CN109149050A - A kind of satellite antenna joint structure - Google Patents
A kind of satellite antenna joint structure Download PDFInfo
- Publication number
- CN109149050A CN109149050A CN201810862862.3A CN201810862862A CN109149050A CN 109149050 A CN109149050 A CN 109149050A CN 201810862862 A CN201810862862 A CN 201810862862A CN 109149050 A CN109149050 A CN 109149050A
- Authority
- CN
- China
- Prior art keywords
- antenna
- fixedly connected
- fixed
- satellite
- joint structure
- 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.)
- Granted
Links
- 230000000694 effects Effects 0.000 claims abstract description 9
- 238000007789 sealing Methods 0.000 claims abstract description 7
- 239000000956 alloy Substances 0.000 claims description 10
- 229910045601 alloy Inorganic materials 0.000 claims description 10
- 230000008602 contraction Effects 0.000 claims description 8
- 230000001681 protective effect Effects 0.000 claims description 7
- 235000005121 Sorbus torminalis Nutrition 0.000 claims description 5
- 244000152100 Sorbus torminalis Species 0.000 claims description 5
- 238000009434 installation Methods 0.000 abstract description 4
- 238000000034 method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 230000003321 amplification Effects 0.000 description 1
- 230000006399 behavior Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000003199 nucleic acid amplification method Methods 0.000 description 1
- 230000005236 sound signal Effects 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/50—Structural association of antennas with earthing switches, lead-in devices or lightning protectors
Landscapes
- Details Of Aerials (AREA)
Abstract
The invention discloses a kind of satellite antenna joint structures, including antenna, one end of the antenna surface is arranged with fixed pushing cylinder, the side of the fixed pushing cylinder and be located at antenna surface be fixedly connected with seal closure cylinder, one end of the antenna and be located at seal closure cylinder internal activity be connected with antenna fixed block, the antenna fixed block is fixedly connected with take-up reel far from the side of seal closure cylinder, link block is fixedly connected on the right side of the antenna fixed block, the surface of link block and be located at antenna fixed block on the right side of be fixedly connected with sealing rubber ring, antenna connection head is fixedly connected on the right side of link block, the present invention relates to satellite antenna technical fields.The satellite antenna joint structure realizes detachably using function, keeps satellite antenna connector more convenient to use, satellite can be disassembled and be transported, it is efficient and convenient when installation, fixed pushing cylinder is pushed can lock forward, so that device is fixed up.
Description
Technical field
The present invention relates to satellite antenna technical field, specially a kind of satellite antenna joint structure.
Background technique
Satellite antenna is exactly the cauldron often said, is a metal paraboloid, is responsible for for satellite-signal being reflected into positioned at focus
In the feed and tuner at place.The effect of satellite antenna is to collect the small-signal transmitted by satellite, and be eliminated as much as noise.
Most of antennas are usually parabolic, there are also multifocal antenna are composed of spherical surface and paraboloid.Satellite letter
Number by focusing on its focal point after the reflection of parabola antenna, satellite television receiving system is by parabola antenna, feedback
Source, tuner, satellite receiver composition complete set Satellite Receiving Station.Parabola antenna, parabola antenna are starry sky
The reflection of satellite-signal energy is converged to a focus.Feed, feed are focal point one poly- satellites of setting in parabola antenna
The loudspeaker of signal, referred to as feed mean the source of energy feeding, it is desirable that all collect the energy for converging to focus.Before
Feedback formula satellite earth antenna substantially uses large angle Behaviors of Corrugated Feeds.Tuner.Tuner be the satellite-signal of sending feed into
Row frequency reducing and signal amplification then pass to satellite receiver.The lower the noise degree of tuner the better.Satellite receiver, satellite
Receiver is that the satellite-signal for carrying out tuner conveying demodulates, and demodulates satellite television picture signal and audio signal.
What existing satellite antenna connector used is mostly integrated connector, inconvenient when installing and using, and is needed
The one transport of antenna and satellite, although some satellite antenna connectors can be dismantled, structure is not perfect, and installation is inconvenient,
It is unfavorable for worker's maintenance, reduces work task efficiency.
Summary of the invention
In view of the deficiencies of the prior art, the present invention provides a kind of satellite antenna joint structure, prior art peace is solved
It is inconvenient when dress uses, it needs the one of antenna and satellite to transport, and installation is inconvenient, is unfavorable for worker's maintenance, reduces
The problem of worker working efficiency.
In order to achieve the above object, the present invention is achieved by the following technical programs: a kind of satellite antenna joint structure, packet
Include antenna, one end of the antenna surface is arranged with fixed pushing cylinder, the side of the fixed pushing cylinder and surface for being located at antenna is solid
Surely it is connected with seal closure cylinder, one end of the antenna and internal activity for being located at seal closure cylinder is connected with antenna fixed block is described
Antenna fixed block is fixedly connected with take-up reel, the company of being fixedly connected on the right side of the antenna fixed block far from the side of seal closure cylinder
It connects block, the surface of the link block and is located on the right side of antenna fixed block and is fixedly connected with sealing rubber ring, the link block
Right side is fixedly connected with antenna connection head, and the inside on the right side of the antenna connection head offers antenna fixation hole, and the antenna is solid
The internal activity for determining hole is connected with signal transmssion line, and the signal transmssion line is fixedly connected far from one end of antenna connection head surface
There is insulating protective sleeve.
Preferably, the left end of the insulating protective sleeve and be located at signal transmssion line surface be fixedly connected with retainer plate, institute
It states the left side of retainer plate and is opened up positioned at the surface of signal transmssion line fluted.
Preferably, the surface of the retainer plate is fixedly connected with alloy antifriction circle, the left side and position of the alloy antifriction circle
Flexible ring is fixedly connected in the outer surface of retainer plate.
Preferably, flexible contraction fixed ring is fixedly connected on the left of the flexible ring, the flexible contraction fixed ring is closed
The outer surface of Jin Naimoquan and flexible ring offers L-type fixed chute.
Preferably, the flexible inner surface for shrinking fixed ring is fixedly connected with rubber washer.
Preferably, the outer surface of the antenna connection head right end and separate wire antenna fixation hole is fixedly connected with anti-slop serrations
Head, the inner surface of the fixed pushing cylinder are fixedly connected with push strut, and the outer surface of the fixed pushing cylinder offers anti-skid chequer.
Beneficial effect
The present invention provides a kind of satellite antenna joint structures.Have it is following the utility model has the advantages that
(1), the satellite antenna joint structure passes through the side in fixed pushing cylinder and is fixedly connected with sealing positioned at the surface of antenna
Cover cylinder, one end of antenna and the internal activity for being located at seal closure cylinder are connected with antenna fixed block, and antenna fixed block is far from seal closure
The side of cylinder is fixedly connected with take-up reel, is fixedly connected with link block on the right side of antenna fixed block, the surface of link block and is located at
It is fixedly connected with sealing rubber ring on the right side of antenna fixed block, antenna connection head is fixedly connected on the right side of link block, is realized
Function is detachably used, keeps satellite antenna connector more convenient to use, satellite can be disassembled and be transported, is installed
When it is efficient and convenient, fixed pushing cylinder is pushed can lock forward, so that device is fixed up.
(2), the satellite antenna joint structure, it is soft by being fixedly connected with flexible contraction fixed ring on the left of flexible ring
Property shrink fixed ring, the outer surface of alloy antifriction circle and flexible ring offers L-type fixed chute, flexibility shrinks the interior of fixed ring
Surface is fixedly connected with rubber washer antenna connection head right end and the outer surface far from line fixation hole is fixedly connected with anti-skidding plush copper,
The inner surface of fixed pushing cylinder is fixedly connected with push strut, and the outer surface of fixed pushing cylinder offers anti-skid chequer, by pushing fixation to push away
Cylinder makes push strut that flexibility is shunk fixed ring and compresses, fix flexible shrink so that push strut moves in L-type fixed chute
Rubber washer is crimped on anti-slop serrations head by ring, so that antenna terminal is fastenedly connected.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is the structural schematic diagram of the present invention fixed pushing cylinder and antenna fixed block；
Fig. 3 is the structural schematic diagram of the fixed pushing cylinder outer surface of the present invention；
Fig. 4 is the partial enlarged view in Fig. 2 of the present invention at A.
In figure: the fixed pushing cylinder of 1- antenna, 2-, 3- seal closure cylinder, 4- antenna fixed block, 5- take-up reel, 6- link block, 7- are close
Seal rubber ring, 8- antenna connection head, 9- antenna fixation hole, 10- signal transmssion line, 11- insulating protective sleeve, 12- retainer plate, 13-
Groove, 14- alloy antifriction circle, 15- flexible ring, 16- flexibility shrink fixed ring, 17-L type fixed chute, 18- rubber washer, 19-
Anti-slop serrations head, 20- push strut, 21- anti-skid chequer.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Fig. 1-4 is please referred to, the present invention provides a kind of technical solution: a kind of satellite antenna joint structure, including antenna 1, day
The one end on 1 surface of line is arranged with fixed pushing cylinder 2, fixes the side of pushing cylinder 2 and is fixedly connected with seal closure positioned at the surface of antenna 1
Cylinder 3, one end of antenna 1 and the internal activity for being located at seal closure cylinder 3 are connected with antenna fixed block 4, and antenna fixed block 4 is far from sealing
The side of cover cylinder 3 is fixedly connected with take-up reel 5, and the right side of antenna fixed block 4 is fixedly connected with link block 6, the surface of link block 6
And the right side for being located at antenna fixed block 4 is fixedly connected with sealing rubber ring 7, the right side of link block 6 is fixedly connected with antenna connection
First 8, the inside on 8 right side of antenna connection head offers antenna fixation hole 9, and the internal activity of antenna fixation hole 9 is connected with signal biography
Defeated line 10, signal transmssion line 10 are fixedly connected with insulating protective sleeve 11 far from the one end on 8 surface of antenna connection head, realize removable
It unloads using function, keeps 1 connector of satellite antenna more convenient to use, satellite can be disassembled and be transported, when installation
It is efficient and convenient, fixed pushing cylinder 2 is pushed can lock forward, so that device is fixed up, the left end of insulating protective sleeve 11
And the surface for being located at signal transmssion line 10 is fixedly connected with retainer plate 12, the left side of retainer plate 12 and is located at signal transmssion line 10
Surface opens up fluted 13, and the surface of retainer plate 12 is fixedly connected with alloy antifriction circle 14, the left side and position of alloy antifriction circle 14
It is fixedly connected with flexible ring 15 in the outer surface of retainer plate 12, the left side of flexible ring 15 is fixedly connected with flexible contraction fixed ring
16, the outer surface that flexibility shrinks fixed ring 16, alloy antifriction circle 14 and flexible ring 15 offers L-type fixed chute 17, flexible
The inner surface for shrinking fixed ring 16 is fixedly connected with rubber washer 18,8 right end of antenna connection head and far from wire antenna fixation hole 9
Outer surface is fixedly connected with anti-slop serrations head 19, and the inner surface of fixed pushing cylinder 2 is fixedly connected with push strut 20, fixes the outer of pushing cylinder 2
Surface offers anti-skid chequer 21, by pushing fixed pushing cylinder 2 to make to push so that push strut 20 moves in L-type fixed chute 17
Flexibility is shunk fixed ring 16 and compressed by bar 20, is crimped onto flexible fixed ring 16 of shrinking on anti-slop serrations head rubber washer 18, makes
1 joint of antenna is obtained to be fastenedly connected.
In use, signal transmssion line 10 is first inserted into the inside of antenna fixation hole 9, so that 8 outer surface of antenna connection head
Anti-slop serrations head 19 is placed into the inside of rubber washer 18, then again pushes fixed pushing cylinder 2 to the left, makes fixed 2 inner surface of pushing cylinder
Push strut 20 is moved downward along L-type fixed chute, and then the fixed pushing cylinder 2 of turn makes push strut 20 be fixed to flexible shrink admittedly again
The surface of ring 16 is determined, so that squeezing for 20 pairs of flexible contraction fixed rings 16 of push strut, rubber washer 18 is expressed to anti-skidding
Antenna 1 can be fixed up by the surface of tooth head 19, when pushing fixed pushing cylinder 2, seal closure cylinder be made to be fastened to seal rubber
On circle 7, seal junction.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of satellite antenna joint structure, including antenna (1), it is characterised in that: the one end on antenna (1) surface is arranged with
Fixed pushing cylinder (2), the side of the fixed pushing cylinder (2) and the surface for being located at antenna (1) are fixedly connected with seal closure cylinder (3), institute
It states one end of antenna (1) and the internal activity positioned at seal closure cylinder (3) is connected with antenna fixed block (4), the antenna fixed block
(4) side far from seal closure cylinder (3) is fixedly connected with take-up reel (5), is fixedly connected on the right side of the antenna fixed block (4)
Link block (6), the surface of the link block (6) and be located at antenna fixed block (4) on the right side of be fixedly connected with sealing rubber ring
(7), it is fixedly connected with antenna connection head (8) on the right side of the link block (6), the inside on the right side of the antenna connection head (8) is opened
Equipped with antenna fixation hole (9), the internal activity of the antenna fixation hole (9) is connected with signal transmssion line (10), and the signal passes
Defeated line (10) is fixedly connected with insulating protective sleeve (11) far from the one end on antenna connection head (8) surface.
2. a kind of satellite antenna joint structure according to claim 1, it is characterised in that: the insulating protective sleeve (11)
The left end and surface for being located at signal transmssion line (10) is fixedly connected with retainer plate (12), the left side of the retainer plate (12) and is located at
The surface of signal transmssion line (10) opens up fluted (13).
3. a kind of satellite antenna joint structure according to claim 2, it is characterised in that: the surface of the retainer plate (12)
It is fixedly connected with alloy antifriction circle (14), the left side of the alloy antifriction circle (14) and the outer surface for being located at retainer plate (12) is fixed
It is connected with flexible ring (15).
4. a kind of satellite antenna joint structure according to claim 3, it is characterised in that: the left side of the flexible ring (15)
It is fixedly connected with flexible contraction fixed ring (16), flexible contraction fixed ring (16), alloy antifriction circle (14) and flexible ring
(15) outer surface offers L-type fixed chute (17).
5. a kind of satellite antenna joint structure according to claim 4, it is characterised in that: the flexible contraction fixed ring
(16) inner surface is fixedly connected with rubber washer (18).
6. a kind of satellite antenna joint structure according to claim 1, it is characterised in that: the antenna connection head (8) is right
The outer surface of end and separate wire antenna fixation hole (9) is fixedly connected with anti-slop serrations head (19), the inner surface of the fixed pushing cylinder (2)
It is fixedly connected with push strut (20), the outer surface of the fixed pushing cylinder (2) offers anti-skid chequer (21).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810862862.3A CN109149050B (en) | 2018-08-01 | 2018-08-01 | Satellite antenna joint structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810862862.3A CN109149050B (en) | 2018-08-01 | 2018-08-01 | Satellite antenna joint structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109149050A true CN109149050A (en) | 2019-01-04 |
| CN109149050B CN109149050B (en) | 2020-12-18 |
Family
ID=64798535
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810862862.3A Expired - Fee Related CN109149050B (en) | 2018-08-01 | 2018-08-01 | Satellite antenna joint structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109149050B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113131188A (en) * | 2021-04-20 | 2021-07-16 | 上海航天测控通信研究所 | Multi-star assembled antenna device |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110065317A1 (en) * | 2007-12-17 | 2011-03-17 | Ds Engineering, Llc | Compression type coaxial cable F-connectors with traveling seal and barbless post |
| CN202121053U (en) * | 2011-06-15 | 2012-01-18 | 胡宇栋 | Antenna waterproof joint |
| CN203103694U (en) * | 2012-12-26 | 2013-07-31 | 江苏明联电子科技有限公司 | Low-echo radiofrequency coaxial connector |
| CN103548206A (en) * | 2011-02-08 | 2014-01-29 | 百通公司 | Cable connectors with biasing elements |
| CN205004523U (en) * | 2015-09-14 | 2016-01-27 | 嘉兴星网通信技术有限公司 | Satellite antenna joint design |
| CN107002927A (en) * | 2014-11-20 | 2017-08-01 | 伊利诺斯工具制品有限公司 | Quick connector |
| CN107516791A (en) * | 2017-08-31 | 2017-12-26 | 南京康派电子有限公司 | A kind of joint connection of big-dipper satellite |
| CN207052854U (en) * | 2017-07-10 | 2018-02-27 | 天津华宁电子有限公司 | The coaxial quick connector of antenna |
| CN207149694U (en) * | 2017-08-11 | 2018-03-27 | 吴生展 | A kind of vehicle-mounted satellite antenna waterproof construction |
| CN207149788U (en) * | 2017-08-31 | 2018-03-27 | 南京康派电子有限公司 | A kind of joint connection of big-dipper satellite |
| CN207474654U (en) * | 2017-11-22 | 2018-06-08 | 广东通宇通讯股份有限公司 | A kind of antenna mounting device |
-
2018
- 2018-08-01 CN CN201810862862.3A patent/CN109149050B/en not_active Expired - Fee Related
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110065317A1 (en) * | 2007-12-17 | 2011-03-17 | Ds Engineering, Llc | Compression type coaxial cable F-connectors with traveling seal and barbless post |
| CN103548206A (en) * | 2011-02-08 | 2014-01-29 | 百通公司 | Cable connectors with biasing elements |
| CN202121053U (en) * | 2011-06-15 | 2012-01-18 | 胡宇栋 | Antenna waterproof joint |
| CN203103694U (en) * | 2012-12-26 | 2013-07-31 | 江苏明联电子科技有限公司 | Low-echo radiofrequency coaxial connector |
| CN107002927A (en) * | 2014-11-20 | 2017-08-01 | 伊利诺斯工具制品有限公司 | Quick connector |
| CN205004523U (en) * | 2015-09-14 | 2016-01-27 | 嘉兴星网通信技术有限公司 | Satellite antenna joint design |
| CN207052854U (en) * | 2017-07-10 | 2018-02-27 | 天津华宁电子有限公司 | The coaxial quick connector of antenna |
| CN207149694U (en) * | 2017-08-11 | 2018-03-27 | 吴生展 | A kind of vehicle-mounted satellite antenna waterproof construction |
| CN107516791A (en) * | 2017-08-31 | 2017-12-26 | 南京康派电子有限公司 | A kind of joint connection of big-dipper satellite |
| CN207149788U (en) * | 2017-08-31 | 2018-03-27 | 南京康派电子有限公司 | A kind of joint connection of big-dipper satellite |
| CN207474654U (en) * | 2017-11-22 | 2018-06-08 | 广东通宇通讯股份有限公司 | A kind of antenna mounting device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113131188A (en) * | 2021-04-20 | 2021-07-16 | 上海航天测控通信研究所 | Multi-star assembled antenna device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109149050B (en) | 2020-12-18 |
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