CN2854837Y - Disk electric slide satellite antenna - Google Patents
Disk electric slide satellite antenna Download PDFInfo
- Publication number
- CN2854837Y CN2854837Y CN 200520086004 CN200520086004U CN2854837Y CN 2854837 Y CN2854837 Y CN 2854837Y CN 200520086004 CN200520086004 CN 200520086004 CN 200520086004 U CN200520086004 U CN 200520086004U CN 2854837 Y CN2854837 Y CN 2854837Y
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- CN
- China
- Prior art keywords
- elevation angle
- adjusting rod
- satellite antenna
- push rod
- rod
- 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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- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
A disc type electric rail satellite antenna consists of a dish surface (1), an elevation angle adjusting rod (2), a bracket (3), an electric push rod and a base. The base consists of an upper disc (4) and a lower disc (5). The electric push rod consists of a decelerating motor (6), screw rod (7) and push rod (8). A hollow rail (10) is erected on arc edge of the lower disc (5), with height consistent with elevation angle of the satellite antenna. The electric push rod drives back-and-forth movement of the screw rod (7) via the decelerating motor (6), and further drives the upper disc (4) to rotate along the hollow rail (10). Adjusting work can be accomplished by only adjusting elevation angle of one satellite for receiving signal. In the utility model, receiving signal is tuned by adjusting height of the hollow rail, so the utility model has the advantages of simple adjusting, time saving, high signal receiving precision, simple integral structure, firm disc base, strong wind resistance, simple circuit, low manufacture cost, easy quality guarantee, and easy popularization.
Description
Technical field
The utility model relates to the satellite-signal receiving equipment, exactly belongs to the satellite signal receiving antenna field.
Background technology
Along with the overhead synchronous satellite in equator is more and more, a surface antenna is difficult to satisfy the demand that many synchronous satellite signals receive, if receive the multi-satellite signal a plurality of antennas need be installed, and the cost height, and it is big to take up space.Present existing reception antenna has polar mounts, twin axle, can solve the hope that a surface antenna receives multi-satellite basically, but these two kinds of antenna structure complexity, debugging difficulty is big, and the cost height.Usually, the polar mounts satellite antenna has three important angles---the elevation angle, due south, pole axis angle and offset angle, these three angles need to adjust repeatedly in debug process, because two universal joints are arranged on the push rod of pole axis satellite antenna, when wind is arranged, be easy to move, and its reception pot moves on inclined shaft, it is very heavy to accept pot load when both sides, burn out motor easily or damage gear, so its power of motor is big, the cost height.And twin axle satellite antenna debugging is simple, but the angle of each satellite that need receive all must be adjusted during debugging, and it has two cover reducing motors, controls the elevation angle and azimuth respectively, a whole set of cost height.
Summary of the invention
The purpose of this utility model provides a kind of simple in structure, debugging convenience, received signal precision height, the electronic rail satellite antenna of disc type that cost is low.
The technical solution adopted in the utility model is: be made up of pot face, elevation angle adjusting rod, support, electric pushrod and base, base is made up of last dish and lower wall, electric pushrod is made up of reducing motor, screw mandrel, push rod, on the arc edge of base lower wall, erect a hollow tracl, the height of hollow tracl is consistent with the elevation scale of satellite antenna, in debug process, only need the harmonize elevation scale of a satellite of received signal can be finished debugging work.
Beneficial effect: received signal of the present utility model is to debug out by the height of hollow tracl, so when debugging be simple, save time, received signal precision height, and overall structure is simple, the disc type base is firm, wind resistance power is strong, circuit is simple, low cost of manufacture, quality guarantee easily, very easily popularize.
Description of drawings
The utility model specification has two width of cloth accompanying drawings, and the drawing of this accompanying drawing is described as follows:
Fig. 1: the utility model schematic diagram
Fig. 2: the utility model hollow tracl schematic diagram
Among the figure: 1 is the pot face, and 2 is elevation angle adjusting rod, and 3 is support, and 4 is last dish, and 5 is lower wall, 6 is reducing motor, and 7 is screw mandrel, and 8 is push rod, and 9-1 and 9-2 are movable axis, and 10 is hollow tracl, 11 is horizontal bearing, and 2-1 is fixing square tube, and 2-2 is automatic adjusting rod, and 2-3 is manual adjusting rod.
Embodiment
The utility model is by pot face 1, elevation angle adjusting rod 2, support 3, electric pushrod and base are formed, base is made up of last dish 4 and lower wall 5, pot face 1 is fixed on going up on the dish 4 of base by elevation angle adjusting rod 2 and support 3, elevation angle adjusting rod 2 and support 3 flexibly connect with pot face 1, electric pushrod is by reducing motor 6, screw mandrel 7, push rod 8 is formed, electric pushrod is fixed on the lower wall 5 by movable axis 9-1, push rod 8 is fixed on the dish 4 by movable axis 9-2, last dish 4 is connected with lower wall 5 usefulness bearing fixing, last dish 4 can rotate on lower wall 5, on the arc edge of lower wall 5, erect a hollow tracl 10, the height of hollow tracl 10 is consistent with the elevation scale of satellite antenna, in elevation angle adjusting rod 2 lower ends horizontal bearing 11 is housed, laterally bearing 11 is installed in the hollow tracl 10, laterally bearing 11 can move along hollow tracl 10 (seeing Fig. 1 and Fig. 2).Wherein, elevation angle adjusting rod 2 by fixing square tube 2-1, automatically adjusting rod 2-2 and manually adjusting rod 2-3 forms, by automatic adjusting rod 2-2 and manual adjusting rod 2-3 adjustment elevation; Electric pushrod drives screw mandrel 7 by reducing motor 6 rotatings and seesaws, and dish 4 rotates along hollow tracl 10 in the drive.
Claims (3)
1, the electronic rail satellite antenna of a kind of disc type, it is characterized in that it is by pot face (1), elevation angle adjusting rod (2), support (3), electric pushrod and base are formed, base is made up of last dish (4) and lower wall (5), pot face (1) is fixed on going up on the dish (4) of base by elevation angle adjusting rod (2) and support (3), elevation angle adjusting rod (2) and support (3) flexibly connect with pot face (1), electric pushrod is by reducing motor (6), screw mandrel (7), push rod (8) is formed, electric pushrod is fixed on the lower wall (5) by movable axis (9-1), push rod (8) is fixed on the dish (4) by movable (axle 9-2), last dish (4) is connected with bearing fixing with lower wall (5), last dish (4) can be gone up at lower wall (5) and rotate, on the arc edge of lower wall (5), erect a hollow tracl (10), the height of hollow tracl (10) is consistent with the elevation scale of satellite antenna, in elevation angle adjusting rod (2) lower end horizontal bearing (11) is housed, laterally bearing (11) is installed in the hollow tracl (10), and laterally bearing (11) can move along hollow tracl (10).
2, the electronic rail satellite antenna of disc type according to claim 1, it is characterized in that described elevation angle adjusting rod (2) by fixing square tube (2-1), adjusting rod (2-2) and manual adjustment rod (2-3) are formed automatically, by automatic adjusting rod (2-2) and manual adjustment rod (2-3) adjustment elevation.
3, the electronic rail satellite antenna of disc type according to claim 1, it is characterized in that described electric pushrod is made up of reducing motor (6), screw mandrel (7), push rod (8), seesaw by the positive and negative drive screw mandrel of reducing motor (6) (7), dish (4) rotates along hollow tracl (10) in the drive.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200520086004 CN2854837Y (en) | 2005-08-04 | 2005-08-04 | Disk electric slide satellite antenna |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200520086004 CN2854837Y (en) | 2005-08-04 | 2005-08-04 | Disk electric slide satellite antenna |
Publications (1)
Publication Number | Publication Date |
---|---|
CN2854837Y true CN2854837Y (en) | 2007-01-03 |
Family
ID=37581473
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 200520086004 Expired - Fee Related CN2854837Y (en) | 2005-08-04 | 2005-08-04 | Disk electric slide satellite antenna |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN2854837Y (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103149482A (en) * | 2013-02-26 | 2013-06-12 | 浙江中星光电子科技有限公司 | Inspection device and method for ship-borne satellite signal receiving antenna |
CN106129581A (en) * | 2016-08-19 | 2016-11-16 | 广州市易恒信息技术有限公司 | A kind of box-type guide rail portable satellite communications antenna |
CN106159410A (en) * | 2016-08-19 | 2016-11-23 | 广州市易恒信息技术有限公司 | A kind of guide tracked portable satellite communications antenna |
CN109066050A (en) * | 2018-08-02 | 2018-12-21 | 林瑞 | A kind of communications satellite antenna bracket and its antenna adjustment method |
CN109888494A (en) * | 2019-03-06 | 2019-06-14 | 张淼淼 | A kind of durable type multifrequency antenna for base station |
CN112928422A (en) * | 2021-01-25 | 2021-06-08 | 楚桂美 | Mounting bracket for satellite communication |
-
2005
- 2005-08-04 CN CN 200520086004 patent/CN2854837Y/en not_active Expired - Fee Related
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103149482A (en) * | 2013-02-26 | 2013-06-12 | 浙江中星光电子科技有限公司 | Inspection device and method for ship-borne satellite signal receiving antenna |
CN103149482B (en) * | 2013-02-26 | 2015-06-10 | 浙江中星光电子科技有限公司 | Inspection device and method for ship-borne satellite signal receiving antenna |
CN106129581A (en) * | 2016-08-19 | 2016-11-16 | 广州市易恒信息技术有限公司 | A kind of box-type guide rail portable satellite communications antenna |
CN106159410A (en) * | 2016-08-19 | 2016-11-23 | 广州市易恒信息技术有限公司 | A kind of guide tracked portable satellite communications antenna |
WO2018032534A1 (en) * | 2016-08-19 | 2018-02-22 | 广州市易恒信息技术有限公司 | Guide rail type portable satellite communication antenna |
CN106129581B (en) * | 2016-08-19 | 2019-02-26 | 广州市易恒信息技术有限公司 | A kind of box-type guide rail portable satellite communications antenna |
CN106159410B (en) * | 2016-08-19 | 2019-07-02 | 广州来电新动力研究中心有限公司 | A kind of guide tracked portable satellite communications antenna |
US10784559B2 (en) | 2016-08-19 | 2020-09-22 | E4E Information Technologies Co., Ltd. | Rail-type portable satellite communication antenna |
CN109066050A (en) * | 2018-08-02 | 2018-12-21 | 林瑞 | A kind of communications satellite antenna bracket and its antenna adjustment method |
CN109888494A (en) * | 2019-03-06 | 2019-06-14 | 张淼淼 | A kind of durable type multifrequency antenna for base station |
CN109888494B (en) * | 2019-03-06 | 2020-11-24 | 江苏三晟信息科技有限公司 | Durable multi-frequency base station antenna |
CN112928422A (en) * | 2021-01-25 | 2021-06-08 | 楚桂美 | Mounting bracket for satellite 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: 20070103 |