CN211655025U - Stable mounting structure for satellite antenna - Google Patents
Stable mounting structure for satellite antenna Download PDFInfo
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- CN211655025U CN211655025U CN201922133226.XU CN201922133226U CN211655025U CN 211655025 U CN211655025 U CN 211655025U CN 201922133226 U CN201922133226 U CN 201922133226U CN 211655025 U CN211655025 U CN 211655025U
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- connecting rod
- satellite antenna
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- rod
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Abstract
The utility model discloses a satellite antenna is with stabilizing mounting structure, including PMKD, with PMKD fixed connection's link, set up the mount in link one side and set up coupling assembling and the adjusting part between mount and the link, the mount is used for installing satellite antenna. The utility model relates to a satellite antenna is with stabilizing mounting structure is convenient for be connected the link with the mount through coupling assembling, and is convenient for according to actual user demand to the effectual stability of being connected of link with the mount of having guaranteed, to the angle between link and the mount adjust, the effectual stability of having guaranteed satellite antenna's received signal, and then the effectual improvement the utility model discloses a use precision.
Description
Technical Field
The utility model relates to a relevant technical field of satellite antenna specifically is a satellite antenna is with stabilizing mounting structure.
Background
The satellite antenna is a pot which is a metal paraboloid and is responsible for reflecting satellite signals to a feed source and a high-frequency head which are positioned at a focus. The satellite antenna is used for collecting weak signals transmitted from the satellite and removing noise as much as possible. Most antennas are generally parabolic, and some multifocal antennas are formed by a combination of a spherical surface and a parabolic surface. The satellite signal is concentrated to its focus after reflection by the parabolic antenna.
The inventor of the utility model finds that the installation structure for the satellite antenna in the prior art has simple structure and single use mode due to the design characteristics of the installation structure, thereby reducing the precision of installing the satellite antenna and further failing to meet various use requirements of the installation structure for the satellite antenna at present;
to this end, we propose a stable mounting structure for a satellite antenna.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a satellite antenna is with stabilizing mounting structure, aim at improving the satellite antenna among the prior art and use mounting structure because and the design characteristics of itself, simple structure and using-way are single, and then have reduced the precision of installing satellite antenna to can't satisfy the problem to the multiple user demand of satellite antenna for mounting structure at present.
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: a stable mounting structure for a satellite antenna comprises a fixed bottom plate, a connecting frame fixedly connected with the fixed bottom plate, a fixed frame arranged on one side of the connecting frame, and a connecting assembly and an adjusting assembly arranged between the fixed frame and the connecting frame, wherein the fixed frame is used for mounting the satellite antenna;
the adjusting assembly comprises a first connecting rod, a second connecting rod, a first connecting shaft and a second connecting shaft, wherein the first connecting shaft is arranged at one end of the first connecting rod and the second connecting rod, and the second connecting shaft is arranged at the other end of the first connecting rod and the second connecting rod;
the traction assembly comprises positioning blocks fixedly arranged on the first connecting rod and the second connecting rod respectively, a second fixing rod arranged between the positioning blocks, a first fixing rod arranged between the upper ends of the fixing frames, a first fixing block and a second fixing block which are arranged on the first fixing rod and the second fixing rod respectively, a traction rod arranged between the first fixing block and the second fixing block, and a connecting torsion spring fixedly arranged between the first fixing rod and the second fixing rod respectively.
The connecting frame is conveniently connected with the fixing frame through the connecting assembly, and the connecting frame is conveniently connected with the fixing frame according to actual use requirements, so that the stability of the connection of the connecting frame and the fixing frame is effectively guaranteed, the angle between the connecting frame and the fixing frame is adjusted, the stability of a receiving signal of the satellite antenna is effectively guaranteed, and the use precision of the satellite antenna is effectively improved;
as a preferable aspect of the utility model, the fixing frame is arranged in a shape of a Chinese character 'jing', the fixing frame is used for being connected with the connecting component, and the lower end of the fixing frame is used for being connected with the adjusting component, thereby effectively improving the use precision of the utility model;
as a preferable aspect of the present invention, the first connecting shaft penetrates through one end of the first connecting rod and one end of the second connecting rod respectively and is hinged to the connecting frame, and the first connecting shaft is fixedly connected to the first connecting rod and the second connecting rod, so that the first connecting rod and the second connecting rod can rotate by a certain angle around the first connecting shaft as a central axis according to actual use requirements, thereby facilitating adjustment of the angle between the connecting frame and the fixing frame;
as a preferred aspect of the present invention, the second connecting shaft respectively penetrates through the other ends of the first connecting rod and the second connecting rod and is fixedly connected to the lower end of the fixing frame, and the second connecting shaft is fixedly connected to the first connecting rod and the second connecting rod, thereby facilitating the connection of the first connecting rod and the second connecting rod via the second connecting shaft, and facilitating the connection of the first connecting rod and the second connecting rod to the fixing frame via the second connecting shaft;
as a preferable aspect of the present invention, the traction rod penetrates through the first fixing block and the second fixing block respectively, and the first fixing block and the second fixing block are provided with through holes adapted to the traction rod, the inner diameter of the through hole is larger than the outer diameter of the traction rod, and the traction rod is fixedly provided with a limit ring, the outer diameter of the limit ring is larger than the outer diameter of the through hole, so as to facilitate the limit of the traction rod by the limit ring;
as the utility model discloses an in preferred aspect, first fixed block and second fixed block respectively with first dead lever and second dead lever fixed connection, and the second dead lever is connected or fixed connection with locating piece rotation each other, and first dead lever is connected with the upper end fixed connection of mount or rotates, and then is convenient for carry out the angle regulation after-fixing frame through the subassembly that draws and is connected with the link according to actual user demand.
Compared with the prior art, the beneficial effects of the utility model are that: the utility model has the characteristics of reasonable in design and easy operation, the utility model relates to a satellite antenna is with stabilizing mounting structure includes PMKD, with PMKD fixed connection's link, setting at the mount of link one side and set up coupling assembling and the adjusting part between mount and the link, the mount is used for installing satellite antenna, and then is convenient for be connected link and mount through coupling assembling, and is convenient for according to actual user demand to the effectual stability of having guaranteed that the link is connected with the mount, adjust the angle between link and the mount, the effectual stability of having guaranteed satellite antenna's acceptance signal, and then the effectual improvement the utility model discloses a use precision.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings that are required to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present invention, and therefore should not be considered as limiting the scope, and for those skilled in the art, other related drawings can be obtained according to the drawings without inventive efforts.
Fig. 1 is a schematic structural view of an overall structure of a stable mounting structure for a satellite antenna according to the present invention;
fig. 2 is a schematic structural view of another view of fig. 1 in a stable mounting structure for a satellite antenna according to the present invention;
fig. 3 is a schematic structural diagram of a stable installation structure for a satellite antenna according to the present invention when in use.
In the figure: 1-connecting frame, 2-fixing frame, 31-first connecting shaft, 32-second connecting shaft, 41-first connecting rod, 42-second connecting rod, 5-traction rod, 61-first fixing rod, 62-second fixing rod, 71-first fixing block, 72-second fixing block, 8-positioning block and 9-connecting torsion spring.
Detailed Description
To make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the drawings of the embodiments of the present invention are combined to clearly and completely describe the technical solutions of the embodiments of the present invention, and obviously, the described embodiments are some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention. Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1, fig. 2 and fig. 3, the present invention provides a technical solution: a stable mounting structure for a satellite antenna comprises a fixed base plate, a connecting frame 1 fixedly connected with the fixed base plate, a fixing frame 2 arranged on one side of the connecting frame 1, and a connecting assembly and an adjusting assembly arranged between the fixing frame 2 and the connecting frame 1, wherein the fixing frame 2 is used for mounting the satellite antenna, so that the connecting frame 1 and the fixing frame 2 can be conveniently connected through the connecting assembly, and the satellite antenna is conveniently connected according to actual use requirements, thereby effectively ensuring the stability of the connection of the connecting frame 1 and the fixing frame 2, adjusting the angle between the connecting frame 1 and the fixing frame 2, effectively ensuring the stability of a signal received by the satellite antenna, and further effectively improving the use precision of the utility model;
referring to fig. 1, 2 and 3, the fixing frame 2 is arranged in a shape of a Chinese character jing, the fixing frame 2 is used for being connected with the connecting assembly, and the lower end of the fixing frame 2 is used for being connected with the adjusting assembly, so that the use precision of the utility model is effectively improved;
referring to fig. 1, 2 and 3, the adjusting assembly includes a first connecting rod 41 and a second connecting rod 42, a first connecting shaft 31 disposed at one end of the first connecting rod 41 and the second connecting rod 42, and a second connecting shaft 32 disposed at the other end of the first connecting rod 41 and the second connecting rod 42, wherein the first connecting shaft 31 respectively penetrates through one end of the first connecting rod 41 and one end of the second connecting rod 42 and is hinged to the connecting frame 1, and the first connecting shaft 31 is fixedly connected to the first connecting rod 41 and the second connecting rod 42, so that the first connecting rod 41 and the second connecting rod 42 can rotate by a certain angle around the first connecting shaft 31 as a central axis according to actual use requirements, thereby facilitating adjustment of the angle between the connecting frame 1 and the fixing frame 2; the second connecting shaft 32 penetrates through the other ends of the first connecting rod 41 and the second connecting rod 42 respectively and is fixedly connected with the lower end of the fixing frame 2, and the second connecting shaft 32 is fixedly connected with the first connecting rod 41 and the second connecting rod 42, so that the first connecting rod 41 and the second connecting rod 42 can be conveniently connected through the second connecting shaft 32, and the first connecting rod 41 and the second connecting rod 42 can be conveniently connected with the fixing frame 2 through the second connecting shaft 32;
referring to fig. 1, 2 and 3, the traction assembly includes a positioning block 8 respectively fixedly disposed on the first connecting rod 41 and the second connecting rod 42, a second fixing rod 62 disposed between the positioning blocks 8, a first fixing rod 61 disposed between the upper ends of the fixing frames 2, a first fixing block 71 and a second fixing block 72 respectively disposed on the first fixing rod 61 and the second fixing rod 62, a traction rod 5 disposed between the first fixing block 71 and the second fixing block 72, and a connecting torsion spring 9 respectively fixedly disposed between the first fixing rod 61 and the second fixing rod 62, the traction rod 5 respectively penetrates through the first fixing block 71 and the second fixing block 72, and the first fixing block 71 and the second fixing block 72 are provided with through holes adapted to the traction rod 5, the inner diameter of the through holes is larger than the outer diameter of the traction rod 5, and the traction rod 5 is fixedly provided with a limit ring, the outer diameter of the limit ring is larger than the outer diameter of the through holes, and then be convenient for carry on spacingly through the spacing ring to traction lever 5, first fixed block 71 and second fixed block 72 respectively with first dead lever 61 and second dead lever 62 fixed connection, and second dead lever 62 and locating piece 8 mutual rotation are connected or fixed connection, first dead lever 61 and the upper end fixed connection or the rotation of mount 2 are connected, and then be convenient for according to actual user demand, through the subassembly of drawing to adjust angle after mount 2 carry on with link 1 being connected.
The working principle is as follows: the utility model discloses a set up PMKD, with PMKD fixed connection's link 1, set up mount 2 in link 1 one side and set up coupling assembling and adjusting part between mount 2 and link 1, mount 2 is used for installing satellite antenna, adjusting part includes head rod 41 and second connecting rod 42, set up the first connecting axle 31 of head rod 41 and second connecting rod 42 one end and set up the second connecting axle 32 at the head rod 41 and the second connecting rod 42 other end, the subassembly that pulls includes the fixed locating piece 8 that sets up respectively on head rod 41 and second connecting rod 42, the second dead lever 62 that sets up between locating piece 8, set up the first dead lever 61 between mount 2 upper end, set up first fixed block 71 and second fixed block 72 on first dead lever 61 and second dead lever 62 respectively, Set up traction lever 5 between first fixed block 71 and second fixed block 72 and respectively fixed set up the connection torsional spring 9 between first dead lever 61 and second dead lever 62, and then be convenient for be connected link 1 with mount 2 through coupling assembling, and be convenient for according to actual user demand, thereby the effectual stability of guaranteeing link 1 and mount 2 and being connected, adjust the angle between link 1 and the mount 2, the effectual stability of having guaranteed satellite antenna's acceptance signal, and then the effectual improvement the utility model discloses a use precision.
The working principle is as follows: the utility model is provided with a fixed bottom plate, a connecting frame fixedly connected with the fixed bottom plate, a fixed frame arranged at one side of the connecting frame, and a connecting component and an adjusting component arranged between the fixed frame and the connecting frame, wherein the fixed frame is used for installing the satellite antenna, the adjusting component comprises a first connecting rod and a second connecting rod, a first connecting shaft arranged at one end of the first connecting rod and the second connecting rod, and a second connecting shaft arranged at the other end of the first connecting rod and the second connecting rod, the traction component comprises a positioning block respectively fixedly arranged on the first connecting rod and the second connecting rod, a second fixing rod arranged between the positioning blocks, a first fixing rod arranged between the upper ends of the fixed frame, a first fixing block and a second fixing block respectively arranged on the first fixing rod and the second fixing rod, a traction rod arranged between the first fixing block and the second fixing block, and a connecting torsion spring respectively fixedly arranged between the first fixing rod and the second fixing rod, and then be convenient for be connected the link with the mount through coupling assembling, and be convenient for according to actual user demand to the effectual stability of having guaranteed that the link is connected with the mount adjusts the angle between link and the mount, the effectual stability of having guaranteed satellite antenna's received signal, and then the effectual improvement the utility model discloses a use precision.
The device obtained through the design can basically improve the problem that the existing installation structure for the satellite antenna is not capable of meeting the use requirements of multiple use requirements of the installation structure for the satellite antenna at present due to the design characteristics of the installation structure and the installation structure, the structure is simple, the use mode is single, and the accuracy of installation of the satellite antenna is further reduced.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (6)
1. The utility model provides a satellite antenna is with stabilizing mounting structure which characterized in that: the satellite antenna fixing device comprises a fixing bottom plate, a connecting frame (1) fixedly connected with the fixing bottom plate, a fixing frame (2) arranged on one side of the connecting frame (1), and a connecting assembly and an adjusting assembly arranged between the fixing frame (2) and the connecting frame (1), wherein the fixing frame (2) is used for mounting a satellite antenna;
the adjusting assembly comprises a first connecting rod (41) and a second connecting rod (42), a first connecting shaft (31) arranged at one end of the first connecting rod (41) and one end of the second connecting rod (42), and a second connecting shaft (32) arranged at the other end of the first connecting rod (41) and the other end of the second connecting rod (42);
the connecting assembly comprises positioning blocks (8) fixedly arranged on a first connecting rod (41) and a second connecting rod (42) respectively, second fixing rods (62) arranged between the positioning blocks (8), first fixing rods (61) arranged between the upper ends of the fixing frames (2), first fixing blocks (71) and second fixing blocks (72) arranged on the first fixing rods (61) and the second fixing rods (62) respectively, traction rods (5) arranged between the first fixing blocks (71) and the second fixing blocks (72) and connecting torsion springs (9) fixedly arranged between the first fixing rods (61) and the second fixing rods (62) respectively.
2. The stable mounting structure for the satellite antenna according to claim 1, wherein the fixing frame (2) is arranged in a shape of a Chinese character jing, the fixing frame (2) is used for being connected with a connecting component, and the lower end of the fixing frame (2) is used for being connected with an adjusting component.
3. The stable mounting structure for satellite antenna as claimed in claim 2, wherein the first connecting shaft (31) penetrates through one end of the first connecting rod (41) and the second connecting rod (42) respectively and is hinged with the connecting frame (1), and the first connecting shaft (31) is fixedly connected with the first connecting rod (41) and the second connecting rod (42).
4. The stable mounting structure for the satellite antenna according to claim 3, wherein the second connecting shaft (32) penetrates through the other ends of the first connecting rod (41) and the second connecting rod (42) and is fixedly connected with the lower end of the fixing frame (2), and the second connecting shaft (32) is fixedly connected with the first connecting rod (41) and the second connecting rod (42).
5. The stable mounting structure for the satellite antenna is characterized in that the draw bar (5) penetrates through the first fixing block (71) and the second fixing block (72) respectively, through holes matched with the draw bar (5) are formed in the first fixing block (71) and the second fixing block (72), the inner diameter of each through hole is larger than the outer diameter of the draw bar (5), a limiting ring is fixedly arranged on the draw bar (5), and the outer diameter of each limiting ring is larger than the outer diameter of each through hole.
6. The stable mounting structure for the satellite antenna according to claim 5, wherein the first fixing block (71) and the second fixing block (72) are respectively fixedly connected with the first fixing rod (61) and the second fixing rod (62), the second fixing rod (62) and the positioning block (8) are mutually rotatably or fixedly connected, and the first fixing rod (61) is fixedly or rotatably connected with the upper end of the fixing frame (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922133226.XU CN211655025U (en) | 2019-12-03 | 2019-12-03 | Stable mounting structure for satellite antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922133226.XU CN211655025U (en) | 2019-12-03 | 2019-12-03 | Stable mounting structure for satellite antenna |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211655025U true CN211655025U (en) | 2020-10-09 |
Family
ID=72694205
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922133226.XU Active CN211655025U (en) | 2019-12-03 | 2019-12-03 | Stable mounting structure for satellite antenna |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211655025U (en) |
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2019
- 2019-12-03 CN CN201922133226.XU patent/CN211655025U/en active Active
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