Ground base station frame for shipborne unmanned aerial vehicle

Abstract

The utility model relates to the technical field of unmanned aerial vehicle ground base stations, in particular to a shipborne unmanned aerial vehicle ground base station frame which comprises communication equipment, an electric cabinet and a mounting frame. The mounting frame comprises a mounting rod assembly, at least three supporting rod assemblies and mounting base assemblies matched with the supporting rod assemblies in number. The electric control box is connected with the mounting rod assembly through a fastener; one end of the mounting rod assembly is connected with the communication equipment; one end of each supporting rod assembly is connected to the other end of the mounting rod assembly through a first hinge piece, each mounting seat assembly comprises a mounting seat and an electromagnet, and one end of each mounting seat is connected to the other end of the supporting rod assembly through a second hinge piece; and each mounting seat is connected with an electromagnet. Compared with the prior art, the mounting rack has the advantages that the mounting rack can be quickly fixed through the electromagnet on the mounting seat assembly, the mounting time is shortened, and the problems of long time consumption and tedious work caused by bolt fixation when the bottom surface base station rack is mounted are solved.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane ground base station technical field especially relates to a kind of unmanned plane ground base station frame for shipborne. BACKGROUND

[0002] With the rapid development of unmanned plane technology, unmanned plane has been widely applied in logistics transportation, inspection, rescue and other fields. In the flight process of unmanned plane, base station frame needs to be used for signal transmission connection between unmanned plane and control station. However, base station frame is often installed outdoors, and it is very difficult and time-consuming to fix the base station frame under the influence of external environment, and it is easy to be damaged. Especially on unstable plane, such as moving ship, it is more difficult to fix the base station frame.

[0003] At present, the existing shipborne base station frame usually fixes the mounting seat of base station frame on the ship plate by bolts or glue. When the mounting seat of base station frame contacts water or other impurities on the ship plate, the bolts are easy to rust, and the bonding performance of glue is also affected, so that the base station frame is unstable, and it is more troublesome to disassemble, which greatly increases the labor cost and reduces the work efficiency. SUMMARY

[0004] Therefore, the utility model aims at providing a kind of unmanned plane ground base station frame for shipborne, which solves the problem of time-consuming and tedious when using bolts to install the existing base station frame through electromagnet on mounting seat assembly.

[0005] To achieve the above purpose, the technical scheme of the utility model is as follows: a kind of unmanned plane ground base station frame for shipborne, comprising: communication equipment, electric control box and mounting rack;The mounting rack includes mounting rod assembly, at least three support rod assemblies and mounting seat assembly matched with the number of support rod assemblies;The electric control box is connected with the mounting rod assembly by fastener;One end of the mounting rod assembly is connected with the communication equipment;One end of each support rod assembly is respectively rotatably connected to the other end of the mounting rod assembly by first hinged member, to realize the separation or folding of the support rod assembly;Each mounting seat assembly includes mounting seat and electromagnet, and one end of each mounting seat is rotatably connected to the other end of the support rod assembly by second hinged member;The other end of each mounting seat is connected with the electromagnet.

[0006] Further, the mounting rod assembly includes first mounting pipe, second mounting pipe, first sleeve, first locking member and connecting plate;One end of the first mounting pipe is connected with the communication equipment, and the other end of the first mounting pipe is arranged in the interior of the second mounting pipe, and the fixed end of the second mounting pipe is connected with the connecting plate;The first sleeve is sleeved outside the second mounting pipe and located at the intersection of the first mounting pipe and the second mounting pipe, and the first locking member fixes the first mounting pipe, the second mounting pipe and the first sleeve together.

[0007] Further, the first sleeve is provided with a first screw hole, and the first locking member abuts against the first mounting pipe through the first screw hole.

[0008] Further, the first mounting pipe and the second mounting pipe are circular pipes, and the inner diameter of the second mounting pipe is greater than the outer diameter of the first mounting pipe.

[0009] Further, each support rod assembly comprises a first connecting lug, a third mounting pipe, a fourth mounting pipe, a second connecting lug, a second sleeve and a second locking member; one end of the first connecting lug is hingedly connected to the connecting plate through a first hinge member; the other end of the second connecting lug is connected to one end of the third mounting pipe; the other end of the third mounting pipe is arranged in the fourth mounting pipe, and the fixed end of the fourth mounting pipe is connected to the second connecting lug; the second sleeve is arranged outside the fourth mounting pipe and located at the joint of the fourth mounting pipe and the third mounting pipe; and the second locking member fixes the third mounting pipe, the fourth mounting pipe and the second sleeve together.

[0010] Further, the second sleeve is provided with a second screw hole, and the second locking member abuts against the third mounting pipe through the second screw hole.

[0011] Further, the third mounting pipe and the fourth mounting pipe are circular pipes, and the inner diameter of the fourth mounting pipe is greater than the outer diameter of the third mounting pipe.

[0012] Further, the third mounting pipe is screwed with the first connecting lug, and the fourth mounting pipe is screwed with the second connecting lug.

[0013] Further, one end of the third mounting pipe connected with the first connecting lug is provided with a first thread, and the first connecting lug is provided with a second thread matched with the first thread; one end of the fourth mounting pipe connected with the second connecting lug is provided with a third thread, and the second connecting lug is provided with a fourth thread matched with the third thread.

[0014] Further, the first thread and the third thread are internal threads, and the second thread and the fourth thread are external threads.

[0015] Compared with the prior art, the utility model can achieve the following beneficial effects:

[0016] 1) The electromagnet on the mounting seat assembly can quickly fix the mounting frame, shorten the installation time, and solve the time-consuming and tedious problem of using bolts to install the existing base station frame.

[0017] 2) The first mounting pipe, the second mounting pipe, the third mounting pipe and the fourth mounting pipe are all circular pipes, which not only reduces the overall weight of the mounting frame, facilitates the operation of the installer, but also provides a wiring space for the power supply wire of the electromagnet, avoiding the corrosion problem caused by the exposed wire.

[0018] 3) the support rod assembly, the mounting rod assembly and the mounting seat assembly are hingedly connected, so that the mounting rack can be quickly folded when not in use, thereby saving the floor space. BRIEF DESCRIPTION OF DRAWINGS

[0019] The accompanying drawings, which form a part of this specification, are included to provide a further understanding of the application, and are incorporated by reference herein. The embodiments disclosed in the drawings are illustrative of the present application and are not meant to limit the present application as well as the explanation is used to explain the present application. In the drawings:

[0020] Figure 1 is a structural schematic view of a shipborne unmanned aerial vehicle ground base station rack according to an embodiment of the present application;

[0021] Figure 2 is a structural schematic view of a mounting rod assembly according to an embodiment of the present application;

[0022] Figure 3 is a structural schematic view of a support rod assembly according to an embodiment of the present application;

[0023] Figure 4 is a structural schematic view of a second connecting lug and a mounting seat assembly hinge according to an embodiment of the present application;

[0024] Figure 5 is a structural schematic view of a shipborne unmanned aerial vehicle ground base station rack after being folded according to an embodiment of the present application.

[0025] The reference signs include: 1, a communication device; 2, an electric control box; 3, a mounting rod assembly; 31, a first mounting pipe; 32, a second mounting pipe; 33, a first sleeve pipe; 34, a first locking piece; 35, a connecting plate; 36, a hinge groove; 37, a connecting hole; 4, a support rod assembly; 41, a first connecting lug; 411, a first cylindrical part; 412, a first hinge part; 42, a third mounting pipe; 43, a fourth mounting pipe; 44, a second connecting lug; 441, a second cylindrical part; 442, a second hinge part; 45, a second sleeve pipe; 46, a second locking piece; 5, a mounting seat assembly; 51, a mounting seat; 52, an electromagnet; 511, a mounting part; 512, a third hinge part; 6, a fastener; 7, a first hinge piece; 8, a second hinge piece. DETAILED DESCRIPTION

[0026] In order to make the purpose, technical scheme and advantages of the present application more clear, the present application is further described in detail below with reference to the drawings and specific embodiments. It should be understood that the specific embodiments described herein are only used to explain the present application, and do not constitute a limitation on the present application.

[0027] It should be noted that the embodiments in the present application and the features in the embodiments can be combined with each other without conflict.

[0028] In the description of the present application, it should be understood that the orientation or positional relationship indicated by the terms "center", "longitudinal", "transverse", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer" and the like is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present application and simplifying the description, and does not indicate or imply that the device or element indicated must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as a limitation on the present application. In addition, the terms "first", "second" and the like are only for the purpose of description, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the technical features indicated. Therefore, the features limited by "first", "second" and the like can explicitly or implicitly include one or more of the features. In the description of the present application, the meaning of "a plurality of" is two or more, unless otherwise specified.

[0029] In the description of the present application, it should be noted that, unless otherwise specified and limited, the terms "mounting", "connection", "connection" should be understood broadly, for example, it can be fixedly connected, or it can be detachably connected, or integrally connected; it can be mechanically connected, or it can be electrically connected; it can be directly connected, or it can be indirectly connected through an intermediate medium, or it can be the communication between two elements. For ordinary skilled in the art, the specific meaning of the above terms in the present application can be understood according to the specific circumstances.

[0030] The present application will be described in detail below with reference to the drawings and in combination with the embodiments.

[0031] As Figures 1 to 5 shown, the unmanned aerial vehicle ground base station rack for shipborne provided by the embodiment of the present application comprises: a communication device 1, an electric control box 2 and a mounting rack. The communication device 1 is used for communication with the unmanned aerial vehicle. The mounting rack comprises a mounting rod assembly 3, at least three support rod assemblies 4 and mounting seat assemblies 5 matched in number with the support rod assemblies 4. The electric control box 2 is connected with the mounting rod assembly 3 through fasteners 6. One end of the mounting rod assembly 3 is connected with the communication device 1. One end of each support rod assembly 4 is rotatably connected to the other end of the mounting rod assembly 3 through a first hinge 7, so as to realize the separation or folding of the support rod assembly 4. In the present embodiment, the number of the support rod assemblies 4 and the mounting seat assemblies 5 is three.

[0032] The electrical box 2 houses a power supply, and its backplate is connected to the mounting rod assembly 3 via fasteners 6. The box 2 also features a network port for network cables and a cable hole for power cables. In this embodiment, fastener 6 is a clamp, one piece of which is secured to the backplate of the box 2.

[0033] The structure of the mounting rod assembly 3 is as follows Figure 2 As shown, it includes a first mounting tube 31, a second mounting tube 32, a first sleeve 33, a first locking member 34 and a connecting plate 35. The first mounting tube 31 and the second mounting tube 32 are both round tubes, and the inner diameter of the second mounting tube 32 is larger than the outer diameter of the first mounting tube 31.

[0034] One end of the first mounting tube 31 is connected to the communication device 1, and the other end of the first mounting tube 31 is inserted into the interior of the second mounting tube 32, so that the first mounting tube 31 can move inside the second mounting tube 32. The fixed end of the second mounting tube 32 is connected to the connecting plate 35. The first sleeve 33 is sleeved on the outside of the second mounting tube 32 and is located at the intersection of the first mounting tube 31 and the second mounting tube 32. The first sleeve 33 is provided with a first screw hole, and the first locking member 34 passes through the first screw hole and abuts against the first mounting tube 31, thereby fixing the first mounting tube 31, the second mounting tube 32 and the first sleeve 33 together. In this embodiment, the first sleeve 33 and the second mounting tube 32 are clearance-fitted.

[0035] The back plate of the electric control box 2 is connected to the second mounting tube 32 via a fastener 6 , and the fastener 6 is located below the first sleeve 33 .

[0036] Three hinge slots 36 are evenly spaced on the outer wall of the connecting plate 35. Connecting holes 37 are provided on both sides of each hinge slot 36. One end of each support rod assembly 4 fits into its corresponding hinge slot 36, and a first hinge 7 passes through the connecting holes 37, hingedly connecting the support rod assembly 4 to the connecting plate 35. The first hinge 7 is a clevis-shaped thumb screw secured to the connecting plate 35 using a nut.

[0037] In this embodiment, the first locking member 34 includes a first screw and a first screw head, and the first screw matches the first screw hole. The connecting plate 35 is triangular in shape, and three hinge slots 36 are respectively provided at the three corners of the connecting plate 35. In other embodiments, the first locking member 34 is a bolt or screw that matches the first screw hole.

[0038] Before the unmanned aerial vehicle ground base stand starts to work, the communication device 1 needs to be lifted to ensure that the communication device 1 and the unmanned aerial vehicle maintain good signal transmission. First, the first mounting pipe 31 is moved along the length direction of the second mounting pipe 32 to the highest position or a position that meets the signal transmission of the communication device 1. Then, the first mounting pipe 31, the second mounting pipe 32 and the first sleeve pipe 33 are fixed together by using the first locking piece 34. When the unmanned aerial vehicle ground base stand does not work, the first locking piece 34 is loosened, and the first mounting pipe 31 is retracted into the second mounting pipe 32 to save space and facilitate storage.

[0039] As shown in FIG. 2, each support rod assembly 4 includes a first connecting ear 41, a third mounting pipe 42, a fourth mounting pipe 43, a second connecting ear 44, a second sleeve pipe 45 and a second locking piece 46. Figure 3 One end of the first connecting ear 41 is hinged to the connecting plate 35 through the first hinge piece 7. The other end of the first connecting ear 41 is connected to one end of the third mounting pipe 42. The other end of the third mounting pipe 42 is arranged inside the fourth mounting pipe 43, and the fixed end of the fourth mounting pipe 43 is connected to the second connecting ear 44. The second sleeve pipe 45 is sleeved outside the fourth mounting pipe 43 and located at the joint of the fourth mounting pipe 43 and the third mounting pipe 42. The second sleeve pipe 45 is provided with a second screw hole, and the second locking piece 46 passes through the second screw hole and abuts against the third mounting pipe 42 to fix the third mounting pipe 42, the fourth mounting pipe 43 and the second sleeve pipe 45 together. In this embodiment, the second sleeve pipe 45 and the fourth mounting pipe 43 are in clearance fit.

[0040] The third mounting pipe 42 and the fourth mounting pipe 43 are both circular pipes, and the inner diameter of the fourth mounting pipe 43 is greater than the outer diameter of the third mounting pipe 42. In this embodiment, the second locking piece 46 includes a second screw rod and a second screw rod head, and the second screw rod matches the second screw hole. In other embodiments, the second locking piece 46 is a bolt or a screw that matches the second screw hole.

[0041] The first mounting pipe 31, the second mounting pipe 32, the third mounting pipe 42 and the fourth mounting pipe 43 are all circular pipes, which not only reduces the overall weight of the mounting stand and facilitates the operation of the installation personnel, but also provides wiring space for the power supply wire of the electromagnet 52 described below, avoiding the corrosion problem caused by the exposed wire.

[0042] The first connecting ear 41 includes a first cylindrical part 411 and a first hinge part 412. The first hinge part 412 is embedded into the hinge groove 36 and hinged to the connecting plate 35 through the first hinge piece 7. The first cylindrical part 411 is screwed to the third mounting pipe 42.

[0043] The second connecting lug 44 comprises a second cylindrical portion 441 and a second hinged portion 442, and the second hinged portion 442 is hinged to the corresponding mounting seat assembly 5 through the second hinge 8. The second cylindrical portion 441 is screwed with the fourth mounting pipe 43.

[0044] Further, the first end of the third mounting pipe 42 connected with the first cylindrical portion 411 is provided with a first thread, and the first cylindrical portion 411 is provided with a second thread matched with the first thread. The fixed end of the fourth mounting pipe 43 is provided with a third thread, and the second cylindrical portion 441 is provided with a fourth thread matched with the third thread. In the embodiment, the first thread and the third thread are internal threads, and the second thread and the fourth thread are external threads.

[0045] Each mounting seat assembly 5 comprises a mounting seat 51 and an electromagnet 52, and the mounting seat 51 comprises a mounting portion 511 and a third hinged portion 512, and the third hinged portion 512 is hinged to the second hinged portion 442 through the second hinge 8. The electromagnet 52 is arranged at the bottom of the mounting portion 511. The electromagnet 52 magnetically fixes the mounting frame on the ship plate after being powered on. The mounting seat assembly 5 is hinged with the support rod assembly 4, which not only can realize the angle adjustment of the mounting seat assembly 5 and the support rod assembly 4, but also is convenient for replacement of the mounting seat assembly 5.

[0046] The first connecting lug 41, the second connecting lug 44 and the mounting seat assembly 5 are all provided with threading holes, and the power line of the electromagnet 52 is sequentially threaded through the threading hole of the mounting seat assembly 5, the threading hole of the second connecting lug 44, the interior of the fourth mounting pipe 43, the interior of the third mounting pipe 42 and the threading hole of the first connecting lug 41, and is connected with the power supply in the electric control box 2, so that the electromagnet 52 is powered while the winding problem of the line is avoided.

[0047] When the unmanned aerial vehicle ground base station frame is not in operation, the electromagnet 52 is powered off, the fastener 6 of the electric control box 2 is loosened and removed, and each support rod assembly 4 is rotated around the first hinge 7 to the mounting rod assembly 3, so that the support rod assembly 4 is folded to save the occupied space.

[0048] The above specific embodiments do not constitute a limitation on the protection scope of the present application. It should be understood by those skilled in the art that various modifications, combinations, sub-combinations and substitutions can be made according to design requirements and other factors. Any modification, equivalent substitution and improvement made within the spirit and principle of the present application shall be included in the protection scope of the present application.

Claims

1. A ground base station for a ship-borne UAV, characterized in that: include: Communication equipment, an electric control box and a mounting frame; the mounting frame includes a mounting rod assembly, at least three support rod assemblies and a mounting seat assembly matching the number of the support rod assemblies; The electric control box is connected to the mounting rod assembly via a fastener; one end of the mounting rod assembly is connected to the communication device; one end of each support rod assembly is rotatably connected to the other end of the mounting rod assembly via a first hinge to achieve separation or folding of the support rod assembly; Each mounting seat assembly includes a mounting seat and an electromagnet. One end of each mounting seat is rotatably connected to the other end of the support rod assembly through a second hinge; the other end of each mounting seat is connected to the electromagnet.

2. The UAV ground base station frame for shipboard use according to claim 1, characterized in that: The mounting rod assembly includes a first mounting tube, a second mounting tube, a first sleeve, a first locking member, and a connecting plate; one end of the first mounting tube is connected to the communication device, the other end of the first mounting tube is disposed inside the second mounting tube, and the fixed end of the second mounting tube is connected to the connecting plate; The first sleeve is sleeved on the outside of the second mounting tube and is located at the junction of the first mounting tube and the second mounting tube. The first locking member fixes the first mounting tube, the second mounting tube and the first sleeve together.

3. The UAV ground base station frame for shipboard use according to claim 2, characterized in that: The first sleeve is provided with a first screw hole, and the first locking piece passes through the first screw hole and abuts against the first mounting tube.

4. The UAV ground base station frame for shipboard use according to claim 2, characterized in that: The first mounting tube and the second mounting tube are both round tubes, and the inner diameter of the second mounting tube is larger than the outer diameter of the first mounting tube.

5. The shipborne UAV ground base station frame according to claim 2, characterized in that: Each of the support rod assemblies includes a first connecting ear, a third mounting tube, a fourth mounting tube, a second connecting ear, a second sleeve, and a second locking member; One end of the first connecting ear is hinged to the connecting plate through the first hinge; the other end of the second connecting ear is connected to one end of the third mounting tube; the other end of the third mounting tube is arranged inside the fourth mounting tube, and the fixed end of the fourth mounting tube is connected to the second connecting ear; the second sleeve is sleeved on the outside of the fourth mounting tube and is located at the intersection of the fourth mounting tube and the third mounting tube; the second locking member fixes the third mounting tube, the fourth mounting tube and the second sleeve together.

6. The shipborne UAV ground base station frame according to claim 5, characterized in that: The second sleeve is provided with a second screw hole, and the second locking piece passes through the second screw hole and abuts against the third mounting tube.

7. The ground base station frame for a shipborne UAV according to claim 5, characterized in that: The third mounting tube and the fourth mounting tube are both round tubes, and the inner diameter of the fourth mounting tube is greater than the outer diameter of the third mounting tube.

8. The shipborne UAV ground base station frame according to claim 5, characterized in that: The third mounting tube is screwed to the first connecting ear, and the fourth mounting tube is screwed to the second connecting ear.

9. The shipborne UAV ground base station according to claim 8, characterized in that: One end of the third mounting tube connected to the first connecting ear is provided with a first thread, and the first connecting ear is provided with a second thread matching the first thread; one end of the fourth mounting tube connected to the second connecting ear is provided with a third thread, and the second connecting ear is provided with a fourth thread matching the third thread.

10. The shipborne UAV ground base station frame according to claim 9, characterized in that: The first thread and the third thread are internal threads, and the second thread and the fourth thread are external threads.

Images