CN207883902U - The mounting structure and satellite communication equipment of antenna - Google Patents
The mounting structure and satellite communication equipment of antenna Download PDFInfo
- Publication number
- CN207883902U CN207883902U CN201820228437.4U CN201820228437U CN207883902U CN 207883902 U CN207883902 U CN 207883902U CN 201820228437 U CN201820228437 U CN 201820228437U CN 207883902 U CN207883902 U CN 207883902U
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- antenna
- rocking arm
- speed reducer
- gear speed
- driving part
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Abstract
The utility model provides a kind of mounting structure and satellite communication equipment of antenna, the mounting structure of antenna, antenna to be installed on satellite communication equipment ontology, including：Rocking arm, the first driving part and worm-gear speed reducer；Rocking arm is rotatably connected on satellite communication equipment ontology, and antenna is connected on rocking arm, and the first driving part is connect by worm-gear speed reducer with rocking arm, to drive rocking arm that antenna is driven to be rotated relative to satellite communication equipment ontology.The utility model have it is simple in structure, be easily installed, and can have the advantages that self-locking function.
Description
Technical field
The utility model is related to field of communication technology, more particularly to the mounting structure and satellite communication equipment of a kind of antenna.
Background technology
At present satellite communication device (including it is vehicle-mounted it is quiet in lead to, vehicle-mounted communication in moving, boat-carrying communication in moving) be by antenna come
Signal of communication is received, is to use to pass through on antenna in the prior art to ensure reception of the antenna to signal of communication
The transmission mechanisms such as gear or synchronous belt are connected on satellite communication equipment, to realize the change of Antenna Operation position, are not only passed
Motivation structure is complicated, difficult to install, and can not achieve self-lock protection.
Utility model content
The main purpose of the utility model is to provide a kind of mounting structure of antenna and satellite communication equipments, not only tie
Structure is simple, is easily installed, and can have self-locking function.
On the one hand the utility model provides a kind of mounting structure of antenna, antenna is installed to satellite communication equipment
On ontology, including：Rocking arm, the first driving part and worm-gear speed reducer；
The rocking arm is rotatably connected on the satellite communication equipment ontology, and the antenna is connected on the rocking arm,
First driving part is connect by the worm-gear speed reducer with the rocking arm, to drive the rocking arm to drive the day
Line is rotated relative to the satellite communication equipment ontology.
More preferably, further include planet-gear speed reducer；
The worm-gear speed reducer is connect by the planet-gear speed reducer with the rocking arm, so that described first drives
Dynamic component passes sequentially through the worm-gear speed reducer and the planet-gear speed reducer drives the rocking arm rotation.
More preferably, it is provided with holder on the satellite communication equipment ontology；
The worm-gear speed reducer is detachably connected on the holder.
More preferably, further include planet-gear speed reducer, the worm-gear speed reducer passes through the planet-gear speed reducer
It is connect with the rocking arm；
The planet-gear speed reducer is detachably connected on the holder.
More preferably, further include connecting flange；
The connecting flange is fixedly connected with the antenna, and is rotatably connected on the rocking arm, described to drive
Antenna is rotated relative to the rocking arm.
More preferably, further include the second driving part；
Second driving part is connect with the connecting flange, to drive the connecting flange to rotate.
More preferably, further include deceleration device；
Second driving part is connect by the deceleration device with the connecting flange.
More preferably, further include rotary shaft and bearing；
The rotary shaft is fixedly connected with the connecting flange, and is connected on the rocking arm by the bearing；
Second driving part is by the deceleration device and the rotation axis connection, so that second driving part
The rotary shaft is driven to drive the connecting flange rotation by the deceleration device.
More preferably, further include control device；
The control device is electrically connected with second driving part, and the control device can acquire the antenna
With the angle information between the rocking arm, and second driving part is controlled according to the information and is worked.
The another aspect of the utility model provides a kind of satellite communication equipment, including the antenna of any of the above technical characteristic
Mounting structure.
The mounting structure of the antenna of the offer of the utility model is rotatably connected using the rocking arm in the satellite communication
On apparatus body, the antenna is connected on the rocking arm, first driving part by the worm-gear speed reducer with
The rocking arm connection, with the technical side for driving the rocking arm that the antenna is driven to be rotated relative to the satellite communication equipment ontology
Case is not only simple in structure, and is easily installed, and can have self-locking function.
Description of the drawings
Attached drawing described herein is used to provide a further understanding of the present invention, and constitutes one of the utility model
Point, the exemplary embodiment of the utility model and the description thereof are used to explain the utility model, does not constitute to the utility model
Improper restriction.In the accompanying drawings：
Fig. 1 is one example structure schematic diagram of mounting structure of the antenna of the utility model；
Fig. 2 is the side view of Fig. 1；
Fig. 3 is rocking arm in Fig. 1 and the first driving part and the second driving part scheme of installation；
Fig. 4 is the connecting flange installation condition schematic diagram in Fig. 1.
In figure：1, antenna；2, satellite communication equipment ontology；3, rocking arm；4, the first driving part；5, turbine and worm slows down
Machine；6, planet-gear speed reducer；7, holder；8, connecting flange；9, the second driving part；10, deceleration device；11, bearing；12、
Rotary shaft.
Specific implementation mode
It is specific below in conjunction with the utility model to keep the purpose of this utility model, technical solution and advantage clearer
Technical solutions of the utility model are clearly and completely described in embodiment and corresponding attached drawing.Obviously, described embodiment
Only it is the utility model a part of the embodiment, instead of all the embodiments.Based on the embodiments of the present invention, this field
The every other embodiment that those of ordinary skill is obtained without making creative work, belongs to the utility model
The range of protection.
As shown in Figure 1, 2, 3, a kind of mounting structure of antenna, antenna 1 is installed to 2 ontology of satellite communication equipment
On, the mounting structure of the antenna includes：Rocking arm 3, the first driving part 4 and turbine worm reducer 5.Rocking arm 3 is rotatably connected
On 2 ontology of satellite communication equipment, antenna 1 is connected on rocking arm 3, the first driving part 4 by turbine worm reducer 5 with shake
Arm 3 connects, to drive rocking arm 3 that antenna 1 is driven to be rotated relative to 2 ontology of satellite communication equipment, to realize antenna 1 relative to satellite
The pitch position of communication equipment 2 is converted.Wherein antenna 1 can be plate aerial.Using such technical solution, not only structure letter
It is single, it is easily installed, and can realize self-locking function by turbine worm reducer 5, avoids in the case of too power-off suddenly,
Antenna straight line declines.The function of doing of turbine worm reducer 5 makes the common knowledge of machinery field, therefore herein to its self-lock mechanism
No longer it is described in detail.
Further, further include planet-gear speed reducer 6 as shown in Fig. 1,2,3；Turbine worm reducer 5 passes through row
Star gear reduction unit 6 is connect with rocking arm 3, so that the first driving part 4 passes sequentially through turbine worm reducer 5 and planetary gear reduction
Fast machine 6 drives rocking arm 3 to rotate.Worm-gear speed reducer 5 is used alone, worm-gear speed reducer 5 is made to undertake heavier loads situation
Lower long-time service generates larger abrasion.Such as it is 1 that reduction ratio, which can be selected, in worm-gear speed reducer 5:180 worm type of reduction gearing
42 stepping, 40 long motor can be selected in (PX110-100,2KG), the first driving part 4, and reduction ratio can be selected in planet-gear speed reducer 6
It is 1:6 planetary reducer (PS60-006,1KG) connection, planetary installation make planet tooth using fixed output end
The mode that wheel decelerator fuselage drives worm type of reduction gearing (TBR60L) to rotate realizes pitching self-locking function.
Specifically, as shown in Figure 1, 2, it is provided with holder 7 on 2 ontology of satellite communication equipment.Turbine worm reducer 5 is removable
It unloads and is connected on holder 7, such as turbine worm reducer 5 can be connected on holder 7 by screw, in order to be torn open to it
It unloads.Equally, planet-gear speed reducer 6 is detachably connected on holder 7, can also specifically screw be used to connect.
Further include connecting flange 8 as shown in Fig. 1,2,4 as a kind of embodiment.Connecting flange 8 is fixed with antenna 1
Connection, and be rotatably connected on rocking arm 3, to drive antenna 1 to be rotated relative to rocking arm 3.In this way when antenna 1 is relative to defending
After pitch position on 2 ontology of star communication equipment determines, antenna 1 can be driven to rotate by connecting flange 8, can rotate to
The optimum position that satellite-signal can be received, to improve signal reception.
Preferably, as shown in Figure 1, 2, further include the second driving part 9, the second driving part 9 is connect with connecting flange 8,
It is rotated to be drivingly connected flange 8.More preferably, further include deceleration device 10；Second driving part 9 is by deceleration device 10 and even
Acting flange 8 connects.It is 1 that wherein reduction ratio, which can be selected, in deceleration device 10:180 worm type of reduction gearing (TBR60L), to realize
To 1 postrotational self-locking of antenna, 28 stepping, 50 long motor can be selected in the second driving part 9.
Further, as shown in figure 4, further including rotary shaft 12 and bearing 11, rotary shaft 12 is fixed with connecting flange 8 to be connected
It connecing, and is connected on rocking arm 3 by bearing 11, the second driving part 9 is connect by deceleration device 10 with rotary shaft 12, so that the
Two driving parts 9 drive rotary shaft 12 that connecting flange 8 is driven to rotate by deceleration device 10.In actual fabrication and installation, rotation
Shaft 12 and connecting flange 8 can be integrally formed making, and the axis of rotary shaft 12 is perpendicular to antenna 1, and both perpendicular to shaking
Arm 3 makes 1 rotary shaft 12 of antenna and rocking arm 3 that shape of chinese word Ji be collectively formed, so that the weight of antenna 1 passes through connecting flange 8, rotation completely
Shaft 12 and bearing 11 are transmitted on rocking arm 3, and the case where avoiding deceleration device 10 from sharing 1 weight of antenna occurs.It rotates simultaneously
Axis 12 is connected to by bearing 11 on rocking arm 3, its rotation can be made lighter, it should be noted that rotary shaft 12 passes through bearing
11 are connected on rocking arm 3, and the connection type of arbitrary achievable goal of the invention can be used, its concrete structure is no longer described in detail herein.
Further include control device (not shown), 9 electricity of control device and the second driving part as a kind of embodiment
Connection, and control device can acquire the angle information between antenna 1 and rocking arm 3, and according to the second driving of information control
Component 9 works.It can be arranged between antenna 1 and rocking arm 3 in control device by way of human-computer exchange when specifically used
Predetermined angle, when the collected angle information of control device is with default and angle difference, control the second driving part 9 work,
Make driving antenna 1 rotation of the second driving part 9 when the collected angle information of control device is identical as default and angle, control
Second driving part 9 is stopped.
The current another aspect of the utility model is invented for realization and provides a kind of satellite communication equipment, including with embodiment institute
The mounting structure of the antenna of description.
Above example makes the utility model have：It is simple in structure, it is easily installed, and can be with the excellent of self-locking function
Point.
The above description is only the embodiments of the present invention, is not intended to limit the utility model, for this field
Technical staff for, various modifications and changes may be made to the present invention.Within the spirit and principle of the utility model,
Any modification, equivalent replacement, improvement and so on should be included within the right of the utility model.
Claims (10)
1. a kind of mounting structure of antenna, antenna (1) to be installed on satellite communication equipment ontology (2), it is characterised in that：
Including：Rocking arm (3), the first driving part (4) and worm-gear speed reducer (5)；
The rocking arm (3) is rotatably connected on the satellite communication equipment ontology (2), and the antenna (1) is connected to described shake
On arm (3), first driving part (4) is connect by the worm-gear speed reducer (5) with the rocking arm (3), with driving
The rocking arm (3) drives the antenna (1) to be rotated relative to the satellite communication equipment ontology (2).
2. the mounting structure of antenna according to claim 1, it is characterised in that：
Further include planet-gear speed reducer (6)；
The worm-gear speed reducer (5) is connect by the planet-gear speed reducer (6) with the rocking arm (3), so that described
First driving part (4) passes sequentially through to be shaken described in the worm-gear speed reducer (5) and the planet-gear speed reducer (6) driving
Arm (3) rotates.
3. the mounting structure of antenna (1) according to claim 1, it is characterised in that：
It is provided with holder (7) on the satellite communication equipment ontology (2)；
The worm-gear speed reducer (5) is detachably connected on the holder (7).
4. the mounting structure of antenna according to claim 3, it is characterised in that：
Further include planet-gear speed reducer (6), the worm-gear speed reducer (5) by the planet-gear speed reducer (6) with
Rocking arm (3) connection；
The planet-gear speed reducer (6) is detachably connected on the holder (7).
5. the mounting structure of antenna according to any one of claims 1 to 4, it is characterised in that：
Further include connecting flange (8)；
The connecting flange (8) is fixedly connected with the antenna (1), and is rotatably connected on the rocking arm (3), to drive
The antenna (1) rotates relative to the rocking arm (3).
6. the mounting structure of antenna according to claim 5, it is characterised in that：
Further include the second driving part (9)；
Second driving part (9) connect with the connecting flange (8), to drive the connecting flange (8) to rotate.
7. the mounting structure of antenna according to claim 6, it is characterised in that：
Further include deceleration device (10)；
Second driving part (9) is connect by the deceleration device (10) with the connecting flange (8).
8. the mounting structure of antenna according to claim 7, it is characterised in that：
Further include rotary shaft (12) and bearing (11)；
The rotary shaft (12) is fixedly connected with the connecting flange (8), and is connected to the rocking arm by the bearing (11)
(3) on；
Second driving part (9) is connect by the deceleration device (10) with the rotary shaft (12), so that described second
Driving part (9) drives the rotary shaft (12) that the connecting flange (8) is driven to rotate by the deceleration device (10).
9. the mounting structure of antenna according to claim 6, it is characterised in that：
It further include control device；
The control device is electrically connected with second driving part (9), and the control device can acquire the antenna
(1) angle information between the rocking arm (3), and second driving part (9) is controlled according to the information and is worked.
10. a kind of satellite communication equipment, it is characterised in that：
Include the mounting structure of the antenna described in claim 1 to 9 any one.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820228437.4U CN207883902U (en) | 2018-02-08 | 2018-02-08 | The mounting structure and satellite communication equipment of antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820228437.4U CN207883902U (en) | 2018-02-08 | 2018-02-08 | The mounting structure and satellite communication equipment of antenna |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207883902U true CN207883902U (en) | 2018-09-18 |
Family
ID=63498096
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820228437.4U Active CN207883902U (en) | 2018-02-08 | 2018-02-08 | The mounting structure and satellite communication equipment of antenna |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207883902U (en) |
-
2018
- 2018-02-08 CN CN201820228437.4U patent/CN207883902U/en active Active
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