CN103338067A - Portable integrated satellite communication station - Google Patents
Portable integrated satellite communication station Download PDFInfo
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- CN103338067A CN103338067A CN 201310231131 CN201310231131A CN103338067A CN 103338067 A CN103338067 A CN 103338067A CN 201310231131 CN201310231131 CN 201310231131 CN 201310231131 A CN201310231131 A CN 201310231131A CN 103338067 A CN103338067 A CN 103338067A
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- pitching
- stepping motor
- transmission mechanism
- orientation
- azimuth
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- 230000005540 biological transmission Effects 0.000 claims abstract description 39
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 14
- 230000000694 effects Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- 230000010287 polarization Effects 0.000 description 1
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Abstract
The invention discloses a portable integrated satellite communication station. The portable integrated satellite communication station is characterized by comprising a direction transmission mechanism, a pitching transmission mechanism and antennas, wherein the pitching transmission mechanism is connected to the upper part of the direction transmission mechanism; a direction shaft is arranged in the vertical direction perpendicular to a base; a direction stepping motor and a direction rotary table are sequentially arranged on the direction shaft from the top down; an inserted pin of a pitching base is connected to the direction rotary table; the direction stepping motor is positioned in the pitching base; a pitching stepping motor is arranged in the pitching base; a rotating shaft is arranged in the horizontal direction of the pitching stepping motor; an antenna frame is arranged at each end of the two ends of the rotating shaft; the antennas are arranged on the antenna frames. Compared with the prior art, the structures of the pitching driven system and the direction driven system are more compact, so that the satellite communication station is smaller in size, lighter in weight, easy to transport and carry, and higher in transmission accuracy.
Description
Technical field
The present invention relates to a kind of satellite communication portable station, particularly a kind of integral type portable satellite communications station.
Background technology
Satellite communication portable station is a kind of satellite communication station of portable extra small bore, it forms satellite communication network by the link with the geostationary orbit communication satellite, multimedia communication services such as support voice, data, audio frequency and video and wide area network access are the excellent means that realizes that remote data transmission, scene of the accident emergency communication and live video relay etc. are professional.Satellite communication portable station adopts orientation, pitching, three servo systems of polarization, can realize that a key is automatically to star.Because satellite communication station for higher to the star required precision, has specific requirement to star speed, therefore, its orientation, pitching transmission mechanism need adopt the precision drive mechanism of big speed ratio.This volume that has caused existing satellite communication portable station is big, Heavy Weight, vanning inconvenience, transportation Portability are poor.
Summary of the invention
The technical issues that need to address of the present invention are at above-mentioned the deficiencies in the prior art, and provide a kind of volume little, and are in light weight, easy to carry, the integral type satellite communication portable station that transmission accuracy is higher.
For solving the problems of the technologies described above, the technical solution used in the present invention is:
A kind of integral type portable satellite communications station is characterized in that: comprise the orientation transmission mechanism, pitching transmission mechanism and antenna, pitching transmission mechanism are connected transmission mechanism top, orientation; Described orientation transmission mechanism comprises base, azimuth axis, and orientation stepping motor and azimuth rotating platform are provided with azimuth axis at the vertical direction perpendicular to base, and orientation stepping motor and azimuth rotating platform are successively set on the azimuth axis from top to bottom; Described pitching transmission mechanism comprises the pitching pedestal, the pitching stepping motor, rotation axis and antenna holder, the pitching base pin is connected on the described azimuth rotating platform, described orientation stepping motor is positioned at the pitching pedestal, the pitching stepping motor is located on the pitching pedestal, is provided with rotation axis in the horizontal direction of pitching stepping motor, is respectively equipped with antenna holder at the two ends of rotation axis; Described antenna is positioned on the antenna holder.
On rotation axis and the both sides that are positioned at the pitching stepping motor pitching harmonic wave speed reducing machine is set respectively.
A ring flange that is used for the fixed antenna frame is set respectively in the outside of described pitching harmonic wave speed reducing machine.
At azimuth axis a manual turntable is set.
At azimuth axis an orientation harmonic wave speed reducing machine is set.
Compared with prior art, a kind of integral type portable satellite communications of the present invention station, its beneficial effect is: volume is little, and is in light weight, transport easy to carry, the transmission accuracy height, it is faster to use speed, it is rapider to adjust angle.
Description of drawings
Fig. 1 is structural representation of the present invention;
Fig. 2 is the stereogram of pitching transmission mechanism and orientation transmission mechanism;
Fig. 3 is the profile of pitching transmission mechanism and orientation transmission mechanism;
Wherein, 1-base, 2-azimuth axis, 3-orientation stepping motor, 4-azimuth rotating platform, 5-pitching pedestal, 6-pitching stepping motor, 7-rotation axis, 8-antenna holder, 9-pitching harmonic wave speed reducing machine, 10-ring flange, 11-manual turntable, 12-orientation harmonic wave speed reducing machine.
Embodiment
Describe the preferred technical solution of the present invention in detail below in conjunction with accompanying drawing.
As shown in the figure, a kind of integral type portable satellite communications of the present invention station is characterized in that: comprise the orientation transmission mechanism, pitching transmission mechanism and antenna, pitching transmission mechanism are connected transmission mechanism top, orientation; Described orientation transmission mechanism comprises base 1, azimuth axis 2, and orientation stepping motor 3 and azimuth rotating platform 4 are provided with azimuth axis 2 at the vertical direction perpendicular to base 1, and orientation stepping motor 3 and azimuth rotating platform 4 are successively set on the azimuth axis 2 from top to bottom; Described pitching transmission mechanism comprises pitching pedestal 5, pitching stepping motor 6, rotation axis 7 and antenna holder 8, pitching pedestal 5 latches are connected on the described azimuth rotating platform 4, described orientation stepping motor 3 is positioned at pitching pedestal 5, pitching stepping motor 6 is located on the pitching pedestal 5, is provided with rotation axis 7 in the horizontal direction of pitching stepping motor 6, is respectively equipped with antenna holder 8 at the two ends of rotation axis 7; Described antenna is positioned on the antenna holder 8.
Whole pitching transmission mechanism and orientation transmission mechanism are integral types, and antenna carries out lifting by the pitching transmission mechanism; In the pitching transmission mechanism, pitching stepping motor 6 provides power, drives rotation axis 7 and rotates, thereby make left antenna holder 8 carry out the pitching swing, makes antenna reach the function of adjusting angle; In the orientation transmission mechanism, orientation stepping motor 3 provides power, azimuth rotating platform 4 is rotated, and azimuth rotating platform 4 is that latch is connected with pitching pedestal 5, so azimuth rotating platform 4 is again to drive whole pitching transmission mechanism to carry out the plane rotation.
On rotation axis 7 and the both sides that are positioned at pitching stepping motor 6 a pitching harmonic wave speed reducing machine 9 is set respectively.
9 pairs of pitching stepping motors of pitching harmonic wave speed reducing machine 6 rotate and have stopped decelerating effect, i.e. reach the effect of deceleration during antenna lift adjustment angle, can also reinforce antenna.
A ring flange 10 that is used for fixed antenna frame 8 is set respectively in the outside of described pitching harmonic wave speed reducing machine 9.
At azimuth axis 2 manual turntable 11 is set.
Prevent when orientation stepping motor 3 from breaking down can't operate as normal situation take place, namely artificial rotation manual rotating disk 11 can drive the orientation transmission mechanism and rotates.
At azimuth axis 2 an orientation harmonic wave speed reducing machine 12 is set.
Can stop decelerating effect to 3 rotations of orientation stepping motor, protect the safety of neat machine and surrounding enviroment.
Compared with prior art, a kind of integral type portable satellite communications of the present invention station, its beneficial effect is: volume is little, and is in light weight, transport easy to carry, the transmission accuracy height, it is faster to use speed, it is rapider to adjust angle.
Claims (5)
1. integral type portable satellite communications station is characterized in that: comprise the orientation transmission mechanism, pitching transmission mechanism and antenna, pitching transmission mechanism are connected transmission mechanism top, orientation; Described orientation transmission mechanism comprises base (1), azimuth axis (2), orientation stepping motor (3) and azimuth rotating platform (4), be provided with azimuth axis (2) at the vertical direction perpendicular to base (1), orientation stepping motor (3) and azimuth rotating platform (4) are successively set on the azimuth axis (2) from top to bottom; Described pitching transmission mechanism comprises pitching pedestal (5), pitching stepping motor (6), rotation axis (7) and antenna holder (8), pitching pedestal (5) latch is connected on the described azimuth rotating platform (4), described orientation stepping motor (3) is positioned at pitching pedestal (5), pitching stepping motor (6) is located on the pitching pedestal (5), is provided with rotation axis (7) in the horizontal direction of pitching stepping motor (6), is respectively equipped with antenna holder (8) at the two ends of rotation axis (7); Described antenna is positioned on the antenna holder (8).
2. a kind of integral type portable satellite communications according to claim 1 station is characterized in that: go up and the both sides that are positioned at pitching stepping motor (6) arrange a pitching harmonic wave speed reducing machine (9) respectively at rotation axis (7).
3. a kind of integral type portable satellite communications according to claim 2 station is characterized in that: a ring flange (10) that is used for fixed antenna frame (8) is set respectively in the outside of described pitching harmonic wave speed reducing machine (9).
4. a kind of integral type portable satellite communications according to claim 1 station is characterized in that: at azimuth axis (2) manual turntable (11) is set.
5. a kind of integral type portable satellite communications according to claim 1 station is characterized in that: at azimuth axis (2) an orientation harmonic wave speed reducing machine (12) is set.
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201310231131 CN103338067A (en) | 2013-06-13 | 2013-06-13 | Portable integrated satellite communication station |
| SG11201408729YA SG11201408729YA (en) | 2013-06-13 | 2014-06-12 | Integrated and detachable portable satellite communication stations |
| PCT/CN2014/079730 WO2014198224A1 (en) | 2013-06-13 | 2014-06-12 | Integrated and disassemblable portable satellite communication station |
| CN201410262098.8A CN104113369B (en) | 2013-06-13 | 2014-06-13 | Integral type and detachable portable satellite communications station |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201310231131 CN103338067A (en) | 2013-06-13 | 2013-06-13 | Portable integrated satellite communication station |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103338067A true CN103338067A (en) | 2013-10-02 |
Family
ID=49246176
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201310231131 Pending CN103338067A (en) | 2013-06-13 | 2013-06-13 | Portable integrated satellite communication station |
| CN201410262098.8A Active CN104113369B (en) | 2013-06-13 | 2014-06-13 | Integral type and detachable portable satellite communications station |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410262098.8A Active CN104113369B (en) | 2013-06-13 | 2014-06-13 | Integral type and detachable portable satellite communications station |
Country Status (1)
| Country | Link |
|---|---|
| CN (2) | CN103338067A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014198224A1 (en) * | 2013-06-13 | 2014-12-18 | 南京中网卫星通信股份有限公司 | Integrated and disassemblable portable satellite communication station |
| CN105305012A (en) * | 2015-12-02 | 2016-02-03 | 湖南创智数码科技股份有限公司 | Satellite portable station |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10965002B2 (en) * | 2016-06-21 | 2021-03-30 | Thrane & Thrane A/S | Antenna and a method of operating it |
| CN109149100B (en) * | 2018-08-24 | 2020-11-24 | 佛山市富乐喜电子信息技术有限公司 | Installation protection device for microstrip planar antenna sensor |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6925951B1 (en) * | 2004-02-09 | 2005-08-09 | Delong Mark | Boat docking rope cuffs |
| CN201033615Y (en) * | 2006-09-14 | 2008-03-12 | 天津富士达自行车有限公司 | Folding box for foldable bicycle |
| CN201130942Y (en) * | 2007-12-17 | 2008-10-08 | 熊猫电子集团有限公司 | Satellite communication apparatus with miniaturization structure |
| CN201259919Y (en) * | 2008-08-21 | 2009-06-17 | 上海杰盛无线通讯设备有限公司 | Portable satellite station antenna transmission construction |
| CN201391704Y (en) * | 2009-03-24 | 2010-01-27 | 上海瑞孚管路系统有限公司 | Quick pipeline connector |
| CN202159759U (en) * | 2011-02-25 | 2012-03-07 | 北京波尔通导科技有限公司 | Vehicle-mounted satellite communication antenna |
| CN102306873A (en) * | 2011-06-22 | 2012-01-04 | 南京中网卫星通信股份有限公司 | Full-automatic satellite antenna with easy-to-disassemble waveband feed source |
| CN102983902B (en) * | 2012-11-30 | 2015-03-25 | 陕西欧赛通信科技有限公司 | 1.2m feedback full-automatic portable emergency satellite communication antenna servo system |
| CN203340074U (en) * | 2013-06-13 | 2013-12-11 | 南京中网卫星通信股份有限公司 | Integrated portable satellite communication station |
| CN103474771B (en) * | 2013-09-26 | 2015-07-01 | 宁波迪泰电子科技有限公司 | Marine satellite antenna |
| CN103746186B (en) * | 2013-12-24 | 2016-02-24 | 山东英特力光通信开发有限公司 | A kind of Portable Ku-waveband marine satcom-on-the-move satellite communication antenna system |
-
2013
- 2013-06-13 CN CN 201310231131 patent/CN103338067A/en active Pending
-
2014
- 2014-06-13 CN CN201410262098.8A patent/CN104113369B/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014198224A1 (en) * | 2013-06-13 | 2014-12-18 | 南京中网卫星通信股份有限公司 | Integrated and disassemblable portable satellite communication station |
| CN105305012A (en) * | 2015-12-02 | 2016-02-03 | 湖南创智数码科技股份有限公司 | Satellite portable station |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104113369A (en) | 2014-10-22 |
| CN104113369B (en) | 2018-03-06 |
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20131002 |