CN204732517U - A kind of New Satellite antenna - Google Patents
A kind of New Satellite antenna Download PDFInfo
- Publication number
- CN204732517U CN204732517U CN201520446181.0U CN201520446181U CN204732517U CN 204732517 U CN204732517 U CN 204732517U CN 201520446181 U CN201520446181 U CN 201520446181U CN 204732517 U CN204732517 U CN 204732517U
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- CN
- China
- Prior art keywords
- support section
- pillar
- sides
- satellite antenna
- pot
- Prior art date
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- Expired - Fee Related
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Abstract
The utility model relates to the communications field, particularly relates to a kind of New Satellite antenna.Comprise basic platform, described basic flat rubber belting comprises pillar, described pillar upper end turning hinge can be connected to satellite pot, described satellite pot both sides comprise support section respectively, described support section can pass basic platform, described support section comprises two parts, and lay respectively at the both sides of pillar and be placed in the below of satellite pot, the lifting of support section can drive satellite pot to turn to.Beneficial effect: not employment goes to turn to, can realize turning to of satellite pot by the lifting of support section, single unit system be turned to more convenient, and operation is gone in not employment specially.
Description
Technical field
The utility model relates to the communications field, particularly relates to a kind of New Satellite antenna.
Background technology
The defect of the technology of existing satellite antenna is:
1. easy ponding corrosion bottom;
2. be difficult to stable elevation;
3. be difficult to effectively self deicing;
4. be difficult to sun-proof.
Utility model content
The object of utility model: in order to provide a kind of New Satellite antenna of better effects if, specific purposes are shown in multiple substantial technological effects of concrete implementation section.
In order to reach as above object, the utility model takes following technical scheme:
A kind of New Satellite antenna, it is characterized in that, comprise basic platform, described basic flat rubber belting comprises pillar, and described pillar upper end turning hinge can be connected to satellite pot, and described satellite pot both sides comprise support section respectively, described support section can pass basic platform, described support section comprises two parts, and lay respectively at the both sides of pillar and be placed in the below of satellite pot, the lifting of support section can drive satellite pot to turn to.
The further technical scheme of the utility model is, described support section is the plate structure of arc, has cylinder below it, and the support component laying respectively at the both sides of pillar has cylinder in below separately.
The further technical scheme of the utility model is, described support section is steel wire, described steel wire can be wrapped in the rotating shaft of middle part, the rotating shaft of described middle part is positioned on the power output shaft of the motor below pillar, the steel wire rope side being positioned at pillar both sides when the axis of rotation of middle part time is shunk, and side unreels.
The further technical scheme of the utility model is, described in be positioned at pillar both sides its stroke of each leisure of steel wire rope on through a pulley.
The further technical scheme of the utility model is, described basic platform comprises a shaking device.
The further technical scheme of the utility model is, described support section comprises an avris bar, and described avris bar comprises sun-proof cloth.
Adopt the utility model of as above technical scheme, have following beneficial effect relative to prior art: not employment goes to turn to, can realize turning to of satellite pot, single unit system is turned to more convenient by the lifting of support section, operation is gone in not employment specially.
Accompanying drawing explanation
In order to further illustrate the utility model, be described further below in conjunction with accompanying drawing:
Fig. 1 is utility model structural representation;
Wherein: 1. pillar; 2. supporting construction; 3. pulley on the right side of; 4. rotating shaft in the middle part of; 5. motor; Pulley on the left of in the of 6; 7. support section; 8. satellite pot; 9. avris bar; 10. sun-proof cloth.
Embodiment
Be described embodiment of the present utility model below in conjunction with accompanying drawing, embodiment does not form restriction of the present utility model:
A kind of New Satellite antenna, it is characterized in that, comprise basic platform, described basic flat rubber belting comprises pillar 1, and described pillar 1 upper end turning hinge can be connected to satellite pot, and described satellite pot both sides comprise support section respectively, described support section can pass basic platform, described support section comprises two parts, and lay respectively at the both sides of pillar and be placed in the below of satellite pot, the lifting of support section can drive satellite pot to turn to.The technique effect of the essence that the technical scheme at this place plays and implementation procedure thereof are as follows: not employment goes to turn to, and can realize turning to of satellite pot, single unit system is turned to more convenient by the lifting of support section, and operation is gone in not employment specially.
As the preferred implementation of one, described support section is the plate structure of arc, has cylinder below it, and the support component laying respectively at the both sides of pillar has cylinder in below separately.The technique effect of the essence that the technical scheme at this place plays and implementation procedure thereof are as follows: plate structure lifting can prop up turning to of satellite pot, in addition, because plate structure itself is with anti-wind action, can effectively prevent dust storm to the erosion of pillar itself and coupling part.
Described support section is steel wire, and described steel wire can be wrapped in the rotating shaft of middle part, and the rotating shaft of described middle part is positioned on the power output shaft of the motor below pillar, and the steel wire rope side being positioned at pillar both sides when the axis of rotation of middle part time is shunk, and side unreels.The technique effect of the essence that the technical scheme at this place plays and implementation procedure thereof are as follows: composition graphs 1, and this place adopts the rotation of motor, and can realize the adjustment of rope capacity, steel cord ends is fixed on the below of satellite pot body.
Through a pulley on described its stroke of each leisure of steel wire rope being positioned at pillar both sides.The technique effect of the essence that the technical scheme at this place plays and implementation procedure thereof are as follows: pulley can conveniently lead, and the pulley at this place is fixed pulley, make its guiding precisely.
Described basic platform comprises a shaking device.The technique effect of the essence that the technical scheme at this place plays and implementation procedure thereof are as follows: when top has sleet to affect communication time, can also shake, facilitate sleet from the removing satellite pot.
Described support section comprises an avris bar, described avris bar comprises sun-proof cloth.The technique effect of the essence that the technical scheme at this place plays and implementation procedure thereof are as follows: sun-proof cloth can prevent satellite pot body to be shone.Sun-proof cloth as the structure of a hard, can also play protective action to pot body simultaneously.
In a creative way, each effect above independently exists, and can also complete the combination of the above results with a nested structure.
It is clear that the technique effect that above structure realizes realizes, if do not consider the technical scheme of adding, this patent title can also be a kind of antenna.Not shown part details.Certainly, satellite pot belongs to prior art, and it is groove-like structure general at present.
It should be noted that, multiple schemes that this patent provides comprise basic scheme own, separate, mutually do not restrict, but it also can combine when not conflicting mutually, reaching multiple effect and jointly realizing.
more than show and describe general principle of the present utility model, principal character and advantage of the present utility model.Those skilled in the art should understand the utility model and not be restricted to the described embodiments; what describe in above-described embodiment and specification just illustrates principle of the present utility model; under the prerequisite not departing from the utility model spirit and scope; the utility model also has various changes and modifications, and these changes and improvements all fall in claimed scope.
Claims (6)
1. a New Satellite antenna, it is characterized in that, comprise basic platform, described basic flat rubber belting comprises pillar (1), described pillar (1) upper end turning hinge can be connected to satellite pot, and described satellite pot both sides comprise support section respectively, described support section can pass basic platform, described support section comprises two parts, and lay respectively at the both sides of pillar and be placed in the below of satellite pot, the lifting of support section can drive satellite pot to turn to.
2. a kind of New Satellite antenna as claimed in claim 1, it is characterized in that, described support section is the plate structure of arc, has cylinder below it, and the support component laying respectively at the both sides of pillar has cylinder in below separately.
3. a kind of New Satellite antenna as claimed in claim 1, it is characterized in that, described support section is steel wire, described steel wire can be wrapped in the rotating shaft of middle part, the rotating shaft of described middle part is positioned on the power output shaft of the motor below pillar, the steel wire rope side being positioned at pillar both sides when the axis of rotation of middle part time is shunk, and side unreels.
4. a kind of New Satellite antenna as claimed in claim 3, is characterized in that, described in be positioned at pillar both sides its stroke of each leisure of steel wire rope on through a pulley.
5. a kind of New Satellite antenna as claimed in claim 1, is characterized in that, described basic platform comprises a shaking device.
6. a kind of New Satellite antenna as claimed in claim 1, is characterized in that, described support section comprises an avris bar, and described avris bar comprises sun-proof cloth.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520446181.0U CN204732517U (en) | 2015-06-26 | 2015-06-26 | A kind of New Satellite antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520446181.0U CN204732517U (en) | 2015-06-26 | 2015-06-26 | A kind of New Satellite antenna |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204732517U true CN204732517U (en) | 2015-10-28 |
Family
ID=54390845
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520446181.0U Expired - Fee Related CN204732517U (en) | 2015-06-26 | 2015-06-26 | A kind of New Satellite antenna |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204732517U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108682955A (en) * | 2018-05-11 | 2018-10-19 | 安徽尼古拉电子科技有限公司 | A kind of integrated terminal antenna based on Beidou navigation technology |
-
2015
- 2015-06-26 CN CN201520446181.0U patent/CN204732517U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108682955A (en) * | 2018-05-11 | 2018-10-19 | 安徽尼古拉电子科技有限公司 | A kind of integrated terminal antenna based on Beidou navigation technology |
| CN108682955B (en) * | 2018-05-11 | 2020-12-29 | 山东天元信息技术集团有限公司 | Integrated terminal antenna based on Beidou navigation technology |
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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: 20151028 Termination date: 20160626 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |