CN207852887U - A kind of satellite antenna angle adjustment mechanism - Google Patents
A kind of satellite antenna angle adjustment mechanism Download PDFInfo
- Publication number
- CN207852887U CN207852887U CN201721829791.4U CN201721829791U CN207852887U CN 207852887 U CN207852887 U CN 207852887U CN 201721829791 U CN201721829791 U CN 201721829791U CN 207852887 U CN207852887 U CN 207852887U
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- CN
- China
- Prior art keywords
- satellite antenna
- actuator
- pair
- mounting plate
- fixed
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses a kind of satellite antenna angle adjustment mechanisms, including substrate, the identical telescope motor of a pair of of structure, mounting plate and satellite antenna, a pair of telescope motor to be placed on substrate, and the mounting plate is fixed on substrate；It further includes：Actuator, drive disk and a pair of of bull stick；The installation plate end face offers sliding slot, the pair of bull stick is fitted in sliding slot, and the drive disk is fixed on a pair of bull stick, and the actuator is fixed on mounting plate centre, the satellite antenna is fixed on drive disk, and the actuator driving end is connect with driving pan bottom.The utility model has the beneficial effects that telescope motor is changed the height of satellite antenna, while the angle problem of satellite antenna can be adjusted accordingly using actuator.
Description
Technical field
The utility model is related to the communications field, especially a kind of satellite antenna angle adjustment mechanism.
Background technology
Continuous with society carries out not, and communication equipment is more and more flourishing, and satellite antenna is needed at installation initial stage
It constantly to be debugged, be finally fixed in an angle, pass through the continuous construction in later stage, it is also necessary to it is adjusted,
When adjusting, needs manually to be adjusted using tool, be not very convenient.
Utility model content
Purpose of the utility model is to solve the above problems, devise a kind of satellite antenna angle adjustment mechanism.
Realize that above-mentioned purpose the technical solution of the utility model is a kind of satellite antenna angle adjustment mechanism, including substrate,
The identical telescope motor of a pair of of structure, mounting plate and satellite antenna, a pair of telescope motor are placed on substrate, the peace
Loading board is fixed on substrate；It further includes：Actuator, drive disk and a pair of of bull stick；The installation plate end face offers sliding slot,
The pair of bull stick is fitted in sliding slot, and the drive disk is fixed on a pair of bull stick, and the actuator is fixed on installation
Plate centre, the satellite antenna are fixed on drive disk, and the actuator driving end is connect with driving pan bottom.
Preferably, fixed frame is equipped between the actuator and mounting plate；The fixed frame is for being fixed actuator.
Preferably, the base plate bottom disposes four supporting blocks；The supporting block is for being supported substrate.
Preferably, the actuator is connected with motor driver by conducting wire；The motor driver be used for actuator into
Row control.
Preferably, more telescopic rods are equipped between the substrate and mounting plate；The telescopic rod is for propping up mounting plate
Support.
The satellite antenna angle adjustment mechanism made using the technical solution of the utility model, the technical program are passed through, are stretched
Contracting motor is changed the height of satellite antenna, while can adjust the angle problem of satellite antenna accordingly using actuator.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of satellite antenna angle adjustment mechanism；
Fig. 2 is a kind of local overlooking structural schematic diagram of satellite antenna angle adjustment mechanism；
Fig. 3 is a kind of local overlooking structural schematic diagram of satellite antenna angle adjustment mechanism；
In figure, 1, substrate；2, telescope motor；3, mounting plate；4, satellite antenna；5, actuator；6, drive disk；7, bull stick；
8, sliding slot；9, fixed frame；10, supporting block；11, motor driver；12, telescopic rod.
Specific implementation mode
It should be noted that：Similar label and letter indicate similar terms in following attached drawing, therefore, once a certain Xiang Yi
It is defined, then it further need not be defined and explained in subsequent attached drawing in a attached drawing.
In the description of the present invention, it should be noted that term "upper", "lower", "vertical", "horizontal", "inner",
The orientation or positional relationship of the instructions such as "outside" is to be based on the orientation or positional relationship shown in the drawings or the utility model product
The orientation or positional relationship usually put when use, is merely for convenience of describing the present invention and simplifying the description, without referring to
Show or imply that signified device or element must have a particular orientation, with specific azimuth configuration and operation, therefore cannot manage
Solution is limitations of the present invention.In addition, term " one ", " two " etc. be only used for distinguish description, and should not be understood as instruction or
Imply relative importance.
The utility model is specifically described below in conjunction with the accompanying drawings, as shown in Figs. 1-3, a kind of satellite antenna angular adjustment
Structure, including substrate 1, the identical telescope motor 2 of a pair of of structure, mounting plate 3 and satellite antenna 4, which is characterized in that Yi Duisuo
It states telescope motor 2 to be placed on substrate 1, the mounting plate 3 is fixed on substrate 1；It further includes：Actuator 5, drive disk 6 with
And a pair of bull stick 7；3 end face of the mounting plate offers sliding slot 8, and the pair of bull stick 7 is fitted in sliding slot 8, the drive disk 6
It is fixed on a pair of bull stick 7, the actuator 5 is fixed on 3 centre of mounting plate, and the satellite antenna 4 is fixed on drive
On Moving plate 6, the actuator 5 drives end to be connect with 6 bottom of drive disk；Fixed frame is equipped between the actuator 5 and mounting plate 3
9；The fixed frame 9 is for being fixed actuator 5；1 bottom of the substrate disposes four supporting blocks 10；The supporting block 10 is used for
Substrate 1 is supported；The actuator 5 is connected with motor driver 11 by conducting wire；The motor driver 11 is used for driving
Moving part 5 is controlled；More telescopic rods 12 are equipped between the substrate 1 and mounting plate 3；The telescopic rod 12 is used for mounting plate 3
It is supported.
When specifically used, at the present apparatus free time, the matched driver of all electrical parts is disposed, and passes through this
Field personnel all actuators, the power supply for referring to dynamical element, electrical part and adaptation will be connected by conducting wire among the above
It connecing, specific connection means, should refer in following operation principles, priority job order is completed to be electrically connected between each electrical part,
Detailed connection means are known in the art technology, following mainly to introduce operation principle and process, are not manufactured to electric-controlled
It is bright.
Single unit system operation principle is as follows：It pushes mounting plate 3 to rise first with telescope motor 2, can adjust and defend accordingly
The height item of star antenna 4, while after actuator 5 makes drive disk 6 be rotated, meanwhile, utilize a pair of of rotating bar and cunning
The cooperation auxiliary drive disk 6 of slot 8 rotates, and to realize the adjusting to drive disk 6, completes the adjusting to satellite antenna 4.
Preferably, further, fixed frame 9 is equipped between actuator 5 and mounting plate 3；The fixed frame 9 is used for
Actuator 5 is fixed.
Preferably, further, 1 bottom of substrate disposes four supporting blocks 10；The supporting block 10 is used for base
Plate 1 is supported.
Preferably, further, actuator 5 is connected with motor driver 11 by conducting wire；The motor drives
Device 11 is for controlling actuator 5.
Preferably, further, more telescopic rods 12 are equipped between substrate 1 and mounting plate 3；The telescopic rod 12
For being supported to mounting plate 3.
Above-mentioned technical proposal only embodies the optimal technical scheme of technical solutions of the utility model, the technology of the art
Personnel embody the principles of the present invention to some variations that some of which part may be made, and belong to the utility model
Protection domain within.
Claims (5)
1. a kind of satellite antenna angle adjustment mechanism, including substrate (1), the identical telescope motor (2) of a pair of of structure, mounting plate
(3) and satellite antenna (4), which is characterized in that a pair of telescope motor (2) is placed on substrate (1), the mounting plate
(3) it is fixed on substrate (1)；It further includes：Actuator (5), drive disk (6) and a pair of of bull stick (7)；The mounting plate (3)
End face offers sliding slot (8), and the pair of bull stick (7) is fitted in sliding slot (8), and the drive disk (6) is fixed on described in a pair
On bull stick (7), the actuator (5) is fixed on mounting plate (3) centre, and the satellite antenna (4) is fixed on drive disk (6)
On, actuator (5) driving end is connect with drive disk (6) bottom.
2. a kind of satellite antenna angle adjustment mechanism according to claim 1, which is characterized in that the actuator (5) with
Fixed frame (9) is equipped between mounting plate (3)；The fixed frame (9) is for being fixed actuator (5).
3. a kind of satellite antenna angle adjustment mechanism according to claim 1, which is characterized in that substrate (1) bottom
Dispose four supporting blocks (10)；The supporting block (10) is for being supported substrate (1).
4. a kind of satellite antenna angle adjustment mechanism according to claim 1, which is characterized in that the actuator (5) is logical
It crosses conducting wire and is connected with motor driver (11)；The motor driver (11) is for controlling actuator (5).
5. a kind of satellite antenna angle adjustment mechanism according to claim 1, which is characterized in that the substrate (1) and peace
More telescopic rods (12) are equipped between loading board (3)；The telescopic rod (12) is for being supported mounting plate (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721829791.4U CN207852887U (en) | 2017-12-25 | 2017-12-25 | A kind of satellite antenna angle adjustment mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721829791.4U CN207852887U (en) | 2017-12-25 | 2017-12-25 | A kind of satellite antenna angle adjustment mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207852887U true CN207852887U (en) | 2018-09-11 |
Family
ID=63418424
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721829791.4U Expired - Fee Related CN207852887U (en) | 2017-12-25 | 2017-12-25 | A kind of satellite antenna angle adjustment mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207852887U (en) |
-
2017
- 2017-12-25 CN CN201721829791.4U patent/CN207852887U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180911 Termination date: 20191225 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |