CN215431386U - Auxiliary tool for satellite antenna panel rivet - Google Patents
Auxiliary tool for satellite antenna panel rivet Download PDFInfo
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- CN215431386U CN215431386U CN202121974148.7U CN202121974148U CN215431386U CN 215431386 U CN215431386 U CN 215431386U CN 202121974148 U CN202121974148 U CN 202121974148U CN 215431386 U CN215431386 U CN 215431386U
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Abstract
An auxiliary tool for a satellite antenna panel rivet comprises an auxiliary panel, a positioning assembly and two supporting seats, wherein a plurality of holes are formed in the surface of the auxiliary panel, rotating shafts are fixedly connected to two sides of the auxiliary panel respectively, the rotating shafts of the auxiliary panel are rotatably connected with the two supporting seats respectively, the positioning assembly comprises a positioning rod, a first bolt hole and a second bolt hole are formed in each rotating shaft, and the first bolt hole and the second bolt hole are crossed and are located in different directions of the rotating shafts; the upper surface of the supporting seat is provided with a first positioning hole and a second positioning hole; the first bolt hole corresponds to the first positioning hole, the second bolt hole corresponds to the second positioning hole, and the positioning rod can be inserted into the first positioning hole through the first bolt hole or inserted into the second positioning hole through the second bolt hole. This application has the very convenient effect of installation rivet.
Description
Technical Field
The application relates to the field of satellite antennas, in particular to an auxiliary tool for a satellite antenna panel rivet.
Background
To satellite antenna panel installation rivet, the satellite antenna panel is parallel with ground, and installer need be located the top or the below of satellite antenna panel, and when up or down up installation rivet down from down, the installation can be very hard.
In view of the above-mentioned related art, the inventor has considered that the satellite antenna panel has a drawback that it is very laborious to set the rivets.
SUMMERY OF THE UTILITY MODEL
In order to solve the problem that there is the mounting rivet very hard in the satellite antenna panel, this application provides a satellite antenna panel auxiliary fixtures for rivet.
The application provides a satellite antenna panel auxiliary fixtures for rivet adopts following technical scheme:
an auxiliary tool for a satellite antenna panel rivet comprises an auxiliary panel, a positioning assembly and two supporting seats, wherein a plurality of holes are formed in the surface of the auxiliary panel, rotating shafts are fixedly connected to two sides of the auxiliary panel respectively, the rotating shafts of the auxiliary panel are rotatably connected with the two supporting seats respectively, the positioning assembly comprises a positioning rod, a first bolt hole and a second bolt hole are formed in each rotating shaft, and the first bolt hole and the second bolt hole are crossed and are located in different directions of the rotating shafts; the upper surface of the supporting seat is provided with a first positioning hole and a second positioning hole; the first bolt hole corresponds to the first positioning hole, the second bolt hole corresponds to the second positioning hole, and the positioning rod can be inserted into the first positioning hole through the first bolt hole or inserted into the second positioning hole through the second bolt hole.
By adopting the technical scheme, the fixed rod can pass through the first bolt hole on the rotating shaft and be inserted into the first positioning hole of the supporting seat, the auxiliary panel can be fixed on the supporting seat, and an installer can conveniently fix the satellite antenna panel on the auxiliary panel; when the auxiliary panel is rotated to the position opposite to the second bolt hole and the second positioning hole, the positioning rod is inserted into the second positioning hole through the second bolt hole, the auxiliary panel is fixed on the supporting seat and is perpendicular to the ground, an installer is located on one side of the auxiliary panel at the moment, and rivets are installed on the satellite antenna panel, so that labor can be saved.
Optionally, the two supporting seats are fixedly connected with bases, through holes are formed in the middle positions of the two bases, bearings are arranged in the two bases, the rotating shaft is fixedly connected with the inner ring surfaces of the bearings, and the bases are fixedly connected with the outer ring surfaces of the bearings.
Through adopting above-mentioned technical scheme, the frictional force between the reducible pivot of bearing in the base and the base, the relative supporting seat of auxiliary panel of being convenient for of bearing rotates.
Optionally, a gasket is fixedly connected to the positioning rod, and the outer diameter of the gasket is larger than the inner diameters of the first bolt hole and the second bolt hole.
By adopting the technical scheme, the gasket can prevent the positioning rod from penetrating through the rotating shaft and being separated from the rotating shaft when the positioning rod is inserted into the first bolt hole or the second bolt hole; whether can also be inconsistent with the pivot through the gasket, whether the therefrom learns the locating lever and fixed good with the supporting seat.
Optionally, a handle is arranged at the top end of the positioning rod.
Through adopting above-mentioned technical scheme, can make things convenient for and laborsaving when plug locating lever.
Optionally, the two side edges of the surface of the auxiliary panel are fixedly connected with arc-shaped limiting plates.
Through adopting above-mentioned technical scheme, the satellite antenna panel is arranged in between two arc limiting plates, and the arc limiting plate can be fixed the both sides of satellite antenna panel to can prevent that the satellite antenna panel from dropping from the both sides of supplementary panel.
Optionally, the surface of arc limiting plate is equipped with a plurality of fixed slots, and the interior anchor ring of fixed slot is the screw thread, and the surperficial swing joint of arc limiting plate has fixed cover, and the both sides edge of fixed cover is equipped with a plurality ofly and fixed slot matched with fixed orifices, and the fixed orifices overhead has the screw, and the screw passes the fixed orifices of fixed cover and the fixed slot threaded connection of arc limiting plate.
Through adopting above-mentioned technical scheme, when the supplementary panel of upset, fixed cover can be used to prevent when the supplementary panel of upset, and the satellite antenna panel that is located above the supplementary panel breaks away from with the supplementary panel.
Optionally, the bottom of the auxiliary panel is fixedly connected with a plurality of reinforcing ribs.
Through adopting above-mentioned technical scheme, increase the strengthening rib in the bottom of auxiliary panel, can avoid auxiliary panel to warp, and strengthen auxiliary panel's steadiness.
Optionally, a groove is formed in the supporting seat, and the positioning rod can pass through the first positioning hole or the second positioning hole and is arranged in the groove.
Through adopting above-mentioned technical scheme, can prevent in the supporting seat because of getting into a large amount of foreign matters, difficult clearance leads to the locating lever to pass first locating hole or second locating hole after, the locating lever can't contact with the bottom of recess.
In summary, the present application includes at least one of the following beneficial technical effects:
1. the fixing rod can pass through the first bolt hole on the rotating shaft and be inserted into the first positioning hole of the supporting seat, the auxiliary panel can be fixed on the supporting seat, and an installer can conveniently fix the satellite antenna panel on the auxiliary panel; rotating the auxiliary panel until the second bolt hole is opposite to the second positioning hole, inserting the positioning rod into the second positioning hole through the second bolt hole, fixing the auxiliary panel on the supporting seat, enabling the auxiliary panel to be perpendicular to the ground, enabling an installer to be located on one side of the auxiliary panel at the moment, and installing rivets on the satellite antenna panel, and being labor-saving;
2. the satellite antenna panel is arranged between the two arc limiting plates, and the two sides of the satellite antenna panel can be fixed by the arc limiting plates, so that the satellite antenna panel can be prevented from falling from the two sides of the auxiliary panel;
3. the surface of arc limiting plate is equipped with a plurality of fixed slots, and the interior anchor ring of fixed slot is the screw thread, and the surperficial swing joint of arc limiting plate has fixed cover, and the both sides edge of fixed cover is equipped with a plurality ofly and fixed slot matched with fixed orifices, and the fixed orifices overhead has the screw, and the screw passes the fixed orifices of fixed cover and the fixed slot threaded connection of arc limiting plate.
Drawings
Fig. 1 is a schematic structural diagram of the whole of the embodiment of the present application.
FIG. 2 is a schematic view showing the structure of the auxiliary panel of the present embodiment.
Fig. 3 is a schematic view showing the structure of the reinforcing bar of the present embodiment.
FIG. 4 is a schematic view showing the supporting seat of the present embodiment.
FIG. 5 is a schematic view showing the positioning assembly of the present embodiment.
Description of reference numerals: 1. an auxiliary panel; 11. an aperture; 12. a rotating shaft; 13. an arc limiting plate; 131. fixing grooves; 14. a fixed cover; 141. a fixing hole; 15. a screw; 16. reinforcing ribs; 2. a positioning assembly; 21. positioning a rod; 211. a handle; 212. a gasket; 22. a first pin hole; 23. a second pin hole; 3. a supporting seat; 31. a base; 32. a bearing; 34. a groove; 35. a first positioning hole; 36. and a second positioning hole.
Detailed Description
The present application is described in further detail below with reference to figures 1-5.
The embodiment of the application discloses satellite antenna panel auxiliary fixtures for rivet.
Referring to fig. 1 and 2, the auxiliary tool for the satellite antenna panel rivet comprises an auxiliary panel 1, a positioning assembly 2 and two supporting seats 3, wherein a plurality of holes 11 are formed in the surface of the auxiliary panel 1, rotating shafts 12 are fixedly connected to two sides of the auxiliary panel 1, and the rotating shafts 12 on the two sides are respectively in rotating connection with the supporting seats 3 on the two sides; the edge of both sides of the upper surface of the auxiliary panel 1 is fixedly connected with an arc-shaped limit plate 13, the arc-shaped limit plates 13 on both sides are provided with a plurality of fixing grooves 131 which are parallel to each other, the inner annular surface of each fixing groove 131 is a thread, the surface of each arc-shaped limit plate 13 is movably connected with a fixing cover 14, each fixing cover 14 consists of a plurality of arc-shaped plates which are parallel to each other and a vertical plate which is perpendicular to the plurality of arc-shaped plates, the edge of both sides of the surface of each fixing cover 14 is provided with a plurality of fixing holes 141 which are matched with the fixing grooves 131, the fixing holes 141 are provided with screws 15, and the screws 15 can penetrate through the fixing holes 141 of the fixing covers 14 to be in threaded connection with the fixing grooves 131 of the arc-shaped limit plates 13; the satellite antenna panel is arranged on the auxiliary panel 1, the arc limiting plates 13 on the two sides can clamp the satellite antenna panel, and the fixing cover 14 can prevent the satellite antenna panel from being separated from the auxiliary panel 1 in the overturning process of the satellite antenna panel.
Referring to fig. 3, a plurality of ribs 16 are fixedly connected to the bottom of the auxiliary panel 1, and the ribs 16 can enhance the stability of the auxiliary panel 1 and prevent the deformation of the auxiliary panel 1.
Referring to fig. 4 and 5, the two support bases 3 are all connected with the base 31 through bolts, a through hole is formed in the middle of each of the two bases 31, the bearing 32 is arranged in each through hole of the base 31, the rotating shaft 12 is fixedly connected with the inner annular surface of the bearing 32, the base 31 is fixedly connected with the outer annular surface of the bearing 32, and the friction force between the rotating shaft 12 and the base 31 can be reduced by the bearing 32.
The positioning assembly 2 comprises a positioning rod 21, a first bolt hole 22 is formed in the rotating shaft 12, a first positioning hole 35 is formed in the upper surface of the supporting seat 3, the first positioning hole 35 corresponds to the first bolt hole 22, a groove 34 is formed in the supporting seat 3, the positioning rod 21 can sequentially penetrate through the first bolt hole 22 and the first positioning hole 35, and the bottom of the positioning rod is arranged in the groove 34 and is in contact with the bottom of the groove 34.
The rotating shaft 12 is provided with a second bolt hole 23, the upper surface of the supporting seat 3 is provided with a second positioning hole 36, the second positioning hole 36 corresponds to the second bolt hole 23, the first bolt hole 22 and the second bolt hole 23 are crossed and positioned at different directions of the rotating shaft 12, and the positioning rod 21 can sequentially pass through the second bolt hole 23 and the second positioning hole 36 and is arranged in the groove 34 to be contacted with the bottom of the groove 34.
Referring to fig. 4, the top end of the positioning rod 21 is fixedly connected with a gasket 212, and whether the positioning rod 21 abuts against the bottom of the groove 34 can be known through whether the gasket 212 abuts against the rotating shaft 12, and the handle 211 is fixedly connected to the gasket 212, when the auxiliary panel 1 needs to be turned over, the positioning rod 21 needs to be pulled out first, and then the positioning rod 21 is inserted into the rotating shaft 12 and the supporting seat 3, so that the handle 211 can more easily insert and pull the positioning rod 21.
The implementation principle of satellite antenna panel appurtenance for rivet is: when the auxiliary panel 1 is parallel to the ground, the positioning rod 21 is inserted into the first positioning hole 35 through the first bolt hole 22, and at this time, if an installer needs to install a rivet, the installer needs to install the rivet on the satellite antenna panel below the auxiliary panel 1 from bottom to top, the satellite antenna panel is arranged on the auxiliary panel 1, and the fixing cover 14 is in threaded connection with the arc-shaped limiting plate 13 of the auxiliary panel 1; when the satellite antenna panel needs to be riveted, the positioning rod 21 is pulled out of the supporting seat 3, the auxiliary panel 1 is turned over until the second bolt hole 23 is opposite to the second positioning hole 36, the positioning rod 21 is inserted into the second positioning hole 36 through the second bolt hole 23, and an installer can conveniently install rivets on the satellite antenna panel only by positioning the positioning rod on the side face of the auxiliary panel 1.
The above embodiments are preferred embodiments of the present application, and the protection scope of the present application is not limited by the above embodiments, so: all equivalent changes made according to the structure, shape and principle of the present application shall be covered by the protection scope of the present application.
Claims (8)
1. The utility model provides a satellite antenna panel auxiliary fixtures for rivet, includes auxiliary panel (1), locating component (2) and two supporting seats (3), its characterized in that: the surface of the auxiliary panel (1) is provided with a plurality of holes (11), two sides of the auxiliary panel (1) are respectively and fixedly connected with a rotating shaft (12), the rotating shaft (12) of the auxiliary panel (1) is respectively and rotatably connected with the two supporting seats (3), the positioning assembly (2) comprises a positioning rod (21), the rotating shaft (12) is provided with a first bolt hole (22) and a second bolt hole (23), and the first bolt hole (22) and the second bolt hole (23) are crossed and are positioned in different directions of the rotating shaft (12); the upper surface of the supporting seat (3) is provided with a first positioning hole (35) and a second positioning hole (36); the first bolt hole (22) corresponds to the first positioning hole (35), the second bolt hole (23) corresponds to the second positioning hole (36), and the positioning rod (21) can be inserted into the first positioning hole (35) through the first bolt hole (22) or inserted into the second positioning hole (36) through the second bolt hole (23).
2. The auxiliary tool for the satellite antenna panel rivet according to claim 1, characterized in that: equal fixedly connected with base (31) on two supporting seats (3), the through-hole has been seted up to the middle part position of two base (31), all is equipped with bearing (32) in two base (31), and pivot (12) and the interior anchor ring fixed connection of bearing (32), base (31) and the outer anchor ring fixed connection of bearing (32).
3. The auxiliary tool for the satellite antenna panel rivet according to claim 1, characterized in that: the positioning rod (21) is fixedly connected with a gasket (212), and the outer diameter of the gasket (212) is larger than the inner diameters of the first bolt hole (22) and the second bolt hole (23).
4. The auxiliary tool for the satellite antenna panel rivet according to claim 3, characterized in that: the top end of the positioning rod (21) is provided with a handle (211).
5. The auxiliary tool for the satellite antenna panel rivet according to claim 1, characterized in that: the two side edges of the surface of the auxiliary panel (1) are fixedly connected with arc-shaped limiting plates (13).
6. The auxiliary tool for the satellite antenna panel rivet according to claim 5, characterized in that: the surface of arc limiting plate (13) is equipped with a plurality of fixed slots (131), and the interior anchor ring of fixed slot (131) is the screw thread, and the surface swing joint of arc limiting plate (13) has fixed cover (14), and the both sides edge of fixed cover (14) is equipped with a plurality ofly and fixed slot (131) matched with fixed orifices (141), and the fixed orifices (141) overhead screw (15), fixed orifices (141) that fixed cover (14) were passed in screw (15) and fixed slot (131) threaded connection of arc limiting plate (13).
7. The auxiliary tool for the satellite antenna panel rivet according to claim 5, characterized in that: the bottom of the auxiliary panel (1) is fixedly connected with a plurality of reinforcing ribs (16).
8. The auxiliary tool for the satellite antenna panel rivet according to claim 1, characterized in that: a groove (34) is arranged in the supporting seat (3), and the positioning rod (21) can pass through the first positioning hole (35) or the second positioning hole (36) and is arranged in the groove (34).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121974148.7U CN215431386U (en) | 2021-08-20 | 2021-08-20 | Auxiliary tool for satellite antenna panel rivet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121974148.7U CN215431386U (en) | 2021-08-20 | 2021-08-20 | Auxiliary tool for satellite antenna panel rivet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215431386U true CN215431386U (en) | 2022-01-07 |
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ID=79695667
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121974148.7U Active CN215431386U (en) | 2021-08-20 | 2021-08-20 | Auxiliary tool for satellite antenna panel rivet |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215431386U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116765311A (en) * | 2023-06-20 | 2023-09-19 | 湖南六九零六信息科技股份有限公司 | Riveting device of parabolic antenna for satellite communication vehicle |
-
2021
- 2021-08-20 CN CN202121974148.7U patent/CN215431386U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116765311A (en) * | 2023-06-20 | 2023-09-19 | 湖南六九零六信息科技股份有限公司 | Riveting device of parabolic antenna for satellite communication vehicle |
| CN116765311B (en) * | 2023-06-20 | 2023-12-12 | 湖南六九零六信息科技股份有限公司 | Riveting device of parabolic antenna for satellite communication vehicle |
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