Adjusting structure for satellite antenna
By designing a satellite antenna adjustment structure that includes a bottom ring, a chute, a clamping groove and other structures, the problem of inconvenient antenna adjustment in the prior art is solved, and the flexible adjustment of the antenna direction and ease of operation are achieved.
Patent Information
- Application Number
- CN202420611275.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-03-27
- Publication Date
- 2025-01-21
- Estimated Expiration
- 2034-03-27
AI Technical Summary
When installing and using existing satellite antennas, they need to be angled to facilitate signal reception, but the base is fixed to the ground, resulting in inconvenient subsequent adjustment.
An adjustment structure for satellite antennas is designed, including a bottom ring, a chute, a clamping groove, a limiting slot, a moving plate, a sliding plate, a clamping plate and other structures. By loosening the locking screw, the user can easily adjust Orientation of support frame and antenna.
It realizes flexible adjustment of the antenna direction, simple and quick operation, and avoids the problems of antenna tilt and inconvenience.
Smart Images

Figure CN222380830U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the field of satellite antennas, in particular to an adjustment structure for satellite antennas. Background Art
[0002] Antennas are widely used in daily life, such as military satellite antennas used in the military and home satellite antennas used in family life, and have become indispensable equipment in daily life. When installing and using home satellite antennas, it is necessary to adjust the angle of the home satellite antenna to facilitate signal reception.
[0003] For example, in the prior art, the patent application with publication number CN 217485708 U has a connection block connected by bolts to the satellite antenna body and its back, a base is arranged below the connection block, an adjusting member is arranged inside the base, the adjusting member includes a round rod arranged inside the base, and the round rod and the base are movably connected, one end of the round rod penetrates the base and is connected to a knob, a first gear is sleeved on the outer surface of the round rod, and the first gear is meshed with a second gear. The utility model uses the coordination between various parts, and when the satellite antenna body needs to be adjusted in angle, the first gear can be separated from the second gear by pressing in the direction of the base, and then rotated, and then the satellite antenna body can be driven to rotate to adjust the angle, thereby achieving the purpose of simple operation and saving time.
[0004] When the antenna bracket is in use, in order to increase the stability of the antenna, the base of the antenna needs to be installed on the ground to avoid the antenna from tilting during subsequent use. However, this will make it inconvenient to adjust the direction of the antenna later, making it inconvenient for users to use it.
[0005] Therefore, it is necessary to provide a satellite antenna adjustment structure to solve the above technical problems. Utility Model Content
[0006] The utility model provides an adjustment structure for a satellite antenna, which solves the problem that it is inconvenient to adjust the direction of the antenna, thereby making it inconvenient for users to use the antenna.
[0007] In order to solve the above technical problems, the utility model provides an adjustment structure for a satellite antenna, comprising:
[0008] Bottom circle;
[0009] A slide groove, wherein the slide groove is provided at the top of the bottom ring, a clamping groove is provided at the bottom of the slide groove, and a limiting groove is provided on the side of the slide groove;
[0010] A movable plate, wherein the movable plates are respectively arranged at the two ends of the top of the bottom circle, a sliding plate is fixedly installed on the bottom of the movable plate, a clamping plate is fixedly installed on the bottom of the sliding plate, a side plate is fixedly installed on one side of the movable plate, a threaded ring is fixedly installed on one side of the side plate, a locking screw is threadedly connected to the inner side of the sliding groove, and the clamping plate is clamped on the inner side of the clamping groove.
[0011] Preferably, a support frame is fixedly mounted on the top of the movable plate, and an antenna is fixedly mounted on one side of the support frame.
[0012] Preferably, mounting plates are fixedly mounted on both sides of the bottom ring.
[0013] Preferably, one end of the locking screw is arranged on the inner side surface of the limiting groove.
[0014] Preferably, a second tooth plate is fixedly mounted on the bottom of the inner side surface of the clamping groove, and a first tooth plate is arranged on the top of the second tooth plate.
[0015] Preferably, the top of the first tooth plate is fixedly mounted on the bottom of the clamping plate, and springs are fixedly mounted on both ends of the top of the clamping plate.
[0016] Preferably, a slide plate is fixedly mounted on the top of the spring, and the slide plate is slidably connected to the outer side surface of the sliding plate.
[0017] Compared with the related art, the satellite antenna adjustment structure provided by the utility model has the following advantages:
[0018] Beneficial effects:
[0019] The utility model provides an adjustment structure for a satellite antenna, which cooperates with each other through structures such as a bottom ring, a sliding groove, a clamping groove, a limit groove, a mounting plate, a movable plate, a sliding plate, a clamping plate, a side plate, a threaded ring and a locking screw. When using the structure, the user only needs to loosen the locking screw and then adjust the direction of the support frame and the antenna. This makes it convenient for the user to adjust the direction of the antenna during subsequent use, and the operation is convenient and quick. BRIEF DESCRIPTION OF THE DRAWINGS
[0020] Figure 1 A schematic structural diagram of a first embodiment of an adjustment structure for a satellite antenna provided by the utility model;
[0021] Figure 2 for Figure 1 A schematic diagram of a partial cross-sectional structure of the bottom ring shown;
[0022] Figure 3 for Figure 1The schematic diagram of the side structure of the movable plate shown;
[0023] Figure 4 for Figure 1 An enlarged schematic diagram of part A is shown;
[0024] Figure 5 A schematic structural diagram of a second embodiment of an adjusting structure for a satellite antenna provided by the utility model;
[0025] Figure 6 for Figure 5 An enlarged schematic diagram of part B is shown.
[0026] Numbers in the figure: 1, bottom ring, 11, sliding groove, 12, snap-on groove, 13, limiting groove, 14, mounting plate, 2, movable plate, 21, sliding plate, 22, snap-on plate, 23, side plate, 24, threaded ring, 25, locking screw, 3, supporting frame, 4, antenna, 5, skateboard, 51, spring, 52, first tooth plate, 53, second tooth plate. DETAILED DESCRIPTION
[0027] The utility model is further described below in conjunction with the accompanying drawings and implementation modes.
[0028] First embodiment
[0029] Please refer to Figure 1 , Figure 2 , Figure 3 , Figure 4 ,in, Figure 1 A schematic structural diagram of a first embodiment of an adjustment structure for a satellite antenna provided by the utility model; Figure 2 for Figure 1 A schematic diagram of a partial cross-sectional structure of the bottom ring shown; Figure 3 for Figure 1 The schematic diagram of the side structure of the movable plate shown; Figure 4 for Figure 1 The enlarged schematic diagram of part A is shown. An adjustment structure for a satellite antenna comprises: a bottom ring 1;
[0030] A slide groove 11, wherein the slide groove 11 is provided at the top of the bottom ring 1, a clamping groove 12 is provided at the bottom of the slide groove 11, and a limiting groove 13 is provided on the side of the slide groove 11;
[0031] The movable plate 2 is respectively arranged at the two ends of the top of the bottom ring 1, and a sliding plate 21 is fixedly installed at the bottom of the movable plate 2, and a clamping plate 22 is fixedly installed at the bottom of the sliding plate 21. A side plate 23 is fixedly installed on one side of the movable plate 2, and a threaded ring 24 is fixedly installed on one side of the side plate 23. The inner side surface of the threaded ring 24 is threadedly connected with a locking screw, the sliding plate 21 is slidably connected to the inner side surface of the slide groove 11, and the clamping plate 22 is clamped to the inner side surface of the clamping groove 12.
[0032] A support frame 3 is fixedly mounted on the top of the movable plate 2 , and an antenna 4 is fixedly mounted on one side of the support frame 3 .
[0033] Mounting plates 14 are fixedly mounted on both sides of the bottom ring 1 .
[0034] One end of the locking screw 25 is disposed on the inner side surface of the limiting groove 13 .
[0035] The sliding plate 21 slides on the inner side of the slide groove 11, and the clamping plate 22 slides on the inner side of the clamping groove 12, so that the movable plate 2 can be limited to prevent the movable plate 2 from falling off from the top of the bottom ring 1;
[0036] The bottom ring 1 can be installed in a limited position by the mounting plate 14 during use;
[0037] The movable plate 2 can be limited by pressing one end of the locking screw 25 against one side of the inner side of the limiting groove 13 .
[0038] The working principle of the satellite antenna adjustment structure provided by the utility model is as follows:
[0039] When the user needs to adjust the direction of the antenna 4, the user can first reverse the locking screw 25 to make one end of the locking screw 25 away from one side of the inner side of the limiting groove 13, and then the user rotates the support frame 3, and then makes the support frame 3 drive the antenna 4 to rotate. At this time, the bottom of the support frame 3 will drive the movable plate 2 to move, and the movable plate 2 will drive the sliding plate 21 to slide on the inner side of the sliding groove 11, and make the clamping plate 22 slide on the inner side of the clamping groove 12. After adjusting the antenna 4 to the appropriate direction, the user rotates the locking screw 25 forward to make the locking screw 25 threadedly connected to the inner side of the thread ring 24, so that one end of the locking screw 25 moves toward one side of the inner side of the limiting groove 13, until one end of the locking screw 25 is pressed against one side of the inner side of the limiting groove 13, thereby limiting the movable plate 2 and the support frame 3.
[0040] Compared with the related art, the satellite antenna adjustment structure provided by the utility model has the following advantages:
[0041] Beneficial effects:
[0042] Through the cooperation of structures such as the bottom ring 1, the slide groove 11, the snap-fit groove 12, the limit groove 13, the mounting plate 14, the movable plate 2, the sliding plate 21, the snap-fit plate 22, the side plate 23, the threaded ring 24 and the locking screw 25, when in use, the user only needs to loosen the locking screw 25, and then the direction of the support frame 3 and the antenna 4 can be adjusted. This makes it convenient for the user to adjust the direction of the antenna 4 during subsequent use, and the operation is convenient and quick.
[0043] Second embodiment
[0044] Please refer to Figure 5 and Figure 6 Based on the satellite antenna adjustment structure provided in the first embodiment of the present application, the second embodiment of the present application proposes another satellite antenna adjustment structure. The second embodiment is only a preferred embodiment of the first embodiment, and the implementation of the second embodiment will not affect the independent implementation of the first embodiment.
[0045] Specifically, the difference of the adjustment structure for a satellite antenna provided in the second embodiment of the present application is that, in the adjustment structure for a satellite antenna, a second tooth plate 53 is fixedly installed on the bottom of the inner side surface of the snap-in groove 12, and a first tooth plate 52 is arranged on the top of the second tooth plate 53.
[0046] The top of the first tooth plate 52 is fixedly mounted on the bottom of the clamping plate 22 , and springs 51 are fixedly mounted on both ends of the top of the clamping plate 22 .
[0047] A slide plate 5 is fixedly mounted on the top of the spring 51 , and the slide plate 5 is slidably connected to the outer side surface of the sliding plate 21 .
[0048] The working principle of the satellite antenna adjustment structure provided by the utility model is as follows:
[0049] When in use, when the angle of the antenna 4 needs to be adjusted, the user can lift the support frame 3 upward, so that the bottom of the support frame 3 drives the movable plate 2 to move upward, so that the movable plate 2 drives the sliding plate 21 and the clamping plate 22 to move upward, so that the bottom of the clamping plate 22 drives the first tooth plate 52 away from the second tooth plate 52, and the top of the clamping plate 22 presses the spring 51, so that the top of the spring 51 drives the top of the slide plate 5 to fit the top of the inner side surface of the clamping groove 12, and then the user rotates the support frame 3, thereby driving the clamping plate 22 to rotate on the inner side surface of the clamping groove 12 to adjust the angle of the antenna 4. After adjusting to a suitable position, the user releases the support frame 3. At this time, the elasticity of the spring 51 can push the clamping plate 22, so that the clamping plate 22 drives the first tooth plate 52 to move downward, so that the first tooth plate 52 and the second tooth plate 53 are engaged, and the support frame 3 is limited.
[0050] Compared with the related art, the satellite antenna adjustment structure provided by the utility model has the following advantages:
[0051] Beneficial effects:
[0052] By means of the cooperation of structures such as the slide plate 5, the spring 51, the first tooth plate 52 and the second tooth plate 53, when in use, by lifting the support frame 3 upward, the movable plate 2 and the clamping plate 22 are lifted upward, so that the first tooth plate 52 and the second tooth plate 53 are separated, thereby facilitating the user to adjust the direction of the support frame 3 and the antenna 4.
[0053] 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. An adjustment structure for a satellite antenna, characterized in that: include: Bottom circle; A slide groove, wherein the slide groove is provided at the top of the bottom ring, a clamping groove is provided at the bottom of the slide groove, and a limiting groove is provided on the side of the slide groove; A movable plate, wherein the movable plates are respectively arranged at the two ends of the top of the bottom circle, a sliding plate is fixedly installed on the bottom of the movable plate, a clamping plate is fixedly installed on the bottom of the sliding plate, a side plate is fixedly installed on one side of the movable plate, a threaded ring is fixedly installed on one side of the side plate, a locking screw is threadedly connected to the inner side of the sliding groove, and the clamping plate is clamped on the inner side of the clamping groove.
2. The satellite antenna adjustment structure according to claim 1, characterized in that: A support frame is fixedly installed on the top of the movable plate, and an antenna is fixedly installed on one side of the support frame.
3. The satellite antenna adjustment structure according to claim 1, characterized in that: Mounting plates are fixedly mounted on both sides of the bottom ring.
4. The satellite antenna adjustment structure according to claim 1, characterized in that: One end of the locking screw is arranged on the inner side surface of the limiting groove.
5. The satellite antenna adjustment structure according to claim 1, characterized in that: A second tooth plate is fixedly mounted on the bottom of the inner side surface of the clamping groove, and a first tooth plate is arranged on the top of the second tooth plate.
6. The satellite antenna adjustment structure according to claim 5, characterized in that: The top of the first tooth plate is fixedly mounted on the bottom of the clamping plate, and springs are fixedly mounted on both ends of the top of the clamping plate.
7. The satellite antenna adjustment structure according to claim 6, characterized in that: A slide plate is fixedly mounted on the top of the spring, and the slide plate is slidably connected to the outer side surface of the sliding plate.
Citation Information
Patent Citations
Adjusting mechanism of satellite antenna
CN217485708U