32) connected to the output shaft of the locking motor (31) and arranged along the long direction of the longitudinal slide groove (242), a clamping claw (33) sleeved on the outside of the rotating shaft (32) and rotating around the axis of the rotating shaft (32) under the drive of the locking motor (31), and a through groove (34) arranged on the support platform (1) and used for one end of the clamping claw (33) to pass through.

7. The UAV take-off and landing device according to claim 1, characterized in that: A sliding mechanism (4) is provided at the bottom of the support platform (1) for controlling the support platform (1) to slide along the longitudinal direction of the transverse slide groove (232) and to cooperate with the vehicle-mounted cabin (5); The sliding mechanism (4) comprises a rack (41) arranged along the long direction of the transverse sliding groove (232) and installed at the bottom of the support platform (1), a gear (43) matched with the rack (41), a sliding drive motor (42) used to drive the gear (43), a guide rail (44) arranged on the vehicle-mounted cabin (5) and used to guide the moving direction of the support platform (1), and a guide groove arranged on the outer side of the support platform (1) and slidably matched with the guide rail (44).

8. A drone cluster transceiver, characterized in that: The invention comprises a vehicle body, a vehicle-mounted cabin (5) installed on the vehicle body, a plurality of sets of UAV take-off and landing devices installed in the vehicle-mounted cabin (5) and as described in any one of claims 1 to 7; a plurality of sets of partitions (50) arranged in the vehicle-mounted cabin (5) at equal intervals along the length direction of the vehicle body; and an installation space for installing the UAV take-off and landing device is formed between two adjacent sets of partitions (50).

9. The drone cluster transceiver device according to claim 8, characterized in that: Multiple groups of drone take-off and landing devices are arranged vertically in each of the installation spaces, and the vertical distance between two adjacent groups of drone cluster transceiver devices is greater than the vertical height of the drones; A mounting frame for mounting on the sliding mechanism (4) and arranged one-to-one with the sliding mechanism (4) is arranged between the two groups of partitions (50); the guide rails (44) are in two groups and are arranged on the side where the partitions (50) are close to each other.

10. The drone cluster transceiver device according to claim 8, characterized in that: The vehicle-mounted cabin (5) comprises a bottom plate (51), end plates (52) arranged on the bottom plate (51) and at both ends along the length direction of the vehicle body, two groups of hatches (53) symmetrically arranged along the length direction of the vehicle body and cooperating with the bottom plate (51) and the end plates (52) to form a receiving and dispatching compartment, and a multi-link driving mechanism (54) hinged to the end plates (52) and the hatches (53) at both ends and used for opening and closing the receiving and dispatching compartment; when the hatches (53) are fully opened, the bottom plate (51) is exposed to the outside and the top surface of the hatches (53) is located below the partition (50); and the partition (50) is mounted on the bottom plate (51).

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