CN104124532A - Combined reflecting surface of satellite antenna - Google Patents
Combined reflecting surface of satellite antenna Download PDFInfo
- Publication number
- CN104124532A CN104124532A CN201410377420.1A CN201410377420A CN104124532A CN 104124532 A CN104124532 A CN 104124532A CN 201410377420 A CN201410377420 A CN 201410377420A CN 104124532 A CN104124532 A CN 104124532A
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- CN
- China
- Prior art keywords
- main body
- reflecting surface
- reflecting
- satellite antenna
- reflecting plate
- 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.)
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- Aerials With Secondary Devices (AREA)
- Details Of Aerials (AREA)
Abstract
The invention relates to a combined reflecting surface of a satellite antenna. The combined reflecting surface comprises a framework and a plurality of reflecting plates, wherein the framework comprises a main body rod and a plurality of branch rods, and the branch rods are arranged at the both sides of the main body rod in an array; the reflecting plates are strip-shaped, through holes matched with the branch rods are processed in the reflecting plates, and the reflecting plates are installed at the both sides of the main body rod through the branch rod array to form the reflecting surface; a support is made from stainless steel, and the reflecting plates are made from aluminium. The reflecting surface disclosed by the invention is detachable, and capable of being detached and stored when not in use, and the detached strip-shaped reflecting surface is smaller in floor space, and more convenient for vehicle-mounted use.
Description
Technical field
The present invention relates to a kind of combined type satellite antenna reflective face, belong to satellite antenna field.
Background technology
The pot body of traditional cooking-pot type satellite antenna is structure as a whole, and is easy to occur dust stratification when not using, and mobile more difficult, and in the time of on being arranged on vehicle, the windage producing during to vehicle mobile is also larger.
Summary of the invention
The technical problem to be solved in the present invention is: overcome technical problem in prior art, provide a kind of.
The technical solution adopted for the present invention to solve the technical problems is:
A combined type satellite antenna reflective face, comprises skeleton and some reflecting plates, and described skeleton comprises main body bar and some poles, and described pole array arrangement is in the both sides of main body bar;
Described reflecting plate is strip, in described reflecting plate inside, is processed with the through hole coordinating with described pole, and the both sides that described reflecting plate is arranged on main body bar by a bar array form reflecting surface;
Described support adopts stainless steel to make, and described reflecting plate is aluminum.
As further innovation of the present invention, the diameter of described pole and main body bar connecting portion is greater than the diameter of pole elongated end.
The invention has the beneficial effects as follows:
Reflecting surface of the present invention is detachable, when not using, reflecting surface can be dismantled and is deposited, and it is less that the strip reflecting surface after pulling down takes up an area space, is more convenient to vehicle-mounted use.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the present invention is further described.
Fig. 1 is generalized section of the present invention;
Fig. 2 is the schematic diagram of skeleton of the present invention;
Fig. 3 is the schematic diagram of reflecting plate of the present invention.
Embodiment
In conjunction with the accompanying drawings, the present invention is further detailed explanation.These accompanying drawings are the schematic diagram of simplification, basic structure of the present invention is only described in a schematic way, so it only show the formation relevant with the present invention.
As shown in Fig. 1 ~ 3, the present invention is a kind of combined type satellite antenna reflective face, comprises skeleton and some reflecting plates 3, and skeleton comprises main body bar 1 and some poles 2, and pole 2 array arrangements are in the both sides of main body bar 1;
Reflecting plate 3 is strip, is processed with the through hole 4 coordinating with pole 2 in reflecting plate 3 inside, and the both sides that reflecting plate 3 is arranged on main body bar 1 by pole 2 arrays form reflecting surface;
Support adopts stainless steel to make, and reflecting plate 3 is aluminum.
The diameter of pole 2 and main body bar 1 connecting portion is greater than the diameter of pole 2 elongated ends.
Under not use state, skeleton can reduce the windage of reflecting surface greatly, when needs are used, as long as reflecting plate is installed on skeleton, and simple and fast.
The above-mentioned foundation desirable embodiment of the present invention of take is enlightenment, and by above-mentioned description, relevant staff can, within not departing from the scope of this invention technological thought, carry out various change and modification completely.The technical scope of this invention is not limited to the content on specification, must determine its technical scope according to claim scope.
Claims (2)
1. a combined type satellite antenna reflective face, is characterized in that: comprise skeleton and some reflecting plates, described skeleton comprises main body bar and some poles, and described pole array arrangement is in the both sides of main body bar;
Described reflecting plate is strip, in described reflecting plate inside, is processed with the through hole coordinating with described pole, and the both sides that described reflecting plate is arranged on main body bar by a bar array form reflecting surface;
Described support adopts stainless steel to make, and described reflecting plate is aluminum.
2. a kind of combined type satellite antenna reflective face as claimed in claim 1, is characterized in that: the diameter of described pole and main body bar connecting portion is greater than the diameter of pole elongated end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410377420.1A CN104124532A (en) | 2014-08-04 | 2014-08-04 | Combined reflecting surface of satellite antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410377420.1A CN104124532A (en) | 2014-08-04 | 2014-08-04 | Combined reflecting surface of satellite antenna |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104124532A true CN104124532A (en) | 2014-10-29 |
Family
ID=51769861
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410377420.1A Pending CN104124532A (en) | 2014-08-04 | 2014-08-04 | Combined reflecting surface of satellite antenna |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104124532A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104579387A (en) * | 2014-12-31 | 2015-04-29 | 健富塑胶五金制品（东莞）有限公司 | Enhanced satellite signal receiver |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6353421B1 (en) * | 2000-09-14 | 2002-03-05 | Ball Aerospace And Technologies Corp. | Deployment of an ellectronically scanned reflector |
| CN2821893Y (en) * | 2005-07-22 | 2006-09-27 | 中卫科技股份有限公司 | Combined antenna disc surface |
| CN201238077Y (en) * | 2008-08-06 | 2009-05-13 | 四川九洲电器集团有限责任公司 | Portable satellite receiving antenna |
| CN201655974U (en) * | 2010-02-11 | 2010-11-24 | 杨瑞雄 | Antenna reflector net |
| CN102683885A (en) * | 2012-04-28 | 2012-09-19 | 深圳光启创新技术有限公司 | Portable satellite antenna and satellite antenna receiving system |
| CN203983502U (en) * | 2014-08-04 | 2014-12-03 | 江苏中寰卫星导航通信有限公司 | A kind of combined type satellite antenna reflective face |
-
2014
- 2014-08-04 CN CN201410377420.1A patent/CN104124532A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6353421B1 (en) * | 2000-09-14 | 2002-03-05 | Ball Aerospace And Technologies Corp. | Deployment of an ellectronically scanned reflector |
| CN2821893Y (en) * | 2005-07-22 | 2006-09-27 | 中卫科技股份有限公司 | Combined antenna disc surface |
| CN201238077Y (en) * | 2008-08-06 | 2009-05-13 | 四川九洲电器集团有限责任公司 | Portable satellite receiving antenna |
| CN201655974U (en) * | 2010-02-11 | 2010-11-24 | 杨瑞雄 | Antenna reflector net |
| CN102683885A (en) * | 2012-04-28 | 2012-09-19 | 深圳光启创新技术有限公司 | Portable satellite antenna and satellite antenna receiving system |
| CN203983502U (en) * | 2014-08-04 | 2014-12-03 | 江苏中寰卫星导航通信有限公司 | A kind of combined type satellite antenna reflective face |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104579387A (en) * | 2014-12-31 | 2015-04-29 | 健富塑胶五金制品（东莞）有限公司 | Enhanced satellite signal receiver |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20141029 |