CN216120697U - Satellite antenna installation device simple to operate - Google Patents
Satellite antenna installation device simple to operate Download PDFInfo
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- CN216120697U CN216120697U CN202122018058.7U CN202122018058U CN216120697U CN 216120697 U CN216120697 U CN 216120697U CN 202122018058 U CN202122018058 U CN 202122018058U CN 216120697 U CN216120697 U CN 216120697U
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- rod
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- satellite antenna
- block
- screw rod
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Abstract
The utility model discloses a satellite antenna installation device simple in operation, which comprises a first installation rod and a top plate, wherein a supporting mechanism is arranged below the first installation rod, a first screw rod is arranged above the first installation rod, a second installation rod is connected to the outside of the first screw rod, a linkage rod is arranged inside the top plate, a conical gear is connected to one side of the linkage rod, a toothed rod is connected to the upper side of the conical gear, a rotating platform is arranged above the toothed rod, a clamping block is arranged above the rotating platform, a fixed seat is connected to one side of the clamping block, a lifting block is connected to one side of the fixed seat, and a second screw rod is connected to the lower side of the lifting block. This satellite antenna installation device easy operation has set up and has turned round piece and gangbar, and installation device drives the satellite antenna and rotates when just passing the piece of turning round, and installation device drives the satellite antenna and goes up and down when the piece is turned round in the reversal, is favorable to the angle of quick adjustment satellite antenna, and the staff's of being convenient for easy operation changes.
Description
Technical Field
The utility model relates to the technical field of satellite antennas, in particular to a satellite antenna mounting device which is simple to operate.
Background
The satellite antenna is a commonly-known cauldron, 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 by a satellite and removing noise as far as possible, most of the antennas are parabolic, and some multi-focus antennas are formed by combining a spherical surface and a paraboloid, and a mounting device is required to be used in the use process of the satellite antenna, but the mounting device of the satellite antenna in the current market still has the following problems:
1. the installation device of the small satellite antenna in the current market needs a large number of tools in the installation process, the transportation process of the installation device is very complicated, and the transportation is more troublesome in the process of carrying a large number of installation devices, so that great inconvenience is brought to workers;
2. in the process of receiving signals by the satellite antenna, the satellite antenna needs to be debugged, so that the satellite antenna is located at the strongest position of the received signals, and needs to be rotated and lifted in the debugging process, so that the operation is very troublesome, and the use of workers is not facilitated.
Aiming at the problems, the novel design is carried out on the basis of the original satellite antenna installation device.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a satellite antenna installation device which is simple to operate, and aims to solve the problems that a large number of tools are required to be used in the installation process of the installation device of the small satellite antenna in the current market, the transportation process of the installation device is very complicated, the transportation is more troublesome in the process of carrying a large number of installation devices, great inconvenience is brought to workers, the satellite antenna needs to be debugged in the process of receiving signals by the satellite antenna, the satellite antenna is positioned at the strongest position of the received signals, the satellite antenna needs to be rotated and lifted in the debugging process, the operation is very troublesome, and the use of the satellite antenna is not facilitated.
In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides a satellite antenna installation device easy operation, includes first installation pole and roof, first installation pole below is provided with supporting mechanism, and is provided with first lead screw above the first installation pole to first lead screw external connection has the second installation pole, the roof is inside to be provided with the gangbar, and gangbar one side is connected with conical gear to the conical gear top is connected with the toothed bar, the toothed bar top is provided with rotary platform, and the rotary platform top is provided with the block to block one side is connected with the fixing base, fixing base one side is connected with the elevator, and the elevator below is connected with the second lead screw to second lead screw one side cover has the belt.
Preferably, the first mounting rod and the splicing block are clamped with each other, the splicing block and the first screw rod are integrally mounted, and the first mounting rod and the second mounting rod form a thread lifting structure through the first screw rod.
Preferably, the supporting mechanism includes first bracing piece, second bracing piece, third bracing piece, runs through pole, dwang, butt joint pole, draw-in groove, first bracing piece one side is connected with the dwang, dwang one side is connected with the butt joint pole, the butt joint pole top is provided with the draw-in groove, the even equidistance distribution of draw-in groove is in first installation pole bottom, draw-in groove and the mutual block of butt joint pole, it runs through first installation pole and butt joint pole to run through the pole.
Preferably, the linkage rod and the bevel gear integrally rotate, the bevel gear is connected with the toothed rod in a meshed mode, the bottom of the toothed rod is connected with a driven gear, and a twisting block is arranged on one side of the linkage rod.
Preferably, a first ratchet wheel and a second ratchet wheel are connected above the toothed rod, the first ratchet wheel and the rotating platform are integrally installed, the second ratchet wheel and the second screw rod form a rotating structure through a belt, and the rotating directions of the first ratchet wheel and the second ratchet wheel are opposite.
Preferably, the second screw rod and the fixed seat form a threaded lifting structure through the lifting block, and the fixed seat and the clamping block are connected in a rotating manner.
Compared with the prior art, the utility model has the beneficial effects that: the satellite antenna installation device with simple operation is provided with a plurality of fixing holes,
1. the supporting mechanism and the mounting rod of the device are all arranged into a clamping structure, so that mounting equipment is not needed in the mounting process, workers can mount the mounting equipment quickly and dismount the mounting equipment quickly, the workers can transport the mounting equipment conveniently, and the transportation cost of the device is reduced conveniently;
2. the torsion block and the linkage rod are arranged, the mounting device drives the satellite antenna to rotate when the torsion block is positively transmitted, and drives the satellite antenna to lift when the torsion block is reversely rotated, so that the angle of the satellite antenna can be quickly adjusted, and the operation of workers is simplified.
Drawings
FIG. 1 is a schematic view of the overall front view structure of the present invention;
FIG. 2 is a schematic front view of the twisting block and the linkage rod of the present invention;
FIG. 3 is a schematic bottom view of the card slot of the present invention;
FIG. 4 is a schematic perspective view of the supporting mechanism of the present invention;
FIG. 5 is an enlarged view of the structure at A in FIG. 2 according to the present invention.
In the figure: 1. a first mounting bar; 2. a support mechanism; 201. a first support bar; 202. a second support bar; 203. a third support bar; 204. penetrating the rod; 205. rotating the rod; 206. a docking rod; 207. a card slot; 3. splicing blocks; 4. a first lead screw; 5. a second mounting bar; 6. a twisting block; 7. a linkage rod; 8. a top plate; 9. a toothed bar; 10. a bevel gear; 11. a belt; 12. rotating the platform; 13. a lifting block; 14. a second lead screw; 15. a fixed seat; 16. a first ratchet tooth; 17. a second ratchet; 18. and a clamping block.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-4, a satellite antenna installation device with simple operation comprises a first installation rod 1 and a top plate 8, in order to rapidly install and disassemble the installation device, a support mechanism 2 is arranged below the first installation rod 1, a first lead screw 4 is arranged above the first installation rod 1, a second installation rod 5 is connected outside the first lead screw 4, the first installation rod 1 and a splicing block 3 are mutually clamped, the splicing block 3 and the first lead screw 4 are integrally installed, the first installation rod 1 and the second installation rod 5 form a thread lifting structure through the first lead screw 4, the support mechanism 2 comprises a first support rod 201, a second support rod 202, a third support rod 203, a penetrating rod 204, a rotating rod 205, a butt joint rod 206 and a clamping groove 207, one side of the first support rod 201 is connected with the rotating rod 205, one side of the rotating rod 205 is connected with the butt joint rod 206, the clamping groove 207 is arranged above the butt joint rod 206, the even equidistance of draw-in groove 207 distributes in first installation pole 1 bottom, draw-in groove 207 and the mutual block of butt joint pole 206 run through pole 204 and run through first installation pole 1 and butt joint pole 206, with first installation pole 1 and the mutual block of supporting mechanism 2, later with first installation pole 1 and second installation pole 5 through first lead screw 4 being connected, accomplish installation device's installation promptly, be favorable to need not to use equipment to accomplish the installation work of device, be convenient for the rapid transit of device.
Referring to fig. 1-5, in order to quickly adjust the angle of the satellite antenna, a linkage rod 7 is disposed inside a top plate 8, a conical gear 10 is connected to one side of the linkage rod 7, a toothed rod 9 is connected to the upper side of the conical gear 10, a rotary platform 12 is disposed above the toothed rod 9, a clamping block 18 is disposed above the rotary platform 12, a fixing seat 15 is connected to one side of the clamping block 18, a lifting block 13 is connected to one side of the fixing seat 15, a second lead screw 14 is connected to the lower side of the lifting block 13, a belt 11 is sleeved on one side of the second lead screw 14, the linkage rod 7 and the conical gear 10 integrally rotate, the conical gear 10 and the toothed rod 9 are connected in a meshing manner, a driven gear is connected to the bottom of the toothed rod 9, a torsion block 6 is disposed on one side of the linkage rod 7, a first ratchet 16 and a second ratchet 17 are connected to the upper side of the toothed rod 9, and first ratchet 16 and rotary platform 12 are integrated installation, and second ratchet 17 passes through belt 11 and second lead screw 14 and constitutes rotating-structure, and first ratchet 16 is opposite with the direction of rotation of second ratchet 17, and second lead screw 14 passes through elevator 13 and fixing base 15 and constitutes screw thread elevation structure, and the connected mode of fixing base 15 and block piece 18 is for rotating the connection, and accessible rotates the piece 6 and accomplishes the rotation of rotary platform 12 and the lift of fixing base 15, be favorable to the staff to operate simplyfication, be convenient for the staff to use.
The working principle is as follows: according to fig. 1-4, firstly, the butt joint rod 206 is inserted into the clamping groove 207 at the bottom of the first installation rod 1, then the penetrating rod 204 sequentially penetrates through the three butt joint rods 206 and the first installation rod 1, then the first support rod 201 is adjusted to be closely attached to the ground through the rotating rod 205, the second support rod 202 and the third support rod 203 are the same as above, then the splicing block 3 and the first lead screw 4 are inserted into the first installation rod 1, then the second installation rod 5 is in threaded splicing with the first lead screw 4, and the second installation rod 5 is rotated when the height of the installation rod needs to be adjusted (the splicing block 3 fixes the first lead screw 4 in the first installation rod 1);
according to the figures 1-5, after the installation of the installation rod, the satellite antenna and the fixed seat 15 are installed, when the angle of the satellite antenna needs to be adjusted after the installation, the forward rotation twisting block 6 enables the linkage rod 7 to rotate forward, the linkage rod 7 drives the toothed rod 9 to rotate forward through the bevel gear 10, so that the first ratchet 16 drives the rotary platform 12 to rotate (at the moment, the second ratchet 17 is not moved), the rotation of the twisting block 6 is stopped after the linkage rod is adjusted to a proper angle, the reverse rotation twisting block 6 enables the second ratchet 17 to rotate (at the moment, the first ratchet 16 is not moved) when the height of the satellite antenna needs to be adjusted, the second ratchet 17 drives the second screw rod 14 to rotate through the belt 11 (the second screw rod 14 is a reciprocating screw rod), the second screw rod 14 and the lifting block 13 generate a threaded motion, so that the lifting block 13 drives the fixed seat 15 to ascend, the other side of the fixed seat 15 is fixed at the rotary platform 12 through the clamping block 18, the lifting to the proper position and the stopping are all required, which is the working process of the whole device, and the content not described in detail in the specification belongs to the prior art known by the professional in the field.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. A satellite antenna installation device easy to operate comprises a first installation rod (1) and a top plate (8), and is characterized in that: the improved structure of the belt conveyor is characterized in that a supporting mechanism (2) is arranged below the first installation rod (1), a first screw rod (4) is arranged above the first installation rod (1), a second installation rod (5) is connected to the outer portion of the first screw rod (4), a linkage rod (7) is arranged inside the top plate (8), a bevel gear (10) is connected to one side of the linkage rod (7), a toothed rod (9) is connected to the upper portion of the bevel gear (10), a rotary platform (12) is arranged above the toothed rod (9), a clamping block (18) is arranged above the rotary platform (12), a fixing seat (15) is connected to one side of the clamping block (18), a lifting block (13) is connected to one side of the fixing seat (15), a second screw rod (14) is connected to the lower portion of the lifting block (13), and a belt (11) is sleeved to one side of the second screw rod (14).
2. A satellite antenna mounting arrangement that is simple to operate as claimed in claim 1, wherein: the first installation rod (1) and the splicing block (3) are clamped with each other, the splicing block (3) and the first screw rod (4) are installed in an integrated mode, and the first installation rod (1) and the second installation rod (5) form a thread lifting structure through the first screw rod (4).
3. A satellite antenna mounting arrangement that is simple to operate as claimed in claim 2, wherein: supporting mechanism (2) include first bracing piece (201), second bracing piece (202), third bracing piece (203), run through pole (204), dwang (205), butt joint pole (206), draw-in groove (207), first bracing piece (201) one side is connected with dwang (205), dwang (205) one side is connected with butt joint pole (206), butt joint pole (206) top is provided with draw-in groove (207), draw-in groove (207) even equidistance distribution is in first installation pole (1) bottom, draw-in groove (207) and butt joint pole (206) block each other, run through pole (204) and run through first installation pole (1) and butt joint pole (206).
4. A satellite antenna mounting arrangement that is simple to operate as claimed in claim 1, wherein: the linkage rod (7) and the bevel gear (10) are integrally rotated, the bevel gear (10) is connected with the toothed rod (9) in a meshed mode, the bottom of the toothed rod (9) is connected with the driven gear, and the twisting block (6) is arranged on one side of the linkage rod (7).
5. An operationally simple satellite antenna mounting apparatus according to claim 4, wherein: a first ratchet wheel ratchet (16) and a second ratchet wheel ratchet (17) are connected above the toothed rod (9), the first ratchet wheel ratchet (16) and the rotary platform (12) are integrally installed, the second ratchet wheel ratchet (17) and the second screw rod (14) form a rotating structure through a belt (11), and the rotating directions of the first ratchet wheel ratchet (16) and the second ratchet wheel ratchet (17) are opposite.
6. A satellite antenna mounting arrangement that is simple to operate as claimed in claim 1, wherein: the second screw rod (14) and the fixed seat (15) form a threaded lifting structure through the lifting block (13), and the fixed seat (15) is connected with the clamping block (18) in a rotating mode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122018058.7U CN216120697U (en) | 2021-08-25 | 2021-08-25 | Satellite antenna installation device simple to operate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122018058.7U CN216120697U (en) | 2021-08-25 | 2021-08-25 | Satellite antenna installation device simple to operate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216120697U true CN216120697U (en) | 2022-03-22 |
Family
ID=80728777
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122018058.7U Active CN216120697U (en) | 2021-08-25 | 2021-08-25 | Satellite antenna installation device simple to operate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216120697U (en) |
-
2021
- 2021-08-25 CN CN202122018058.7U patent/CN216120697U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20221230 Address after: No. 31-201, Junggar Road, Karamay District, Karamay City, Xinjiang Uygur Autonomous Region Patentee after: Xinjiang TIANLIAN Remote Sensing Technology Co.,Ltd. Address before: 312000 No. 66 - 9, Jiaoyu Road, Paojiang, Shaoxing, Zhejiang Patentee before: Zhang Xiao |
|
| TR01 | Transfer of patent right |