Loading and unloading mechanism for low-altitude emergency communication support equipment

Abstract

The utility model discloses a low-altitude emergency communication support equipment loading and unloading mechanism, which belongs to the technical field of emergency communication equipment and comprises communication equipment, a connecting assembly is arranged on the top surface of the communication equipment, a buffer assembly is arranged on the bottom surface of the communication equipment, and the connecting assembly comprises a connecting seat; according to the unmanned aerial vehicle, the blocking frame is arranged in the unmanned aerial vehicle, and through the design, when the communication equipment is hung in the air through the unmanned aerial vehicle, the support below the unmanned aerial vehicle only needs to stretch into the connecting base, and then the unmanned aerial vehicle and the communication equipment can be connected by clamping the support through the blocking frame; according to the communication device, the unmanned aerial vehicle is arranged in the center of the communication device, so that the communication device can be rapidly hung, the communication device can rapidly cover the communication device, and in the clamping process through the blocking frame, the unmanned aerial vehicle can be located in the center of the communication device through limiting of the push plate so that the unmanned aerial vehicle can be kept stable.

Description

Technical Field

[0001] This utility model belongs to the field of emergency communication equipment technology, and in particular relates to a loading and unloading mechanism for low-altitude emergency communication support equipment. Background Technology

[0002] Emergency communication equipment refers to the communication means and equipment used to ensure rescue, emergency relief and necessary communication during emergencies. It can provide stable and reliable communication support in various emergency situations, thereby facilitating information transmission and ensuring that information transmission can still be maintained in various emergency situations. Nowadays, in order to facilitate the coverage of emergency communication equipment signals, drones are used to bring communication equipment to low altitudes for information transmission.

[0003] When suspending communication equipment in the air using drones, the equipment needs to be installed on the drone. However, due to the inherent danger of drone propellers, the drone often needs to be shut down during installation, which takes time and prevents timely coverage. To address these issues, a low-altitude emergency communication support equipment loading and unloading mechanism is urgently needed. Utility Model Content

[0004] The purpose of this utility model is to solve the problem that when communication equipment is suspended in the air by a drone, it is necessary to install the communication equipment onto the drone. However, due to the certain danger of the drone's propeller, the drone often needs to be stopped during installation, which takes a certain amount of time and results in the inability to achieve timely coverage of the communication equipment. Therefore, a low-altitude emergency communication support equipment loading and unloading mechanism is proposed.

[0005] To achieve the above objectives, the present invention adopts the following technical solution: a loading and unloading mechanism for low-altitude emergency communication support equipment, comprising a communication device, a connecting component on the top surface of the communication device, and a buffer component on the bottom surface of the communication device; the connecting component includes a connecting seat, a pushing frame slidably mounted on the connecting seat through a groove therein, an electric push rod fixedly mounted on one side of the pushing frame, a blocking frame fixedly mounted on the other side of the pushing frame, a push plate slidably mounted on the connecting seat through a groove therein, a connecting rod fixedly mounted on one side of the push plate, and a first spring fixedly mounted on one side of the push plate.

[0006] As a further description of the above technical solution:

[0007] The connecting rod is slidably connected to the connecting seat through a groove opened in the connecting seat, and one end of the connecting rod is in contact with the inclined groove opened on one side of the push frame, and the contact surface is an inclined surface.

[0008] As a further description of the above technical solution:

[0009] The connecting seat is fixedly connected to the communication device through a slot opened on the top surface of the communication device, and one end of the electric push rod is fixedly connected to the communication device.

[0010] As a further description of the above technical solution:

[0011] The blocking frame is slidably connected to the connecting seat through a groove opened in the connecting seat, and the top surface of the connecting seat is provided with a groove.

[0012] As a further description of the above technical solution:

[0013] The buffer assembly includes a housing, which is slidably connected to the bottom of the communication device. A damping rod is fixedly installed at the bottom of the housing, and a second spring is provided on the outer wall of the damping rod.

[0014] As a further description of the above technical solution:

[0015] The damping rod and the top of the second spring are both fixedly connected to the ground of the communication equipment. A heat sink is fixedly installed at the bottom of the housing, and a connecting block is fixedly installed on the bottom surface of the communication equipment.

[0016] As a further description of the above technical solution:

[0017] A mounting bracket is fixedly installed on the bottom surface of the connecting block, and the mounting bracket is slidably installed with the connecting bracket through a groove opened on one side of the mounting bracket.

[0018] As a further description of the above technical solution:

[0019] A heat sink is fixedly installed on one side of the connecting frame, and the heat sink and the heat dissipation holes of the heat sink are staggered.

[0020] In summary, due to the adoption of the above technical solution, the beneficial effects of this utility model are:

[0021] 1. In this utility model, by incorporating a blocking frame, when suspending the communication equipment via a drone, the drone is moved above the communication equipment, causing the support below the drone to fall into the groove on the top surface of the connecting seat. This activates an electric push rod to push the push frame, causing the blocking frame to move. The blocking frame then blocks and compresses the crossbar on the support below the drone. Simultaneously, during the movement of the push frame, a push plate pushes the support below the drone, moving the drone and ensuring it is positioned in the center of the communication equipment. This design allows for the connection between the drone and the communication equipment simply by inserting the support below the drone into the connecting seat when suspending the communication equipment via a drone. The blocking frame clamps the support, quickly suspending the communication equipment and enabling rapid coverage. Furthermore, during the clamping process, the push plate limits the drone's position, ensuring it remains stable in the center of the communication equipment.

[0022] 2. In this utility model, by incorporating a second spring, during the drone's descent, the outer shell contacts the ground first, and the impact during descent is reduced by the second spring and damping rod. Simultaneously, when the drone comes to a complete stop and the outer shell fully contacts the ground, the drone's weight compresses the second spring and damping rod, causing the mounting bracket to move downwards, thus bringing the heat sink and heat sink cover into contact. This design achieves buffering during descent through the second spring and damping rod, reducing the possibility of damage to the communication equipment. Furthermore, during descent, the weight of the drone and communication equipment compresses the second spring, causing the heat sink and heat sink cover to fit together. Since the heat dissipation holes on the heat sink and heat sink cover are staggered, all heat dissipation holes are blocked, preventing dust from entering through the heat dissipation holes after descent. Attached Figure Description

[0023] Figure 1 This is a three-dimensional structural diagram of a loading and unloading mechanism for low-altitude emergency communication support equipment.

[0024] Figure 2 This is a three-dimensional exploded view of a loading and unloading mechanism for low-altitude emergency communication support equipment.

[0025] Figure 3 This is an exploded three-dimensional structural diagram of the connecting components in the loading and unloading mechanism of a low-altitude emergency communication support equipment.

[0026] Figure 4 This is a three-dimensional exploded view of the buffer component in the loading and unloading mechanism of a low-altitude emergency communication support equipment.

[0027] Legend:

[0028] 1. Communication equipment; 2. Connecting assembly; 21. Blocking frame; 22. Push plate; 23. Connecting rod; 24. First spring; 25. Pushing frame; 26. Electric push rod; 27. Connecting seat; 3. Buffer assembly; 31. Heat sink; 32. Connecting frame; 33. Connecting block; 34. Mounting frame; 35. Damping rod; 36. Second spring; 37. Heat sink cover; 38. Housing. Detailed Implementation

[0029] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of the present utility model.

[0030] Please see Figures 1-4 This utility model provides a technical solution: a loading and unloading mechanism for low-altitude emergency communication support equipment, including a communication device 1, a connecting component 2 on the top surface of the communication device 1, and a buffer component 3 on the bottom surface of the communication device 1; the connecting component 2 includes a connecting seat 27, a pushing frame 25 is slidably installed on the connecting seat 27 through a groove therein, an electric push rod 26 is fixedly installed on one side of the pushing frame 25, a blocking frame 21 is fixedly installed on the other side of the pushing frame 25, a push plate 22 is slidably installed on the connecting seat 27 through a groove therein, a connecting rod 23 is fixedly installed on one side of the push plate 22, and a first spring 24 is fixedly installed on one side of the push plate 22.

[0031] The connecting rod 23 is slidably connected to the connecting seat 27 through a groove. One end of the connecting rod 23 contacts the inclined groove on one side of the push frame 25, and the contact surface is inclined. The connecting seat 27 is fixedly connected to the communication device 1 through a groove on the top surface. One end of the electric push rod 26 is fixedly connected to the communication device 1. The blocking frame 21 is slidably connected to the connecting seat 27 through a groove. The top surface of the connecting seat 27 has a groove.

[0032] The specific implementation method is as follows: When the communication device 1 is suspended by the drone, the drone is moved above the communication device 1 and the bracket below the drone falls into the groove on the top surface of the connecting seat 27. This activates the electric push rod 26 to push the push frame 25 to move and drive the blocking frame 21 to move. This causes the blocking frame 21 to block and squeeze the crossbar on the bracket below the drone. At the same time, during the movement of the push frame 25, the connecting rod 23 can be squeezed through the inclined groove on one side of the push frame 25, thereby driving the connecting rod 23 and the push plate 22 to move. The push plate 22 then pushes the bracket below the drone to move the drone, so that the drone can be positioned in the middle of the communication device 1.

[0033] The buffer assembly 3 includes a housing 38, which is slidably connected to the bottom of the communication device 1. A damping rod 35 is fixedly installed at the bottom of the housing 38. A second spring 36 is provided on the outer wall of the damping rod 35. The top ends of the damping rod 35 and the second spring 36 are fixedly connected to the ground of the communication device 1. A heat sink 37 is fixedly installed at the bottom of the housing 38. A connecting block 33 is fixedly installed on the bottom surface of the communication device 1. A mounting bracket 34 is fixedly installed on the bottom surface of the connecting block 33. A connecting bracket 32 ​​is slidably installed on the mounting bracket 34 through a slot on one side. A heat sink 31 is fixedly installed on one side of the connecting bracket 32. The heat sink 31 and the heat sink 37 have staggered heat dissipation holes.

[0034] The specific implementation method is as follows: During the landing process of the drone, the outer shell 38 makes contact with the ground first, and the impact during the fall can be reduced by the second spring 36 and the damping rod 35, thereby avoiding damage to the communication equipment 1 due to excessive impact during landing. At the same time, when the drone comes to a complete stop and the outer shell 38 makes full contact with the ground, the weight of the drone causes the second spring 36 and the damping rod 35 to compress, and drives the mounting bracket 34 to move downward, thereby making the heat sink 31 fit with the heat sink cover 37.

[0035] Working principle: When the communication device 1 is suspended by the drone, the drone is moved above the communication device 1, and the bracket below the drone falls into the groove on the top surface of the connecting seat 27. This activates the electric push rod 26 to move the push frame 25, which in turn moves the blocking frame 21. The blocking frame 21 then blocks and compresses the crossbar on the support below the drone. Simultaneously, during the movement of the push frame 25, the inclined groove on one side of the push frame 25 compresses the connecting rod 23, thereby moving the connecting rod 23 and the push plate 22. The push plate 22 then pushes the drone... The support below the drone moves the drone, allowing it to be positioned in the middle of the communication device 1. During the drone's descent, the outer shell 38 contacts the ground first, and the second spring 36 and damping rod 35 reduce the impact of the fall, thus preventing the communication device 1 from being damaged by excessive impact during descent. When the drone comes to a complete stop and the outer shell 38 makes full contact with the ground, the weight of the drone compresses the second spring 36 and damping rod 35, causing the mounting bracket 34 to move downward, thereby bringing the heat sink 31 into contact with the heat sink cover 37.

[0036] The above description is only a preferred embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any equivalent substitutions or changes made by those skilled in the art within the technical scope disclosed in the present utility model, based on the technical solution and the inventive concept of the present utility model, should be included within the protection scope of the present utility model.

Claims

1. A low-altitude emergency communication support equipment loading and unloading mechanism, comprising a communication equipment (1), characterized in that: The communication equipment (1) top surface is equipped with connecting assembly (2), the communication equipment (1) bottom surface is equipped with buffer assembly (3);The connecting assembly (2) includes connecting seat (27), the connecting seat (27) is slidably installed with push frame (25) through the slot in it, the push frame (25) one side is fixedly installed with electric push rod (26), the push frame (25) other side is fixedly installed with blocking frame (21), the connecting seat (27) is slidably installed with push plate (22) through the slot in it, the push plate (22) one side is fixedly installed with connecting rod (23), the push plate (22) one side is fixedly installed with first spring (24).

2. The loading and unloading mechanism of the low-altitude emergency communication support equipment according to claim 1, characterized in that, The connecting rod (23) is slidably connected with the connecting seat (27) through the slot in it, and the connecting rod (23) is in contact with the inclined slot in the push frame (25) on one side and the contact surface is inclined.

3. The low-altitude emergency communication support equipment handling mechanism according to claim 2, characterized in that, The connecting seat (27) is fixedly connected with the communication equipment (1) through the slot in the top surface of the communication equipment (1), and one end of the electric push rod (26) is fixedly connected with the communication equipment (1).

4. The low-altitude emergency communication support equipment handling mechanism according to claim 3, characterized in that, The blocking frame (21) is slidably connected with the connecting seat (27) through the slot in it, and the connecting seat (27) top surface is provided with a groove.

5. The low-altitude emergency communication support equipment handling mechanism according to claim 4, characterized in that, The buffer assembly (3) includes an outer shell (38), the outer shell (38) is slidably connected with the communication equipment (1) bottom end, the outer shell (38) inner bottom end is fixedly installed with damping rod (35), the damping rod (35) outer wall is provided with second spring (36).

6. The low-altitude emergency communication support equipment handling mechanism according to claim 5, characterized in that, The damping rod (35) and the second spring (36) top end are fixedly connected with the ground of the communication equipment (1), the outer shell (38) bottom end is fixedly installed with heat dissipation cover (37), and the communication equipment (1) bottom surface is fixedly installed with connecting block (33).

7. The low-altitude emergency communication support equipment handling mechanism according to claim 6, characterized in that, The connecting block (33) bottom surface is fixedly installed with mounting bracket (34), and the mounting bracket (34) is slidably installed with connecting frame (32) through the slot in one side thereof.

8. The low-altitude emergency communication support equipment handling mechanism according to claim 7, characterized in that, The connecting frame (32) one side is fixedly installed with heat dissipation plate (31), and the heat dissipation plate (31) is staggered with the heat dissipation hole of the heat dissipation cover (37) and is discharged.

Images