Integrated foldable airborne monitoring device

Abstract

The utility model discloses an integrated folding type airborne monitoring equipment, including receiver unit and antenna unit, one side of antenna unit is rotatively connected with one side of receiver unit, and antenna unit and receiver unit are also connected through cable, and the mounting hole position that can be connected with the unmanned plane hole position is arranged on receiver unit. The utility model carries out effective combination to receiver unit and antenna unit, and the quick -mounting structure is not needed between both, and the cable is not needed external connection. Through the integrated folding type structure of the utility model, the volume of airborne monitoring equipment can be effectively reduced, the equipment erection time is greatly shortened, and the antenna unit is automatically entered into the locking state through the telescopic lock tongue after unfolding. It can carry unmanned plane and carry out airborne monitoring, and can also be used in portable installation. The utility model is small in size, light in weight and convenient to fold, and greatly improves the use convenience of airborne monitoring equipment.

Description

Technical Field

[0001] This utility model relates to a folding monitoring device, specifically an integrated folding airborne monitoring device, belonging to the field of monitoring equipment technology. Background Technology

[0002] With the rapid development of the radio spectrum and the low-altitude economy, traditional ground-based monitoring methods are often limited by complex geographical environments and multipath effects, frequently falling into the predicament of being "invisible, inaccurate, and unable to keep up," making it difficult to meet the needs of rapid, efficient, and accurate interference detection. Therefore, airborne monitoring equipment has been more widely used.

[0003] Currently, many airborne monitoring devices employ a separate structure for the receiver and antenna units. This existing structure may present the following technical problems:

[0004] 1) The receiver unit and antenna unit are separate structures, which makes installation between the two inconvenient.

[0005] 2) The receiver unit and antenna unit are bulky after disassembly and assembly, making them inconvenient to store and carry.

[0006] 3) If an external connector is used to connect the receiver unit and the antenna unit, the connector and cable will be exposed, resulting in poor aesthetics;

[0007] 4) If a cluster connector is used to connect the receiver unit and the antenna unit, the connector cost will be high. Utility Model Content

[0008] The purpose of this invention is to provide an integrated foldable airborne monitoring device, in order to solve the problems of installation difficulties, complex structure, and inconvenience of carrying in the prior art.

[0009] This utility model is specifically implemented as follows:

[0010] An integrated foldable airborne monitoring device includes a receiver unit and an antenna unit. One side of the antenna unit is rotatably connected to one side of the receiver unit, and the antenna unit and the receiver unit are connected by a cable.

[0011] The antenna unit is located at the bottom of the receiver unit when folded, and is perpendicular to the receiver unit when unfolded.

[0012] A further step is:

[0013] The antenna unit is unfolded and folded via a rotating shaft.

[0014] A further step is:

[0015] The antenna unit has a groove on its side panel, through which cables are routed.

[0016] A further step is:

[0017] The antenna unit's housing is made of a non-metallic material.

[0018] A further step is:

[0019] The receiver unit housing has ball screws on both sides of the bottom, and the antenna unit has side plate grooves on the inner side of the side plates. When the antenna unit is folded, the metal beads in the ball screws fall into the side plate grooves, thereby fixing the position of the antenna unit.

[0020] A further step is:

[0021] The receiver unit is equipped with telescopic locking tongues on both sides for limiting the position of the antenna unit.

[0022] A button-type telescopic mechanism is installed on the receiver unit. The button-type telescopic mechanism is connected to the telescopic latch. Pressing the button of the button-type telescopic mechanism will retract the telescopic latch.

[0023] A further step is:

[0024] The aforementioned button-type telescopic mechanism includes a button, a positioning seat below the button, a movable block inside the positioning seat, and the button connected to the movable block. Two uprights are located on either side of the lower part of the movable block, each upright having an inwardly inclined surface on its inner side. A compression spring is located below the movable block, and the compression spring is connected to a left slider and a right slider. Both the left and right sliders have left and right grooves to accommodate the lower uprights of the movable block. The upper part of the left and right grooves near the springs has left and right inclined surfaces, respectively. A cover plate is provided on one side of the button-type telescopic mechanism. Telescopic locking tongues are provided at the ends of the left and right sliders.

[0025] A further step is:

[0026] The receiver unit is provided with mounting holes for connecting to the UAV mounting holes.

[0027] This invention effectively combines the receiver unit and antenna unit, eliminating the need for a quick-release structure and external cable connections. The integrated folding structure significantly reduces the size of the aerial monitoring equipment, greatly shortening setup time. The antenna unit automatically locks itself via a telescopic latch after unfolding. It can be used with drones for aerial monitoring or for portable installation. Its small size, light weight, and easy folding greatly improve the usability of aerial monitoring equipment. Attached Figure Description

[0028] Figure 1 This is a schematic diagram of the unfolded structure of one embodiment of the present invention;

[0029] Figure 2 This is a schematic diagram of the folded and stowed structure according to one embodiment of the present invention;

[0030] Figure 3 This is a schematic diagram of an embodiment of the present invention featuring a drone.

[0031] Figure 4 This is an exploded view of a button-type telescopic mechanism in one embodiment of the present invention;

[0032] Figure 5 This is a cross-sectional view of a button-type telescopic mechanism in one embodiment of the present invention;

[0033] Figure 6 This is a schematic diagram of the button-type telescopic mechanism after being pressed in one embodiment of the present invention. Detailed Implementation

[0034] The present invention will now be described in further detail with reference to the accompanying drawings and specific embodiments.

[0035] As attached Figure 1 , 2 As shown, the integrated foldable airborne monitoring device includes a receiver unit 1 and an antenna unit 2. One side of the antenna unit 2 is rotatably connected to one side of the receiver unit 1, and the antenna unit and the receiver unit are also connected by a cable.

[0036] The antenna unit 2, when folded, is located at the bottom of the receiver unit 1, and when unfolded, it is perpendicular to the receiver unit 1. That is, when the integrated foldable ascent monitoring device is not in operation, the antenna unit 2 is folded and distributed at the bottom of the receiver unit 1. When the antenna unit 2 is in operation, it needs to be rotated 90° to maintain a perpendicular state to the receiver unit 1.

[0037] The antenna unit 2 is unfolded and folded via the installed rotating shaft 4.

[0038] The side panel of antenna unit 2 has a groove through which the cable is routed. In other words, the cable is concealed, with its components distributed within the groove on the side panel of antenna unit 2. It then enters the receiver unit 1's internal structure via the inner ring of the rotating shaft on the side of the receiver unit 1's housing.

[0039] The outer shell of the antenna unit 2 is made of non-metallic material, which can meet the wave transmission requirements of the antenna frequency band.

[0040] The receiver unit's housing is made of aluminum alloy, which facilitates heat conduction and electromagnetic shielding of the various modules within the receiver unit.

[0041] The receiver unit 1 has ball screws 5 on both sides of the bottom of the housing, and the antenna unit 2 has side plate grooves on the inner side of the two side plates. When the antenna unit is folded, the metal beads in the ball screws 5 fall into the side plate grooves, thereby fixing the position of the antenna unit.

[0042] The glass ball screw 5 uses a threaded glass ball, and its height can be adjusted to control the tightness of the connection with the side plate of the antenna unit 2.

[0043] The receiver unit is provided with telescopic locking tongues 6 on both sides for limiting the position of the antenna unit.

[0044] A button-type telescopic mechanism 3 is installed on the receiver unit. The button-type telescopic mechanism 3 is connected to the telescopic latch 6. When the button of the button-type telescopic mechanism 3 is pressed, the telescopic latch 6 will retract.

[0045] As attached Figure 4 and 5 As shown in the figure, as an embodiment of the present invention, a button-type telescopic mechanism is provided, including a button 31, a positioning seat 32 below the button 31, a movable block 33 inside the positioning seat 32, the button 31 being connected to the movable block 33, two columns on both sides of the lower part of the movable block 33, the inner side of the columns having an inwardly inclined surface 331, a compression spring 37 below the movable block, the compression spring 37 being connected to the left slider 34 and the right slider 35 respectively, wherein the left slider 34 and the right slider 35 are each provided with a left groove 341 and a right groove 351 for accommodating the lower columns of the movable block 33, the upper part of the left groove 341 and the right groove 351 near the spring 37 having a left inclined surface 342 and a right inclined surface 352, respectively, and a cover plate 36 is provided on one side of the button-type telescopic mechanism. Telescopic locking tongues 6 are respectively provided at the ends of the left slider 34 and the right slider 35.

[0046] As attached Figure 5 and 6 As shown, under normal circumstances, spring 37 can apply elastic force to the left slider 34 and right slider 35, thereby keeping the telescopic latch 6 in the pop-out state and limiting the antenna unit 2 in the unfolded state. When the antenna unit 2 is to be folded, after pressing the button 31 of the push-button telescopic mechanism 3, the two inclined surfaces 331 of the column of the movable block 33 apply pressure to the left inclined surface 342 of the left groove 341 and the right inclined surface 352 of the right groove 351, respectively. As a result, the movable block slides downward, causing the left and right grooves to move towards the center. At the same time, it causes the left slider 34 and right slider 35 to retract towards the center, causing the telescopic latch 6 to retract.

[0047] When antenna unit 2 is flipped to the vertical position, telescopic locking tongue 6 limits and locks antenna unit 2; when antenna unit 2 needs to be retracted, simply press the button in the push-button telescopic mechanism 3, telescopic locking tongue 6 will retract, and then antenna unit 2 will be retracted to the bottom of receiver unit 1.

[0048] As attached Figure 3 As shown, in actual use, the receiver unit can be connected to the drone's mounting hole 7 through the mounting hole 7, making it easy to mount on the drone for takeoff monitoring.

[0049] This embodiment provides an integrated folding aerial monitoring device with an integrated structural design. The combination of a button-type telescopic mechanism and ball screws allows for easy folding and retraction of the receiver and antenna units. When the device is in operation, simply fold the antenna unit 90 degrees. Once folded in place, the telescopic locking tongue automatically engages the antenna unit, ensuring a perpendicular relationship between the antenna and receiver units. When the device is not in operation, simply fold the antenna unit another 90 degrees, retracting it below the receiver unit and securing it. The overall size is compact when folded. The cable connection between the antenna and receiver units requires no adapter connectors, and the cabling is concealed, significantly improving aesthetics. The device is also compact and lightweight when folded. It is easy to use and requires no disassembly, achieving rapid deployment.

[0050] Although the present invention has been described herein with reference to illustrative embodiments, the above embodiments are merely preferred embodiments of the present invention, and the implementation of the present invention is not limited to the above embodiments. It should be understood that those skilled in the art can design many other modifications and implementations, which will fall within the scope and spirit of the principles disclosed in this application.

Claims

1. An integrated foldable ascent monitoring device, comprising a receiver unit and an antenna unit, characterized in that: One side of the antenna unit is rotatably connected to one side of the receiver unit. The antenna unit and the receiver unit are also connected by a cable. The receiver unit is provided with mounting holes that can be connected to the drone's mounting points.

2. The integrated foldable ascent monitoring device according to claim 1, characterized in that: The antenna unit is located at the bottom of the receiver unit (1) after being folded, and is perpendicular to the receiver unit after being unfolded.

3. The integrated foldable ascent monitoring device according to claim 1, characterized in that: The antenna unit is unfolded and folded via a rotating shaft.

4. The integrated foldable ascent monitoring device according to claim 1, characterized in that: The antenna unit has a groove on its side panel, through which cables are routed.

5. The integrated foldable ascent monitoring device according to claim 1, characterized in that: The antenna unit's housing is made of a non-metallic material.

6. The integrated foldable ascent monitoring device according to claim 1, characterized in that: The receiver unit's housing is made of aluminum alloy.

7. The integrated foldable ascent monitoring device according to claim 1, characterized in that: The receiver unit housing has ball screws on both sides of the bottom, and the antenna unit has side plate grooves on the inner side of the side plates. When the antenna unit is folded, the metal beads in the ball screws fall into the side plate grooves, thereby fixing the position of the antenna unit.

8. The integrated foldable ascent monitoring device according to claim 7, characterized in that: The glass ball screw uses threaded glass balls.

9. The integrated foldable ascent monitoring device according to claim 1, characterized in that: The receiver unit is equipped with telescopic locking tongues on both sides for limiting the position of the antenna unit.

10. The integrated foldable ascent monitoring device according to claim 9, characterized in that: A button-type telescopic mechanism is installed on the receiver unit. The button-type telescopic mechanism includes a button, a positioning seat below the button, a movable block inside the positioning seat, and the button connected to the movable block. There are two columns on both sides of the lower part of the movable block. The inner side of the column has an inwardly inclined surface. There is a compression spring below the movable block, which is connected to the left slider and the right slider respectively. The left slider and the right slider are each provided with a left groove and a right groove to accommodate the lower column of the movable block. The upper part of the left groove and the right groove near the spring has a left inclined surface and a right inclined surface. A cover plate is provided on one side of the button-type telescopic mechanism, and telescopic locking tongues are provided at the ends of the left slider and the right slider respectively.

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