CN103296377B - A kind of satellite tv antenna support and its satellite television receiving system - Google Patents
A kind of satellite tv antenna support and its satellite television receiving system Download PDFInfo
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- CN103296377B CN103296377B CN201210050856.0A CN201210050856A CN103296377B CN 103296377 B CN103296377 B CN 103296377B CN 201210050856 A CN201210050856 A CN 201210050856A CN 103296377 B CN103296377 B CN 103296377B
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Abstract
The invention discloses a kind of satellite tv antenna support, the satellite tv antenna support includes the base of support satellite tv antenna, the pole of support feed and feed adjusting means.Satellite tv antenna support of the invention, the feed adjusting means with unique design, can adjust the angle of feed, be conducive to the flexible reception of satellite TV signal.In addition, present invention also offers a kind of satellite television receiving system with above-mentioned satellite tv antenna support.
Description
Technical field
The present invention relates to the communications field, connect more specifically to a kind of satellite tv antenna support and its satellite television
Receipts system.
Background technology
The satellite that traditional satellite television receiving system is made up of parabola antenna, feed, tuner, DVB
Grounded receiving station.Parabola antenna is responsible for reflexing to satellite-signal in the feed and tuner of focal point.Feed be
The loudspeaker for being used to collect satellite-signal that the focal point of parabola antenna is set, also known as corrugated horn.Its major function has
Two：One is to collect the electromagnetic wave signal that antenna is received, and is transformed into signal voltage, supply high frequency head.Two is to receiving
Electromagnetic wave carry out polarization conversion.Tuner LNB (also known as frequency demultiplier) is that the satellite-signal for sending feed carries out frequency reducing and letter
Number amplification then passes to DVB.Generally can be divided into C-band frequency LNB (3.7GHz-4.2GHz, 18-21V) and Ku ripples
Band frequency LNB (10.7GHz-12.75GHz, 12-14V).The workflow of LNB is exactly that satellite high-frequency signals first are amplified into number
100000 times recycle local oscillation circuit to change to intermediate frequency 950MHz-2050MHz high-frequency signals afterwards, are beneficial to coaxial cable
Transmission and the demodulation of DVB work.DVB is to be demodulated the satellite-signal that tuner conveying comes, and is solved
Recall satellite television image or data signal and audio signal.
When receiving satellite-signal, parallel electromagnetic wave is converged on feed after parabola antenna reflects.Generally, throw
The corresponding feed of object plane antenna is an electromagnetic horn.
Usual satellite tv antenna is supported on ground or the tip position of other buildings using satellite television support, to connect
Satellite TV signal is received, but in traditional satellite television receiving system, feed is fixedly connected with satellite television support,
Its position is fixed, it is impossible to adjust the angle of feed, and this is particularly disadvantageous in offset-fed satellite tv antenna.
The content of the invention
The technical problems to be solved by the invention are, for the drawbacks described above of existing satellite television receiving system, there is provided
A kind of adjustable satellite tv antenna support of feed location.
The technical solution adopted for the present invention to solve the technical problems is：A kind of satellite tv antenna support, the satellite
TV antenna support includes the pole of the base of support satellite tv antenna and support feed, and the satellite tv antenna support is also
Including the feed adjusting means for adjusting feed angle, the feed adjusting means includes the connecting plate of connection pole, is used for
First hold assembly and the second hold assembly of feed are clamped from opposite sides, the connecting plate has the installation portion of connection pole
And first arm and the second arm of installation portion both sides are formed in, first hold assembly includes what is be fixedly connected with feed
First clamping section and it is formed on the first clamping section side wall and the first rotating shaft above the first arm, the first rotating shaft
Top is covered with the first briquetting, and first briquetting is fixed on the first arm, and the top of first briquetting offers insertion
The first screwed hole, the lower ending opening of the first screwed hole is provided with the first rotary knob rod, institute just to first rotating shaft in the first screwed hole
Stating the second hold assembly includes the second clamping section for being fixedly connected with feed and is formed on the second clamping section side wall and positioned at the
The second rotating shaft above two arms, is covered with the second briquetting above second rotating shaft, second briquetting is fixed on second
On arm, the top of second briquetting offers the second screwed hole of insertion, and the lower ending opening of the second screwed hole is just to second
Rotating shaft, is provided with the second rotary knob rod in the second screwed hole.
Further, the first rotating shaft is coaxially disposed with the second rotating shaft.
Further, the installation portion of the connecting plate has the square box being set on pole, the square box and pole
It is bolted to connection.
Further, the first rotating shaft is stretched out one end of the first briquetting and is provided with knob.
Further, the base includes being supported on the carriage at satellite tv antenna back, the middle part of the carriage
Position is fixedly installed mounting seat, and one end of the pole is fixedly connected in mounting seat.
Further, the base includes the hinge that the hinged seat and hinged seat that are fixed in mounting seat are rotatably connected
Joint and the articulated joint connecting portion for connecting and the portions being connected with connecting portion.
Further, the articulated joint is placed in hinged seat, and the both sides of hinged seat are symmetrically arranged with the first sliding groove and
Two sliding grooves, articulated joint is realized rotatably being connected by through articulated joint with hinged seat with the first screw rod of hinged seat, and first
The two ends of screw rod are provided with two the first location nuts, also including the second screw rod through the first sliding groove and the second sliding groove,
The two ends of the first screw rod are provided with two the second location nuts.
Satellite tv antenna support of the invention, the feed adjusting means with unique design, can adjust feed
Angle, be conducive to the flexible reception of satellite TV signal.
In addition, present invention also offers a kind of satellite television receiving system, including satellite tv antenna, feed, connection feedback
The tuner and connection tuner DVB in source, the satellite television receiving system also include above-mentioned satellite tv antenna
Support.
Further, the feed is corrugated horn.
Further, the feed is integrally formed with tuner.
Brief description of the drawings
Fig. 1 is the structural representation of a form of satellite tv antenna of the invention；
Fig. 2 is the perspective diagram of the one of metamaterial unit of core layer of the invention；
Fig. 3 is the structural representation of core layer of the invention；
Fig. 4 is the structural representation of impedance matching layer lamella of the invention；
Fig. 5 is the schematic diagram of the metal micro structure of plane flakes of the invention；
Fig. 6 is a kind of derived structure of the metal micro structure of the plane flakes shown in Fig. 5；
Fig. 7 is a kind of distressed structure of the metal micro structure of the plane flakes shown in Fig. 5.
Fig. 8 is the first stage of the differentiation of the topology of the metal micro structure of plane flakes；
Fig. 9 is the second stage of the differentiation of the topology of the metal micro structure of plane flakes；
Figure 10 is the structural representation of the satellite tv antenna of another kind embodiment of the invention；
Figure 11 is the structural representation of the satellite television receiving system of an embodiment of the present invention；
Figure 12 is another visual angle figures of Figure 11；
Figure 13 is the structural representation of feed adjusting means of the invention；
Figure 14 is another visual angle figure of Figure 13.
Specific embodiment
As shown in Figure 1 to Figure 3, it is a form of satellite tv antenna of the invention, it is in tabular, the satellite television
Antenna includes being arranged on the metamaterial panel 100 at the rear of feed 1, and the feed 1 is arranged on the lower edge of metamaterial panel 100, institute
Stating metamaterial panel 100 includes core layer 10 and the reflecting plate 200 being arranged on the side surface of core layer one, and the core layer 10 is wrapped
Include that thickness is identical and index distribution identical multiple core layers 11, the core layer includes the first base material of sheet
13 and multiple first man-made microstructures 12 for being arranged in the first base material 13, feed central shaft Z1 and metamaterial panel 100
Axis Z2 has angle (Z3 is the parallel lines of Z1) feed 1 of the axis Z1 in certain angle theta, i.e. Fig. 1 and straight line Z3
Not on the axis Z2 of metamaterial panel 100, the offset-fed of antenna is realized.Other feed is traditional corrugated horn.Core
The vertical sectional shape of synusia layer can be with square, circular or ellipse according to different needs.In addition, in the present invention, reflecting plate is tool
There is the metallic reflection plate on smooth surface, for example, can be copper coin, aluminium sheet or iron plate of polishing etc., may also be PEC (preferable conductances
Body) reflecting surface.
In the present invention, the index distribution of the core layer meets equation below：
Vseg=s+ λ * NUMseg (2)；
Wherein, n (r) represents that radius is the refractive index value at r in core layer；
S is vertical ranges of the feed equivalent point X to metamaterial panel；The equivalent point X of feed is actually antenna herein
Feed point (point that electromagnetic wave is focused in feed)；The folder of the feed central shaft Z1 and axis Z2 of metamaterial panel 100
When angle θ changes, s can also occur slight change.
nmaxRepresent the maximum of the refractive index of core lamella；
nminRepresent the minimum value of the refractive index of core lamella；
λ represents the wavelength of the electromagnetic wave that frequency is center of antenna frequency；
Floor is represented and rounded downwards, for example, working as(r is in a certain number range) is less than 1 more than or equal to 0
When, NUMseg takes 0, whenWhen (r is in a certain number range) is less than 2 more than or equal to 1, NUMseg takes 1, according to this class
Push away.
The metamaterial panel determined by formula (1) to formula (4), enables to the electromagnetic wave that feed sends through Meta Materials
Being capable of the outgoing in the form of plane wave after panel.
In the present invention, as shown in figure 3, the first base material 13 includes first prebasal plate 131 and the first metacoxal plate of sheet
132, the multiple first man-made microstructure 12 is folded between the first prebasal plate 131 and the first metacoxal plate 132.Preferably, institute
The thickness of core layer is stated for 0.818mm, wherein, the thickness of the first prebasal plate and the first metacoxal plate is 0.4mm, Duo Ge
The thickness of one man-made microstructure is 0.018mm.
In the present invention, the metamaterial panel 100 also includes being arranged on the impedance matching layer of another side surface of core layer 10
20, the impedance matching layer 20 includes thickness identical multiple impedance matching layer lamella 21, and the impedance matching layer lamella 21 is wrapped
Multiple second man-made microstructures (not indicated in figure) for including the second base material 23 of sheet and being arranged on the second base material 23 are described
The index distribution of impedance matching layer lamella meets equation below：
λ=(nmax-nmin)*(d1+2*d2) (6)；
Wherein, i represents the numbering of impedance matching layer lamella, and the numbering near the impedance matching layer lamella of feed is m, by presenting
Source is sequentially reduced to core layer direction, numbering, and the numbering near the impedance matching layer lamella of core layer is 1；
Above-mentioned nmaxWith nminMaxima and minima with the refractive index of core layer is identical；
D1 is the product of the thickness of impedance matching layer, the i.e. thickness of impedance matching layer lamella and the number of plies.
D2 is the product of the thickness of core layer, the i.e. thickness of core layer and the number of plies.
In the present invention, second base material 23 includes second prebasal plate 231 and the second metacoxal plate 232 of sheet, described many
Individual second man-made microstructure is folded between the second prebasal plate 231 and the second metacoxal plate 232.Preferably, the impedance matching layer
The thickness of lamella is 0.818mm, wherein, the thickness of the second prebasal plate and the second metacoxal plate is 0.4mm, and multiple second is artificial micro-
The thickness of structure is 0.018mm.
Formula (6) for determining the thickness of core layer and matching layer, after the thickness of core layer determines, using formula (6)
The thickness of matching layer is can obtain, is the number of stories m for obtaining impedance matching layer divided by every layer of thickness with this thickness.
In the present invention, any longitudinal section of metamaterial panel is of similar shape and area, i.e., core layer with match
Layer is of similar shape longitudinal section with area, and longitudinal section herein refers to vertical with its axis in metamaterial panel cuing open
Face.The longitudinal section of the metamaterial panel is square, circular or ellipse, it is preferable that the vertical of the metamaterial flat lens cuts
Face is square, and the metamaterial panel for so obtaining is easily worked.Preferably, the longitudinal section of metamaterial panel of the invention is the length of side
It is the square of 400mm.
In one embodiment of the invention, the satellite tv antenna has following parameter：
The centre frequency of the satellite tv antenna is 12.5GHZ；Working frequency range is 12.25 to 12.75；
Feed equivalent point to metamaterial panel vertical range s be 0.203m；
Feed central shaft is 39 degree with angle theta formed by the plane where metamaterial panel；
The number of plies of core layer is 3 layers, and the thickness d 2 of core layer is 2.454mm；
The number of plies of impedance matching layer lamella is 4 layers, and the thickness d 1 of impedance matching layer is 3.272mm；
The maximum n of the refractive index of core lamellamaxIt is 5.35；
The minimum value n of the refractive index of core lamellaminIt is 1.91.
In another embodiment of the present invention, the satellite tv antenna has following parameter：
The centre frequency of the satellite tv antenna is 12.5GHZ, wherein：
Feed equivalent point X to the vertical range s of metamaterial panel is 0.218m；
Feed central shaft is 42 degree with angle theta formed by the plane where metamaterial panel；
The number of plies of core layer is 3 layers, and the thickness d 2 of core layer is 2.454mm；
The number of plies of impedance matching layer lamella is 4 layers, and the thickness d 1 of impedance matching layer is 3.272mm；
The maximum n of the refractive index of core lamellamaxIt is 5.12；
The minimum value n of the refractive index of core lamellaminIt is 1.91.
In above-mentioned two embodiment, parameter s is different from θ, other all sames.Because, when feed central shaft Z1 with it is super
When angle theta where material panel 100 changes, the position of feed equivalent point X can also change, therefore, s can also occur
Slight change.Certainly according to other needs, θ can also have other angles.By emulation, optimal angle, θ can be obtained.
In the present invention, first man-made microstructure, the second man-made microstructure are the metal being made up of copper cash or silver wire
Micro-structural, the metal micro structure is respectively attached to the by etching, plating, carve, photoetching, the method that electronics is carved or ion is carved
One base material, the second base material.Preferably, first man-made microstructure, the second man-made microstructure are the plane snowflake shown in Fig. 5
The metal micro structure of shape develops the metal micro structure of the multiple different topology for obtaining by topology.
In the present invention, core layer can be obtained by the following method, i.e., in the first prebasal plate and the first metacoxal plate
The surface overlying copper of any one, then logical overetched method obtains multiple first metal micro structures (multiple micro- knots of first metal
The shape of structure is obtained by Computer Simulation in advance with arrangement), finally the first prebasal plate is pressed together on respectively with the first metacoxal plate
Together, that is, core layer of the invention is obtained, the method for pressing can be direct hot pressing, or connect using PUR
Connect, the connection of other machinery formula, such as bolt connection are may also be certainly.
Similarly, impedance matching layer lamella can also be obtained using identical method.Then respectively by multiple core layers
Pressing one, that is, form core layer of the invention；Equally, multiple impedance matching layer lamellas are pressed into one, that is, forms this
The impedance matching layer of invention；Core layer, impedance matching layer pressing one are obtained into metamaterial panel of the invention.
In the present invention, the first base material, the second base material are by ceramic material, macromolecular material, ferroelectric material, ferrite material
Or ferromagnetic material etc. is obtained.Macromolecular material is available F4B composites, FR-4 composites etc..Preferably, the present invention
In, first prebasal plate and the first metacoxal plate of the first base material use identical FR-4 composites；Equally, in the present invention,
Second prebasal plate and the second metacoxal plate of second base material are also adopted by identical FR-4 composites.
Fig. 5 show the schematic diagram of the metal micro structure of plane flakes, and the metal micro structure of described flakes has
It is mutually perpendicular to the length of the first metal wire J1 and the second the metal wire J2, the first metal wire J1 and the second metal wire J2 for dividing equally
Identical, the first metal wire J1 two ends are connected with two first metal branch F1, the first metal wire J1 of equal length
Two ends are connected on two midpoints of the first metal branch F1, and the second metal wire J2 two ends are connected with two of equal length
Second metal branch F2, the second metal wire J2 two ends are connected on two midpoints of the second metal branch F2, and described first
The equal length of metal branch F1 and the second metal branch F2.
Fig. 6 is a kind of derived structure of the metal micro structure of the plane flakes shown in Fig. 5.It is in each first metal point
The two ends of branch F1 and each the second metal branch F2 are respectively connected with identical 3rd metal branch F3, and the corresponding 3rd
End points of the midpoint of metal branch F3 respectively with the first metal branch F1 and the second metal branch F2 is connected.The rest may be inferred, this hair
The bright metal micro structure that can also derive other forms.
Fig. 7 is a kind of distressed structure of the metal micro structure of the plane flakes shown in Fig. 5, the micro- knot of metal of this kind of structure
Structure, the first metal wire J1 and the second metal wire J2 are not straight lines, but folding line, and the first metal wire J1 is equal with the second metal wire J2
Be provided with two kink WZ, but the first metal wire J1 and the second metal wire J2 be still it is vertical divide equally, bent by setting
Relative position of the direction in portion with kink on the first metal wire and the second metal wire so that the metal micro structure shown in Fig. 7
All overlapped with artwork to the figure that any direction is rotated by 90 ° with the axis of the second metal wire intersection point around perpendicular to the first metal wire.
Furthermore it is also possible to there are other to deform, for example, the first metal wire J1 and the second metal wire J2 are respectively provided with multiple kink WZ.
In the present invention, the core layer 11 can be divided into the Meta Materials list multiple as shown in Figure 2 of array arrangement
First D, each metamaterial unit D include prebasal plate unit U, metacoxal plate unit V and be arranged on base board unit U, metacoxal plate unit V it
Between the first man-made microstructure 12, the length, width and height of usual metamaterial unit D no more than 1/5th wavelength, preferably ten/
One wavelength, therefore, the working frequency according to antenna can determine the size of metamaterial unit D.Fig. 2 is the technique of painting of perspective, with table
Show the position in the metamaterial unit D of the first man-made microstructure, as shown in Fig. 2 first man-made microstructure is sandwiched in substrate list
Between first U, metacoxal plate unit V, surface where it is represented with SR.
Known refractive indexWherein μ is relative permeability, and ε is relative dielectric constant, and μ and ε is collectively referred to as electromagnetism ginseng
Number.It is demonstrated experimentally that when electromagnetic wave is by refractive index dielectric material heterogeneous, can be to the big direction deviation of refractive index.Relative
(1 is generally near in the case that magnetic conductivity is certain), refractive index is only relevant with dielectric constant, in the case where the first base material is selected,
Using the first man-made microstructure only to electric field response the arbitrary value of metamaterial unit refractive index can be realized (in certain limit
It is interior), under the center of antenna frequency (12.5GHZ), using simulation software, such as CST, MATLAB, obtain a certain by emulating
The dielectric constant of the man-made microstructure (metal micro structure of plane flakes as shown in Figure 5) of given shape is with topology
Refractive index variable change situation, you can list one-to-one data, you can design we needs specific refractive index
The core layer 11 of distribution, can similarly obtain the index distribution of impedance matching layer lamella, so as to obtain whole Meta Materials
The index distribution of panel 100.
In the present invention, the structure design of core layer can be obtained by Computer Simulation (CST emulation), specific as follows：
(1) the attachment base material (the first base material) of the first metal micro structure is determined.This it is bright in, the first base material first before
Substrate is made with the first metacoxal plate of identical FR-4 composites, and described FR-4 composites are made predetermined with one
Dielectric constant, such as dielectric constant is 3.3 FR-4 composites.
(2) size of metamaterial unit is determined.The size of the size of metamaterial unit is obtained by the centre frequency of antenna, profit
Its wavelength is obtained with frequency, then takes length CD and width of the numerical value less than 1/5th of wavelength as metamaterial unit D
Degree KD.In the present invention, the metamaterial unit D is that CD long as shown in Figure 2 and width KD is 2.5mm, thickness HD for 0.818mm
Square platelet.
(3) material and topological structure of metal micro structure are determined.In the present invention, the material of metal micro structure is copper, metal
The topological structure of micro-structural is the metal micro structure of the plane flakes shown in Fig. 5, and W is consistent everywhere for its line width；Topology herein
Structure, refers to the basic configuration of topology differentiation.
(4) the topology parameter of metal micro structure is determined.As shown in figure 5, in the present invention, the metal of plane flakes is micro-
The topology parameter of structure includes the length a of the line width W, the first metal wire J1 of metal micro structure, the first metal branch F1's
Length b.
(5) the differentiation restrictive condition of the topology of metal micro structure is determined.In the present invention, the topological shape of metal micro structure
The differentiation restrictive condition of shape has, and the minimum spacing WL between metal micro structure is (i.e. as shown in figure 8, metal micro structure and Meta Materials
The side long of unit or the distance of broadside are WL/2), the line width W of metal micro structure, the size of metamaterial unit；Due to processing technology
Limitation, WL is more than or equal to 0.1mm, and equally, line width W is also intended to more than or equal to 0.1mm.In the present invention, WL takes 0.1mm, and W takes
0.3mm, the size of metamaterial unit is length and a width of 2.5mm, and thickness is 0.818mm, now the topology of metal micro structure
Parameter only has two variables of a and b.The topology of metal micro structure by the differentiation mode as shown in Fig. 8 to Fig. 9, correspondence
In a certain CF (such as 12.5GHZ), a continuous variations in refractive index scope can be obtained.
Specifically, the differentiation of the topology of the metal micro structure includes that two stages, (it is basic that topology is developed
It is shaped as the metal micro structure shown in Fig. 5)：
First stage：According to restrictive condition is developed, in the case where b values keep constant, a values are changed to most from minimum value
Big value, the metal micro structure in this evolution process is " ten " font when minimum value (a take except).In the present embodiment, the minimum of a
Value is 0.3mm (line width W), and the maximum of a is (CD-WL), i.e. 2.5-0.1mm, then the maximum of a is 2.4mm.Therefore, exist
In first stage, the differentiation of the topology of metal micro structure is as shown in figure 8, i.e. from the square JX1 that the length of side is W, gradually drill
Become maximum " ten " font topology JD1, in maximum " ten " font topology JD1, the first metal wire J1 and the
Two metal wire J2 length are 2.4mm, and width W is 0.3mm.In the first phase, with the topology of metal micro structure
Differentiation, the refractive index of corresponding metamaterial unit continuously increases ((CF of respective antenna one), when frequency is
During 12.5GHZ, the minimum value n of the corresponding refractive index of metamaterial unitminIt is 1.91.
Second stage：According to restrictive condition is developed, when a increases to maximum, a keeps constant；Now, by b from minimum
Value increases continuously maximum, and the metal micro structure in this evolution process is plane flakes.In the present embodiment, the minimum of b
Value is 0.3mm (line width W), and the maximum of b is (CD-WL-2W), i.e. 2.5-0.1-2*0.3mm, then the maximum of b is
1.8mm.Therefore, in second stage, the differentiation of the topology of metal micro structure is as shown in figure 9, i.e. from maximum " ten " word
Shape topology JD1, is gradually evolved into the topology JD2 of the plane flakes of maximum, maximum plane flakes herein
Topology JD2 refer to that the first metal branch J1 can not extend again with the length b of the second metal branch J2, otherwise
One metal branch will intersect with the second metal branch, and the maximum of b is 1.8mm.Now, the first metal wire and the second metal
Line length is 2.4mm, and width is 0.3mm, and the length of the first metal branch and the second metal branch is 1.8mm, width
It is 0.3mm.In second stage, with the differentiation of the topology of metal micro structure, the folding of corresponding metamaterial unit
Penetrate rate and continuously increase (CF of respective antenna one), when frequency is 12.5GHZ, the corresponding refractive index of metamaterial unit is most
Big value nmaxIt is 5.6.
The variations in refractive index scope (1.91-5.6) for obtaining metamaterial unit by above-mentioned differentiation meets design needs.If
The variations in refractive index scope that above-mentioned differentiation obtains metamaterial unit is unsatisfactory for designing needs, and such as maximum is too small, then change WL
With W, emulate again, the variations in refractive index scope until obtaining our needs.
According to formula (1), after a series of metamaterial unit for obtaining will be emulated according to its corresponding refractive index arrangement
(actually arrangement of multiple first man-made microstructures of different topology shape in the first base material), can obtain the present invention
Core layer.
Similarly, impedance matching layer lamella of the invention can be obtained.
Figure 10 is the structural representation of satellite tv antenna another kind embodiment of the invention.In this embodiment, it is different
It is that metamaterial panel 100 is divided into four cell boards 1000, the longitudinal section of each cell board is the square that the length of side is 200mm,
Between four cell boards 1000 by way of being hinged, can fold.So be conducive to antenna processing and manufacturing and
Install and safeguard, multiple cell boards are removably connected, or multiple cell boards can be folded by rotatable connected mode, be made
Satellite tv antenna of the invention is obtained when carrying, the area of very little is only occupied.The formation of cell board 1000 can have following two
The mode of kind：
(1) isolated after overall processing in flakes, this mode is adapted to the metamaterial flat of less area.
(2) the overall structure parameter of metamaterial panel is designed, multiple cell boards 1000 is divided into before manufacture, it is right
These cell boards are individually fabricated.This mode is especially suitable for the metamaterial panel processing of ultra-large type.
Cell board, preferably by same size, so conveniently stacks, and the quantity of cell board can be as needed
Setting.
Multiple cell boards 1000 are removably connected, for example, can be bolt connection, be bonded, snap connection.This implementation
In example, it is preferable that multiple cell boards 1000 can be folded by rotatable connected mode.
In addition, as shown in figure 11, the present invention is also provided present invention also offers a kind of satellite television receiving system, including feedback
Source 1, the tuner 30 of connection feed 1 and with tuner 30 by the DVB (not indicated in figure) of cable connection, above-mentioned
Satellite tv antenna TX and support satellite tv antenna satellite tv antenna support, the satellite tv antenna TX sets
At the rear of feed 1.In the present invention, the feed 1 is traditional corrugated horn.DVB is also existing with tuner
Technology, no longer state herein.
In addition, in the present invention, the incoming frequency of tuner used is 12.25~12.75GHz, and local frequency is
11300MHz, output frequency is 950~1450MHz, can watch most of Ku band satellites TV.Preferably, the feed with
Tuner is integrally formed, to mitigate overall weight.
In the present invention, as shown in Figure 11 to 14, the satellite tv antenna support includes support satellite tv antenna
The pole 4 and the feed adjusting means 500 for adjusting feed angle of base 3 and support feed 1, the feed adjusting means
500 include the connecting plate 5 of connection pole 4, the first hold assembly 6 and the second clamping part for clamping feed 1 from opposite sides
Part 7, the connecting plate 5 has the installation portion 53 of connection pole 4 and is formed in first arm 51 and the of the both sides of installation portion 53
Two arms 52, first hold assembly 6 includes the first clamping section 61 being fixedly connected with feed 1 and is formed in the first clamping section
On 61 side walls and positioned at the first rotating shaft 62 of the top of the first arm 51, the top of the first rotating shaft 62 is covered with the first briquetting 8,
First briquetting 8 is fixed on the first arm 51, and the top of first briquetting 8 offers the first screwed hole 81 of insertion,
The lower ending opening of the first screwed hole 81 is provided with the first rotary knob rod XN1, described just to first rotating shaft 62 in first screwed hole 81
Two hold assemblies 7 include the second clamping section 71 being fixedly connected with feed 1 and are formed on the side wall of the second clamping section 71 and are located at
Second rotating shaft 72 of the top of the second arm 52, the top of second rotating shaft 72 is covered with the second briquetting 9, second briquetting 9
It is fixed on the second arm 52, the top of second briquetting 9 offers the second screwed hole 91 of insertion, the second screwed hole 91
Lower ending opening just to the second rotating shaft 72, is provided with the second rotary knob rod XN2 in the second screwed hole 30.
In the present invention, the first rotating shaft 62 is coaxially disposed with the second rotating shaft 72.
In the present invention, the installation portion of the connecting plate has the square box 530 being set on pole, the square box 530
It is bolted to connection with pole 4.
In the present invention, one end that the first rotating shaft stretches out the first briquetting 8 is provided with knob XN, in addition to being easy to directly perceived
Reading angle, index dial 50 can also be set on the first clamping section 61, on the first arm 42 set pointer 60, with indicate
Feed angle.
The operation principle of the adjustment feed angle of feed adjusting means 5 is following (it is assumed that original state is fixed on certain for feed
One angle)：
Outwards rotate the first rotary knob rod XN1 and the second rotary knob rod XN2 so that first rotating shaft 62 is loose with the second rotating shaft 72
Open, now, then rotate the knob XN in first rotating shaft, you can the angle of adjustment feed, the number of degrees are directly read from index dial is
Can；After the completion of adjustment, the fastening feed that the first rotary knob rod XN1 and the second rotary knob rod XN2 can again is rotated by opposite direction.
In the present invention, the base 3 includes being supported on the carriage 31 at satellite tv antenna TX backs, carriage 31 with defend
Star television antenna TX is fixedly connected, and the medium position of the carriage 31 is fixedly installed mounting seat 32, one end of the pole 4
It is fixedly connected in mounting seat 32.
In the present invention, the base 3 also includes that the hinged seat 33 and hinged seat 33 that are fixed in mounting seat 32 are rotatable
The connecting portion 35 of articulated joint 34 and articulated joint 34 connection of connection and the portions 36 being connected with connecting portion 35.
In the present invention, the articulated joint 34 is placed in hinged seat 33, and the both sides of hinged seat 33 are symmetrically arranged with the first slip
The sliding groove 332 of groove 331 and second, articulated joint 34 is realized by through articulated joint with hinged seat 33 with the first screw rod 37 of hinged seat
Rotatable connection, the two ends of the first screw rod 37 are provided with two the first location nuts 38, and the base also includes running through first
Second screw rod 39 of the sliding groove 332 of sliding groove 331 and second, the two ends of the first screw rod 39 are provided with two the second location nuts
40。
In the present invention, the first screw rod is to play rotary shaft, to allow that satellite tv antenna is adjusted towards (alignment
Satellite)；And the second screw rod then plays the role of positioning, i.e., adjusted after in satellite tv antenna, be located at that position
Put (after two-point locating, i.e., can not rotate).
Embodiments of the invention are described above in conjunction with accompanying drawing, but the invention is not limited in above-mentioned specific
Implementation method, above-mentioned specific embodiment is only schematical, rather than restricted, one of ordinary skill in the art
Under enlightenment of the invention, in the case of present inventive concept and scope of the claimed protection is not departed from, can also make a lot
Form, these are belonged within protection of the invention.
Claims (9)
1. a kind of satellite tv antenna support, the satellite tv antenna support includes the base and branch of support satellite tv antenna
Support the pole of feed, it is characterised in that the satellite tv antenna includes being arranged on the metamaterial panel at feed rear, described to defend
Star TV antenna support also includes the feed adjusting means for adjusting feed angle, and the feed adjusting means includes connection branch
The connecting plate of bar, the first hold assembly and the second hold assembly for clamping feed from opposite sides, the connecting plate have
The installation portion for connecting pole and the first arm and the second arm that are formed in installation portion both sides, first hold assembly include
With the first clamping section that feed is fixedly connected and be formed on the first clamping section side wall and above the first arm first turn
Axle, is covered with the first briquetting above the first rotating shaft, first briquetting is fixed on the first arm, first briquetting
Top offer the first screwed hole of insertion, the lower ending opening of the first screwed hole just to first rotating shaft, stretch by the first rotating shaft
The one end for going out the first briquetting is provided with knob, and the first rotary knob rod is provided with the first screwed hole, and second hold assembly includes
With the second clamping section that feed is fixedly connected and be formed on the second clamping section side wall and above the second arm second turn
Axle, is covered with the second briquetting above second rotating shaft, second briquetting is fixed on the second arm, second briquetting
Top offer the second screwed hole of insertion, the lower ending opening of the second screwed hole sets just to the second rotating shaft in the second screwed hole
It is equipped with the second rotary knob rod.
2. satellite tv antenna support according to claim 1, it is characterised in that the first rotating shaft is same with the second rotating shaft
Axle is set.
3. satellite tv antenna support according to claim 1, it is characterised in that the installation portion of the connecting plate has set
The square box on pole is located at, the square box is bolted to connection with pole.
4. the satellite tv antenna support according to claims 1 to 3 any one, it is characterised in that the base includes
The carriage at satellite tv antenna back is supported on, the medium position of the carriage is fixedly installed mounting seat, the pole
One end be fixedly connected in mounting seat.
5. satellite tv antenna support according to claim 4, it is characterised in that the base includes being fixed on mounting seat
On hinged seat and hinged seat rotatably connection articulated joint and articulated joint connection connecting portion and be connected with connecting portion
Portions.
6. satellite tv antenna support according to claim 5, it is characterised in that the articulated joint is placed in hinged seat,
The both sides of hinged seat are symmetrically arranged with the first sliding groove and the second sliding groove, and articulated joint is with hinged seat by through articulated joint and hinge
First screw rod of joint chair realizes rotatable connection, and the two ends of the first screw rod are provided with two the first location nuts, also including passing through
The second screw rod of the first sliding groove and the second sliding groove is worn, the two ends of the first screw rod are provided with two the second location nuts.
7. a kind of satellite television receiving system, including satellite tv antenna, feed, the tuner of connection feed and connection tuner
DVB, it is characterised in that the satellite tv antenna includes being arranged on the metamaterial panel at feed rear, the satellite
TV receiving system also includes the satellite tv antenna support as described in claim 1 to 6 any one.
8. satellite television receiving system according to claim 7, it is characterised in that the feed is corrugated horn.
9. satellite television receiving system according to claim 8, it is characterised in that the feed and the bodily form of tuner one
Into.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210050856.0A CN103296377B (en) | 2012-02-29 | 2012-02-29 | A kind of satellite tv antenna support and its satellite television receiving system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210050856.0A CN103296377B (en) | 2012-02-29 | 2012-02-29 | A kind of satellite tv antenna support and its satellite television receiving system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103296377A CN103296377A (en) | 2013-09-11 |
| CN103296377B true CN103296377B (en) | 2017-06-23 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210050856.0A Active CN103296377B (en) | 2012-02-29 | 2012-02-29 | A kind of satellite tv antenna support and its satellite television receiving system |
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| Country | Link |
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| CN (1) | CN103296377B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108152794A (en) * | 2017-12-22 | 2018-06-12 | 安徽仁信安防电子工程有限公司 | A kind of marine exploration marine radar direction adjusting apparatus and displacement method |
| CN111430874B (en) * | 2020-04-21 | 2021-07-09 | 北京行晟科技有限公司 | Phased array antenna system |
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| CN2252415Y (en) * | 1996-01-23 | 1997-04-16 | 成都星海电子研究所 | Satellite receiving antenna |
| US5714960A (en) * | 1995-07-21 | 1998-02-03 | Daewoo Electronics Co., Ltd. | Parabolic antenna |
| EP0843381A2 (en) * | 1996-11-15 | 1998-05-20 | Yagi Antenna Co., Ltd. | Multibeam antenna |
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| JP2011087184A (en) * | 2009-10-16 | 2011-04-28 | Dx Antenna Co Ltd | Horn antenna apparatus |
| WO2011108015A1 (en) * | 2010-03-04 | 2011-09-09 | Telespazio S.P.A. | Transportable satellite 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 |
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| US4563687A (en) * | 1984-02-06 | 1986-01-07 | Gte Communications Products Corporation | Adjustable antenna mount |
| US5714960A (en) * | 1995-07-21 | 1998-02-03 | Daewoo Electronics Co., Ltd. | Parabolic antenna |
| CN2252415Y (en) * | 1996-01-23 | 1997-04-16 | 成都星海电子研究所 | Satellite receiving antenna |
| EP0843381A2 (en) * | 1996-11-15 | 1998-05-20 | Yagi Antenna Co., Ltd. | Multibeam antenna |
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| JP2011087184A (en) * | 2009-10-16 | 2011-04-28 | Dx Antenna Co Ltd | Horn antenna apparatus |
| WO2011108015A1 (en) * | 2010-03-04 | 2011-09-09 | Telespazio S.P.A. | Transportable satellite antenna |
| CN101931116A (en) * | 2010-07-12 | 2010-12-29 | 四川湖山电器有限责任公司 | Portable paraboloid satellite earth antenna capable of being rapidly erected and folded |
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103296377A (en) | 2013-09-11 |
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