CN201226373Y - Double-frequency band laminated medium loading helical antenna - Google Patents
Double-frequency band laminated medium loading helical antenna Download PDFInfo
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- CN201226373Y CN201226373Y CNU2008200505167U CN200820050516U CN201226373Y CN 201226373 Y CN201226373 Y CN 201226373Y CN U2008200505167 U CNU2008200505167 U CN U2008200505167U CN 200820050516 U CN200820050516 U CN 200820050516U CN 201226373 Y CN201226373 Y CN 201226373Y
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Abstract
The utility model relates to a dual-band laminated medium loaded helical antenna, which comprises an upper cylindrical body and a lower cylindrical body which are coaxially laminated; the two cylindrical bottoms surfaces and bottoms are respectively provided with a metal layer; four metal plates are arranged at the top end; the length of two metal plates is different from the length of the other two; one end of each metal plate extends in the radial direction from the centers of the cylindrical bodies to the surrounding edges of the top surface and then extends to the metal layer in the axial direction along the helical path on the top surface; the ends of the opposite surfaces of two adjacent metal plates of the upper cylindrical body are connected with each other to form two groups of antennas; the four metal plates of the upper cylindrical body and the lower cylindrical body are respectively connected with the top end surface of the lower cylindrical body; a cable which is embedded into the axial through hole comprises an insulation body; the surface of the insulation body is covered by a conductive shielding layer; a feeding needle is arranged at the center of the insulation body; the two ends of the feeding pin extend out of the through hole; the top end of the conductive shielding layer is connected with one group of antennas of the upper cylindrical body; the top end of the feeding needle is connected with the other group of antennas of the upper cylindrical body; and the metal layers on the bottom surface of the upper cylindrical body and the lower cylindrical body contact with the corresponding horizontal section of the conductive shielding layer. The utility model has the advantages of small size and good performance.
Description
Technical field
The utility model relates to a kind of antenna, particularly a kind ofly can work in two-band, and can effectively dwindle antenna volume, is applicable to the lamination medium loading helical antenna structure of handheld terminal.
Background technology
The beginning of this century, along with GPS (global positioning system) opens for free to civil area, GPS has developed into an industry of growing up at a high speed.The civil area of GPS has comprised a plurality of fields such as land transport, sea transport, civil aviation, communication, mapping, building, mining, agricultural, electric power system, medical applications, scientific research, household electrical appliances, amusement at present.2007, Chinese GPS entered a comprehensive outbreak period.The fast development of GPS industry has influenced the development of other parallel industrial chains, and its overlapping is merged, and makes hand-held terminal devices such as PDA, the MP4 have the GPS function in a large number, camera, mobile phone become the big main flow on the market now.What is particularly worth mentioning is that the GPS mobile phone has become a big hot topic of mobile phone industry.Mobile phone development till now, for function development near the limit, provide more applications and the service be the new direction that conventional mobile phone manufacturer is groping.The GPS mobile phone can expedite the emergence of a lot of application relevant with the position, thereby extends brand-new business model.Therefore, GPS is expected to continue the another bright spot of taking pictures, become after the music cell-phone function.
Simultaneously, along with popularizing that GPS uses, the application that some are special as integrated detection of high accuracy or difference baseline system, has proposed new requirement to gps system.Gps system must be operated in L1/L2 simultaneously, and (L1:1575MHZ is L2:1227MHZ) on two frequencies.
Antenna receives from the space electromagnetic wave that satellite is launched, and is converted into the radio-frequency current signal as " knowledge " of GPS receiver.Because microelectric technique development, receiver chip can Highgrade integrations, size is relatively little.But the miniaturization of antenna will be subjected to the restriction of Several Factors.Theoretically, antenna size is directly proportional with the wavelength of signal, by selecting high dielectric constant materials for use, can reduce the wavelength of signal in the material, and then reduce the size of antenna, but undersized, antenna can face the problem of gain and bandwidth decline again.Because the design feature of antenna is difficult to large-scale pipeline production, so cost is higher relatively.In a word, antenna has become the bottleneck of restriction handhold GPS equipment size, is the key factor of restriction handhold GPS equipment reception and cost simultaneously.Therefore, press for that a kind of volume is little, cost is low, reception is good, and can be operated in the GPS handheld terminal antenna of GPS L1, L2 two-band simultaneously.
Because gps signal is a circularly polarised wave, all GPS reception antennas all are the circular polarization working methods.Be limited to the restriction of various conditions such as gps antenna size, directivity and polarization performance, the structure type of gps antenna in the market mainly contains plate type antenna and two kinds of structures of four-arm spiral antenna.
Plate type antenna generally possesses preferable directional characteristic, in the time of directly over satellite is positioned at antenna, has maximum receiving gain.Be suitable for mainly in the end product of the GPS navigation of top.The plate type antenna biggest advantage is made relatively exactly and is easier to, but because the size of antenna aperature is common decision of ground plane dimensions by the size and the below radiation process of radiation assembly, so the receiving sensitivity of antenna is affected easily.
Four-arm spiral antenna is proposed in nineteen sixty-eight by C.C.kilgus the earliest.This structure is made up of four metal spiral lines, by suitably selecting the physical size of wire spiral, and to four helixes present respectively with have 90 the degree phase differences constant-amplitude signal, just can produce cordate circular polarization directional diagram, have the advantage that does not need the ground connection reflecting plate.Particularly when hanging down the elevation angle, its circular polarization performance also can satisfy the requirement of gps system, therefore is highly suitable for the action handheld navigation product that all requires energy freely use in all directions.Yet because four-arm spiral antenna is the mode of resonance antenna, frequency band is too narrow, can not adapt to the requirement of the two-frequency operation of gps system.
Lamensdorf has proposed a kind of double-frequency GPS antenna based on four arm helical structures, by introducing lamped element, make this antenna work in GPS L1 (1575MHZ) and two frequency ranges of L2 (1227MHZ), and all show good circular polarization performance two frequency ranges.This antenna is made up of four individual pen wire spirals, and every length is a wavelength, corresponding low frequency L2 frequency range.At the vertex feed of spiral, every spiral is respectively the signal feed of 0,90,180,270 degree with phase place.The bottom open circuit of spiral.In order to realize dual frequency characteristics, have a slit at the ad-hoc location of helix, wire spiral is cut to two parts up and down, two parts up and down that the LC shunt-resonant circuit that constitutes with a lamped element makes wire spiral are continuous again on electric.The LC shunt-resonant circuit is equivalent to a switch, and selecting suitable L and C value to make its resonance frequency is high band L1, and therefore at high band L1 place, its resistance is infinitely great, is equivalent to open circuit.At low-frequency range L2 place, its resistance is very little, can do suitable compensation by the length of fine setting wire spiral, and the top and the bottom short circuit of wire spiral is linked to each other.Therefore, whole wire spiral (comprising upper and lower two parts and LC loop) is at low frequency L2 place resonance, and the upper part of wire spiral has so just reached the purpose of two-frequency operation at high band L1 place resonance.
Also the someone has proposed another Double-frequency antenna structure---eight arm helical antennas.Between the interval of each feed helix of traditional four-arm spiral antenna, establish a parasitic helix again, constitute eight arm helical antennas with rotation direction.Also can regard that two pairs of shapes are similar as, coaxial placement, but the different four-arm spiral antenna of brachium.Only original four helixes are carried out feed,, but encourage by electromagnetic coupled not to four root parasitism helix feeds.Four arm helixes of feed and parasitic four arm helixes surround coaxial respectively and have the cylinder of differing heights and diameter, make the length difference of inside and outside two groups of helicals.The length of feed four arm spirals is λ
1/ 2, the length of parasitic four arm spirals is λ
2/ 2, this antenna just can be operated in λ like this
1, λ
2On two different operating frequencies, obtain the two-frequency operation characteristic.
2007, there is the scholar to propose the double frequency reception antenna of a kind of GPS/CNSS of being used for.By with two group of 1/4th circle, length is inside and outside nested coaxial the putting together of the four-arm spiral antenna of 1/4th wavelength, and inside and outside two group of four arm spiral carried out feed respectively, the length of two group of four arm spiral corresponds respectively to two different resonance frequencys, thereby realizes GPS and CNSS two-frequency operation.
Above-mentioned antenna is owing to be the half-wavelength of free space or the resonance structure of 3/4 wavelength all, and for the application of hand-held set, the size of these antenna is too big.
Calendar year 2001, the Oliver Leisten of Britain Sarantel antenna company has proposed a kind of novel four-arm spiral antenna---and medium loads four-arm spiral antenna (DQHA).Radiating principal is made up of four wire spirals, and the length of every spiral arm is about λ/2, is wrapped on the medium post of high-k (ε r=36).The bottom of helix is connected with a sleeve balun.This antenna by a coaxial line that passes the medium axis of a cylinder heart in top-fed.This four-arm spiral antenna can be regarded as by the both arms spiral of two quadratures to be formed, electric current from coaxial inner conductor along helix toward dirty, through the edge of balun and diameter over against that root helix, get back to coaxial outer conductor.In order to realize 90 degree phase difference feeds, the length of two both arms spirals of fine setting makes a both arms spiral be longer than resonance length slightly, and producing a phase angle is the input impedance of+45 degree; Make another one both arms spiral be shorter than resonance length slightly, produce intersecting of one-45 degree.The bottom of Balun links to each other with the outer conductor of coaxial line, highly be λ/4 (λ is a guide wavelength), the top that is equivalent at Balun has produced an open circuit, electric current is only flowed along the top of Ba Lun, antenna and unbalanced feed system are kept apart, reduced the hand-held influence of human body antenna performance.
Method by above-mentioned medium loads has not only realized undersized antenna, and most of near-field energy is coupled to the medium the inside, and is very little in the near-field energy of medium outside, is used on the GPS hand-held set, and tissue is very little to the influence of its generation.The antenna of this structure has also comprised complete balun circuit (Balun) design simultaneously, antenna and unbalanced feed system are kept apart in this design, not only further reduced the hand-held influence of human body to it, and can isolated antennas the signal of periphery, therefore can allow the antenna of various functions and be stored in the minimum space and can not interfere with each other.Become more diversified for integration function, and emphasize compact hand-held electronic product, the importance of this characteristic is ineffable.Based on above-mentioned perfect performance, this antenna is rated as a revolutionary invention, is known as the gps antenna of suitable mobile handheld terminal by industry.
In addition, Oliver Leisten also loads four-arm spiral antenna to medium and has proposed multiple different design and processing method, yet this antenna also fails to be implemented in two-band work.The GPS handheld terminal antenna that can be operated in GPS L1, L2 two-band simultaneously rarely has report so far, and the medium loading helical antenna of energy two-band work does not see that so far any document or patent report are arranged.
The utility model content
The purpose of this utility model is to overcome the shortcoming of prior art, provides a kind of and can work in two-band, and can effectively dwindle antenna volume, be applicable to the lamination medium loading helical antenna of handheld terminal.
Be the technical scheme that realizes that the purpose of this utility model adopts: a kind of double-frequency band lamination medium loading helical antenna comprises:
Two one thin one thick coaxial columns, its shaft core position is provided with a through hole; Described two column bottom end faces and bottom circumferential outer surface are equipped with metal level; Described thin column inserts from the top of described thick column, and fits tightly with it;
The top end surface of two described columns respectively is laid with four radiation sheet metals, one end of each described radiation sheet metal is radially extended by the center of two described columns respectively, after extending to its top periphery, again respectively at the circumferential surface of two described columns, according to helical-like path, extend to the described metal level place of its bottom circumferential outer surface vertically, and contact with described metal level; On the top end surface of described thin column, the relative surface end of per two adjacent radiation sheet metals is connected to each other, and forms two groups of antenna structures; The end that four radiation sheet metals on the described thin column contact with described thick column is connected with corresponding radiation sheet metal on the described thick column respectively on the surface on described thick column top;
In four radiation sheet metals on the described thin column, the length of two radiation sheet metals that the position is relative is greater than relative two radiation sheet metals in addition in position; In four radiation sheet metals on the described thick column, the length of two radiation sheet metals that the position is relative is greater than relative two radiation sheet metals in addition in position;
One coaxial cable, embed the bottom that described through hole is interior and described thick column is stretched out in the bottom, comprise an insulator, this insulator outer fringe surface is coated with a conduction shielding layer, this insulator center is provided with a feeding needle, the top of this feeding needle stretches out the top of described thin column, the top of described conduction shielding layer is connected with the end that one group of antenna structure of described thin column is positioned at thin column top, the top of described feeding needle is connected with the end that another group antenna structure of described thin column is positioned at thin column top, the corresponding section with the level of described conduction shielding layer of the metal level of described thick column bottom end face contacts, and the corresponding section with the level of described conduction shielding layer of the metal level of described thin column bottom end face contacts.
In order to realize the utility model better, described two columns are made by dielectric material.
Described thin column bottom circumferential outer surface has among the described thick column top of one section insertion of metal level.
The top end surface of the top end surface of described thin column and described thick column is in same horizontal plane.
The described metal level that is positioned at thin column bottom circumferential outer surface, its electrical length h
1Be 1/8 λ
1＜h
1＜3/8 λ
1The described metal level that is positioned at thick column bottom circumferential outer surface, its electrical length h
2Be 1/8 λ
2＜h
2＜3/8 λ
2λ wherein
1Be the wavelength of antenna first working frequency range, λ
2Be the wavelength of antenna second working frequency range, λ
1＜λ
2
Four radiation sheet metals on the described thin column, wherein the length L of relative two radiation sheet metals in position is 1/2 λ
1＜L＜3/5 λ
1, the relative length L of two radiation sheet metals in addition in position is 2/5 λ
1＜L＜1/2 λ
1Four radiation sheet metals on the described thick column, wherein the length L of relative two radiation sheet metals in position is 1/2 λ
2＜L＜3/5 λ
2, the relative length L of two radiation sheet metals in addition in position is 2/5 λ
2＜L＜1/2 λ
2λ wherein
1Be the wavelength of antenna first working frequency range, λ
2Be the wavelength of antenna second working frequency range, λ
1＜λ
2
Described dielectric material is a ceramic material.
Described dielectric material is a macromolecular material.
The relative dielectric constant ε of described dielectric material
r5.
Described two columns are by DIELECTRIC CONSTANT
rThe column that different dielectric materials is made.
The utility model with respect to the advantage and the effect of prior art is: (1) the utility model is realized the work of two-band circular polarization with two coaxial being superimposed of four-arm spiral antenna structure.Load by medium, not only dwindled the size of whole helical antenna effectively, and the near-field energy of antenna all is coupled in the medium, can greatly reduce near the influence of the tissue of antenna or other medium to antenna performance; (2) by special barron structure design, antenna and unbalanced feed system are kept apart the influence that when having avoided human body hand-held antenna current has been distributed.Therefore, even this antenna also can keep good directivity and circular polarization performance under hand-held and situation that human body is very close, can be widely used in hand-held navigator or other satellite communication devices such as GPS mobile phone, PDA, camera.
Description of drawings
Fig. 1 is a kind of structural representation of the utility model double-frequency band lamination medium loading helical antenna;
Fig. 2 is the another kind of structural representation of the utility model double-frequency band lamination medium loading helical antenna;
Fig. 3 is the partial enlarged drawing of A among Fig. 2;
Fig. 4 is the partial enlarged drawing of B among Fig. 2;
Fig. 5 is another structural representation of the utility model double-frequency band lamination medium loading helical antenna;
Fig. 6 is another structural representation of the utility model double-frequency band lamination medium loading helical antenna;
Fig. 7 is that the double-frequency band lamination medium loading helical antenna to Fig. 1 and Fig. 2 carries out the results measured schematic diagram.
Embodiment
Below in conjunction with embodiment and accompanying drawing the utility model is described in further detail, but execution mode of the present utility model is not limited thereto.
Basic structure of the present utility model such as Fig. 1, Fig. 2, Fig. 5 and shown in Figure 6, following embodiment all adopts this basic structure: this antenna is made of column 20 and column 30, the diameter proportion of two columns does not require from the principle, for the processing of reality and easy to make, the diameter ratio of getting column 30 and column 20〉1.2; The aspect ratio of two columns can be arbitrary value from the principle, but for reality processing and easy to make, column 30 gets 1～4 with the aspect ratio of column 20: 1; Column 20 and 30 bottom circumferential outer surface all have layer of metal layer 22,32, bottom end face also all has layer of metal layer 23,33, metal level 22,32 and bottom end face metal level 23,33 fuse, and just as two top metal caps, are enclosed within the bottom of column 20,30;
The diameter of column 20 is less than the diameter of column 30, the top that column 20 inserts columns 30, and fit tightly with column 30, both form an overall structure;
The top end surface of column 20 is laid with four radiation sheet metals 211,212,213,214, the top end surface of column 30 is laid with four radiation sheet metals 311,312,313,314, radiation sheet metal 211,212,213,214,311,312,313,314 respectively by column 20, radially extend respectively at 30 center, when extending to column 20 respectively, behind 30 the top periphery, again in column 20,30 circumferential surface, according to helical-like path, extend to column 20 vertically, the metal level 22 of 30 bottom circumferential outer surfaces, 32 places, and with metal level 22,32 contact; On the top end surface of column 20, per two the adjacent radiation sheet metals 211 and 212,213 and 214 the opposite end of practising physiognomy are connected to each other, and form two groups of antenna structures; The end that four radiation sheet metals 211,212,213,214 on the column 20 contact with column 30 on the surface on column 30 tops, respectively with column 30 on 311,312,313,314 being connected of four radiation sheet metals.
The shaft core position of column 20,30 offers a through hole 24,34, and through hole 24,34 is embedded in a coaxial cable 35, and the bottom that coaxial cable 35 penetrated and stretched out column 30 from the bottom of column 30 passes from the top of column 20; Coaxial cable 35 comprises an insulator 353, the outer fringe surface of insulator 353 is coated with a conduction shielding layer (or shield wire) 352, the center of insulator 353 is provided with a feeding needle 351, signal by feeding needle 351, when in coaxial cable 35, transmitting, conducted electricity the covering of shielding layer 352, and not by other Electromagnetic Interference.The top of conduction shielding layer (or shield wire) 352, be connected with 212 ends that are positioned at column 20 tops with one group of antenna structure 211 of column 20, the top of feeding needle 351 then is connected with the end that another group antenna structure 213 and 214 of column 20 is positioned at column 20 tops; Conduction shielding layer 352 contacts with metal level 33 when passing the bottom end face of column 30, conduction shielding layer 352 contacts with metal level 23 when passing the bottom end face of column 20, the bottom of feeding needle 351 is used for received satellite-signal is sent to receiving system as the feed side of the utility model medium loading helical antenna structure.
The electrical length h of the metal level 22 of column 20 bottom circumferential outer surfaces
1Be 1/8 λ
1＜h
1＜3/8 λ
1, the electrical length h of the metal level 32 of column 30 bottom circumferential outer surfaces
2Be 1/8 λ
2＜h
2＜3/8 λ
2, λ wherein
1Be the wavelength of antenna first working frequency range, λ
2Be the wavelength of antenna second working frequency range, λ
1＜λ
2The metal level 22,32 that is positioned at two column bottom circumferential outer surfaces is with the metal level 23,33 and the feed coaxial cable that are positioned at the column bottom end face, constituted a Balun (balance-imbalance converter), this Balun can keep apart this antenna and unbalanced feed system, to guarantee stable antenna performance.
The concrete structure of antenna as shown in Figure 1, the metal level 22 on the column 20 all is inserted into the top of column 30, both fit tightly and form an overall structure.
Radiation sheet metal 211,212,213,214 extends according to helical-like path along the side of column 20, but they have different length, the pitch that radiation sheet metal 211 and 213 pitch are a bit larger tham radiation sheet metal 212 and 214 so just can be so that the length of radiation sheet metal 211 and 213 be 0.45 λ
1, be shorter than half-wavelength slightly; Radiation sheet metal 212 and 214 length are 0.55 λ
1, be longer than half-wavelength slightly, wherein λ
1Wavelength for antenna first working frequency range; Radiation sheet metal 311,312,313,314 extends according to helical-like path along the side of column 30, but they have different length, the pitch that radiation sheet metal 311 and 313 pitch are a bit larger tham radiation sheet metal 312 and 314 makes that so the length of radiation sheet metal 311 and 313 is 0.45 λ
2, be shorter than half-wavelength slightly; Radiation sheet metal 312 and 314 length are 0.55 λ
2, be longer than half-wavelength slightly, wherein λ
2Wavelength for antenna second working frequency range; On the top end surface of column 30, an end of radiation sheet metal 311,312,313,314 is connected with metal level 22 contact positions at it with four radiation sheet metals 211,212,213,214 of column 20 respectively.Thus formed medium loading helical antenna structure, between radiation sheet metal 211,212,213,214 and radiation sheet metal 311,312,313,314 all can produce 90 ° phase difference, so this antenna just can be at λ
1, λ
2Two working frequency range all have the ability that wide angle receives the circular polarization satellite-signal.
Under frequency 1575MHZ and 1227MHZ, by dielectric constant be 39 dielectric material to make diameter be 10 millimeters, highly be 17.7 millimeters column 20 (corresponding λ
1Be 32 millimeters), the height of the metal level 22 of its bottom circumferential outer surface is 5.6 millimeters; By dielectric constant be 21 dielectric material to make diameter be 17 millimeters, highly be 28 millimeters column 30 (corresponding λ
2It is 63 millimeters), the height of the metal level 32 of its bottom circumferential outer surface is 8.5 millimeters, make double-frequency band lamination medium loading helical antenna according to said structure, the return loss of surveying this antenna as shown in Figure 7, two of return loss smallest point are respectively 1575MHZ and 1227MHZ to deserved frequency among Fig. 7, value for-15.7dB and-9.2dB, corresponding to L1 and the L2 frequency of GPS.
At this moment, if again with another Double-frequency antenna structure---eight arm helical antennas compare with it because eight arm helical antennas employing air is a dielectric matrix, then its size will for: diameter is about 50 millimeters, highly is about 100 millimeters.So lamination medium loading helical antenna of the present utility model, volume-diminished about 65%.
The concrete structure of antenna is as shown in Figure 2: the bottom circumferential outer surface metal level 22 of column 20 all is inserted into the top of column 30, and both fit tightly and form an overall structure.
Radiation sheet metal 211,212,213,214 extends according to helical-like path along the side of column 20, and they have identical pitch, for the length that realizes radiation sheet metal 212 and 214 approximately than radiation sheet metal 211 and 213 long 0.05 λ
1, dug two little grooves (as shown in Figure 3), wherein λ at metal level 22 and radiation sheet metal 212 and 214 touching positions
1Wavelength for antenna first working frequency range; Similar, radiation sheet metal 311,312,313,314 extends according to helical-like path along the side of column 30, and they have identical pitch, for the length that realizes radiation sheet metal 312 and 314 approximately than radiation sheet metal 311 and 313 long 0.05 λ
2, dug two little grooves (as shown in Figure 4), wherein λ at metal level 32 and radiation sheet metal 312 and 314 touching positions
2Wavelength for antenna second working frequency range; One end of radiation sheet metal 311,312,313,314 is connected with metal level 22 contact positions at it with four radiation sheet metals 211,212,213,214 of column 20 respectively.This medium loading helical antenna structure, between radiation sheet metal 211,212,213,214 and radiation sheet metal 311,312,313,314 all can produce 90 ° phase difference, can be at λ
1, λ
2Two working frequency range all have the ability that wide angle receives the circular polarization satellite-signal.
Under frequency 1575MHZ and 1227MHZ, be that 18.6 dielectric material is made diameter and is 13 millimeters, highly is 19.7 millimeters column 20 (corresponding λ by dielectric constant
1Be 47 millimeters), the height of the metal level 22 of its bottom circumferential outer surface is 6.4 millimeters; By dielectric constant is that 21 dielectric material is made diameter and is 17 millimeters, highly is 28 millimeters column 30 (corresponding λ
2Be 63 millimeters), the height of the metal level 32 of its bottom circumferential outer surface is 8.5 millimeters; Press said structure and make double-frequency band lamination medium loading helical antenna, the return loss of surveying this antenna as shown in Figure 7, two of return loss smallest point are respectively 1575MHZ and 1227MHZ to deserved frequency among Fig. 7, be worth for-15.7dB and-9.2dB, corresponding to L1 and the L2 frequency of GPS.
Embodiment 3
The concrete structure of antenna is as shown in Figure 1: column 20 is that 7.0 dielectric material is made by dielectric constant, and the electrical length of metal level 22 is 0.31 λ
1Column 30 is that 6.0 dielectric material is made by dielectric constant, and the electrical length of metal level 32 is 0.27 λ
2Column 30 is 1.5 with the diameter ratio of column 20, and height ratio is 1.43, and the metal level 22 of column 20 bottom circumferential outer surfaces all is inserted into the top of column 30, and both fit tightly and form an overall structure.
For realizing producing 90 ° phase difference between the radiation sheet metal 211,212,213,214, radiation sheet metal 211 and 213 is with the linearity path, and along the side of column 20, shape extends in the shape of a spiral, and the length that centers on column 20 is 0.48 λ
1, radiation sheet metal 212 and 214 is then with the serpentine shape path, and along the side of described column 20, shape extends in the shape of a spiral, and the length that centers on described column is 0.53 λ
1Similar, for realizing producing 90 ° phase difference between the radiation sheet metal 311,312,313,314, radiation sheet metal 311 and 313 is with the linearity path, and along the side of described column 30, shape extends in the shape of a spiral, and the length that centers on described column is 0.48 λ
2, radiation sheet metal 312 and 314 is then with the serpentine shape path, and along the side of described column 30, shape extends in the shape of a spiral, and the length that centers on described column is 0.53 λ
2Wherein, λ
1Be the wavelength of antenna first working frequency range, λ
2Be the wavelength of antenna second working frequency range, λ
1＜λ
2On the top end surface of column 30, an end of radiation sheet metal 311,312,313,314 is connected with metal level 22 contact positions at it with four radiation sheet metals 211,212,213,214 of column 20 respectively.This medium loading helical antenna structure, between radiation sheet metal 211,212,213,214 and radiation sheet metal 311,312,313,314 all can produce 90 ° phase difference, can be at λ
1, λ
2Two working frequency range all have the ability that wide angle receives the circular polarization satellite-signal.
Embodiment 4
The concrete structure of antenna is as shown in Figure 5: column 20 is that 7.0 dielectric material is made by dielectric constant, and the electrical length of metal level 22 is 0.23 λ
1Column 30 is that 8.0 dielectric material is made by dielectric constant, and the electrical length of metal level 32 is 0.28 λ
2Column 30 is 1.25 with the diameter ratio of column 20, and height ratio is 1.26, and half of column 20 is inserted into the top of column 30, and both fit tightly and form an overall structure.
Radiation sheet metal 211,212,213,214 extends according to helical-like path along the side of column 20, but they have different length, the pitch that radiation sheet metal 211 and 213 pitch are a bit larger tham radiation sheet metal 212 and 214 so just can be so that the length of radiation sheet metal 211 and 213 be 0.46 λ
1, be shorter than half-wavelength slightly; Radiation sheet metal 212 and 214 length are 0.52 λ
1, be longer than half-wavelength slightly.Radiation sheet metal 311,312,313,314 extends according to helical-like path along the side of column 30, but they have different length, the pitch that radiation sheet metal 311 and 313 pitch are a bit larger tham radiation sheet metal 312 and 314 makes that so the length of radiation sheet metal 311 and 313 is 0.46 λ
2, be shorter than half-wavelength slightly; Radiation sheet metal 312 and 314 length are 0.52 λ
2, be longer than half-wavelength slightly, wherein λ
1Be the wavelength of antenna first working frequency range, λ
2Be the wavelength of antenna second working frequency range, λ
1＜λ
2On the top end surface of column 30, an end of radiation sheet metal 311,312,313,314 is connected with the end that four radiation sheet metals 211,212,213,214 of column 20 are positioned at column 20 circumferential surfaces respectively.Thus formed medium loading helical antenna structure, between radiation sheet metal 211,212,213,214 and radiation sheet metal 311,312,313,314 all can produce 90 ° phase difference, so this antenna just can be at λ
1, λ
2Two working frequency range all have the ability that wide angle receives the circular polarization satellite-signal.
The concrete structure of antenna is as shown in Figure 6: column 20 is that 8.0 dielectric material is made by dielectric constant, and the electrical length of metal level 22 is 0.2 λ
1Column 30 is that 7.0 dielectric material is made by dielectric constant, and the electrical length of metal level 32 is 0.18 λ
2Column 30 is 1.6 with the diameter ratio of column 20, and height ratio is 1.47, and the top end surface of the top end surface of column 20 and column 30 is in same horizontal plane, and both fit tightly and form an overall structure;
Radiation sheet metal 211,212,213,214 extends according to helical-like path along the side of column 20, but they have different length, the pitch that radiation sheet metal 211 and 213 pitch are a bit larger tham radiation sheet metal 212 and 214 so just can be so that the length of radiation sheet metal 211 and 213 be 0.47 λ
1, be shorter than half-wavelength slightly; Radiation sheet metal 212 and 214 length are 0.54 λ
1, be longer than half-wavelength slightly.Radiation sheet metal 311,312,313,314 extends according to helical-like path along the side of column 30, but they have different length, the pitch that radiation sheet metal 311 and 313 pitch are a bit larger tham radiation sheet metal 312 and 314 makes that so the length of radiation sheet metal 311 and 313 is 0.47 λ
2, be shorter than half-wavelength slightly; Radiation sheet metal 312 and 314 length are 0.54 λ
2, be longer than half-wavelength slightly, wherein λ
1Be the wavelength of antenna first working frequency range, λ
2Be the wavelength of antenna second working frequency range, λ
1＜λ
2On the top end surface of column 30, an end of radiation sheet metal 311,312,313,314 is connected with four radiation sheet metals, 211,212,213,214 peripheral regions at column 20 of column 20 respectively.Thus formed medium loading helical antenna structure, between radiation sheet metal 211,212,213,214 and radiation sheet metal 311,312,313,314 all can produce 90 ° phase difference, so this antenna just can be at λ
1, λ
2Two working frequency range all have the ability that wide angle receives the circular polarization satellite-signal.
By the measured result of antenna as can be seen, the medium loading helical antenna structure that the utility model is made is not only at λ
1, λ
2Two working frequency range all show good circular polarization satellite-signal receiving ability, and by medium loading and complete barron structure design, not only the size of antenna is very little, even this antenna also keeps good directivity and circular polarization performance under hand-held and situation that human body is very close.Can be widely used in hand-held navigator or other satellite communication devices such as mobile phone, PDA.
The foregoing description is the utility model preferred implementation; but execution mode of the present utility model is not restricted to the described embodiments; anyly do not deviate from the change done under spirit of the present utility model and the principle, modification, substitute, combination, simplify; all should be the substitute mode of equivalence, be included within the protection range of the present utility model.
Claims (10)
1. a double-frequency band lamination medium loading helical antenna is characterized in that, comprising:
Two one thin one thick coaxial columns, its shaft core position is provided with a through hole; Described two column bottom end faces and bottom circumferential outer surface are equipped with metal level; Described thin column inserts from the top of described thick column, and fits tightly with it;
The top end surface of two described columns respectively is laid with four radiation sheet metals, one end of each described radiation sheet metal is radially extended by the center of two described columns respectively, after extending to its top periphery, again respectively at the circumferential surface of two described columns, according to helical-like path, extend to the described metal level place of its bottom circumferential outer surface vertically, and contact with described metal level; On the top end surface of described thin column, the relative surface end of per two adjacent radiation sheet metals is connected to each other, and forms two groups of antenna structures; The end that four radiation sheet metals on the described thin column contact with described thick column is connected with corresponding radiation sheet metal on the described thick column respectively on the surface on described thick column top;
In four radiation sheet metals on the described thin column, the length of two radiation sheet metals that the position is relative is greater than relative two radiation sheet metals in addition in position; In four radiation sheet metals on the described thick column, the length of two radiation sheet metals that the position is relative is greater than relative two radiation sheet metals in addition in position;
One coaxial cable, embed the bottom that described through hole is interior and described thick column is stretched out in the bottom, comprise an insulator, this insulator outer fringe surface is coated with a conduction shielding layer, this insulator center is provided with a feeding needle, the top of this feeding needle stretches out the top of described thin column, the top of described conduction shielding layer is connected with the end that one group of antenna structure of described thin column is positioned at thin column top, the top of described feeding needle is connected with the end that another group antenna structure of described thin column is positioned at thin column top, the corresponding section with the level of described conduction shielding layer of the metal level of described thick column bottom end face contacts, and the corresponding section with the level of described conduction shielding layer of the metal level of described thin column bottom end face contacts.
2. according to the described double-frequency band lamination medium loading helical antenna of claim 1, it is characterized in that described two columns are made by dielectric material.
3. according to the described double-frequency band lamination medium loading helical antenna of claim 1, it is characterized in that described thin column bottom circumferential outer surface has among the described thick column top of one section insertion of metal level.
4. according to the described double-frequency band lamination medium loading helical antenna of claim 1, it is characterized in that the top end surface of the top end surface of described thin column and described thick column is in same horizontal plane.
5. according to claim 1,3 or 4 described double-frequency band lamination medium loading helical antennas, it is characterized in that the described metal level that is positioned at thin column bottom circumferential outer surface, its electrical length h
1Be 1/8 λ
1＜h
1＜3/8 λ
1The described metal level that is positioned at thick column bottom circumferential outer surface, its electrical length h
2Be 1/8 λ
2＜h
2＜3/8 λ
2λ wherein
1Be the wavelength of antenna first working frequency range, λ
2Be the wavelength of antenna second working frequency range, λ
1＜λ
2
6. according to claim 1,3 or 4 described double-frequency band lamination medium loading helical antennas, it is characterized in that, four radiation sheet metals on the described thin column, wherein the length L of relative two radiation sheet metals in position is 1/2 λ
1＜L＜3/5 λ
1, the relative length L of two radiation sheet metals in addition in position is 2/5 λ
1＜L＜1/2 λ
1Four radiation sheet metals on the described thick column, wherein the length L of relative two radiation sheet metals in position is 1/2 λ
2＜L＜3/5 λ
2, the relative length L of two radiation sheet metals in addition in position is 2/5 λ
2＜L＜1/2 λ
2λ wherein
1Be the wavelength of antenna first working frequency range, λ
2Be the wavelength of antenna second working frequency range, λ
1＜λ
2
7. according to the described double-frequency band lamination medium loading helical antenna of claim 2, it is characterized in that described dielectric material is a ceramic material.
8. according to the described double-frequency band lamination medium loading helical antenna of claim 2, it is characterized in that described dielectric material is a macromolecular material.
9. according to the described double-frequency band lamination medium loading helical antenna of claim 2, it is characterized in that the relative dielectric constant ε of described dielectric material
r5.
10. according to claim 1 or 2 described double-frequency band lamination medium loading helical antennas, it is characterized in that described two columns are by DIELECTRIC CONSTANT
rThe column that different dielectric materials is made.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008200505167U CN201226373Y (en) | 2008-07-10 | 2008-07-10 | Double-frequency band laminated medium loading helical antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008200505167U CN201226373Y (en) | 2008-07-10 | 2008-07-10 | Double-frequency band laminated medium loading helical antenna |
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| Publication Number | Publication Date |
|---|---|
| CN201226373Y true CN201226373Y (en) | 2009-04-22 |
Family
ID=40599273
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008200505167U Expired - Lifetime CN201226373Y (en) | 2008-07-10 | 2008-07-10 | Double-frequency band laminated medium loading helical antenna |
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| CN (1) | CN201226373Y (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101316005B (en) * | 2008-07-10 | 2012-02-15 | 华南理工大学 | Double-frequency band lamination medium loading helical antenna |
| CN102931468A (en) * | 2012-11-16 | 2013-02-13 | 上海宇航系统工程研究所 | Double-frequency quadrifilar helix antenna |
| CN104466344A (en) * | 2014-12-15 | 2015-03-25 | 信维创科通信技术（北京）有限公司 | Single-port and dual-frequency dual-circularly polarized antenna |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101316005B (en) * | 2008-07-10 | 2012-02-15 | 华南理工大学 | Double-frequency band lamination medium loading helical antenna |
| CN102931468A (en) * | 2012-11-16 | 2013-02-13 | 上海宇航系统工程研究所 | Double-frequency quadrifilar helix antenna |
| CN102931468B (en) * | 2012-11-16 | 2015-03-11 | 上海宇航系统工程研究所 | Double-frequency quadrifilar helix antenna |
| CN104393400B (en) * | 2014-11-25 | 2017-02-22 | 重庆大学 | Circular polarization frequency express substation small antenna based on capacitive loading parasitic ring |
| CN104466344A (en) * | 2014-12-15 | 2015-03-25 | 信维创科通信技术（北京）有限公司 | Single-port and dual-frequency dual-circularly polarized antenna |
| CN104577315A (en) * | 2014-12-17 | 2015-04-29 | 华南理工大学 | Novel stack-based planar inverted-F antenna applied to human body implantable equipment |
| CN108091995A (en) * | 2018-01-25 | 2018-05-29 | 电信科学技术第研究所有限公司 | A kind of eight arm spiral circular polarisation dual-band antennas suitable for laser direct structuring technique |
| CN108091995B (en) * | 2018-01-25 | 2023-09-22 | 电信科学技术第一研究所有限公司 | Eight-arm spiral circular polarization dual-frequency antenna suitable for laser direct structuring technology |
| EP3522298A1 (en) * | 2018-02-06 | 2019-08-07 | Harris Solutions NY, Inc. | Dual band octafilar antenna |
| US10700428B2 (en) | 2018-02-06 | 2020-06-30 | Harris Solutions NY, Inc. | Dual band octafilar antenna |
| CN112615131A (en) * | 2020-11-20 | 2021-04-06 | 嘉兴佳利电子有限公司 | Method for optimizing performance of four-arm helical antenna |
| CN112615131B (en) * | 2020-11-20 | 2022-07-15 | 嘉兴佳利电子有限公司 | Method for optimizing performance of four-arm helical antenna |
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| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20090422 Effective date of abandoning: 20080710 |