CN206585059U - A kind of steady type and the satellite antenna of energy automatic fine tuning - Google Patents

A kind of steady type and the satellite antenna of energy automatic fine tuning Download PDF

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Publication number
CN206585059U
CN206585059U CN201720324326.9U CN201720324326U CN206585059U CN 206585059 U CN206585059 U CN 206585059U CN 201720324326 U CN201720324326 U CN 201720324326U CN 206585059 U CN206585059 U CN 206585059U
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CN
China
Prior art keywords
satellite
disk
support frame
satellite reception
reception disk
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
Application number
CN201720324326.9U
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Chinese (zh)
Inventor
张萤
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tianjin Ding Ding Communication Technology Co Ltd
Original Assignee
Tianjin Ding Ding Communication Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Tianjin Ding Ding Communication Technology Co Ltd filed Critical Tianjin Ding Ding Communication Technology Co Ltd
Priority to CN201720324326.9U priority Critical patent/CN206585059U/en
Application granted granted Critical
Publication of CN206585059U publication Critical patent/CN206585059U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of steady type and the satellite antenna of energy automatic fine tuning, including electric pushrod, signal receiver support bar and satellite reception disk, support frame is provided with below the satellite reception disk, and the junction of satellite reception disk and support frame is provided with packing ring, lower position inside support frame as described above close to satellite reception disk is provided with servomotor, the servomotor is electrically connected with external control panel, electric pushrod in the utility model can effectively promote expansion link to carry out small stretching motion, it is convenient that satellite antenna is finely adjusted, solve the regulation problem for needing manually to carry out satellite;Servomotor can voluntarily carry out rotating, drive whole satellite antenna to be rotated by the roller below support frame, realize the accurate fine setting of satellite antenna;Packing ring is used for paving in satellite reception disk, prevents satellite reception disk from directly being contacted with support frame, easily produces corrosion problem.

Description

A kind of steady type and the satellite antenna of energy automatic fine tuning
Technical field
The utility model belongs to communication technical field, and in particular to a kind of steady type and the satellite antenna of energy automatic fine tuning.
Background technology
The species of satellite antenna is a lot, can be divided into analog satellite receiver, digital satellite receiver and multisatellite and connect Receipts machine, card (box) is received in addition with digital satellite.It is to receive the simulation section launched on satellite early stage that analog satellite receiver, which is, Mesh and design, satellite television receiver refers to satellite frequency demultiplier LNB output signals being converted to AV signal or penetrated The electronic equipment of frequency signal.Analog satellite television receiver -- reception is analog signal, because of most of signal at present It is digitized into, has disappeared substantially.Digital satellite television receiver -- reception is data signal, is the more commonly used at present connect Receipts machine, divides plug-in card teaching machine, free machine, high clear etc. again.
But satellite antenna in the market is not only complicated, and function is single, it is necessary to manually be defended The adjustment of star antenna, the accuracy of adjustment is relatively low, and many times, it is necessary to two people work simultaneously, a people in outdoor, Indoors, mobile range is difficult to control to one people, compares the energy for wasting people, and operation difficulty is larger, is also needed after mobile completion Pushed down with weight, may be during pushing down, and micro- position for moving satellite antenna, generally, work amplitude It is larger.
Utility model content
The purpose of this utility model is the satellite antenna for providing a kind of steady type and energy automatic fine tuning, to solve the above-mentioned back of the body The adjustment of satellite antenna is manually carried out the need for being proposed in scape technology, the accuracy of adjustment is relatively low, and many times, Need two people to work simultaneously, a people in outdoor, a people indoors the problem of.
To achieve the above object, the utility model provides following technical scheme:A kind of steady type and can automatic fine tuning defend Star antenna, including electric pushrod, signal receiver support bar and satellite reception disk, the lower section of the satellite reception disk are set There is support frame, and the junction of satellite reception disk and support frame is provided with inside packing ring, support frame as described above close to satellite reception The lower position of disk is provided with servomotor, and the servomotor is electrically connected with external control panel, described electronic to push away Bar is arranged on satellite reception disk, and expansion link, the electric pushrod and outside chain of command are provided with above electric pushrod Plate is electrically connected with, and is provided with signal receiver, the signal at the top position of satellite reception disk on electric pushrod Receiver is electrically connected with external control panel, and the signal receiver support bar is arranged on signal receiver.
It is preferred that, the left side for being internally provided with close gear-box inside gear-box, and electric pushrod of the electric pushrod Lower position is provided with motor, and the gear-box is connected with motor by axis of rotation.
It is preferred that, the servomotor is connected with satellite reception disk by axis of rotation.
It is preferred that, the satellite reception disk is fixedly connected with support frame by packing ring.
It is preferred that, the signal receiver support bar is fixedly connected with satellite reception disk by elastomeric pad.
Compared with prior art, the beneficial effects of the utility model are:
(1), the electric pushrod in the utility model can effectively promote expansion link to carry out small stretching motion, convenient pair Satellite antenna is finely adjusted, and solves the regulation problem for needing manually to carry out satellite.
(2), the servomotor in the utility model can voluntarily carry out rotating, be driven by the roller below support frame whole Individual satellite antenna is rotated, and realizes the accurate fine setting of satellite antenna.
(3), the packing ring in the utility model is softer, is mainly used to pave in satellite reception disk, prevents satellite from connecing Receive disk directly to contact with support frame, easily produce corrosion problem.
(4), the signal receiver support bar in the utility model is can to carry out fine motion according to the position of expansion link, Movement is more convenient, and the globality of connection is preferable, smoothly can support signal receiver.
(5), the satellite reception disk in the utility model is the structure of spill, facilitates the reception of satellite-signal so that connect The collection of letters number is more accurate, with certain focussing force.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the structural representation of the utility model satellite reception disk;
Fig. 3 is the structural representation of the utility model electric pushrod;
In figure:1- electric pushrods, 2- signal receivers, 3- expansion links, 4- signal receivers support bar, 5- support frames, 6- Servomotor, 7- packing rings, 8- satellite receptions disk, 9- gear-boxes, 10- motors.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made The every other embodiment obtained, belongs to the scope of the utility model protection.
Fig. 1, Fig. 2 and Fig. 3 are referred to, the utility model provides a kind of technical scheme:A kind of steady type and energy automatic fine tuning Satellite antenna, including electric pushrod 1, signal receiver support bar 4 and satellite reception disk 8, the lower section of satellite reception disk 8 Support frame 5 is provided with, and the junction of satellite reception disk 8 and support frame 5 is provided with packing ring 7, the inside of support frame 5 is close to satellite The lower position for receiving disk 8 is provided with servomotor 6, and servomotor 6 is electrically connected with external control panel, electric pushrod 1 is arranged on satellite reception disk 8, and the top of electric pushrod 1 is provided with expansion link 3, electric pushrod 1 and external control panel It is electrically connected with, and is provided with signal receiver 2 on electric pushrod 1 at the top position of satellite reception disk 8, signal is received Device 2 is electrically connected with external control panel, and signal receiver support bar 4 is arranged on signal receiver 2.
The accurate micro-shifting of expansion link 3 is moved for convenience, in the present embodiment, it is preferred that electric pushrod 1 is internally provided with tooth Roller box 9, and the inside of electric pushrod 1 is provided with motor 10, gear-box 9 and motor 10 close to the left side lower position of gear-box 9 Connected by axis of rotation.
In order to realize in the first successive step of whole satellite antenna, the present embodiment, it is preferred that servomotor 6 and satellite reception Disk 8 is connected by axis of rotation.
Relative friction forces for satellite reception disk 8 in movement with support frame 5 are smaller, in the present embodiment, it is preferred that Satellite reception disk 8 is fixedly connected with support frame 5 by packing ring 7.
The movement of signal receiver support bar 4 for convenience, but do not depart from satellite reception disk 8, the present embodiment, it is excellent Choosing, signal receiver support bar 4 is fixedly connected with satellite reception disk 8 by elastomeric pad.
Electric pushrod 1 in the utility model is mainly made up of motor 10, gear-box 9, ball screw and workbench, is passed through Motor 10 is rotated with moving gear, and gear drives whole gear-box 9 to be run, so as to drive ball screw to carry out work Make, on the workbench that expansion link 3 is connected in roller bearing screw mandrel, so that workbench drives expansion link 3 to carry out stretching motion;This practicality is new Servomotor 6 in type refers to the engine of control machinery element operating, is a kind of subsidy indirect gear shift device of motor.Servo electricity The servomotor of machine 6 can make control speed, and positional precision is very accurate, and voltage signal can be converted into torque and rotating speed to drive Control object, the rotor speed of servomotor 6 by input signal control, and can fast reaction, in automatic control system, as holding Units, and with characteristics such as electromechanical time constant small, the linearity is high, pickup voltages, the electric signal received can be converted into Angular displacement or angular speed output on motor reel.
Operation principle of the present utility model and use flow:Satellite antenna is connected into external power source, passes through servo electricity first Machine 6 is tentatively aligned to one of satellite-signal, by the work of servomotor 6, is driven rotating shaft to be rotated, is entirely defended so as to drive Star antenna or even the roller of lower section are moved, and the bottom plate below roller is directly fixedly connected with the earth bolt, by satellite reception Disk 8 is turned to behind suitable position, drives expansion link 3 to carry out flexible work by the work of electric pushrod 1, so that signal connects Receiving device support bar 4 follows the progress micro-shifting of expansion link 3 to move, and is reached for the operation that signal receiver 2 is micro-adjusted, whole process is led to Mechanically actuated is crossed, operating efficiency is higher.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art, It is appreciated that these embodiments can be carried out in the case where not departing from principle of the present utility model and spirit a variety of changes, repaiies Change, replace and modification, scope of the present utility model is defined by the appended claims and the equivalents thereof.

Claims (5)

1. a kind of steady type and the satellite antenna of energy automatic fine tuning, including electric pushrod(1), signal receiver support bar(4)With Satellite reception disk(8), it is characterised in that:The satellite reception disk(8)Lower section be provided with support frame(5), and satellite connects Receive disk(8)With support frame(5)Junction be provided with packing ring(7), support frame as described above(5)Internal close satellite reception disk (8)Lower position be provided with servomotor(6), the servomotor(6)It is electrically connected with external control panel, the electricity Dynamic push rod(1)Installed in satellite reception disk(8)On, and electric pushrod(1)Top be provided with expansion link(3), it is described electronic Push rod(1)It is electrically connected with external control panel, and electric pushrod(1)Upper close satellite reception disk(8)Top position at It is provided with signal receiver(2), the signal receiver(2)It is electrically connected with external control panel, the signal receiver branch Strut(4)Installed in signal receiver(2)On.
2. a kind of steady type according to claim 1 and the satellite antenna of energy automatic fine tuning, it is characterised in that:It is described electronic Push rod(1)Be internally provided with gear-box(9), and electric pushrod(1)Internal close gear-box(9)Left side lower position set It is equipped with motor(10), the gear-box(9)With motor(10)Connected by axis of rotation.
3. a kind of steady type according to claim 1 and the satellite antenna of energy automatic fine tuning, it is characterised in that:The servo Motor(6)With satellite reception disk(8)Connected by axis of rotation.
4. a kind of steady type according to claim 1 and the satellite antenna of energy automatic fine tuning, it is characterised in that:The satellite Receive disk(8)With support frame(5)Pass through packing ring(7)It is fixedly connected.
5. a kind of steady type according to claim 1 and the satellite antenna of energy automatic fine tuning, it is characterised in that:The signal Receiver support bar(4)With satellite reception disk(8)It is fixedly connected by elastomeric pad.
CN201720324326.9U 2017-03-30 2017-03-30 A kind of steady type and the satellite antenna of energy automatic fine tuning Expired - Fee Related CN206585059U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720324326.9U CN206585059U (en) 2017-03-30 2017-03-30 A kind of steady type and the satellite antenna of energy automatic fine tuning

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720324326.9U CN206585059U (en) 2017-03-30 2017-03-30 A kind of steady type and the satellite antenna of energy automatic fine tuning

Publications (1)

Publication Number Publication Date
CN206585059U true CN206585059U (en) 2017-10-24

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108377165A (en) * 2018-04-20 2018-08-07 中蕊(武汉)光电科技有限公司 A kind of Ultraviolet Communication equipment and its operating method
CN109088644A (en) * 2018-09-27 2018-12-25 杜都 A kind of artificial intelligence sender unit of 5G communication network enhancing signal strength
CN109524784A (en) * 2018-11-26 2019-03-26 西安华运天成通讯科技有限公司 A kind of satellite signal receiver adjustment seat
CN110336966A (en) * 2019-05-29 2019-10-15 泉州天地星电子有限公司 A kind of combined receiver for satellite television

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108377165A (en) * 2018-04-20 2018-08-07 中蕊(武汉)光电科技有限公司 A kind of Ultraviolet Communication equipment and its operating method
CN108377165B (en) * 2018-04-20 2023-10-10 中蕊(武汉)光电科技有限公司 Ultraviolet communication equipment and operation method thereof
CN109088644A (en) * 2018-09-27 2018-12-25 杜都 A kind of artificial intelligence sender unit of 5G communication network enhancing signal strength
CN109088644B (en) * 2018-09-27 2020-01-31 智联信通科技股份有限公司 Artificial intelligence signal transmitting device for enhancing signal strength of 5G communication networks
CN109524784A (en) * 2018-11-26 2019-03-26 西安华运天成通讯科技有限公司 A kind of satellite signal receiver adjustment seat
CN110336966A (en) * 2019-05-29 2019-10-15 泉州天地星电子有限公司 A kind of combined receiver for satellite television
CN110336966B (en) * 2019-05-29 2022-07-12 泉州天地星电子有限公司 Combined satellite television receiver

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CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20171024

Termination date: 20200330