CN116454630B - Driving transmission device of satellite antenna - Google Patents
Driving transmission device of satellite antenna Download PDFInfo
- Publication number
- CN116454630B CN116454630B CN202310705486.8A CN202310705486A CN116454630B CN 116454630 B CN116454630 B CN 116454630B CN 202310705486 A CN202310705486 A CN 202310705486A CN 116454630 B CN116454630 B CN 116454630B
- Authority
- CN
- China
- Prior art keywords
- rotating
- fixedly connected
- satellite antenna
- rod
- box
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 230000005540 biological transmission Effects 0.000 title claims abstract description 47
- 230000007246 mechanism Effects 0.000 claims abstract description 31
- 244000309464 bull Species 0.000 claims abstract description 21
- 238000003756 stirring Methods 0.000 claims description 19
- 230000000149 penetrating effect Effects 0.000 claims description 7
- 238000009434 installation Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 4
- 230000001276 controlling effect Effects 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
- H01Q3/08—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02D—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
- Y02D30/00—Reducing energy consumption in communication networks
- Y02D30/70—Reducing energy consumption in communication networks in wireless communication networks
Landscapes
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
The invention discloses a driving transmission device of a satellite antenna, which comprises a rotating frame, wherein the rotating frame is internally connected with a rotating ring in a rotating way, a plurality of clamping teeth are fixedly connected onto the rotating ring, an opening is formed in the bottom of the rotating frame, and an adjusting mechanism is fixedly connected to the bottom of the rotating frame; all be provided with location protection machanism on four sides around adjustment mechanism, through the first bull stick of forward rotation, make first bull stick drive rotate the box and take place to rotate, it rotates and can drive the satellite antenna body and rotate to rotate the box, make the angle of satellite antenna body change, through the first bull stick of reverse rotation, make first bull stick drive the rotation of swivel becket, the rotation of swivel becket drives the satellite antenna body and rotates, thereby change the azimuth that makes the satellite antenna body change, and only rely on the first bull stick of forward and backward rotation to control the angle of satellite antenna body, not only the simple operation, can also the regulation satellite antenna body of wide angle range, make it can better receive the signal.
Description
Technical Field
The invention relates to the field of satellite antennas, in particular to a driving transmission device of a satellite antenna.
Background
The satellite antenna is a metal paraboloid and is responsible for reflecting satellite signals into a feed source and a tuner which are positioned at a focus; the satellite antenna is used for collecting weak signals transmitted by satellites and removing noise as much as possible;
most satellite antennas are directly fixed on a fixed object, and after the fixed object and the angle of the satellite antennas are adjusted, the operation can be omitted, but the satellite antennas are not applied to the fixed object and can also be applied to mobile carriers, such as ships on the sea;
because the ship runs on the sea surface, the ship can bump under the influence of sea waves, various angles of the satellite antenna need to be continuously adjusted in order to enable the satellite antenna to more comprehensively receive signals, and the traditional satellite antenna is limited in angle adjustment and range and easy to lose signal reception.
Disclosure of Invention
The present invention is directed to a driving transmission device for a satellite antenna, so as to solve the above technical problems.
The invention aims to solve the technical problems, and is realized by adopting the following technical scheme:
the driving transmission device of the satellite antenna comprises a rotating frame, wherein the rotating frame is internally connected with a rotating ring in a rotating way, a plurality of clamping teeth are fixedly connected onto the rotating ring, an opening is formed in the bottom of the rotating frame, and an adjusting mechanism is fixedly connected to the bottom of the rotating frame;
the adjusting mechanism is used for controlling the rotation of the satellite antenna body at a plurality of angles;
the positioning protection mechanisms are arranged on the front side, the rear side, the left side and the right side of the adjusting mechanism and used for fixedly placing the satellite antenna body, and the positioning protection mechanisms are used for protecting the satellite antenna body.
Preferably, the adjusting mechanism comprises a hollow base, a rotating groove is formed in the top of the hollow base, a rotating box is connected in the rotating groove in a rotating mode, a forward transmission assembly is fixedly connected to the bottom of the rotating box, and the forward transmission assembly is connected with the hollow base in a rotating mode.
Preferably, the hollow base is provided with a first rotating rod in a penetrating manner, the first rotating rod is rotationally connected with the hollow base, the hollow base and the forward transmission assembly are fixedly connected with belt pulleys, and the two belt pulleys are connected through a connecting belt.
Preferably, the reverse transmission assembly is fixedly connected to the top of the forward transmission assembly, the reverse transmission assembly is fixedly connected with the rotating box, the first conical gear is fixedly connected to the top of the reverse transmission assembly, the second conical gear is meshed with the first conical gear, the fifth rotating shaft is fixedly connected to the second conical gear, the fifth rotating shaft is rotationally connected with the rotating frame, the second transmission gear is fixedly connected to the fifth rotating shaft, and the second transmission gear is meshed with the plurality of clamping teeth.
Preferably, the inside of the rotating ring is connected with the fixed ring through a rotating mechanism, and the fixed ring is fixedly connected with the satellite antenna body;
the rotating mechanism is used for controlling the overturning angle of the satellite antenna body.
The beneficial effects of the invention are as follows:
1. according to the invention, the first rotating rod is rotated forward to drive the rotating box to rotate, the rotating box rotates to drive the satellite antenna body to rotate, so that the angle of the satellite antenna body is changed, and the first rotating rod is rotated in the reverse direction to drive the rotating ring to rotate, so that the azimuth angle of the satellite antenna body is changed, the angle of the satellite antenna body is controlled by only rotating the first rotating rod in the forward and reverse directions, the operation is convenient, the satellite antenna body can be regulated in a large angle range, and signals can be better received.
2. Through rotating the fixed ring, can make fixed ring move satellite antenna body and adjust the angle of looking up, and after adjusting to appointed position, the accessible presses the push rod, spacing push rod makes the push rod drive spacing head spacing seventh bull stick to when accomplishing the regulation of angle, can also carry out fine location, avoid the angle of adjusting to take place the deviation, influence satellite antenna body received signal.
3. The satellite antenna body is positioned at the appointed position through the positioning grooves, and the first connecting plate and the second connecting plate are rotationally connected, so that the first connecting plate and the second connecting plate can be vertically erected completely when the satellite antenna body is not used, the satellite antenna body is wrapped, and the satellite antenna body is protected.
4. As the surface of the satellite antenna body can form X, Y two axes, when the satellite antenna body turns over along the X axis, the elevation angle changes, when the satellite antenna body rotates along the Y axis, the azimuth angle changes, and the signal can be better received through the change of different angles, and the effect of receiving the signal can be better played due to the large rotating angle range.
Drawings
FIG. 1 is a schematic diagram of the structure of the present invention;
FIG. 2 is a schematic view of the internal structure of the hollow base of the present invention;
FIG. 3 is a schematic view of a forward drive assembly of the present invention;
FIG. 4 is a schematic view of a reverse drive assembly of the present invention;
FIG. 5 is a schematic view of the positioning cap of the present invention;
FIG. 6 is a schematic view of a positioning protection mechanism according to the present invention;
FIG. 7 is a schematic view of the structure of the connecting mechanism of the present invention;
FIG. 8 is an enlarged schematic view of portion A of FIG. 2;
FIG. 9 is an enlarged schematic view of portion B of FIG. 2;
fig. 10 is an enlarged schematic view of a portion C of fig. 6.
Reference numerals: 1. a hollow base; 2. a rotating groove; 3. a first rotating lever; 4. rotating the box; 5. a first connection plate; 6. a rotating frame; 7. a rotating ring; 8. a fixing ring; 9. a satellite antenna body; 10. a rotary tube; 11. a connecting belt; 12. a belt pulley; 13. a first rotating disc; 14. a second rotating rod; 15. a first clamping groove; 16. a first elastic driving piece; 17. a first dial; 18. a positioning plate; 19. a third rotating rod; 20. a first bevel gear; 21. a fourth rotating lever; 22. a first transmission gear; 23. a fixed rod; 24. a connecting disc; 25. a second toggle plate; 26. a second rotating disc; 27. a second elastic driving piece; 28. a ball bearing; 29. a second clamping groove; 30. positioning the cap; 31. latch teeth; 32. a second bevel gear; 33. a second transmission gear; 34. a fifth rotating shaft; 35. an opening; 36. a second connecting plate; 37. a sixth rotating rod; 38. a positioning frame; 39. a positioning block; 40. a positioning groove; 41. a push rod; 42. a limit rod; 43. a sliding frame; 44. an auxiliary tube; 45. a spring; 46. a slide plate; 47. a limit groove; 48. a seventh rotating lever; 49. a limiting block; 50. and (3) a mounting box.
Detailed Description
In order that the manner in which the above recited features, objects and advantages of the present invention are obtained, a more particular description of the invention will be rendered by reference to specific embodiments thereof which are illustrated in the appended drawings. Based on the examples in the embodiments, those skilled in the art can obtain other examples without making any inventive effort, which fall within the scope of the invention.
Specific embodiments of the present invention are described below with reference to the accompanying drawings.
Example 1:
as shown in fig. 1-10, a driving transmission device of a satellite antenna comprises a rotating frame 6, wherein the rotating frame 6 is internally and rotatably connected with a rotating ring 7, a plurality of latches 31 are fixedly connected to the rotating ring 7, an opening 35 is formed in the bottom of the rotating frame 6, and an adjusting mechanism is fixedly connected to the bottom of the rotating frame 6;
the adjusting mechanism is used for controlling the rotation of the satellite antenna body 9 at a plurality of angles;
the front, back, left and right sides of the adjusting mechanism are provided with positioning protection mechanisms, the positioning protection mechanisms are used for fixedly placing the satellite antenna body 9, and the positioning protection mechanisms are used for protecting the satellite antenna body 9;
the adjusting mechanism comprises a hollow base 1, a rotating groove 2 is formed in the top of the hollow base 1, a rotating box 4 is connected in the rotating groove 2 in a rotating mode, a forward transmission assembly is fixedly connected to the bottom of the rotating box 4, and the forward transmission assembly is connected with the hollow base 1 in a rotating mode;
the hollow base 1 is provided with a first rotating rod 3 in a penetrating manner, the first rotating rod 3 is rotationally connected with the hollow base 1, the hollow base 1 and the forward transmission assembly are fixedly connected with belt pulleys 12, and the two belt pulleys 12 are connected through a connecting belt 11;
the top of the forward transmission assembly is fixedly connected with a reverse transmission assembly, the reverse transmission assembly is fixedly connected with the rotating box 4, the top of the reverse transmission assembly is fixedly connected with a first conical gear 20, a second conical gear 32 is meshed with the first conical gear 20, a fifth rotating shaft 34 is fixedly connected to the second conical gear 32, the fifth rotating shaft 34 is rotationally connected with the rotating frame 6, a second transmission gear 33 is fixedly connected to the fifth rotating shaft 34, and the second transmission gear 33 is meshed with the plurality of clamping teeth 31;
the forward transmission assembly comprises a first rotating disc 13, the first rotating disc 13 is fixedly connected with the rotating box 4, the first rotating disc 13 is rotationally connected with the hollow base 1, a first clamping groove 15 is formed in the middle of the first rotating disc 13 in a penetrating manner, a first stirring disc 17 is arranged in the first clamping groove 15, a second rotating rod 14 is arranged on the first stirring disc 17 in a penetrating manner, the bottom of the second rotating rod 14 is rotationally connected with the hollow base 1, the second rotating rod 14 is fixedly connected with the belt pulley 12, the top of the second rotating rod 14 is fixedly connected with the reverse transmission assembly, a first elastic stirring sheet 16 is fixedly connected on the first stirring disc 17, and a torsion spring is arranged in the first elastic stirring sheet 16;
the reverse transmission assembly comprises a ball bearing 28, a plurality of fixed rods 23 are fixedly connected to the outer side of the ball bearing 28, the fixed rods 23 are fixedly connected with a rotating box 4, a connecting disc 24 is fixedly connected to the inside of the ball bearing 28, the connecting disc 24 is fixedly connected with a second rotating disc 14, the top of the connecting disc 24 is fixedly connected with a second rotating disc 26, a second clamping groove 29 is formed in the middle of the second rotating disc 26 in a penetrating manner, a second stirring disc 25 is internally provided with a second elastic stirring sheet 27, torsion springs are arranged in the second elastic stirring sheet 27, the top of the second stirring disc 25 is fixedly connected with a third rotating rod 19, the third rotating rod 19 is rotationally connected with a positioning plate 18, the positioning plate 18 is fixedly connected with the rotating box 4, the positioning plate 18 is rotationally connected with a fourth rotating rod 21, the fourth rotating rod 21 is fixedly connected with a first transmission gear 22 on the third rotating rod 19, two first transmission gears 22 are meshed, and the fourth rotating rod 21 is fixedly connected with a first conical gear 20;
through forward rotation of the first rotating rod 3, the first rotating rod 3 drives the second rotating rod 14 to rotate through the connecting belt 11 and the belt pulley 12, the second rotating rod 14 rotates to drive the first shifting disc 17 to rotate, the first shifting disc 17 rotates to drive the first elastic shifting disc 16 to rotate, and the first elastic shifting disc 16 is clamped inside the first clamping groove 15 on the rotating disc, so that the first elastic shifting disc 16 drives the first rotating disc 13 to rotate together, the first rotating disc 13 drives the rotating box 4 to rotate, the rotating box 4 rotates to drive the satellite antenna body 9 to rotate, the angle of the satellite antenna body 9 is effectively changed, and the adjusting effect is achieved;
through the reverse rotation first bull stick 3, first bull stick 3 can drive the connection pad 24 and rotate, connection pad 24 drives the rotation of second rolling disc 26, the spacing second elasticity plectrum 27 of second draw-in groove 29 that sets up in the middle is passed through to second rolling disc 26, make the second elasticity plectrum 27 drive second plectrum 25 rotate, second plectrum 25 drive third bull stick 19 bull stick, third bull stick 19 passes through first drive gear 22 and drives the rotation of fourth bull stick 21, fourth bull stick 21 passes through first conical gear 20, second conical gear 32 drives the rotation of fifth bull stick, the rotation of fifth bull stick drives second drive gear 33, the rotation of second drive gear 33 drives the rotation of swivel joint 7 through a plurality of clamping teeth 31 with it, the rotation of swivel joint 7 can drive satellite antenna body 9 and rotate, thereby can effectually change the azimuth of satellite antenna body 9, and adjustable angle scope is big.
Example 2:
as shown in fig. 1 to 10, in the case where the other portions are the same as in embodiment 1, this embodiment differs from embodiment 1 in that: the rotating mechanism comprises a rotating tube 10, the rotating tube 10 is fixedly connected with a rotating ring 7, a seventh rotating rod 48 is rotatably connected inside the rotating tube 10, the seventh rotating rod 48 is fixedly connected with a fixed ring 8, a plurality of limiting grooves 47 are formed in the seventh rotating rod 48, an installation box 50 is fixedly connected to the top and the bottom of the rotating tube 10, a sliding plate 46 is slidably connected inside the installation box 50, a plurality of limiting blocks 49 are fixedly connected to the bottom of the sliding plate 46, a push rod 41 penetrates through the installation box 50, the push rod 41 is fixedly connected with the sliding plate 46, a spring 45 is sleeved on the push rod 41, one end of the spring 45 is fixedly connected with the sliding plate 46, the other end of the spring 45 is fixedly connected with the installation box 50, the other end of the push rod 41 is fixedly connected with the installation box 50, an auxiliary tube 44 is fixedly connected to one end of the installation box 50, which is far away from the rotating tube 10, of the auxiliary tube 44 is fixedly connected with a plurality of sliding frames 43, and a limiting rod 42 is slidably connected inside the sliding frame 43;
the fixed ring 8 is rotated, so that the fixed ring 8 drives the satellite antenna body 9 to turn up and down, when the satellite antenna body 9 turns to a proper angle, the push rod 41 can be pressed, the push rod 41 drives the push rod to be close to the seventh rotating rod 48, and the push rod drives the limiting block 49 to be close to the seventh rotating rod 48, so that the limiting block 49 is clamped with the limiting groove 47 on the seventh rotating rod 48, and the effect of limiting the seventh rotating rod 48 is achieved;
when stopper 49 and spacing groove 47 joint, push rod 41 also will be located inside auxiliary pipe 44, can promote gag lever post 42 at this moment, makes the spacing push rod 41 of gag lever post 42, and stopper 49 will be closely laminated all the time with the draw-in groove like this, can be fine play the effect of location, avoid appearing the problem of angular offset.
Example 3:
as shown in fig. 1 to 10, in the case where the other portions are the same as in embodiment 1, this embodiment differs from embodiment 1 in that: the positioning protection mechanism comprises a second connecting plate 36, mounting grooves are formed in the top and the bottom of the second connecting plate 36, a sixth rotating rod 37 is rotatably connected in the mounting grooves, two ends of the sixth rotating rod 37 are flush with two ends of the second connecting plate 36, a first connecting plate 5 is fixedly connected to the sixth rotating rod 37, and the first connecting plate 5 close to the bottom of the second connecting plate 36 of the hollow base 1 is fixedly connected with the hollow base 1;
the second connecting plate 36 is provided with a plurality of positioning grooves 40;
a positioning block 39 is fixedly connected to the sixth rotating rod 37, a positioning frame 38 is fixedly connected to the second connecting plate 36, a positioning cap 30 is inserted onto the positioning block 39, and the positioning cap 30 is inserted into the positioning frame 38;
when the satellite antenna body 9 needs to find a position capable of being placed, the first connecting plate 5 and the second connecting plate 36 can be pulled, and the first connecting plate 5 and the second connecting plate 36 are rotationally connected, so that the angle can be randomly adjusted;
when the first connecting plate 5 and the second connecting plate 36 are tiled on the ground, the first connecting plate 5 and the second connecting plate 36 can be positioned at a position required to be placed by means of the positioning groove 40 on the second connecting plate 36, so that the satellite antenna body 9 can be indirectly placed in a specified manner;
when the satellite antenna body 9 is not required to be used, the first connecting plate 5 and the second connecting plate 36 can be directly erected, a baffle is formed by the first connecting plate 5 and the second connecting plate 36 to play a role in protecting the periphery, and the top can be plugged by matching with an external top cover;
when the first connecting plate 5 and the second connecting plate 36 are in the adjusted shape, the positioning cap 30 can be placed in the positioning frame 38, so that the positioning cap 30 can be inserted into the positioning frame 38 and the positioning block 39, the sixth rotating rod 37 is limited, the first connecting plate 5 connected with the sixth rotating rod 37 cannot rotate, and control is convenient.
The foregoing has shown and described the basic principles, principal features and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the above-described embodiments, and that the above-described embodiments and descriptions are only preferred embodiments of the present invention, and are not intended to limit the invention, and that various changes and modifications may be made therein without departing from the spirit and scope of the invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (3)
1. A drive transmission for a satellite antenna, comprising a turret (6), characterized in that: the rotating frame (6) is internally connected with the rotating ring (7) in a rotating way, the rotating ring (7) is internally connected with the fixed ring (8) through a rotating mechanism, the fixed ring (8) is fixedly connected with the satellite antenna body (9), the rotating ring (7) is fixedly connected with a plurality of clamping teeth (31), an opening (35) is formed in the bottom of the rotating frame (6), and the bottom of the rotating frame (6) is fixedly connected with an adjusting mechanism;
the adjusting mechanism is used for controlling the rotation of the satellite antenna body (9) at a plurality of angles;
the positioning protection mechanisms are arranged on the front side, the rear side, the left side and the right side of the adjusting mechanism and are used for fixedly placing the satellite antenna body (9), and the positioning protection mechanisms are used for protecting the satellite antenna body (9);
the adjusting mechanism comprises a hollow base (1), a rotating groove (2) is formed in the top of the hollow base (1), a rotating box (4) is connected inside the rotating groove (2) in a rotating mode, a forward transmission assembly is fixedly connected to the bottom of the rotating box (4), and the forward transmission assembly is connected with the hollow base (1) in a rotating mode;
the positioning protection mechanism comprises a second connecting plate (36), wherein the top and the bottom of the second connecting plate (36) are provided with mounting grooves, a sixth rotating rod (37) is rotatably connected in the mounting grooves, two ends of the sixth rotating rod (37) are flush with two ends of the second connecting plate (36), a first connecting plate (5) is fixedly connected to the sixth rotating rod (37), and the first connecting plate (5) close to the bottom of the second connecting plate (36) of the hollow base (1) is fixedly connected with the hollow base (1);
a plurality of positioning grooves (40) are formed in the second connecting plate (36);
a positioning block (39) is fixedly connected to the sixth rotating rod (37), a positioning frame (38) is fixedly connected to the second connecting plate (36), a positioning cap (30) is inserted onto the positioning block (39), and the positioning cap (30) is inserted into the positioning frame (38);
the device is characterized in that the top of the forward transmission assembly is fixedly connected with a reverse transmission assembly, the reverse transmission assembly is fixedly connected with a rotating box (4), the top of the reverse transmission assembly is fixedly connected with a first conical gear (20), a second conical gear (32) is meshed with the first conical gear (20), a fifth rotating shaft (34) is fixedly connected with the second conical gear (32), the fifth rotating shaft (34) is rotationally connected with a rotating frame (6), a second transmission gear (33) is fixedly connected with the fifth rotating shaft (34), and the second transmission gear (33) is meshed with a plurality of clamping teeth (31);
the forward transmission assembly comprises a first rotating disc (13), the first rotating disc (13) is fixedly connected with a rotating box (4), the first rotating disc (13) is rotationally connected with a hollow base (1), a first clamping groove (15) is formed in the middle of the first rotating disc (13), a first stirring disc (17) is arranged in the first clamping groove (15), a first elastic stirring disc (16) is fixedly connected to the first stirring disc (17), a torsion spring is arranged in the first elastic stirring disc (16), a second rotating rod (14) is arranged on the first stirring disc (17) in a penetrating mode, the bottom of the second rotating rod (14) is rotationally connected with the hollow base (1), the second rotating rod (14) is fixedly connected with a belt pulley (12), the top of the second rotating rod (14) is fixedly connected with a reverse transmission assembly, the reverse transmission assembly comprises a ball bearing (28), a plurality of fixing rods (23) are fixedly connected to the outer sides of the ball bearing (28), the fixing rods (23) are fixedly connected with the rotating box (4), the second rotating rod (24) is fixedly connected with the first rotating rod (24) and the second rotating rod (24) in a fixed connection mode, the utility model discloses a rotary box, including first rotating plate (19), second rotating plate (26), second draw-in groove (29) have been run through in the middle of second rotating plate (26), second draw-in groove (29) inside be provided with second stir dish (25), fixedly connected with second elasticity stir piece (27) on second stir dish (25), the inside torsion spring that has of second elasticity stir piece (27), second stir dish (25) top fixedly connected with third bull stick (19), rotate on third bull stick (19) and be connected with locating plate (18), locating plate (18) and rotation box (4) fixed connection, rotate on locating plate (18) and be connected with fourth bull stick (21), all fixedly connected with first drive gear (22) on fourth bull stick (21) and the third bull stick (19), two first drive gear (22) meshing, fourth bull stick (21) and first conical gear (20) fixed connection.
2. A satellite antenna drive transmission according to claim 1, wherein: the novel rotary shaft type motor is characterized in that a first rotary rod (3) penetrates through the hollow base (1), the first rotary rod (3) is rotationally connected with the hollow base (1), belt pulleys (12) are fixedly connected to the hollow base (1) and the forward transmission assembly, and the two belt pulleys (12) are connected through a connecting belt (11).
3. A satellite antenna drive transmission according to claim 1, wherein: the rotating mechanism is used for controlling the overturning angle of the satellite antenna body (9);
the rotating mechanism comprises a rotating tube (10), the rotating tube (10) is fixedly connected with a rotating ring (7), a seventh rotating rod (48) is connected in the rotating tube (10) in a rotating way, the seventh rotating rod (48) is fixedly connected with a fixed ring (8), a plurality of limit grooves (47) are formed in the seventh rotating rod (48), a mounting box (50) is fixedly connected to the top and the bottom of the rotating tube (10), a sliding plate (46) is connected to the inside of the mounting box (50) in a sliding way, a plurality of limit blocks (49) are fixedly connected to the bottom of the sliding plate (46), a push rod (41) is arranged on the mounting box (50) in a penetrating way, the push rod (41) is fixedly connected with the sliding plate (46), a spring (45) is sleeved on the push rod (41), one end of the spring (45) is fixedly connected with the sliding plate (46), the other end of the spring (45) is fixedly connected with the mounting box (50), the other end of the push rod (41) is fixedly connected with the box (50), one end of the box (50) is far away from the rotating tube (10) and the auxiliary tube (44) is fixedly connected with the sliding frame (44), and a limiting rod (42) is connected inside the sliding frame (43) in a sliding way.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310705486.8A CN116454630B (en) | 2023-06-15 | 2023-06-15 | Driving transmission device of satellite antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310705486.8A CN116454630B (en) | 2023-06-15 | 2023-06-15 | Driving transmission device of satellite antenna |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN116454630A CN116454630A (en) | 2023-07-18 |
| CN116454630B true CN116454630B (en) | 2023-09-05 |
Family
ID=87130560
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310705486.8A Active CN116454630B (en) | 2023-06-15 | 2023-06-15 | Driving transmission device of satellite antenna |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN116454630B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118040323B (en) * | 2024-04-12 | 2024-06-18 | 银河航天(西安)科技有限公司 | Multi-angle rotating support and satellite antenna |
Citations (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20060124063A (en) * | 2005-05-30 | 2006-12-05 | 충남대학교산학협력단 | A satellite antenna |
| KR20070060630A (en) * | 2005-12-09 | 2007-06-13 | 한국전자통신연구원 | Antenna system for tracking satellite |
| WO2011013853A2 (en) * | 2009-07-29 | 2011-02-03 | Hitachi Koki Co., Ltd. | Impact tool |
| JP2011074613A (en) * | 2009-09-29 | 2011-04-14 | Miwa Lock Co Ltd | Cylinder lock, dedicated key for use in the cylinder lock, change key, master key, and key for construction |
| WO2011121262A1 (en) * | 2010-03-31 | 2011-10-06 | Corcost Limited | Multi axis manoeuvrable platform |
| CN107490731A (en) * | 2016-06-13 | 2017-12-19 | 深圳光启创新技术有限公司 | Antenna house test device |
| EP3291367A1 (en) * | 2016-08-30 | 2018-03-07 | Thales | System for assembling two parts in a motion transmitting device |
| CN208257811U (en) * | 2018-05-31 | 2018-12-18 | 广东思启信息科技有限公司 | A kind of intelligence satellite communication device |
| CN109935952A (en) * | 2017-12-16 | 2019-06-25 | 高焕云 | A kind of communication engineering antenna holder |
| CN110686061A (en) * | 2019-08-26 | 2020-01-14 | 重庆宏美科技有限公司 | Auxiliary output protection mechanism |
| CN210897633U (en) * | 2019-12-03 | 2020-06-30 | 青田百凯通讯科技有限公司 | Satellite antenna mounting rack convenient to adjust |
| CN215680970U (en) * | 2021-07-08 | 2022-01-28 | 合肥若森智能科技有限公司 | Vehicle-mounted satellite communication antenna |
| CN114069193A (en) * | 2021-11-12 | 2022-02-18 | 山东利欧节能科技有限公司 | Satellite antenna based on 5G communication and use method thereof |
| CN114069194A (en) * | 2021-11-14 | 2022-02-18 | 中国电子科技集团公司第五十四研究所 | Small-profile three-axis communication-in-motion antenna |
| CN114267933A (en) * | 2021-12-13 | 2022-04-01 | 西安电子工程研究所 | Wheel rail type three-axis stable following radar antenna base |
| CN217093167U (en) * | 2022-03-18 | 2022-08-02 | 江西秀拓地坪材料有限公司 | Preparation facilities convenient to processing waterborne epoxy coating curing agent |
| CN115465481A (en) * | 2022-09-15 | 2022-12-13 | 上海卫星工程研究所 | Gravity unloading device for three-dimensional space unfolding process of inter-satellite antenna and using method |
| CN115465470A (en) * | 2022-06-28 | 2022-12-13 | 西北工业大学 | Aircraft ground equivalent test revolving stage device |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100733961B1 (en) * | 2005-10-20 | 2007-06-29 | 한국전자통신연구원 | Pedestal apparatus and satellite-tracking antenna having pedestal apparatus |
| US8059048B2 (en) * | 2008-03-11 | 2011-11-15 | Her Majesty The Queen In Right Of Canada, As Represented By The Minister Of Industry, Through The Communications Research Centre Canada | Rotating antenna steering mount |
| US10610010B2 (en) * | 2017-09-18 | 2020-04-07 | Fellowes, Inc. | Multi-positional articulating platform system |
-
2023
- 2023-06-15 CN CN202310705486.8A patent/CN116454630B/en active Active
Patent Citations (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20060124063A (en) * | 2005-05-30 | 2006-12-05 | 충남대학교산학협력단 | A satellite antenna |
| KR20070060630A (en) * | 2005-12-09 | 2007-06-13 | 한국전자통신연구원 | Antenna system for tracking satellite |
| WO2011013853A2 (en) * | 2009-07-29 | 2011-02-03 | Hitachi Koki Co., Ltd. | Impact tool |
| JP2011074613A (en) * | 2009-09-29 | 2011-04-14 | Miwa Lock Co Ltd | Cylinder lock, dedicated key for use in the cylinder lock, change key, master key, and key for construction |
| WO2011121262A1 (en) * | 2010-03-31 | 2011-10-06 | Corcost Limited | Multi axis manoeuvrable platform |
| CN107490731A (en) * | 2016-06-13 | 2017-12-19 | 深圳光启创新技术有限公司 | Antenna house test device |
| EP3291367A1 (en) * | 2016-08-30 | 2018-03-07 | Thales | System for assembling two parts in a motion transmitting device |
| CN109935952A (en) * | 2017-12-16 | 2019-06-25 | 高焕云 | A kind of communication engineering antenna holder |
| CN208257811U (en) * | 2018-05-31 | 2018-12-18 | 广东思启信息科技有限公司 | A kind of intelligence satellite communication device |
| CN110686061A (en) * | 2019-08-26 | 2020-01-14 | 重庆宏美科技有限公司 | Auxiliary output protection mechanism |
| CN210897633U (en) * | 2019-12-03 | 2020-06-30 | 青田百凯通讯科技有限公司 | Satellite antenna mounting rack convenient to adjust |
| CN215680970U (en) * | 2021-07-08 | 2022-01-28 | 合肥若森智能科技有限公司 | Vehicle-mounted satellite communication antenna |
| CN114069193A (en) * | 2021-11-12 | 2022-02-18 | 山东利欧节能科技有限公司 | Satellite antenna based on 5G communication and use method thereof |
| CN114069194A (en) * | 2021-11-14 | 2022-02-18 | 中国电子科技集团公司第五十四研究所 | Small-profile three-axis communication-in-motion antenna |
| CN114267933A (en) * | 2021-12-13 | 2022-04-01 | 西安电子工程研究所 | Wheel rail type three-axis stable following radar antenna base |
| CN217093167U (en) * | 2022-03-18 | 2022-08-02 | 江西秀拓地坪材料有限公司 | Preparation facilities convenient to processing waterborne epoxy coating curing agent |
| CN115465470A (en) * | 2022-06-28 | 2022-12-13 | 西北工业大学 | Aircraft ground equivalent test revolving stage device |
| CN115465481A (en) * | 2022-09-15 | 2022-12-13 | 上海卫星工程研究所 | Gravity unloading device for three-dimensional space unfolding process of inter-satellite antenna and using method |
Non-Patent Citations (1)
| Title |
|---|
| 新型活齿分度凸轮机构的原理及动态静力分析;沈煜;杨玉虎;张大卫;刘泽富;;天津大学学报(第08期);全文 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN116454630A (en) | 2023-07-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN116454630B (en) | Driving transmission device of satellite antenna | |
| CN204885442U (en) | Worm gear driven antenna actuating mechanism | |
| EP0843381A3 (en) | Multibeam antenna | |
| CA2160801A1 (en) | Msat mast antenna with reduced frequency scanning | |
| CN109066052A (en) | Lead to satellite antenna mounting during a kind of twin shaft self-locking type is quiet | |
| CN205564991U (en) | During moving, new face small -size triaxial leads to satellite communications antenna | |
| CN109935955A (en) | A kind of communication antenna convenient for adjusting | |
| US3530477A (en) | Scanning antenna having drive motors fixed with respect to the antenna | |
| CN111800151B (en) | 5G signal receiving device | |
| CN205564957U (en) | Novel on -board satellite lead to antenna system in moving | |
| IL272961B2 (en) | Antenna for receiving data from low earth orbit satellites | |
| CN205564967U (en) | On -board satellite receiving antenna | |
| GB1477325A (en) | Antenna scan apparatus | |
| CN208076810U (en) | A kind of automatic focusing device | |
| DE4307675A1 (en) | Satellite TV receiver for multiple satellites - has fixed dish with feed-horn mounted in such way to allow adjustment to receive signals from one or more nearby satellites. | |
| FR1259139A (en) | Scanning horn and reflector antenna | |
| CN210607586U (en) | Electronic communication antenna device | |
| CN219937373U (en) | Satellite antenna | |
| CN110174680A (en) | A kind of location receivers with satellite navigation function | |
| CN221226566U (en) | Gravity self-balancing flat antenna tracking device | |
| CN221102392U (en) | Antenna with rust-resistant mounting structure | |
| CN218827855U (en) | Short wave log-periodic antenna with adjustable wave beam elevation angle | |
| CN212695317U (en) | High-safety portable television antenna | |
| CN219243186U (en) | Receiver with signal enhancement function | |
| CN220209279U (en) | Portable antenna every single move pivot angle locking device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |