Honeycomb device of fixed-wing unmanned aerial vehicle

Abstract

The fixed-wing unmanned aerial vehicle honeycomb device comprises a base and a vehicle body, a supporting platform is fixed to the base through a plurality of supporting legs, a plurality of supporting seats are fixed to the supporting platform at intervals, sliding grooves are formed in the supporting seats, two limiting seats are arranged on the supporting seats at intervals, and the limiting seats are fixed to the supporting platform through the supporting legs. Wherein the bottom of one limiting seat is fixed to the supporting seat, the bottom of the other limiting seat is in sliding connection with the sliding groove, the machine body is placed on the supporting seat and located between the two limiting seats, a lead screw is movably arranged in the sliding groove through a bearing, the lead screw penetrates through the bottoms of the limiting seats, and the limiting seats are arranged on the supporting seat. The unmanned aerial vehicle honeycomb fixing structure solves the problem that when an existing unmanned aerial vehicle honeycomb is used in windy weather, due to lack of a fixing structure, the existing unmanned aerial vehicle honeycomb is easily blown by wind and falls onto the ground to be broken.

Description

Technical Field

[0001] The utility model relates to the field of unmanned aerial vehicles, in particular to a honeycomb device for fixed-wing unmanned aerial vehicles. Background Art

[0002] A fixed-wing UAV airport, referred to as a "beehive", is usually a fixed or mobile UAV airport that provides temporary placement and supply conditions for fixed-wing UAVs.

[0003] When the existing fixed-wing drone hive is used in windy weather, it is easy to be blown by the wind and fall to the ground and be damaged due to the lack of a fixed structure.

[0004] Therefore, it is necessary to provide a new fixed-wing UAV honeycomb device to solve the above-mentioned technical problems. Utility Model Content

[0005] In order to solve the above technical problems, the utility model provides a fixed-wing UAV honeycomb device, which solves the problem that the existing UAV honeycomb is easily blown by the wind and falls to the ground and is damaged due to the lack of a fixed structure when used in windy weather.

[0006] The fixed-wing UAV honeycomb device provided by the utility model comprises a base and a body, a support platform is fixed on the base through a plurality of support legs, a plurality of support seats are fixed on the support platform at intervals, and a slide groove is provided on the support seat;

[0007] Two limiting seats are arranged on the support seat at intervals, wherein the bottom of one limiting seat is fixed on the support seat, and the bottom of the other limiting seat is slidably connected to the slide groove, the machine body is placed on the support seat, and the machine body is located between the two limiting seats.

[0008] In a preferred embodiment, a silicone protective pad is provided on the surface of the limiting seat.

[0009] In a preferred embodiment, a screw rod is movably arranged inside the slide groove through a bearing, the screw rod passes through the bottom of the limit seat, and the screw rod is threadedly connected to the limit seat.

[0010] In a preferred embodiment, one end of the screw rod extends out of the support seat and is fixed with a hexagonal block.

[0011] In a preferred embodiment, a timing alarm and a charging socket are provided on one side of the support seat, and the timing alarm and the charging socket are installed on the support platform;

[0012] A plurality of lockers are installed at intervals on the base, and a fire extinguisher is placed inside the lockers;

[0013] A plurality of partitions are fixed on the support platform at intervals.

[0014] In a preferred embodiment, a support shaft is movably provided at the bottom of the body, and a gun camera is installed at the bottom of the support shaft;

[0015] A transmission worm wheel is installed on the support shaft, a bearing seat is fixed at the bottom of the body, a transmission worm is movably arranged on the bearing seat through a bearing, the transmission worm is meshed with the transmission worm wheel, and the transmission worm is driven by a motor.

[0016] Beneficial effects of the utility model:

[0017] 1. When using this drone honeycomb device, the user can place the drone on the support seat, and then use a wrench to turn the hexagonal block to drive the screw rod to rotate so that the limit seat can slide along the slide groove. The two limit seats close to each other can fix the body to prevent it from falling from the support platform and being damaged. The charging socket is convenient for users to charge the body. At the same time, a timer alarm can be set to alarm and remind when the charging time is reached to avoid damage to the drone battery due to excessive charging time;

[0018] 2. By setting a gun camera at the bottom of the body, the drone can have a shooting function. By starting the motor, the transmission worm can be driven to rotate. Under the transmission action of the transmission worm and the transmission worm wheel, the support shaft can rotate accordingly and drive the gun camera to complete the angle adjustment. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 A three-dimensional view of the overall structure of the honeycomb device for a fixed-wing UAV provided by the utility model;

[0020] Figure 2 A top view of the local structure of the honeycomb device of a fixed-wing UAV provided by the utility model;

[0021] Figure 3 A schematic diagram of the structure of the support base provided by the utility model;

[0022] Figure 4 This is a schematic structural diagram of a machine body provided by the utility model.

[0023] Numbers in the figure: 1. Base; 2. Support legs; 3. Support platform; 4. Support seat; 5. Slide; 6. Limit seat; 7. Body; 8. Silicone protective pad; 9. Screw; 10. Hexagonal block; 11. Timing alarm; 12. Charging socket; 13. Locker; 14. Fire extinguisher; 15. Support shaft; 16. Gun camera; 17. Transmission worm gear; 18. Transmission worm; 19. Bearing seat; 20. Partition. DETAILED DESCRIPTION

[0024] The utility model is further described below in conjunction with the accompanying drawings and implementation modes.

[0025] Please refer to Figure 1 , Figure 2 , Figure 3 as well as Figure 4 ,in Figure 1 A three-dimensional view of the overall structure of the honeycomb device for a fixed-wing UAV provided by the utility model; Figure 2 A top view of the local structure of the honeycomb device of a fixed-wing UAV provided by the utility model; Figure 3 A schematic diagram of the structure of the support base provided by the utility model; Figure 4 This is a schematic structural diagram of a machine body provided by the utility model.

[0026] In the specific implementation process, Figure 1-Figure 4 As shown, it includes a base 1 and a body 7, a supporting platform 3 is fixed on the base 1 through a plurality of supporting legs 2, a plurality of supporting seats 4 are fixed on the supporting platform 3 at intervals, a slide groove 5 is provided on the supporting seat 4, two limiting seats 6 are arranged on the supporting seat 4 at intervals, the bottom of one of the limiting seats 6 is fixed on the supporting seat 4, and the bottom of the other limiting seat 6 is slidably connected to the slide groove 5, the body 7 is placed on the supporting seat 4, and the body 7 is located between the two limiting seats 6, and a silicone protective pad 8 is arranged on the surface of the limiting seat 6, which can protect the body 7 and prevent the limiting seat 6 from causing residual deformation on the surface of the body 7.

[0027] A screw rod 9 is movably arranged inside the slide groove 5 through a bearing, and the screw rod 9 passes through the bottom of the limit seat 6, and the screw rod 9 is threadedly connected to the limit seat 6. One end of the screw rod 9 extends out of the support seat 4 and is fixed with a hexagonal block 10. When the drone honeycomb device is in use, the user can place the drone on the support seat 4, and then use a wrench to turn the hexagonal block 10 to drive the screw rod 9 to rotate, so that the limit seat 6 can slide along the slide groove 5, and the body 7 can be fixed by two limit seats 6 close to each other.

[0028] A timing alarm 11 and a charging socket 12 are provided on one side of the support seat 4, and the timing alarm 11 and the charging socket 12 are installed on the support platform 3. A plurality of lockers 13 are installed at intervals on the base 1, and a fire extinguisher 14 is placed inside the lockers 13. A plurality of partitions 20 are fixed at intervals on the support platform 3, and the support platform 3 can be divided into different areas by the partitions 20 to ensure the orderliness of the placement of the drone.

[0029] A support shaft 15 is movably provided at the bottom of the body 7, a gun camera 16 is installed at the bottom of the support shaft 15, a transmission worm gear 17 is installed on the support shaft 15, a bearing seat 19 is fixed at the bottom of the body 7, a transmission worm 18 is movably provided on the bearing seat 19 through a bearing, the transmission worm 18 is meshed with the transmission worm gear 17, the transmission worm 18 is driven by a motor, and the gun camera 16 is arranged at the bottom of the body 7, so that the drone can have a shooting function, and the transmission worm 18 can be driven to rotate by starting the motor, and under the transmission action of the transmission worm 18 and the transmission worm gear 17, the support shaft 15 can rotate accordingly and drive the gun camera 16 to complete the angle adjustment.

[0030] Working principle of the utility model: when the drone honeycomb device is used, the user can place the drone on the support seat 4, and then use a wrench to rotate the hexagonal block 10 to drive the screw rod 9 to rotate so that the limit seat 6 can slide along the slide groove 5, and the body 7 can be fixed by two limit seats 6 close to each other, and the user can charge the body 7 through the charging socket 12. At the same time, a timing alarm 11 is set to alarm and remind when the charging time is reached, so as to avoid damage to the drone battery caused by too long charging time;

[0031] By arranging a gun camera 16 at the bottom of the body 7, the drone can have a shooting function. By starting the motor, the transmission worm 18 can be driven to rotate. Under the transmission action of the transmission worm 18 and the transmission worm wheel 17, the support shaft 15 can rotate accordingly and drive the gun camera 16 to complete the angle adjustment.

[0032] The circuits and controls involved in the present invention are all prior art and will not be described in detail here.

[0033] The above description is only an embodiment of the present invention, and does not limit the patent scope of the present invention. Any equivalent structure or equivalent process transformation made by using the contents of the specification and drawings of the present invention, or directly or indirectly applied in other related technical fields, are also included in the patent protection scope of the present invention.

Claims

1. A fixed-wing UAV honeycomb device, comprising a base (1) and a body (7), wherein a support platform (3) is fixed to the base (1) via a plurality of support legs (2), characterized in that: A plurality of support seats (4) are fixed at intervals on the support platform (3), and a slide groove (5) is provided on the support seat (4); Two limiting seats (6) are arranged on the support seat (4) at intervals, wherein the bottom of one of the limiting seats (6) is fixed on the support seat (4), and the bottom of the other limiting seat (6) is slidably connected to the slide groove (5), and the machine body (7) is placed on the support seat (4), and the machine body (7) is located between the two limiting seats (6).

2. The fixed-wing UAV honeycomb device according to claim 1, characterized in that: A silicone protective pad (8) is provided on the surface of the limiting seat (6).

3. The fixed-wing UAV honeycomb device according to claim 2, characterized in that: A screw rod (9) is movably arranged inside the slide groove (5) via a bearing, the screw rod (9) passes through the bottom of the limiting seat (6), and the screw rod (9) is threadedly connected to the limiting seat (6).

4. The fixed-wing UAV honeycomb device according to claim 3, characterized in that: One end of the screw rod (9) extends out of the support seat (4) and is fixed with a hexagonal block (10).

5. The fixed-wing UAV honeycomb device according to claim 4, characterized in that: A timing alarm (11) and a charging socket (12) are provided on one side of the support seat (4), and the timing alarm (11) and the charging socket (12) are installed on the support platform (3); A plurality of lockers (13) are installed at intervals on the base (1), and a fire extinguisher (14) is placed inside the lockers (13); A plurality of partitions (20) are fixed at intervals on the support platform (3).

6. The fixed-wing UAV honeycomb device according to claim 5, characterized in that: A support shaft (15) is movably provided at the bottom of the body (7), and a gun-type camera (16) is installed at the bottom of the support shaft (15); A transmission worm wheel (17) is mounted on the support shaft (15); a bearing seat (19) is fixed to the bottom of the machine body (7); a transmission worm (18) is movably arranged on the bearing seat (19) via a bearing; the transmission worm (18) is meshed with the transmission worm wheel (17); and the transmission worm (18) is driven by a motor.

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