CN109962328A - The wall mounting structure of SOTM satellite antenna - Google Patents
The wall mounting structure of SOTM satellite antenna Download PDFInfo
- Publication number
- CN109962328A CN109962328A CN201910237317.XA CN201910237317A CN109962328A CN 109962328 A CN109962328 A CN 109962328A CN 201910237317 A CN201910237317 A CN 201910237317A CN 109962328 A CN109962328 A CN 109962328A
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- synchronous pulley
- thin
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- wall
- bearing
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Classifications
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- 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
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
- H01Q1/282—Modifying the aerodynamic properties of the vehicle, e.g. projecting type aerials
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
- H01Q1/285—Aircraft wire antennas
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/32—Adaptation for use in or on road or rail vehicles
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/34—Adaptation for use in or on ships, submarines, buoys or torpedoes
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- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
The invention discloses a kind of wall mounting structures of SOTM satellite antenna, including the first mounting structure comprising thin-wall bearing one and synchronous pulley one, polarized disc are mounted on synchronous pulley one；Second mounting structure comprising thin-wall bearing two and synchronous pulley two, pitching disk are mounted on synchronous pulley two；Third mounting structure comprising thin-wall bearing three and synchronous pulley three, dumb card are mounted on synchronous pulley three；Synchronous pulley one is fixed on the inner ring of thin-wall bearing one, synchronous pulley two is fixed on the inner ring of thin-wall bearing two, synchronous pulley three is fixed on the inner ring of thin-wall bearing three；The outer ring of thin-wall bearing one, thin-wall bearing two and thin-wall bearing three is both secured to support ring seat.The overall profile height of the SOTM satellite antenna of wall mounting structure of the present invention installation can reduce to 10CM or so, compared to the prior art in one third, guarantee effective use space to greatest extent.
Description
Technical field
The present invention relates to SOTM satellite antenna technical fields, and in particular to a kind of wall-mounted peace of SOTM satellite antenna
Assembling structure
Background technique
SOTM satellite antenna communication system is a kind of Modern Satellite communication for capableing of uninterrupted real time communication during exercise
System.The antenna system can guarantee satellite in the various carrier moving process such as vehicle, steamer, aircraft always to satelloid
Communication is successive, to realize the transmittability of the business such as continual voice, data, image in movement.It is traditional it is dynamic in
Exceedingly high line, mostly parabola antenna and flat plate array antenna, technology maturation, performance are stablized.When the disadvantage is that volume is big, weight
Weight, drive mechanism are complicated, and especially profile is relatively high, and general height is all in 30CM or more, it is difficult to and carrier is conformal, causes windage
Bigger, energy consumption is high.
Summary of the invention
The technical problem to be solved in the present invention is to provide a kind of wall mounting structure of SOTM satellite antenna, being based on should
The SOTM satellite antenna overall profile height of wall mounting structure installation can reduce to one third in the prior art,
Guarantee effective use space to greatest extent；Meanwhile based on the SOTM satellite antenna after wall mounting structure installation
Windage can be effectively reduced, energy consumption is saved, greatly the high problem of alleviation fever, energy consumption；Simple with structure, small in size,
It is light-weight, easily conformal, be easy to the characteristics of hidden, easy to install, high reliablity.
In order to solve the above-mentioned technical problems, the present invention provides a kind of wall mounting structure of SOTM satellite antenna,
The SOTM satellite antenna has polarized disc, pitching disk and the dumb card successively installed along axial direction, the in-wall mounting knot
Structure includes,
First mounting structure comprising thin-wall bearing one and synchronous pulley one, the polarized disc are mounted on synchronous pulley one
On, the synchronous pulley one is rotated by synchronous belt one and power source；
Second mounting structure comprising thin-wall bearing two and synchronous pulley two, the pitching disk are mounted on synchronous pulley two
On, the synchronous pulley two is rotated by synchronous belt two and power source；
And third mounting structure comprising thin-wall bearing three and synchronous pulley three, the dumb card are mounted on synchronous belt
On wheel three, the synchronous pulley three is rotated by synchronous belt three and power source；
The synchronous pulley one is fixed on the inner ring of thin-wall bearing one, the synchronous pulley two is fixed on thin-wall bearing two
Inner ring, the synchronous pulley three are fixed on the inner ring of thin-wall bearing three；The thin-wall bearing one, thin-wall bearing two and thin-wall bearing
Three outer ring is both secured to support ring seat；
Or the synchronous pulley one is fixed on the outer ring of thin-wall bearing one, the synchronous pulley two is fixed on thin-wall bearing
The outer ring of thin-wall bearing three is fixed in two outer ring, the synchronous pulley three；The thin-wall bearing one, thin-wall bearing two and thin-walled
The inner ring of bearing three is both secured to support ring seat.
It further comprise that synchronous pulley is abutted at the top of one inner ring of thin-wall bearing in a preferred embodiment of the present invention
One, its inner ring bottom abuts bearing pressure ring one, its outer ring top abuts bearing pressure ring two, its outer ring bottom abuts support ring seat；
The inner ring surface of the thin-wall bearing one abuts synchronous pulley one, its outer ring surface abuts support ring seat；The bearing pressure ring one and same
It is fixed to walk belt wheel one, the bearing pressure ring two and support ring seat are fixed.
It further comprise that synchronous pulley is abutted at the top of two inner ring of thin-wall bearing in a preferred embodiment of the present invention
Two, its inner ring bottom abuts bearing pressure ring three, its outer ring top abuts bearing pressure ring four, its outer ring bottom abuts support ring seat；
The inner ring surface of the thin-wall bearing two abuts synchronous pulley two, its outer ring surface abuts support ring seat；The bearing pressure ring three and same
It is fixed to walk belt wheel two, the bearing pressure ring four and support ring seat are fixed.
In a preferred embodiment of the present invention, further comprise abutted at the top of three inner ring of thin-wall bearing coupling ring, its
Inner ring bottom abuts synchronous pulley three, its outer ring top abuts support ring seat, its outer ring bottom abuts bearing pressure ring five；It is described thin
The inner ring surface of wall bearing three abuts the outer ring surface of coupling ring, its outer ring surface abuts support ring seat；The bearing pressure ring five and support
Ring seat is fixed, and the coupling ring is fixed with dumb card and synchronous pulley three respectively, and the dumb card passes through coupling ring and synchronous belt
Wheel three is fixed.
It further comprise that the synchronous pulley one has the first driving section and the first peace in a preferred embodiment of the present invention
Dress portion；Synchronous belt 1 is installed, the circumferential one week interference close-fitting of the polarized disc is fixed on the first mounting portion on first driving section
On；First mounting portion circumferentially fixed by fastener close-fitting by one week bottom and the top of bearing pressure ring one.
It further comprise that the synchronous pulley two has the second driving section and the second peace in a preferred embodiment of the present invention
Dress portion；Synchronous belt 2 is installed, the pitching disk ring was fixed on second by fastener close-fitting to one week on second driving section
On mounting portion；Second mounting portion circumferentially fixed by fastener close-fitting by one week bottom and the top of bearing pressure ring three.
It further comprise that there is the synchronous pulley three third driving section and third to pacify in a preferred embodiment of the present invention
Dress portion；Synchronous belt three is installed, the dumb card is circumferential to be fixed on connection by fastener close-fitting in one week on the third driving section
On ring, the coupling ring is circumferential to be fixed on third mounting portion for one week by fastener close-fitting.
It further comprise that five circumferential one week top of bearing pressure ring passes through fastening in a preferred embodiment of the present invention
Part close-fitting is fixed in support ring seat；The circumferential one week bottom of bearing pressure ring four is fixed on support ring seat by fastener close-fitting
On；The circumferential one week bottom of bearing pressure ring two is fixed in support ring seat by fastener close-fitting.
In a preferred embodiment of the present invention, further comprise the fastener be screw.
It further comprise the synchronous pulley one, synchronous pulley two, synchronous pulley three in a preferred embodiment of the present invention
Power source be servo motor.
Beneficial effects of the present invention:
The wall mounting structure of the application, is designed by wall mounted versions, the thin-walled of three disks of SOTM satellite antenna
Bearing be stably fixed to stand support ring seat on, three disks with respective thin-wall bearing inner ring or outer ring rotating, three
Dish structure is compact, and movement is mutually indepedent, ensure that effective use space to greatest extent, and being based on should wall mounting structure peace
The overall profile height of the SOTM satellite antenna of dress can reduce to 10CM or so, compared to the prior art in three/
One；Meanwhile the SOTM satellite antenna based on wall mounting structure installation can effectively reduce windage, save energy consumption,
The greatly high problem of alleviation fever, energy consumption；It is simple with structure, small in size, light-weight, easily it is conformal, be easy to hidden, Yi An
The characteristics of dress, high reliablity.
Detailed description of the invention
Fig. 1 is the perspective view at the first visual angle of wall mounting structure in the preferred embodiment of the present invention；
Fig. 2 is the perspective view at the second visual angle of wall mounting structure in the preferred embodiment of the present invention
Fig. 3 is perspective view of the wall mounting structure shown in Fig. 2 after the section view of the direction A-A；
Fig. 4 is the enlarged diagram of part B in Fig. 3；
Fig. 5 is Fig. 4 structural schematic diagram unlabeled.
Figure label explanation: 1- polarized disc, 3- pitching disk, 5- dumb card；
21- thin-wall bearing one, 22- synchronous pulley one, 23- synchronous belt one, 24- bearing pressure ring one, 25- bearing pressure ring two,
The first driving section 26-, the first mounting portion of 27-；
41- thin-wall bearing two, 42- synchronous pulley two, 43- synchronous belt two, 44- bearing pressure ring three, 45- bearing pressure ring four,
The second driving section 46-, the second mounting portion of 47-；
61- thin-wall bearing three, 62- synchronous pulley three, 63- synchronous belt three, 64- bearing pressure ring five, 65- support ring seat, 66-
Coupling ring, 67- third driving section, 68- third mounting portion.
Specific embodiment
The present invention will be further explained below with reference to the attached drawings and specific examples, so that those skilled in the art can be with
It more fully understands the present invention and can be practiced, but illustrated embodiment is not as a limitation of the invention.
Embodiment one
The present invention discloses a kind of wall mounting structure of SOTM satellite antenna, and above-mentioned SOTM satellite antenna has axis
Polarized disc 1, pitching disk 3 and the dumb card 5 successively installed upwards, herein, the disk of 5 three of polarized disc 1, pitching disk 3 and dumb card
The heart is located on same axis.Above-mentioned SOTM satellite antenna passes through the polarized disc 1, pitching disk 3 and orientation of optimizing structure design
Disk 5 is coaxial, installs, and successively installation along the vertical direction, during actual use, the wave beam of azimuth plane is realized in the rotation of dumb card 5
Scanning, the rotation of pitching disk 3 are realized that the beam scanning of polarizing angle is realized in the beam scanning in pitching face, the rotation of polarized disc 1, with this, are led to
It crosses three disks of control respectively independently to rotate, can be realized antenna always to satelloid.It is wall-mounted in the present embodiment technical solution
Mounting structure is used for in-wall mounting polarized disc 1, pitching disk 3 and dumb card 5, and three disks turn with the inner ring of respective thin-wall bearing
Dynamic, the outer ring of the thin-wall bearing of three disks is stably fixed in the support ring seat stood, and three disks are mutually independent to each other
Movement ensure that effective use space to greatest extent, the overall profile of SOTM satellite antenna can greatly be reduced with this
Highly.
Shown in referring to Fig.1~5, above-mentioned wall mounting structure includes the first mounting structure for being successively layered setting, second
Mounting structure, third mounting structure and support ring seat 65:
First mounting structure includes thin-wall bearing 1 and synchronous pulley 1, and above-mentioned polarized disc 1 is mounted on synchronous pulley
On one 22, above-mentioned synchronous pulley 1 is rotated by synchronous belt 1 and servo motor.
Second mounting structure includes thin-wall bearing 2 41 and synchronous pulley 2 42, and above-mentioned pitching disk 3 is mounted on synchronous pulley
On 2 42, above-mentioned synchronous pulley 2 42 is rotated by synchronous belt 2 43 and servo motor.
Third mounting structure includes thin-wall bearing 3 61 and synchronous pulley 3 62, and above-mentioned dumb card 5 is mounted on synchronous pulley
On 3 62, above-mentioned synchronous pulley 3 62 is rotated by synchronous belt 3 63 and servo motor.
Above-mentioned synchronous pulley 1 is fixed on the inner ring of thin-wall bearing 1, above-mentioned synchronous pulley 2 42 is fixed on thin wall shaft
Hold 2 41 inner ring, above-mentioned synchronous pulley 3 62 is fixed on the inner ring of thin-wall bearing 3 61；Above-mentioned thin-wall bearing 1, thin wall shaft
Hold 2 41 and thin-wall bearing 3 61 outer ring be both secured to support ring seat 65.
Its specific structure is as follows:
One, thin-wall bearing 1
Synchronous pulley 1 is abutted shown in referring to Fig.1~5, at the top of above-mentioned one 21 inner ring of thin-wall bearing, its inner ring bottom is supported
Bearing pressure ring 2 25 is abutted at the top of spindle bearing ring 1, its outer ring, its outer ring bottom abuts support ring seat 65；Above-mentioned thin wall shaft
The inner ring surface for holding 1 abuts synchronous pulley 1, its outer ring surface abuts support ring seat 65；Above-mentioned bearing pressure ring 1 with it is synchronous
Belt wheel 1 is fixed, and above-mentioned bearing pressure ring 2 25 and support ring seat 65 are fixed.Further, above-mentioned synchronous pulley 1 has the
One driving section 26 and the first mounting portion 27；Synchronous belt 1 is installed, above-mentioned polarized disc 1 is one week circumferential on above-mentioned first driving section 26
Interference close-fitting is fixed on the first mounting portion 27；Above-mentioned first mounting portion 27 circumferentially one week bottom and bearing pressure ring 1
Top is fixed by fastener close-fitting.
Two, thin-wall bearing 2 41
Synchronous pulley 2 42 is abutted shown in referring to Fig.1~5, at the top of above-mentioned 2 41 inner ring of thin-wall bearing, its inner ring bottom is supported
Bearing pressure ring 4 45 is abutted at the top of spindle bearing ring 3 44, its outer ring, its outer ring bottom abuts support ring seat 65；Above-mentioned thin wall shaft
The inner ring surface for holding 2 41 abuts synchronous pulley 2 42, its outer ring surface abuts support ring seat 65；Above-mentioned bearing pressure ring 3 44 with it is synchronous
Belt wheel 2 42 is fixed, and above-mentioned bearing pressure ring 4 45 and support ring seat 65 are fixed.Further, above-mentioned synchronous pulley 2 42 has the
Two driving sections 46 and the second mounting portion 47；Synchronous belt 2 43 is installed, above-mentioned pitching disk 3 is one week circumferential on above-mentioned second driving section 46
It is fixed on the second mounting portion 47 by fastener close-fitting；Above-mentioned second mounting portion 47 circumferentially one week bottom and bearing pressure ring
3 44 top is fixed by fastener close-fitting.
Three, thin-wall bearing 3 61
Coupling ring 66 is abutted shown in referring to Fig.1~5, at the top of above-mentioned 3 61 inner ring of thin-wall bearing, its inner ring bottom abuts together
Walk belt wheel 3 62, its outer ring top abuts support ring seat 65, its outer ring bottom abuts bearing pressure ring 5 64；Above-mentioned thin-wall bearing three
61 inner ring surface abuts the outer ring surface of coupling ring 66, its outer ring surface abuts support ring seat 65；Above-mentioned bearing pressure ring 5 64 and support
Ring seat 65 is fixed, and above-mentioned coupling ring 66 is fixed with dumb card 5 and synchronous pulley 3 62 respectively, and above-mentioned dumb card 5 passes through coupling ring
66 is fixed with synchronous pulley 3 62.Further, above-mentioned synchronous pulley 3 62 has third driving section 67 and third mounting portion 68；
Synchronous belt 3 63 is installed, above-mentioned dumb card 5 is circumferential to be fixed on connection by fastener close-fitting in one week on above-mentioned third driving section 67
On ring 66, above-mentioned coupling ring 66 is circumferential to be fixed on third mounting portion 68 for one week by fastener close-fitting.Above-mentioned bearing pressure ring five
64 one week top of circumferential direction are fixed in support ring seat 65 by fastener close-fitting；The circumferential one week bottom of bearing pressure ring 4 45 is logical
Fastener close-fitting is crossed to be fixed in support ring seat 65；The circumferential one week bottom of bearing pressure ring 2 25 is fixed on by fastener close-fitting
It supports in ring seat 65.
More than, in the present embodiment technical solution, all close-fittings are fixed it is preferable to use screw, and fixation is stablized, energy
Enough match the high-speed rotation of each disk of satellite antenna.
More than, entire mounting structure is axially upper successively fixed, radially limits each other, installs the three of SOTM satellite antenna
A disk (polarized disc, pitching disk and dumb card) dismounts very convenient, quick afterwards, while can greatly reduce communication in moving satellite day
The overall profile height of line guarantees effective use space to greatest extent.Whole profile is high after SOTM satellite antenna installation
Degree can accomplish 10CM or so, be equivalent to the one third of the prior art, realize the ultra-low profile design of SOTM satellite antenna, tool
Have structure it is simple, it is small in size, light-weight, easily conformal, be easy to the characteristics of hidden, easy to install, high reliablity,
SOTM satellite antenna based on wall mounting structure installation can effectively reduce windage, save energy consumption,
The greatly high problem of alleviation fever, energy consumption.
Embodiment two
Above-mentioned wall mounting structure includes the first mounting structure, the second mounting structure, the third peace for being successively layered setting
Assembling structure and support ring seat 65:
First mounting structure includes thin-wall bearing 1 and synchronous pulley 1, and above-mentioned polarized disc 1 is mounted on synchronous pulley
On one 22, above-mentioned synchronous pulley 1 is rotated by synchronous belt 1 and servo motor.
Second mounting structure includes thin-wall bearing 2 41 and synchronous pulley 2 42, and above-mentioned pitching disk 3 is mounted on synchronous pulley
On 2 42, above-mentioned synchronous pulley 2 42 is rotated by synchronous belt 2 43 and servo motor.
Third mounting structure includes thin-wall bearing 3 61 and synchronous pulley 3 62, and above-mentioned dumb card 5 is mounted on synchronous pulley
On 3 62, above-mentioned synchronous pulley 3 62 is rotated by synchronous belt 3 63 and servo motor.
Above-mentioned synchronous pulley 1 is fixed on the outer ring of thin-wall bearing 1, above-mentioned synchronous pulley 2 42 is fixed on thin wall shaft
Hold 2 41 outer ring, above-mentioned synchronous pulley 3 62 is fixed on the outer ring of thin-wall bearing 3 61；The thin-wall bearing 1, thin wall shaft
Hold 2 41 and thin-wall bearing 3 61 inner ring be both secured to support ring seat 65.
The difference between this embodiment and the first embodiment lies in: three synchronous pulleys are different with the support fixation position of ring seat 65,
And the structure design of corresponding respectively different fixed positions.
More than, embodiment one is preferred embodiment of the present application, has the spy for being easier to dismounting compared to embodiment two
Point, the profile elevations h of SOTM satellite antenna are better than embodiment two.But in embodiment two after wall mounting structure installation
The profile elevations h of SOTM satellite antenna is designed still better than structure in the prior art.
In addition, the application wall mounting structure designs, the driven Design of synchronous pulley and synchronous belt cooperation is selected, compared to
The design of bevel gear cooperation spur gear in the prior art, structure is simpler, and occupied space is few, is conducive to reduce overall profile height
While have the characteristics that high transmission accuracy
Embodiment described above is only to absolutely prove preferred embodiment that is of the invention and being lifted, protection model of the invention
It encloses without being limited thereto.Those skilled in the art's made equivalent substitute or transformation on the basis of the present invention, in the present invention
Protection scope within.Protection scope of the present invention is subject to claims.
Claims (10)
1. a kind of wall mounting structure of SOTM satellite antenna, the SOTM satellite antenna has successively to be installed along axial direction
Polarized disc, pitching disk and dumb card, it is characterised in that: the wall mounting structure includes,
First mounting structure comprising thin-wall bearing one and synchronous pulley one, the polarized disc are mounted on synchronous pulley one, institute
State being rotated by synchronous belt one and power source of synchronous pulley one；
Second mounting structure comprising thin-wall bearing two and synchronous pulley two, the pitching disk are mounted on synchronous pulley two, institute
State being rotated by synchronous belt two and power source of synchronous pulley two；
And third mounting structure comprising thin-wall bearing three and synchronous pulley three, the dumb card are mounted on synchronous pulley three
On, the synchronous pulley three is rotated by synchronous belt three and power source；
The synchronous pulley one is fixed on the inner ring of thin-wall bearing one, the synchronous pulley two is fixed on the interior of thin-wall bearing two
Circle, the synchronous pulley three are fixed on the inner ring of thin-wall bearing three；The thin-wall bearing one, thin-wall bearing two and thin-wall bearing three
Outer ring be both secured to support ring seat；
Or the synchronous pulley one is fixed on the outer ring of thin-wall bearing one, the synchronous pulley two is fixed on thin-wall bearing two
The outer ring of thin-wall bearing three is fixed in outer ring, the synchronous pulley three；The thin-wall bearing one, thin-wall bearing two and thin-wall bearing
Three inner ring is both secured to support ring seat.
2. the wall mounting structure of SOTM satellite antenna as described in claim 1, it is characterised in that: the thin-wall bearing
Synchronous pulley one is abutted at the top of one inner ring, its inner ring bottom abuts bearing pressure ring one, bearing pressure ring two is abutted at the top of its outer ring, it
Outer ring bottom abuts support ring seat；The inner ring surface of the thin-wall bearing one abuts synchronous pulley one, its outer ring surface abuts support ring
Seat；The bearing pressure ring one and synchronous pulley one are fixed, and the bearing pressure ring two and support ring seat are fixed.
3. the wall mounting structure of SOTM satellite antenna as described in claim 1, it is characterised in that: the thin-wall bearing
Synchronous pulley two is abutted at the top of two inner rings, its inner ring bottom abuts bearing pressure ring three, bearing pressure ring four is abutted at the top of its outer ring, it
Outer ring bottom abuts support ring seat；The inner ring surface of the thin-wall bearing two abuts synchronous pulley two, its outer ring surface abuts support ring
Seat；The bearing pressure ring three and synchronous pulley two are fixed, and the bearing pressure ring four and support ring seat are fixed.
4. the wall mounting structure of SOTM satellite antenna as described in claim 1, it is characterised in that: the thin-wall bearing
Coupling ring is abutted at the top of three inner rings, its inner ring bottom abuts synchronous pulley three, support ring seat, its outer ring bottom are abutted at the top of its outer ring
Portion abuts bearing pressure ring five；The inner ring surface of the thin-wall bearing three abuts the outer ring surface of coupling ring, its outer ring surface abuts support ring
Seat；The bearing pressure ring five and support ring seat are fixed, and the coupling ring is fixed with dumb card and synchronous pulley three respectively, the side
Position disk is fixed by coupling ring and synchronous pulley three.
5. the wall mounting structure of SOTM satellite antenna as claimed in claim 2, it is characterised in that: the synchronous pulley
One has the first driving section and the first mounting portion；Synchronous belt 1 is installed, the polarized disc is one week circumferential on first driving section
Interference close-fitting is fixed on the first mounting portion；Circumferentially one week bottom and the top of bearing pressure ring one are logical for first mounting portion
Fastener close-fitting is crossed to fix.
6. the wall mounting structure of SOTM satellite antenna as claimed in claim 3, it is characterised in that: the synchronous pulley
Two have the second driving section and the second mounting portion；Synchronous belt two, the pitching disk ring Xiang Yizhou are installed on second driving section
It is fixed on the second mounting portion by fastener close-fitting；Second mounting portion circumferentially one week bottom and bearing pressure ring three
Top is fixed by fastener close-fitting.
7. the wall mounting structure of SOTM satellite antenna as claimed in claim 4, it is characterised in that: the synchronous pulley
Three have third driving section and third mounting portion；Synchronous belt three is installed, the dumb card is one week circumferential on the third driving section
It is fixed on coupling ring by fastener close-fitting, the coupling ring is circumferential to be fixed on third mounting portion by fastener close-fitting in one week
On.
8. the wall mounting structure of SOTM satellite antenna as claimed in claim 4, it is characterised in that: the bearing pressure ring
Five one week top of circumferential direction are fixed in support ring seat by fastener close-fitting；The circumferential one week bottom of bearing pressure ring four passes through tight
Firmware close-fitting is fixed in support ring seat；The circumferential one week bottom of bearing pressure ring two is fixed on support ring seat by fastener close-fitting
On.
9. such as the wall mounting structure of the described in any item SOTM satellite antennas of claim 5~8, it is characterised in that: institute
Stating fastener is screw.
10. the wall mounting structure of SOTM satellite antenna as described in claim 1, it is characterised in that: the synchronous belt
Take turns one, synchronous pulley two, the power source of synchronous pulley three is servo motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910237317.XA CN109962328A (en) | 2019-03-27 | 2019-03-27 | The wall mounting structure of SOTM satellite antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910237317.XA CN109962328A (en) | 2019-03-27 | 2019-03-27 | The wall mounting structure of SOTM satellite antenna |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109962328A true CN109962328A (en) | 2019-07-02 |
Family
ID=67024988
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910237317.XA Withdrawn CN109962328A (en) | 2019-03-27 | 2019-03-27 | The wall mounting structure of SOTM satellite antenna |
Country Status (1)
| Country | Link |
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| CN (1) | CN109962328A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111129694A (en) * | 2019-12-06 | 2020-05-08 | 宁波大学 | Assembly structure of VICTS phased array panel array antenna |
| CN111129693A (en) * | 2019-12-06 | 2020-05-08 | 宁波大学 | Assembly structure for VICTS phased array panel array antenna |
-
2019
- 2019-03-27 CN CN201910237317.XA patent/CN109962328A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111129694A (en) * | 2019-12-06 | 2020-05-08 | 宁波大学 | Assembly structure of VICTS phased array panel array antenna |
| CN111129693A (en) * | 2019-12-06 | 2020-05-08 | 宁波大学 | Assembly structure for VICTS phased array panel array antenna |
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Application publication date: 20190702 |
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| WW01 | Invention patent application withdrawn after publication |