CN204350150U - Spinning Positioning Satellite receiver - Google Patents
Spinning Positioning Satellite receiver Download PDFInfo
- Publication number
- CN204350150U CN204350150U CN201520014710.XU CN201520014710U CN204350150U CN 204350150 U CN204350150 U CN 204350150U CN 201520014710 U CN201520014710 U CN 201520014710U CN 204350150 U CN204350150 U CN 204350150U
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- CN
- China
- Prior art keywords
- satellite receiver
- base
- motor
- support column
- controller
- 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
Spinning Positioning Satellite receiver, comprise base, mounted motor, thrust bearing and controller in base, the output shaft of motor connects driving gear, thrust bearing coordinates supporting seat is installed, supporting seat is installed vertical support column, base offers through hole, support column installs reflector through via top, and controller can control electric machine rotation.The utility model adjusts motor under the control of the controller and rotates, and driven by motor driving gear rotates, thus drives driven gear to rotate, thus drives reflector to satelloid by support column.
Description
Technical field
The utility model belongs to satellite reception field, specifically a kind of spinning Positioning Satellite receiver.
Background technology
At present, along with popularizing of satellite receiver, satellite is widely used in life, but present satellite receiver all needs manually to star, after satellite reception apparatus is good, just can not move, as encountered bad weather, causing satellite to move, needing the personage of specialty to carry out star, to star more complicated, satellite receiver is caused to assemble complicated.
Utility model content
The utility model provides a kind of spinning Positioning Satellite receiver, in order to solve defect of the prior art.
The utility model is achieved by the following technical programs:
Spinning Positioning Satellite receiver, comprise base, mounted motor, thrust bearing and controller in base, the output shaft of motor connects driving gear, thrust bearing coordinates supporting seat is installed, supporting seat is installed vertical support column, base offers through hole, support column installs reflector through via top, and controller can control electric machine rotation.
Spinning Positioning Satellite receiver as above, described base installs end wall bracket, and roller bearing is installed in the end of end wall bracket, and roller bearing coordinates with support column.
Spinning Positioning Satellite receiver as above, GPS module, single-chip microcomputer and relay are set in described controller, GPS module is by the coordinate information at satellite receiver place transmission single-chip microcomputer, single-chip microcomputer passes through Control motor according to the coordinate information received, thus automatically right by the angle of inclination of motor adjustment base.
Spinning Positioning Satellite receiver as above, described satellite receiver arranges tuner, high frequency tuner circuit comprises resonator, amplifying circuit, frequency mixer and filter circuit, the signal that satellite antenna receives is transferred to amplifying circuit after filter circuit, by frequency mixer frequency modulation after amplifying circuit, described resonator is connected electrically in frequency mixer, for frequency mixer provides local frequency, described filter circuit comprises transport and placing device A1, the inverting input of described transport and placing device A1 is by resistance R1 series connection ground connection, series resistance R2 between the inverting input of described transport and placing device A1 and output, series resistance R5 between the in-phase input end of described transport and placing device A1 and input, series resistance R3 and electric capacity C1 on the in-phase input end of described transport and placing device A1, electric capacity C2 is connected in parallel on the two ends of electric capacity C1 and resistance R5.
The utility model has the advantages that: the utility model adjusts motor under the control of the controller and rotates, and driven by motor driving gear rotates, thus drive driven gear to rotate, thus drive reflector to satelloid by support column.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is the utility model structural representation; Fig. 2 is utility model works schematic diagram; Fig. 3 is the utility model circuit diagram.
Embodiment
For making the object of the utility model embodiment, technical scheme and advantage clearly, below in conjunction with the accompanying drawing in the utility model embodiment, technical scheme in the utility model embodiment is clearly and completely described, obviously, described embodiment is the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
Spinning Positioning Satellite receiver, as shown in Figure 1, comprise base 11, in base 1, mounted motor 6, thrust bearing 7 and controller, the output shaft of motor 6 connects driving gear 5, thrust bearing 7 coordinates and installs supporting seat 8, supporting seat 8 is installed vertical support column 2, base 11 is offered through hole 10, support column 2 installs reflector 1 through through hole 10 top, and controller can control motor 6 and rotate.The utility model adjusts motor 6 under the control of the controller and rotates, and motor 6 drives driving gear 5 to rotate, thus drives driven gear 9 to rotate, thus drives reflector 1 pair of satelloid by support column 2.
Concrete, in order to increase the stability turned in journey, described base 11 installs end wall bracket 4, roller bearing 3 is installed in the end of end wall bracket 4, and roller bearing 3 coordinates with support column 2.
Further, as shown in Figure 2, GPS module, single-chip microcomputer and relay are set in the controller described in the present embodiment, GPS module is by the coordinate information at satellite receiver place transmission single-chip microcomputer, single-chip microcomputer passes through Control motor according to the coordinate information received, thus automatically right by the angle of inclination of motor adjustment base.
Further, as shown in Figure 3, the present embodiment satellite receiver arranges tuner, high frequency tuner circuit comprises resonator, amplifying circuit, frequency mixer and filter circuit, the signal that satellite antenna receives is transferred to amplifying circuit after filter circuit, by frequency mixer frequency modulation after amplifying circuit, resonator is connected electrically in frequency mixer, for frequency mixer provides local frequency, filter circuit is as shown in Fig. 2, comprise transport and placing device A1, the inverting input of transport and placing device A1 is by resistance R1 series connection ground connection, series resistance R2 between the inverting input of transport and placing device A1 and output, series resistance R5 between the in-phase input end of transport and placing device A1 and input, series resistance R3 and electric capacity C1 on the in-phase input end of described transport and placing device A1, electric capacity C2 is connected in parallel on the two ends of electric capacity C1 and resistance R5.
Last it is noted that above embodiment is only in order to illustrate the technical solution of the utility model, be not intended to limit; Although be described in detail the utility model with reference to previous embodiment, those of ordinary skill in the art is to be understood that: it still can be modified to the technical scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature; And these amendments or replacement, do not make the essence of appropriate technical solution depart from the spirit and scope of each embodiment technical scheme of the utility model.
Claims (4)
1. spinning Positioning Satellite receiver, it is characterized in that: comprise base (11), base (1) interior mounted motor (6), thrust bearing (7) and controller, the output shaft of motor (6) connects driving gear (5), thrust bearing (7) upper cooperation installs supporting seat (8), supporting seat (8) is upper installs vertical support column (2), base (11) is offered through hole (10), support column (2) installs reflector (1) through through hole (10) top, and controller can control motor (6) and rotate.
2. spinning Positioning Satellite receiver according to claim 1, is characterized in that: described base (11) installs end wall bracket (4), and roller bearing (3) is installed in the end of end wall bracket (4), and roller bearing (3) coordinates with support column (2).
3. spinning Positioning Satellite receiver according to claim 1, it is characterized in that: GPS module, single-chip microcomputer and relay are set in described controller, GPS module is by the coordinate information at satellite receiver place transmission single-chip microcomputer, single-chip microcomputer passes through Control motor according to the coordinate information received, thus adjusts the angle of inclination of base automatically to star by motor.
4. according to spinning Positioning Satellite receiver according to claim 1, it is characterized in that: described satellite receiver arranges tuner, high frequency tuner circuit comprises resonator, amplifying circuit, frequency mixer and filter circuit, the signal that satellite antenna receives is transferred to amplifying circuit after filter circuit, by frequency mixer frequency modulation after amplifying circuit, described resonator is connected electrically in frequency mixer, for frequency mixer provides local frequency, described filter circuit comprises transport and placing device A1, the inverting input of described transport and placing device A1 is by resistance R1 series connection ground connection, series resistance R2 between the inverting input of described transport and placing device A1 and output, series resistance R5 between the in-phase input end of described transport and placing device A1 and input, series resistance R3 and electric capacity C1 on the in-phase input end of described transport and placing device A1, electric capacity C2 is connected in parallel on the two ends of electric capacity C1 and resistance R5.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520014710.XU CN204350150U (en) | 2015-01-09 | 2015-01-09 | Spinning Positioning Satellite receiver |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520014710.XU CN204350150U (en) | 2015-01-09 | 2015-01-09 | Spinning Positioning Satellite receiver |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204350150U true CN204350150U (en) | 2015-05-20 |
Family
ID=53233387
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520014710.XU Expired - Fee Related CN204350150U (en) | 2015-01-09 | 2015-01-09 | Spinning Positioning Satellite receiver |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204350150U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108987890A (en) * | 2018-09-17 | 2018-12-11 | 广州玛夫信息科技有限公司 | A kind of signal detection receiving device |
| CN110601703A (en) * | 2019-09-20 | 2019-12-20 | 孙凤山 | Signal receiver with adjustable 5G communication |
-
2015
- 2015-01-09 CN CN201520014710.XU patent/CN204350150U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108987890A (en) * | 2018-09-17 | 2018-12-11 | 广州玛夫信息科技有限公司 | A kind of signal detection receiving device |
| CN110601703A (en) * | 2019-09-20 | 2019-12-20 | 孙凤山 | Signal receiver with adjustable 5G communication |
| CN110601703B (en) * | 2019-09-20 | 2021-06-04 | 赛特斯信息科技股份有限公司 | Signal receiver with adjustable 5G communication |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150520 Termination date: 20160109 |