WO2012122794A1 - Antenna and mimo antenna having the antenna - Google Patents

Antenna and mimo antenna having the antenna Download PDF

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Publication number
WO2012122794A1
WO2012122794A1 PCT/CN2011/080437 CN2011080437W WO2012122794A1 WO 2012122794 A1 WO2012122794 A1 WO 2012122794A1 CN 2011080437 W CN2011080437 W CN 2011080437W WO 2012122794 A1 WO2012122794 A1 WO 2012122794A1
Authority
WO
WIPO (PCT)
Prior art keywords
metal piece
antenna
metal
microgroove
feed line
Prior art date
Application number
PCT/CN2011/080437
Other languages
French (fr)
Chinese (zh)
Inventor
刘若鹏
徐冠雄
杨松涛
石小红
张洋洋
Original Assignee
深圳光启高等理工研究院
深圳光启创新技术有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from CN201110062188.9A external-priority patent/CN102683805B/en
Priority claimed from CN2011101451457A external-priority patent/CN102810734A/en
Priority claimed from CN2011101449372A external-priority patent/CN102800936A/en
Priority claimed from CN201110145005.XA external-priority patent/CN102800939B/en
Priority claimed from CN2011101451993A external-priority patent/CN102800945A/en
Priority claimed from CN201110145107.1A external-priority patent/CN103036015B/en
Priority claimed from CN2011101451673A external-priority patent/CN102800942A/en
Priority claimed from CN201110144982.8A external-priority patent/CN102800937B/en
Priority claimed from CN201110145181.3A external-priority patent/CN102891355B/en
Application filed by 深圳光启高等理工研究院, 深圳光启创新技术有限公司 filed Critical 深圳光启高等理工研究院
Publication of WO2012122794A1 publication Critical patent/WO2012122794A1/en

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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/36Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
    • H01Q1/38Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith formed by a conductive layer on an insulating support
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/36Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith

Definitions

  • Antenna and MIMO antenna having the same
  • the present invention relates to the field of communications, and in particular to an antenna and a MIMO antenna having the same.
  • the RF module mainly includes main components such as mixing, power amplifier, filtering, RF signal transmission, matching network and antenna.
  • the antenna acts as the radiating unit and receiving device of the final RF signal, and its working characteristics will directly affect the working performance of the entire electronic system.
  • important indicators such as antenna size, bandwidth, gain, and radiation efficiency are limited by basic physical principles (gain limits at fixed dimensions, bandwidth limits, etc.). The basic principle of the limits of these indicators makes antenna miniaturization technically far more difficult than other devices, and due to the complexity of electromagnetic field analysis of RF devices, approaching these limits has become a huge technical challenge.
  • the demand for multi-mode services is becoming more and more important in systems such as wireless communications, wireless access, satellite communications, and wireless data networks.
  • the demand for multimode services further increases the complexity of miniaturized antenna multimode designs.
  • multimode impedance matching of antennas has become a bottleneck in antenna technology.
  • MIMO multi-input and multi-output systems
  • conventional terminal communication antennas are mainly designed based on the radiation principle of electric monopoles or dipoles, such as the most commonly used planar anti-F antenna (PIFA).
  • PIFA planar anti-F antenna
  • the radiated operating frequency of a conventional antenna is directly related to the size of the antenna, and the bandwidth is positively correlated with the area of the antenna, so that the design of the antenna usually requires a physical length of half a wavelength.
  • additional impedance matching network design is required before feeding the antenna.
  • the impedance matching network additionally increases the feeder design of the electronic system and increases the RF.
  • the area of the system also matches the network and introduces a lot of energy loss. It is difficult to meet the system design requirements of low power consumption. Therefore, the miniaturized, multi-mode new antenna technology has become an important technical bottleneck of contemporary electronic integrated systems.
  • the antennas required to be designed must have strong adaptability. And versatility.
  • the original technology will encounter problems of versatility and performance differences in use.
  • a technical problem to be solved by the present invention is that there is a large difference in the working environment and electromagnetic characteristics of the antenna in different products, resulting in a large difference in antenna performance in design and use, and an antenna is provided, the antenna having Strong adaptability and versatility.
  • a technical solution adopted by the present invention to solve the technical problem is: providing an antenna, including a first dielectric substrate, a first feed line, and a first metal piece attached to a surface of the first dielectric substrate, wherein the first feed line is fed by a coupling method Into the first metal piece, the first metal piece is hollowed out with a first micro-groove structure to form a first metal trace on the first metal piece, and the antenna is pre-configured with a space for the electronic component to be embedded.
  • a technical solution adopted by the present invention to solve the technical problem is: providing a MIMO antenna, comprising: a plurality of antennas, each of the antennas comprising a first dielectric substrate, a first feed line, and a first surface attached to a surface of the first dielectric substrate a metal piece, the first feed line is fed into the first metal piece by coupling, and the first metal piece is hollowed out with a first micro-groove structure to form a metal trace on the first metal piece, and the antenna is pre-configured with a space for the electronic component to be embedded.
  • the space in which the electronic components are embedded can be fine-tuned by changing the performance of the embedded electronic components to design an antenna that satisfies the requirements of adaptability and versatility.
  • Figure 1 is a perspective structural view of a first embodiment of an antenna of the present invention
  • FIGS. 2 to 4 are schematic structural views of a second embodiment of the antenna of the present invention.
  • Figure 5 is a front perspective structural view of a third embodiment of the antenna of the present invention.
  • Figure 6 is a rear perspective structural view of a third embodiment of the antenna of the present invention.
  • Figure 7 is a perspective structural view of a fourth embodiment of the antenna of the present invention.
  • Figure 8 is a perspective structural view of a fifth embodiment of the antenna of the present invention.
  • Figure 9 is a front perspective structural view of a sixth embodiment of the antenna of the present invention.
  • FIG. 10 is a rear perspective structural view of a sixth embodiment of the antenna of the present invention.
  • FIG. 1 is a view of a side view of a first dielectric substrate of a seventh embodiment of the antenna of the present invention
  • FIG. 2 is a perspective view of a first dielectric substrate of a seventh embodiment of the antenna of the present invention; a structural view of a second dielectric substrate of the seventh embodiment;
  • FIG. 14 is a front perspective structural view of an eighth embodiment of the antenna of the present invention.
  • 16 is a schematic diagram of a complementary open resonant ring structure
  • 17 is a schematic view of a complementary spiral structure
  • ⁇ 8 is a schematic view of the structure of the open spiral ring
  • 19 is a schematic view of a double-open spiral ring structure
  • Figure 20 is a schematic view showing the structure of a complementary bending line
  • FIG. 21 is a schematic diagram showing the geometry of the complementary open resonant ring structure shown in FIG. 16;
  • FIG. 22 is a schematic exploded view of the complementary open resonant ring structure shown in FIG.
  • FIG. 23 is a schematic structural view of three complementary open resonant ring structures shown in FIG. 16;
  • FIG. 24 is a view showing two complementary open resonant ring structures shown in FIG. 16 and the complementary helical structure shown in FIG. Composite schematic
  • FIG. 25 is a schematic structural view of the four complementary open resonant ring structure arrays shown in FIG. 16.
  • a portion of the metal sheet drawing hatching is a metal wiring
  • a blank portion (a hollow portion) on the metal sheet indicates a microgroove structure.
  • feeders are also indicated by hatching.
  • Fig. 1 is a perspective structural view of a first embodiment of the present invention. In order to better describe the structure of the antenna of the present invention, Fig. 1 adopts a perspective view method.
  • the antenna 100 of the present invention includes a first dielectric substrate 1, a first feed line 2, and a first metal piece 4 attached to a surface of the first dielectric substrate 1.
  • the first feed line 2 is fed into the first through coupling.
  • the metal piece 4, the first metal piece 4 is hollowed out with a first micro-groove structure 41 to form a first metal trace 42 on the first metal piece, and the antenna 100 is pre-set with a space for the electronic component to be embedded.
  • the portion of the metal piece 4 on which the hatching is drawn is the first metal trace 42, and the blank portion (the hollow portion) on the first metal piece 4 indicates the first microgroove structure 41.
  • the first feed line 2 is also indicated by a hatching.
  • the first feed line 2 is disposed around the first metal piece 4 to effect signal coupling. Further, the first metal piece 4 may or may not be in contact with the first feed line 2. When the first metal piece 4 is in contact with the first feed line 2, the first feed line 2 is inductively coupled with the first metal piece 4, and when the first metal piece 4 is not in contact with the first feed line 2, the feed line 2 and the metal piece 4 Capacitive coupling between.
  • the space in which the predetermined electronic component is embedded in the antenna 100 is, for example, the space 51 on the first feeder 2, the space 53 between the first feeder 2 and the first metal piece 4, and the first metal trace 42.
  • the reserved position of the space on the antenna 100 of the present invention is not limited to the above five forms, and the space is only required to be disposed on the antenna.
  • the space may also be disposed on the first dielectric substrate 1.
  • the electronic component of the present invention is an inductive electronic component, a capacitive electronic component or a resistor. By incorporating such electronic components into the reserved space of the antenna, various performances of the antenna can be improved.
  • the purpose of embedding the inductive electronic component is to increase the inductance value of the internal resonant structure of the metal piece. Thereby adjusting the resonant frequency and working bandwidth of the antenna.
  • the resonant performance of the metal sheet can be altered by embedding capacitive electronic components to ultimately improve the Q value of the antenna and the resonant operating point.
  • resistors can be embedded to improve the radiation resistance of the antenna.
  • the number of embedded inductive electronic components, capacitors, or resistors, and the number of embedded antennas may be determined according to actual needs, which is not specifically limited in the present invention.
  • the inductance of the added inductive electronic component ranges from 0 to 5 uH. If too large an alternating signal is consumed by the inductive component, the radiation efficiency of the antenna is affected.
  • the capacitance value of the added capacitive electronic component is usually in the range of 0-2 pF, but the embedded capacitance value may exceed the range of 0-2 pF as the antenna operating frequency changes.
  • the antenna of the embodiment has good radiation characteristics of multiple frequency bands, and the five main radiation frequencies are distributed from 900 MHz to 5.5 GHz, covering almost GSM, CDMA, Bluetooth, W-Lan (IEEE 802.il protocol), GPS.
  • the main communication frequencies such as TD-LTE, have very high integration and can change the operating frequency of the antenna by adjusting the inductance value on the feeder.
  • the antenna performance parameters can be adjusted by adding electronic components with different parameters. Therefore, the antenna of the present invention can have the same structure without adding any components, only by adding different electronic components at different positions, and parameters of the electronic components (inductance value, resistance value, capacitance value) to realize different antennas. Performance parameters. That is: versatility is achieved and production costs can be significantly reduced.
  • the space of the present invention may be a pad or a vacancy.
  • the structure of the pad can be seen on the pad on a common board.
  • the design of its size will vary according to different needs.
  • the dielectric substrate is made of a ceramic material, a polymer material, a ferroelectric material, a ferrite material or a ferromagnetic material.
  • it is made of a polymer material, specifically, a polymer material such as FR-4 or F4B.
  • the metal piece is a copper piece or a silver piece. It is preferably a copper sheet, which is inexpensive and has good electrical conductivity.
  • the feeder is made of the same material as the metal piece, preferably copper.
  • PCB printed circuit board
  • RFID RFID is the abbreviation of Radio Frequency Identification, that is, radio frequency identification technology, commonly known as electronic label
  • processing method of conductive silver paste ink various types can be The flexible PCB processing of the deformation device, the processing method of the iron piece antenna, and the processing method of the combination of the iron piece and the PCB.
  • the combination of iron sheet and PCB processing means that the precise processing of the PCB is used to complete the processing of the antenna microgroove structure, and the iron piece is used to complete other auxiliary parts.
  • it can be processed by etching, electroplating, drilling, photolithography, electron engraving or ion engraving.
  • Fig. 2 is a perspective structural view of a second embodiment of the antenna of the present invention.
  • the main difference between this embodiment and the first embodiment is that, in the embodiment, the first metal piece 4 is further hollowed out with a third groove structure 43, wherein the first groove structure 41 and the third groove structure 43 are asymmetrically arranged.
  • the first microgroove structure 41 and the third microgroove structure 43 are asymmetrically arranged
  • Both the first microgroove structure 41 and the third microgroove structure 43 do not constitute an axisymmetric structure.
  • an axis of symmetry is not found on the surface a of the first microgroove structure 41 and the third microgroove structure 43 so that the first microgroove structure 41 and the third microgroove structure 43 are opposite to each other. Symmetrical axisymmetric setting.
  • the first groove structure 41 and the third groove structure 43 are asymmetric in structure, so the capacitance and inductance at the two positions are different, thereby generating at least two different resonance points, and the resonance point is not easily offset, Conducive to the antenna multi-mode.
  • the first groove structure 41 of the present invention may have the same structural form as the third groove structure 43, or may be different. And the degree of asymmetry of the first microgroove structure 41 and the third microgroove structure 43 can be adjusted as needed. This enables a rich, adjustable multimode resonance.
  • the present invention can also provide more microgroove structures on the same piece of metal as needed, so that the antenna has more than three different resonant frequencies.
  • the case where the asymmetry is set in the present invention may be at least several cases as shown in Figs. 2 to 4 .
  • Figure 2 shows the first case of an asymmetric structure.
  • the first microgroove structure 41 and the third microgroove structure 43 on the surface of the dielectric substrate a are both open spiral loop structures, and the first microgroove structure 41 and the third microgroove structure 43 are not in communication, but The difference in size results in asymmetry in the structure of the two, such that the antenna 100 has at least two resonant frequencies.
  • Figure 3 shows the second case of an asymmetric structure.
  • the first microgroove structure 41 and the third microgroove structure 43 on the surface of the dielectric substrate a are both open spiral ring structures and have the same size, the first microgroove structure 41 and the third microgroove.
  • the structure 43 is not in communication, but due to the positional arrangement of both the first microgroove structure 41 and the third trough structure 43, the asymmetry of the structures is caused.
  • Figure 4 shows the third case of an asymmetric structure.
  • the first microgroove structure 41 on the surface of the dielectric substrate a is a complementary spiral structure
  • the third microgroove structure 43 is an open spiral ring structure
  • the first microgroove structure 41 and the third microgroove structure 43 are not In common, it is apparent that the first microgroove structure 41 and the third microgroove structure 43 are asymmetrical.
  • the first groove structure 41 and the third groove The structure 43 can also achieve communication of the first groove structure 41 and the third groove structure 43 by hollowing out a new groove on the first metal piece 4. After the communication, the first groove structure 41 and the third groove structure 43 are still asymmetric structures, and therefore, the effect of the present invention is not greatly affected, and the antenna can be made to have at least two resonance frequencies.
  • a reserved space (not labeled) for embedding the electronic component is also disposed on the antenna, by adding different parameters in the reserved space ( The electronic components of the inductance value, the resistance value, and the capacitance value can adjust the antenna performance parameters, thereby improving the versatility of the antenna.
  • the reserved space may be disposed, for example, on the feeder, between the feeder and the metal sheet, on the metal trace, or on the first microgroove structure.
  • the arrangement principle and arrangement manner of the reserved space for embedding the electronic component are the same as those described in the foregoing first embodiment, and thus will not be described again.
  • FIG. 5 to 6 are schematic views showing the structure of a third embodiment of the antenna of the present invention, wherein Fig. 5 is a front (a) side perspective view of the third embodiment of the antenna of the present invention, and Fig. 6 is a rear (b side) perspective view thereof.
  • the main difference between the third embodiment and the second embodiment is that a metal piece and a feed line are further attached on the surface of the b opposite to the surface a of the dielectric substrate, and the metal piece and the feed line attached to the a surface and the b surface of the dielectric substrate
  • the structure is the same. That is, the projections of the first feed line 2, the first metal piece 4, the first micro-groove structure 41, and the third micro-slot structure 43 on the b-surface are respectively associated with the second feed line 8, the second metal piece 7, and the second on the b-surface.
  • the microgroove structure 71 and the fourth microgroove structure 72 are coincident, and the first feed line 2 and the second feed line 8 are electrically connected by a metallized through hole 10 opened on the first dielectric substrate 1.
  • a reserved space (not labeled) for embedding an electronic component is also disposed on the antenna, by adding different parameters in the reserved space ( The electronic components of the inductance value, the resistance value, and the capacitance value can adjust the antenna performance parameters, thereby improving the versatility of the antenna.
  • the reserved space may be disposed, for example, on the feeder, between the feeder and the metal sheet, on the metal trace, or on the first microgroove structure.
  • the setting principle and setting manner of the reserved space for embedding the electronic component are the same as those described in the foregoing first embodiment, and thus are no longer Narration.
  • FIG. 7 is a perspective structural view of a fourth embodiment of an antenna according to the present invention. As shown in FIG. 7, the fourth embodiment is different from the first embodiment in that, in this embodiment, the antenna 100 further includes a second The metal piece 3 and the second metal piece 3 are disposed opposite to the first metal piece 4 and are electrically connected to the first feed line 2.
  • the first metal piece 4 is disposed opposite to the second metal piece 3 with a medium therebetween, and the medium may be a high molecular polymer, a ceramic material or the like, or may be air.
  • the medium is air
  • the first feed line 2 and the second metal piece 3 are electrically connected by a wire.
  • the medium is a polymer or a ceramic material
  • the first feed line 2 and the second metal piece 3 form a metallization on the medium.
  • the through holes 9 are electrically connected to each other.
  • the medium is made of polytetrafluoroethylene (FR-4) and the second metal piece 3 and the first feed line 2 are electrically connected through the metallized through holes 9.
  • FR-4 polytetrafluoroethylene
  • the electromagnetic wave of the low frequency band corresponds to a longer wavelength.
  • the length of the electric radiation of the antenna feed line is increased to make the length of the feed line longer, which is disadvantageous to the miniaturization of the antenna as a whole and is long.
  • the feeder causes the feeder loss to increase, which causes the antenna performance to degrade.
  • the antenna 100 of the present invention solves the above problem of the existing antenna by adding the second metal piece 3.
  • the problem is solved by the principle that the second metal piece 3 is capacitively coupled with the first metal piece 4, and is applied to the first metal piece 4.
  • the formed first microgroove structure 41 is coupled to feed.
  • the second metal piece 3 is coupled to the first micro-slot structure 41 formed on the first metal piece 4 to effectively reduce the coupling of the first micro-slot structure 41 formed on the first metal piece 4 by the first feed line 2 demand. Therefore, when the antenna 100 operates in the low frequency band, it is not necessary to increase the length of the first feeder 2, and the area of the second metal sheet 3 coupled with the feeding is easy to adjust, and the second metal sheet 3 is coupled and fed only for the different working frequency bands. The area is fine.
  • a reserved space (not labeled) for embedding an electronic component is also disposed on the antenna, by adding different parameters (inductance value, The electronic components of the resistance value and the capacitance value can adjust the antenna performance parameters, thereby improving the versatility of the antenna.
  • the reserved space may be disposed, for example, on the feeder, between the feeder and the metal sheet, on the metal trace, or on the first microgroove structure.
  • the setting principle and setting manner of the reserved space for embedding the electronic component are the same as those described in the foregoing first embodiment, and thus will not be described herein. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
  • FIG. 8 is a perspective structural view of a fifth embodiment of the antenna of the present invention.
  • the antenna 100 further includes a second dielectric substrate 5 covering the first metal piece 4.
  • the antenna 100 since the metal piece 4 is located between the first dielectric substrate 1 and the second dielectric substrate 5, the antenna 100 needs to pass through the second dielectric substrate 5 when receiving or transmitting electromagnetic waves, thereby making the antenna 100 as a whole.
  • the distributed capacitance increases, and the increase of the distributed capacitance can effectively reduce the operating frequency of the antenna. Therefore, the antenna can still work well at low frequencies without changing the length of the feeder, satisfying the requirements of small antenna size, low operating frequency and wideband multimode. .
  • a reserved space (not labeled) for embedding the electronic component is also disposed on the antenna, by adding different parameters (inductance value, The electronic components of the resistance value and the capacitance value can adjust the antenna performance parameters, thereby improving the versatility of the antenna.
  • the reserved space may be disposed, for example, on the feeder, between the feeder and the metal sheet, on the metal trace, or on the first microgroove structure.
  • the setting principle and setting manner of the reserved space for embedding the electronic component are the same as those described in the foregoing first embodiment, and thus will not be described herein.
  • FIG. 9 is a detailed front view of a fifth embodiment of the antenna of the present invention
  • FIG. 10 is a front perspective view of the fifth embodiment of the antenna of the present invention. Structure diagram.
  • the sixth embodiment is different from the first embodiment in that, in this embodiment, the antenna 100 further includes a second metal piece 7, and the second metal piece 7 is attached to the first dielectric substrate 1 and a surface (b surface), a second feed line 8 is disposed around the second metal piece 7, the second feed line 8 is fed into the second metal piece 7 by coupling, and the second metal piece 7 is hollowed out with the second micro groove structure 71 to A second metal trace 72 is formed on the second metal piece 7, and the first feed line 2 is electrically connected to the second feed line 8.
  • the first feed line 2 and the second feed line 8 are electrically connected by a metallized through hole 10 opened in the first dielectric substrate 1.
  • a second metal strip 7 disposed on the other surface of the first dielectric substrate 1 and a second metal strip 7 disposed on the other surface of the first dielectric substrate 1 are added to the first embodiment.
  • This design is equivalent to increasing the physical length of the antenna. (The actual length does not increase;), so that the RF antenna operating at very low operating frequencies can be designed in a very small space. Solve the physical limitation of the controlled space area of the antenna when the traditional antenna operates at low frequencies.
  • the structures attached to the a surface and the b surface of the first dielectric substrate 1 are the same, that is, the first feed line 2 and the first metal piece 4 are The projection of the b surface coincides with the second feed line 8 and the second metal piece 7, respectively.
  • a reserved space (not labeled) for embedding the electronic component is also disposed on the antenna, by adding different parameters in the reserved space ( The electronic components of the inductance value, the resistance value, and the capacitance value can adjust the antenna performance parameters, thereby improving the versatility of the antenna.
  • the reserved space may be disposed, for example, on the feeder, between the feeder and the metal sheet, on the metal trace, or on the first microgroove structure.
  • the arrangement principle and arrangement manner of the reserved space for embedding the electronic component are the same as those described in the foregoing first embodiment, and thus will not be described herein.
  • FIG. 11 is a perspective view of the first dielectric substrate of the seventh embodiment of the antenna of the present invention
  • FIG. 12 is the antenna of the present invention
  • FIG. 13 is a structural view of a second dielectric substrate 2 of a seventh embodiment of the antenna of the present invention.
  • the present embodiment provides the following improvements on the basis of the sixth embodiment: a second dielectric substrate 2 is disposed, and the surface of the second dielectric substrate 2 coincides with the surface A of the first dielectric substrate 1, The other surface of the two dielectric substrates 2 that is not overlapped with the first dielectric substrate 1 is provided with a third metal piece 30.
  • a metallized via 23 is formed on the second dielectric substrate 2, and the metal via 23 electrically connects the second feed line 2 and the third metal piece 30. Since the area of the coupling feeding of the third metal piece 30 is easy to adjust, it is only necessary to adjust the coupling feeding area of the third metal piece 30 for the different working frequency bands.
  • the antenna is also disposed.
  • the antenna performance parameters can be adjusted, thereby improving the antenna. Universality.
  • the reserved space may be disposed, for example, on the feeder, between the feeder and the metal sheet, on the metal trace, or on the first microgroove structure.
  • the setting principle and setting manner of the reserved space for embedding the electronic component are the same as those described in the foregoing first embodiment, and thus will not be described herein.
  • Fig. 14 is a front perspective view of the eighth embodiment of the antenna of the present invention
  • Fig. 15 is a rear perspective view of the eighth embodiment of the antenna of the present invention. Structure diagram.
  • the eighth embodiment is improved on the basis of the seventh embodiment described above: further recessed on the first metal piece 4 has a third microgroove structure 43, the third microgroove structure 43 and the first The microgroove structure 41 is asymmetrically disposed.
  • the first microgroove structure 41 and the third microgroove structure 43 form a first metal trace 42 on the first metal piece 4, and the second metal strip 7 is further hollowed out to have a fourth microgroove structure.
  • the second microgroove structure 71 and the fourth microgroove structure 73 form a second metal trace 72 on the second metal piece 7.
  • the asymmetrical arrangement described above is specifically described in the second embodiment of the present invention, and is not described herein again.
  • the technical effect is that at least two different resonance points can be generated, and the resonance point is not easily offset. , is conducive to the rich multi-mode of the antenna.
  • a reserved space (not labeled) for embedding an electronic component is also disposed on the antenna, by adding different parameters in the reserved space ( The electronic components of the inductance value, the resistance value, and the capacitance value can adjust the antenna performance parameters, thereby improving the versatility of the antenna.
  • the reserved space may be disposed, for example, on the feeder, between the feeder and the metal sheet, on the metal trace, or on the first microgroove structure.
  • the setting principle and setting manner of the reserved space for embedding the electronic component are the same as those described in the foregoing first embodiment, and thus will not be described herein.
  • the microgroove structure may be the complementary open resonant ring structure shown in FIG. 16, the complementary spiral structure shown in FIG. 17, and the open spiral shown in FIG.
  • One of the ring structure, the double-open spiral ring structure shown in FIG. 19, and the complementary bent line structure shown in FIG. 20 is derived from one of the foregoing structures, a plurality of structural composites or a The microgroove structure obtained by the structural array.
  • geometric derivation refers to structural derivation with similar functions and different shapes, for example, derived from a box-like structure to a curve-like structure. , triangle class structure and other different polygon class structures.
  • the extended derivative here is to open a new groove on the basis of FIG. 16 to FIG. 20 to form a new groove structure; taking the complementary open resonant ring structure shown in FIG. 16 as an example, FIG. 21 is a schematic diagram of the geometrical derivative thereof.
  • Figure 22 is a schematic representation of its geometry.
  • the composite here means that the microgroove structures of FIGS. 16 to 20 are superposed to form a new microgroove structure, as shown in FIG. 23, after the composite of the complementary open resonant ring structures shown in FIG.
  • Schematic diagram of the structure as shown in FIG. 24, a schematic structural view of the complementary open resonant ring structure shown in FIG. 16 and the complementary spiral structure shown in FIG.
  • the array here refers to a plurality of groove structures formed on the same metal sheet by a plurality of groove structures shown in FIG. 16 to FIG. 20, and as shown in FIG. 25, a plurality of complementary openings as shown in FIG. Schematic diagram of the structure after the resonant ring structure array.
  • the invention has been described by taking the open spiral ring structure shown in Fig. 18 as an example.
  • the present invention also provides a MIMO antenna, which is composed of a plurality of antennas disclosed in any one of the above one to seven embodiments.
  • a MIMO antenna On a MIMO antenna, each antenna is simultaneously transmitted and received simultaneously.
  • the MIMO antenna can greatly increase the information throughput and transmission distance of the system without increasing the bandwidth or total transmission power loss.
  • the MIMO antenna of the present invention also has high isolation and strong anti-interference ability between multiple antennas.
  • the first feeder of each antenna is electrically connected to the second feeder and then connected to a receiver/transmitter, and all the receivers/transmitters are connected to a baseband signal processor.

Abstract

Disclosed is an antenna comprising a first dielectric substrate, a first feeder cable, and a first metal sheet attached to a surface of the first dielectric substrate. The first feeder cable is fed into the first metal sheet by coupling. The first metal sheet has engraved thereon a first micro-groove structure to form on the first metal sheet a first metal trace. The antenna is pre-provided with a space for embedding an electronic component. Also provided is an MIMO antenna comprising a plurality of the antenna. In the present invention, by providing in the antenna the space for embedding the electronic component, the performance of the antenna can be fine-tuned by modifying the performance of the embedded electronic component, thus producing antennae that satisfy the requirements of adaptability and versatility.

Description

天线及具有该天线的 MIMO天线  Antenna and MIMO antenna having the same
【技术领域】  [Technical Field]
本发明属于通信领域,具体地, 涉及一种天线及具有该天线的 MIMO天线。  The present invention relates to the field of communications, and in particular to an antenna and a MIMO antenna having the same.
【背景技术】 【Background technique】
随着半导体工艺的高度发展, 对当今的电子系统集成度提出了越来越高的 要求, 器件的小型化成为了整个产业非常关注的技术问题。 然而, 不同于 IC芯 片遵循 "摩尔定律"的发展,作为电子系统的另外重要组成一一射频模块,却面临 着器件小型化的高难度技术挑战。 射频模块主要包括了混频、 功放、 滤波、 射 频信号传输、 匹配网络与天线等主要器件。 其中, 天线作为最终射频信号的辐 射单元和接收器件, 其工作特性将直接影响整个电子系统的工作性能。 然而天 线的尺寸、 带宽、 增益、 辐射效率等重要指标却受到了基本物理原理的限制(固 定尺寸下的增益极限、 带宽极限等)。 这些指标极限的基本原理使得天线的小型 化技术难度远远超过了其它器件, 而由于射频器件的电磁场分析的复杂性, 逼 近这些极限值都成为了巨大的技术挑战。  With the rapid development of semiconductor technology, higher and higher requirements have been placed on the integration of electronic systems today, and the miniaturization of devices has become a technical issue of great concern to the entire industry. However, unlike IC chips, which follow the development of Moore's Law, as an important component of electronic systems, RF modules face the difficult technical challenges of miniaturization of devices. The RF module mainly includes main components such as mixing, power amplifier, filtering, RF signal transmission, matching network and antenna. Among them, the antenna acts as the radiating unit and receiving device of the final RF signal, and its working characteristics will directly affect the working performance of the entire electronic system. However, important indicators such as antenna size, bandwidth, gain, and radiation efficiency are limited by basic physical principles (gain limits at fixed dimensions, bandwidth limits, etc.). The basic principle of the limits of these indicators makes antenna miniaturization technically far more difficult than other devices, and due to the complexity of electromagnetic field analysis of RF devices, approaching these limits has become a huge technical challenge.
同时, 随着现代电子系统的复杂化, 多模服务的需求在无线通信、 无线接 入、 卫星通信、 无线数据网络等系统中变得越来越重要。 而多模服务的需求进 一步增大了小型化天线多模设计的复杂度。 除去小型化的技术挑战, 天线的多 模阻抗匹配也成为了天线技术的瓶颈。 另一方面, 多输入多输出系统( MIMO ) 在无线通信、 无线数据服务领域的高速发展更进一步苛刻地要求了天线尺寸的 小型化并同时保证良好的隔离度、 辐射性能以及抗干扰能力。 然而, 传统的终 端通信天线主要基于电单极子或偶极子的辐射原理进行设计, 比如最常用的平 面反 F天线 (PIFA)。 传统天线的辐射工作频率直接和天线的尺寸正相关, 带宽 和天线的面积正相关, 使得天线的设计通常需要半波长的物理长度。 在一些更 为复杂的电子系统中, 天线需要多模工作, 就需要在馈入天线前额外的阻抗匹 配网络设计。 但阻抗匹配网络额外的增加了电子系统的馈线设计、 增大了射频 系统的面积同时匹配网络还引入了不少的能量损耗, ^艮难满足低功耗的系统设 计要求。 因此, 小型化、 多模式的新型天线技术成为了当代电子集成系统的一 个重要技术瓶颈。 At the same time, with the complication of modern electronic systems, the demand for multi-mode services is becoming more and more important in systems such as wireless communications, wireless access, satellite communications, and wireless data networks. The demand for multimode services further increases the complexity of miniaturized antenna multimode designs. In addition to the technical challenges of miniaturization, multimode impedance matching of antennas has become a bottleneck in antenna technology. On the other hand, the rapid development of multi-input and multi-output systems (MIMO) in the field of wireless communication and wireless data services has further demanded the miniaturization of antenna sizes while ensuring good isolation, radiation performance and anti-interference ability. However, conventional terminal communication antennas are mainly designed based on the radiation principle of electric monopoles or dipoles, such as the most commonly used planar anti-F antenna (PIFA). The radiated operating frequency of a conventional antenna is directly related to the size of the antenna, and the bandwidth is positively correlated with the area of the antenna, so that the design of the antenna usually requires a physical length of half a wavelength. In some more complex electronic systems, where the antenna requires multimode operation, additional impedance matching network design is required before feeding the antenna. However, the impedance matching network additionally increases the feeder design of the electronic system and increases the RF. The area of the system also matches the network and introduces a lot of energy loss. It is difficult to meet the system design requirements of low power consumption. Therefore, the miniaturized, multi-mode new antenna technology has become an important technical bottleneck of contemporary electronic integrated systems.
同时, 天线在不同的产品中工作的环境及电磁特性存在较大的差异性, 将 会导致天线性能在设计和使用中存在较大的差异, 所以要求设计出的天线必须 具有较强的适应性及通用性。 综上所述, 原有的技术在使用中将就会遇到通用 性及性能差异性的问题。  At the same time, there are large differences in the environment and electromagnetic characteristics of the antennas operating in different products, which will result in large differences in antenna performance in design and use. Therefore, the antennas required to be designed must have strong adaptability. And versatility. In summary, the original technology will encounter problems of versatility and performance differences in use.
【发明内容】 [Summary of the Invention]
本发明要解决的一个技术问题是, 针对天线在不同产品中工作环境及电磁 特性存在较大的差异性, 导致天线性能在设计和使用中存在较大的差异, 提供 一种天线, 该天线具有较强的适应性及通用性。  A technical problem to be solved by the present invention is that there is a large difference in the working environment and electromagnetic characteristics of the antenna in different products, resulting in a large difference in antenna performance in design and use, and an antenna is provided, the antenna having Strong adaptability and versatility.
本发明为解决技术问题而采用的一个技术方案是: 提供一种天线, 包括第 一介质基板、 第一馈线、 附着在第一介质基板一表面的第一金属片, 第一馈线 通过耦合方式馈入第一金属片, 第一金属片上镂空有第一微槽结构以在第一金 属片上形成第一金属走线, 天线预设有供电子元件嵌入的空间。  A technical solution adopted by the present invention to solve the technical problem is: providing an antenna, including a first dielectric substrate, a first feed line, and a first metal piece attached to a surface of the first dielectric substrate, wherein the first feed line is fed by a coupling method Into the first metal piece, the first metal piece is hollowed out with a first micro-groove structure to form a first metal trace on the first metal piece, and the antenna is pre-configured with a space for the electronic component to be embedded.
本发明为解决技术问题而采用的一个技术方案是: 提供一种 MIMO天线, 包括多个天线, 每一该天线包括第一介质基板、 第一馈线、 附着在第一介质基 板一表面的第一金属片, 第一馈线通过耦合方式馈入第一金属片, 第一金属片 上镂空有第一微槽结构以在第一金属片上形成金属走线, 天线预设有供电子元 件嵌入的空间 置供电子元件嵌入的空间, 可以通过改变嵌入的电子元件的性能对天线的性能 进行微调, 设计出满足适应性及通用性的要求的天线。 【附图说明】 A technical solution adopted by the present invention to solve the technical problem is: providing a MIMO antenna, comprising: a plurality of antennas, each of the antennas comprising a first dielectric substrate, a first feed line, and a first surface attached to a surface of the first dielectric substrate a metal piece, the first feed line is fed into the first metal piece by coupling, and the first metal piece is hollowed out with a first micro-groove structure to form a metal trace on the first metal piece, and the antenna is pre-configured with a space for the electronic component to be embedded. The space in which the electronic components are embedded can be fine-tuned by changing the performance of the embedded electronic components to design an antenna that satisfies the requirements of adaptability and versatility. [Description of the Drawings]
图 1是本发明天线的第一实施例的立体结构图;  Figure 1 is a perspective structural view of a first embodiment of an antenna of the present invention;
图 2至图 4是本发明天线的第二实施例的的结构示意图;  2 to 4 are schematic structural views of a second embodiment of the antenna of the present invention;
图 5是本发明的天线第三实施例的正面立体结构图;  Figure 5 is a front perspective structural view of a third embodiment of the antenna of the present invention;
图 6是本发明的天线第三实施例的背面立体结构图;  Figure 6 is a rear perspective structural view of a third embodiment of the antenna of the present invention;
图 7是本发明的天线第四实施例的立体结构图;  Figure 7 is a perspective structural view of a fourth embodiment of the antenna of the present invention;
图 8是本发明的天线第五实施例的立体结构图;  Figure 8 is a perspective structural view of a fifth embodiment of the antenna of the present invention;
图 9是本发明的天线第六实施例的正面立体结构图;  Figure 9 is a front perspective structural view of a sixth embodiment of the antenna of the present invention;
10是本发明的天线第六实施例的背面立体结构图;  10 is a rear perspective structural view of a sixth embodiment of the antenna of the present invention;
1是本发明的天线第七实施例的第一介质基板的 A面视角结构图; ί2是本发明的天线第七实施例的第一介质基板的 Β面视角结构图; 是本发明的天线第七实施例的第二介质基板的结构图;  1 is a view of a side view of a first dielectric substrate of a seventh embodiment of the antenna of the present invention; FIG. 2 is a perspective view of a first dielectric substrate of a seventh embodiment of the antenna of the present invention; a structural view of a second dielectric substrate of the seventh embodiment;
14是本发明的天线第八实施例的正面立体结构图;  14 is a front perspective structural view of an eighth embodiment of the antenna of the present invention;
是本发明的天线第八实施例的背面立体结构图;  Is a rear perspective structural view of an eighth embodiment of the antenna of the present invention;
16为互补式开口谐振环结构的示意图;  16 is a schematic diagram of a complementary open resonant ring structure;
17所示为互补式螺旋线结构的示意图;  17 is a schematic view of a complementary spiral structure;
ί 8所示为开口螺旋环结构的示意图;  ί 8 is a schematic view of the structure of the open spiral ring;
19所示为双开口螺旋环结构的示意图;  19 is a schematic view of a double-open spiral ring structure;
图 20所示为互补式弯折线结构的示意图;  Figure 20 is a schematic view showing the structure of a complementary bending line;
图 21为图 16所示的互补式开口谐振环结构其几何形状衍生示意图; 图 22为图 16所示的互补式开口谐振环结构其扩展衍生示意图;  21 is a schematic diagram showing the geometry of the complementary open resonant ring structure shown in FIG. 16; FIG. 22 is a schematic exploded view of the complementary open resonant ring structure shown in FIG.
图 23为三个图 16所示的互补式开口谐振环结构的复合后的结构示意图; 图 24为两个图 16所示的互补式开口谐振环结构与图 17所示互补式螺旋线 结构的复合示意图;  23 is a schematic structural view of three complementary open resonant ring structures shown in FIG. 16; FIG. 24 is a view showing two complementary open resonant ring structures shown in FIG. 16 and the complementary helical structure shown in FIG. Composite schematic
图 25为四个图 16所示的互补式开口谐振环结构组阵后的结构示意图。 【具体实施方式】 FIG. 25 is a schematic structural view of the four complementary open resonant ring structure arrays shown in FIG. 16. FIG. 【detailed description】
本发明实施例的相关附图中, 说明如下: 金属片画剖面线的部分为金属走 线, 金属片上的空白部分(镂空的部分)表示微槽结构。 另外, 馈线也用剖面 线表示。  In the related drawings of the embodiments of the present invention, the following description is made as follows: a portion of the metal sheet drawing hatching is a metal wiring, and a blank portion (a hollow portion) on the metal sheet indicates a microgroove structure. In addition, feeders are also indicated by hatching.
首先参见图 1对本发明的第一实施例作出具体介绍, 其中, 图 1是本发明 第一实施例的立体结构图。 为了更好的描述本发明的天线的结构, 图 1 采用透 视图画法。  First, a first embodiment of the present invention will be specifically described with reference to Fig. 1. Fig. 1 is a perspective structural view of a first embodiment of the present invention. In order to better describe the structure of the antenna of the present invention, Fig. 1 adopts a perspective view method.
如图 1所示, 本发明的天线 100包括第一介质基板 1、 第一馈线 2、 附着在 第一介质基板 1一表面的第一金属片 4,第一馈线 2通过耦合方式馈入第一金属 片 4, 第一金属片 4上镂空有第一微槽结构 41以在第一金属片上形成第一金属 走线 42, 天线 100预设有供电子元件嵌入的空间。  As shown in FIG. 1, the antenna 100 of the present invention includes a first dielectric substrate 1, a first feed line 2, and a first metal piece 4 attached to a surface of the first dielectric substrate 1. The first feed line 2 is fed into the first through coupling. The metal piece 4, the first metal piece 4 is hollowed out with a first micro-groove structure 41 to form a first metal trace 42 on the first metal piece, and the antenna 100 is pre-set with a space for the electronic component to be embedded.
在图 1中, 金属片 4上的画剖面线的部分为第一金属走线 42, 第一金属片 4上的空白部分(镂空的部分)表示第一微槽结构 41。 另外, 第一馈线 2也用 剖面线表示。  In Fig. 1, the portion of the metal piece 4 on which the hatching is drawn is the first metal trace 42, and the blank portion (the hollow portion) on the first metal piece 4 indicates the first microgroove structure 41. In addition, the first feed line 2 is also indicated by a hatching.
第一馈线 2围绕第一金属片 4设置以实现信号耦合。 另外第一金属片 4与 第一馈线 2可以接触, 也可以不接触。 当第一金属片 4与第一馈线 2接触时, 第一馈线 2与第一金属片 4之间感性耦合, 当第一金属片 4与第一馈线 2不接 触时, 馈线 2与金属片 4之间容性耦合。  The first feed line 2 is disposed around the first metal piece 4 to effect signal coupling. Further, the first metal piece 4 may or may not be in contact with the first feed line 2. When the first metal piece 4 is in contact with the first feed line 2, the first feed line 2 is inductively coupled with the first metal piece 4, and when the first metal piece 4 is not in contact with the first feed line 2, the feed line 2 and the metal piece 4 Capacitive coupling between.
本实施例中, 天线 100上预设的供电子元件嵌入的空间例如为第一馈线 2 上的空间 51 , 第一馈线 2与第一金属片 4之间的空间 53 , 第一金属走线 42上 的空间 55、 56, 第一微槽结构 41上的空间 57。  In this embodiment, the space in which the predetermined electronic component is embedded in the antenna 100 is, for example, the space 51 on the first feeder 2, the space 53 between the first feeder 2 and the first metal piece 4, and the first metal trace 42. The upper space 55, 56, the space 57 on the first microgroove structure 41.
当然, 本发明的天线 100上空间的预留位置并不限于上述五种形式, 空间 只要设置在天线上即可。 例如, 空间还可以设置在第一介质基板 1上。  Of course, the reserved position of the space on the antenna 100 of the present invention is not limited to the above five forms, and the space is only required to be disposed on the antenna. For example, the space may also be disposed on the first dielectric substrate 1.
本发明的所述电子元件为感性电子元件、 容性电子元件或者电阻。 在天线 的预留空间中加入此类电子元件后, 可以改善天线的各种性能。  The electronic component of the present invention is an inductive electronic component, a capacitive electronic component or a resistor. By incorporating such electronic components into the reserved space of the antenna, various performances of the antenna can be improved.
具体而言, 嵌入感性电子元件的目的是增加金属片内部谐振结构的电感值, 从而对天线的谐振频率及工作带宽起到调节的作用。 Specifically, the purpose of embedding the inductive electronic component is to increase the inductance value of the internal resonant structure of the metal piece. Thereby adjusting the resonant frequency and working bandwidth of the antenna.
运用公式: f=l/ ( 2ji ^^ ) , 可知电感值的大小和工作频率的平方成反比, 电容值的大小和工作频率的平方成反比, 所以当天线需要的工作频率为较低工 作频率时, 通过适当的嵌入电感或感性电子元件实现。  Using the formula: f=l/ ( 2ji ^^ ), it can be seen that the magnitude of the inductance is inversely proportional to the square of the operating frequency. The magnitude of the capacitance is inversely proportional to the square of the operating frequency, so when the antenna requires a lower operating frequency This is achieved by appropriate embedded inductors or inductive electronic components.
类似的, 可以通过嵌入容性电子元件改变金属片的谐振性能, 以最终改善 天线的 Q值及谐振工作点。  Similarly, the resonant performance of the metal sheet can be altered by embedding capacitive electronic components to ultimately improve the Q value of the antenna and the resonant operating point.
我们知道,通频带 BW与谐振频率 w0和品质因数 Q的关系为: BW=wo/Q , 此式表明, Q越大则通频带越窄, Q越小则通频带越宽。另有: Q=wL/R=l/wRC , 其中, Q是品质因素; w是电路谐振时的电源频率; L是电感; R是串的电阻; C是电容 , 由 Q=wL/R=l/wRC公式可知, Q和 C呈反比, 因此, 可以通过加 入容性电子元件来减小 Q值, 使通频带变宽。  We know that the relationship between the passband BW and the resonant frequency w0 and the quality factor Q is: BW=wo/Q. This equation shows that the larger the Q, the narrower the passband, and the smaller the Q, the wider the passband. Another: Q=wL/R=l/wRC, where Q is the quality factor; w is the power frequency of the circuit resonance; L is the inductance; R is the resistance of the string; C is the capacitance, by Q=wL/R= The l/wRC formula shows that Q and C are inversely proportional. Therefore, the Q value can be reduced by adding capacitive electronic components to widen the passband.
除了嵌入电感和 /或电容, 还可以嵌入电阻, 改善天线的辐射电阻。  In addition to embedding inductors and / or capacitors, resistors can be embedded to improve the radiation resistance of the antenna.
当然, 馈线上的空间也可以是多个, 其中分别嵌入电阻以及感性电子元件, 既实现了工作频率的调节, 又能改善天线的辐射电阻。 此外, 未加入电子元件 的空间可用导线短接。  Of course, there may be multiple spaces on the feeder line, in which resistors and inductive electronic components are respectively embedded, which not only realizes the adjustment of the operating frequency, but also improves the radiation resistance of the antenna. In addition, the space where no electronic components are added can be shorted by wires.
实际中, 天线上是嵌入感性电子元件、 电容还是电阻, 以及嵌入的个数, 则可以根据实际需要而定, 本发明对此不做具体限定。  In practice, the number of embedded inductive electronic components, capacitors, or resistors, and the number of embedded antennas may be determined according to actual needs, which is not specifically limited in the present invention.
本实施例中, 加入的感性电子元件的电感值范围在 0-5uH之间, 若太大交 变信号将会被感性元件消耗从而影响到天线的辐射效率。  In this embodiment, the inductance of the added inductive electronic component ranges from 0 to 5 uH. If too large an alternating signal is consumed by the inductive component, the radiation efficiency of the antenna is affected.
本实施例中,加入的容性电子元件的电容值范围通常在 0-2pF之间, 不过随 着天线工作频率的变化嵌入的电容值也可能超出 0-2pF的范围。  In this embodiment, the capacitance value of the added capacitive electronic component is usually in the range of 0-2 pF, but the embedded capacitance value may exceed the range of 0-2 pF as the antenna operating frequency changes.
本实施例的所述天线具有多个频段的良好辐射特性, 五个主要辐射频率从 900MHz—直分布到 5.5GHz,几乎涵盖了 GSM、CDMA、蓝牙、 W-Lan( IEEE802. i l 协议)、 GPS、 TD-LTE 等各个主要的通信频率, 具有非常高的集成度且可通过 对馈线上的电感值进行调节达到改变天线工作频率的目的。 本发明中, 通过加入不同参数的电子元件, 可以实现天线性能参数的可调。 因此, 本发明的天线在不加入任何元件之前可以是一样的结构, 只是通过在不 同位置加入不同的电子元件, 以及电子元件的参数(电感值、 电阻值、 电容值), 来实现不同天线的性能参数。 即: 实现了通用性, 可以大幅降低生产成本。 The antenna of the embodiment has good radiation characteristics of multiple frequency bands, and the five main radiation frequencies are distributed from 900 MHz to 5.5 GHz, covering almost GSM, CDMA, Bluetooth, W-Lan (IEEE 802.il protocol), GPS. The main communication frequencies, such as TD-LTE, have very high integration and can change the operating frequency of the antenna by adjusting the inductance value on the feeder. In the present invention, the antenna performance parameters can be adjusted by adding electronic components with different parameters. Therefore, the antenna of the present invention can have the same structure without adding any components, only by adding different electronic components at different positions, and parameters of the electronic components (inductance value, resistance value, capacitance value) to realize different antennas. Performance parameters. That is: versatility is achieved and production costs can be significantly reduced.
本发明的所述空间可以是焊盘, 也可以是一个空缺。 焊盘的结构可以参见 普通的电路板上的焊盘。 当然, 其尺寸的设计根据不同的需要会有所不同。  The space of the present invention may be a pad or a vacancy. The structure of the pad can be seen on the pad on a common board. Of course, the design of its size will vary according to different needs.
另外, 本发明中, 介质基板由陶瓷材料、 高分子材料、 铁电材料、 铁氧材 料或铁磁材料制成。 优选地, 由高分子材料制成, 具体地可以是 FR-4、 F4B等 高分子材料。  Further, in the present invention, the dielectric substrate is made of a ceramic material, a polymer material, a ferroelectric material, a ferrite material or a ferromagnetic material. Preferably, it is made of a polymer material, specifically, a polymer material such as FR-4 or F4B.
本发明中, 金属片为铜片或银片。 优选为铜片, 价格低廉, 导电性能好。 本发明中, 馈线选用与金属片同样的材料制成, 优选为铜。  In the present invention, the metal piece is a copper piece or a silver piece. It is preferably a copper sheet, which is inexpensive and has good electrical conductivity. In the present invention, the feeder is made of the same material as the metal piece, preferably copper.
本发明中, 关于天线的加工制造, 只要满足本发明的设计原理, 可以采用 各种制造方式。最普通的方法是使用各类印刷电路板(PCB )的制造方法, 当然, 金属化的通孔, 双面覆铜的 PCB制造也能满足本发明的加工要求。 除此加工方 式, 还可以根据实际的需要引入其它加工手段, 比如 RFID ( RFID 是 Radio Frequency Identification的缩写, 即射频识别技术, 俗称电子标签) 中所使用的 导电银浆油墨加工方式、 各类可形变器件的柔性 PCB加工、 铁片天线的加工方 式以及铁片与 PCB组合的加工方式。 其中,铁片与 PCB组合加工方式是指利用 PCB 的精确加工来完成天线微槽结构的加工, 用铁片来完成其它辅助部分。 另 外, 还可以通过蚀刻、 电镀、 钻刻、 光刻、 电子刻或离子刻的方法来加工。  In the present invention, as for the processing and manufacturing of the antenna, various manufacturing methods can be employed as long as the design principle of the present invention is satisfied. The most common method is to use a variety of printed circuit board (PCB) manufacturing methods. Of course, metallized through-hole, double-sided copper-clad PCB fabrication can also meet the processing requirements of the present invention. In addition to this processing method, other processing means can be introduced according to actual needs, such as RFID (RFID is the abbreviation of Radio Frequency Identification, that is, radio frequency identification technology, commonly known as electronic label), the processing method of conductive silver paste ink, various types can be The flexible PCB processing of the deformation device, the processing method of the iron piece antenna, and the processing method of the combination of the iron piece and the PCB. Among them, the combination of iron sheet and PCB processing means that the precise processing of the PCB is used to complete the processing of the antenna microgroove structure, and the iron piece is used to complete other auxiliary parts. In addition, it can be processed by etching, electroplating, drilling, photolithography, electron engraving or ion engraving.
以下将参见图 2-4对本发明第二实施例作出详细介绍, 其中, 图 2本发明的 天线第二实施例的立体结构图。  The second embodiment of the present invention will be described in detail below with reference to Figs. 2-4, wherein Fig. 2 is a perspective structural view of a second embodiment of the antenna of the present invention.
请参见图 2, 如图 2所示, 本实施例与第一实施例的主要区别在于, 在本实 施例中, 第一金属片 4上进一步镂空有第三 槽结构 43 , 其中第一 槽结构 41 与第三 槽结构 43为非对称设置。  Referring to FIG. 2, as shown in FIG. 2, the main difference between this embodiment and the first embodiment is that, in the embodiment, the first metal piece 4 is further hollowed out with a third groove structure 43, wherein the first groove structure 41 and the third groove structure 43 are asymmetrically arranged.
在本实施例中, "第一微槽结构 41与第三微槽结构 43非对称设置" 是指, 第一微槽结构 41与第三微槽结构 43两者不构成轴对称结构。 换句话说, 即在 第一微槽结构 41与第三微槽结构 43所依附设置的 a表面上找不到一根对称轴, 使得第一微槽结构 41与第三微槽结构 43相对该对称轴对称设置。 In the present embodiment, "the first microgroove structure 41 and the third microgroove structure 43 are asymmetrically arranged" means that Both the first microgroove structure 41 and the third microgroove structure 43 do not constitute an axisymmetric structure. In other words, an axis of symmetry is not found on the surface a of the first microgroove structure 41 and the third microgroove structure 43 so that the first microgroove structure 41 and the third microgroove structure 43 are opposite to each other. Symmetrical axisymmetric setting.
本发明中, 第一 槽结构 41与第三 槽结构 43结构非对称, 因此两个位 置上的电容与电感会有所不同, 从而产生至少两个不同的谐振点, 而且谐振点 不易抵消, 有利于实现天线丰富的多模化。  In the present invention, the first groove structure 41 and the third groove structure 43 are asymmetric in structure, so the capacitance and inductance at the two positions are different, thereby generating at least two different resonance points, and the resonance point is not easily offset, Conducive to the antenna multi-mode.
本发明的第一 槽结构 41与第三 槽结构 43的结构形式可以一样, 也可 以不一样。 并且第一微槽结构 41与第三微槽结构 43的非对称程度可以根据需 要调节。 从而实现丰富的可调节的多模谐振。  The first groove structure 41 of the present invention may have the same structural form as the third groove structure 43, or may be different. And the degree of asymmetry of the first microgroove structure 41 and the third microgroove structure 43 can be adjusted as needed. This enables a rich, adjustable multimode resonance.
并且本发明根据需要, 在同一片金属片上还可以设置更多的微槽结构, 以 使得所述的天线具有三个以上的不同的谐振频率。  Moreover, the present invention can also provide more microgroove structures on the same piece of metal as needed, so that the antenna has more than three different resonant frequencies.
具体的, 本发明中非对称设置的情形至少可以为图 2至图 4所示的几个情 形。  Specifically, the case where the asymmetry is set in the present invention may be at least several cases as shown in Figs. 2 to 4 .
图 2所示为非对称结构的第一种情形。 如图 2所示, 处于介质基板 a表面 的第一微槽结构 41及第三微槽结构 43其均为开口螺旋环结构, 第一微槽结构 41及第三微槽结构 43不相通, 但是其尺寸的不同导致二者结构的非对称, 使得 天线 100具有至少两个以上的谐振频率。  Figure 2 shows the first case of an asymmetric structure. As shown in FIG. 2, the first microgroove structure 41 and the third microgroove structure 43 on the surface of the dielectric substrate a are both open spiral loop structures, and the first microgroove structure 41 and the third microgroove structure 43 are not in communication, but The difference in size results in asymmetry in the structure of the two, such that the antenna 100 has at least two resonant frequencies.
图 3所示为非对称结构的第二种情形。 如图 3所示, 处于介质基板 a表面 的第一微槽结构 41及第三微槽结构 43其均为开口螺旋环结构, 且具有相同的 尺寸, 第一微槽结构 41及第三微槽结构 43不相通, 但是由于第一微槽结构 41 及第三 槽结构 43二者位置上的设置导致二者结构的非对称。  Figure 3 shows the second case of an asymmetric structure. As shown in FIG. 3, the first microgroove structure 41 and the third microgroove structure 43 on the surface of the dielectric substrate a are both open spiral ring structures and have the same size, the first microgroove structure 41 and the third microgroove. The structure 43 is not in communication, but due to the positional arrangement of both the first microgroove structure 41 and the third trough structure 43, the asymmetry of the structures is caused.
图 4所示为非对称结构的第三种情形。 本实施例中, 处于介质基板 a表面 的第一微槽结构 41为互补式螺旋线结构, 第三微槽结构 43为开口螺旋环结构 , 第一微槽结构 41及第三微槽结构 43不相通, 很明显, 第一微槽结构 41及第三 微槽结构 43非对称。  Figure 4 shows the third case of an asymmetric structure. In this embodiment, the first microgroove structure 41 on the surface of the dielectric substrate a is a complementary spiral structure, and the third microgroove structure 43 is an open spiral ring structure, and the first microgroove structure 41 and the third microgroove structure 43 are not In common, it is apparent that the first microgroove structure 41 and the third microgroove structure 43 are asymmetrical.
另外, 在上述的图 2至图 4的三个实施例中, 第一 槽结构 41及第三 槽 结构 43还可以通过在第一金属片 4上镂空一条新的槽来实现第一 槽结构 41 及第三 槽结构 43的连通。 连通后第一 槽结构 41及第三 槽结构 43仍然为 非对称结构, 因此, 对本发明的效果不会有太大的影响, 同样可以使得天线具 有至少两个以上的谐振频率。 In addition, in the above three embodiments of FIG. 2 to FIG. 4, the first groove structure 41 and the third groove The structure 43 can also achieve communication of the first groove structure 41 and the third groove structure 43 by hollowing out a new groove on the first metal piece 4. After the communication, the first groove structure 41 and the third groove structure 43 are still asymmetric structures, and therefore, the effect of the present invention is not greatly affected, and the antenna can be made to have at least two resonance frequencies.
值得注意的是, 在第二实施例中, 如图 2至图 4所示, 在天线上亦设置有 供电子元件嵌入的预留空间(未标示),通过在预留空间中加入不同参数(电感值、 电阻值、 电容值) 的电子元件, 可实现天线性能参数的可调, 由此提高天线的 通用性。 其中, 预留空间例如可以设置于馈线上、 馈线与金属片之间、 金属走 线上或是第一微槽结构上。 换而言之, 在第二实施例中, 供电子元件嵌入的预 留空间的设置原理与设置方式与前述第一实施例中描述的相同, 因而在此不再 赘述。  It should be noted that, in the second embodiment, as shown in FIG. 2 to FIG. 4, a reserved space (not labeled) for embedding the electronic component is also disposed on the antenna, by adding different parameters in the reserved space ( The electronic components of the inductance value, the resistance value, and the capacitance value can adjust the antenna performance parameters, thereby improving the versatility of the antenna. The reserved space may be disposed, for example, on the feeder, between the feeder and the metal sheet, on the metal trace, or on the first microgroove structure. In other words, in the second embodiment, the arrangement principle and arrangement manner of the reserved space for embedding the electronic component are the same as those described in the foregoing first embodiment, and thus will not be described again.
图 5至图 6为本发明天线的第三实施例的结构示意图, 其中, 图 5是本发 明的天线第三实施例的正面 (a面)立体图, 图 6为其背面 (b面)立体图。  5 to 6 are schematic views showing the structure of a third embodiment of the antenna of the present invention, wherein Fig. 5 is a front (a) side perspective view of the third embodiment of the antenna of the present invention, and Fig. 6 is a rear (b side) perspective view thereof.
第三实施例与第二实施例的主要区别在于,在与介质基板的 a表面相对的 b 表面上进一步附着有金属片和馈线, 且介质基板的 a表面及 b表面上附着的金 属片与馈线的结构相同。 即: 第一馈线 2、 第一金属片 4、 第一微槽结构 41、 第 三微槽结构 43在 b表面的投影分别与 b表面上的第二馈线 8、 第二金属片 7、 第二微槽结构 71、 第四微槽结构 72重合, 第一馈线 2与第二馈线 8通过在第一 介质基板 1上开的金属化通孔 10电连接。 当然, 这只是一个优选的方案, a表 面与 b表面的天线结构根据需要也可以不同。  The main difference between the third embodiment and the second embodiment is that a metal piece and a feed line are further attached on the surface of the b opposite to the surface a of the dielectric substrate, and the metal piece and the feed line attached to the a surface and the b surface of the dielectric substrate The structure is the same. That is, the projections of the first feed line 2, the first metal piece 4, the first micro-groove structure 41, and the third micro-slot structure 43 on the b-surface are respectively associated with the second feed line 8, the second metal piece 7, and the second on the b-surface. The microgroove structure 71 and the fourth microgroove structure 72 are coincident, and the first feed line 2 and the second feed line 8 are electrically connected by a metallized through hole 10 opened on the first dielectric substrate 1. Of course, this is only a preferred solution, and the antenna structure of the a surface and the b surface may be different as needed.
值得注意的是, 在第三实施例中, 如图 5至图 6所示, 在天线上亦设置有 供电子元件嵌入的预留空间(未标示),通过在预留空间中加入不同参数(电感值、 电阻值、 电容值) 的电子元件, 可实现天线性能参数的可调, 由此提高天线的 通用性。 其中, 预留空间例如可以设置于馈线上、 馈线与金属片之间、 金属走 线上或是第一微槽结构上。 换而言之, 在第三实施例中, 供电子元件嵌入的预 留空间的设置原理与设置方式与前述第一实施例中描述的相同, 因而在此不再 赘述。 It should be noted that, in the third embodiment, as shown in FIG. 5 to FIG. 6, a reserved space (not labeled) for embedding an electronic component is also disposed on the antenna, by adding different parameters in the reserved space ( The electronic components of the inductance value, the resistance value, and the capacitance value can adjust the antenna performance parameters, thereby improving the versatility of the antenna. The reserved space may be disposed, for example, on the feeder, between the feeder and the metal sheet, on the metal trace, or on the first microgroove structure. In other words, in the third embodiment, the setting principle and setting manner of the reserved space for embedding the electronic component are the same as those described in the foregoing first embodiment, and thus are no longer Narration.
请参见图 7, 为本发明的天线第四实施例的立体结构图, 如图 7所示, 第四 实施方式与第一实施例的区别在于, 在本实施例中, 天线 100进一步包括第二 金属片 3 , 第二金属片 3与第一金属片 4相对设置且与第一馈线 2电连接。  FIG. 7 is a perspective structural view of a fourth embodiment of an antenna according to the present invention. As shown in FIG. 7, the fourth embodiment is different from the first embodiment in that, in this embodiment, the antenna 100 further includes a second The metal piece 3 and the second metal piece 3 are disposed opposite to the first metal piece 4 and are electrically connected to the first feed line 2.
第一金属片 4与第二金属片 3相对设置且两者之间存在介质, 介质可为高 分子聚合物、 陶瓷材料等, 也可为空气。 当介质为空气时, 第一馈线 2 与第二 金属片 3 通过导线电连接, 当介质为高分子聚合物或陶瓷材料时, 第一馈线 2 与第二金属片 3通过在介质上形成金属化通孔 9而相互电连接。  The first metal piece 4 is disposed opposite to the second metal piece 3 with a medium therebetween, and the medium may be a high molecular polymer, a ceramic material or the like, or may be air. When the medium is air, the first feed line 2 and the second metal piece 3 are electrically connected by a wire. When the medium is a polymer or a ceramic material, the first feed line 2 and the second metal piece 3 form a metallization on the medium. The through holes 9 are electrically connected to each other.
本发明中, 介质采用聚四氟乙烯(FR-4 )并通过金属化通孔 9 电连接第二 金属片 3和第一馈线 2。  In the present invention, the medium is made of polytetrafluoroethylene (FR-4) and the second metal piece 3 and the first feed line 2 are electrically connected through the metallized through holes 9.
现有天线在工作在低频时, 低频段的电磁波对应的波长较长, 根据天线设 计原理, 天线馈线的电辐射长度将要增大使得馈线长度变长, 不利于天线整体 的小型化并且较长的馈线使得馈线损耗增大从而使得天线性能下降的问题。  When the existing antenna operates at a low frequency, the electromagnetic wave of the low frequency band corresponds to a longer wavelength. According to the antenna design principle, the length of the electric radiation of the antenna feed line is increased to make the length of the feed line longer, which is disadvantageous to the miniaturization of the antenna as a whole and is long. The feeder causes the feeder loss to increase, which causes the antenna performance to degrade.
本发明天线 100通过加设第二金属片 3 以解决上述现有天线的问题, 其问 题解决的原理是: 第二金属片 3与第一金属片 4容性耦合, 对第一金属片 4上 形成的第一微槽结构 41耦合馈电。 第二金属片 3对第一金属片 4上形成的第一 微槽结构 41耦合馈电有效的减少了第一馈线 2对第一金属片 4上形成的第一微 槽结构 41耦合馈电的需求。 因此当天线 100工作于低频段时无需增加第一馈线 2长度, 且第二金属片 3耦合馈电的面积易于调节, 针对不同的工作频段只需筒 单的调整第二金属片 3耦合馈电面积即可。  The antenna 100 of the present invention solves the above problem of the existing antenna by adding the second metal piece 3. The problem is solved by the principle that the second metal piece 3 is capacitively coupled with the first metal piece 4, and is applied to the first metal piece 4. The formed first microgroove structure 41 is coupled to feed. The second metal piece 3 is coupled to the first micro-slot structure 41 formed on the first metal piece 4 to effectively reduce the coupling of the first micro-slot structure 41 formed on the first metal piece 4 by the first feed line 2 demand. Therefore, when the antenna 100 operates in the low frequency band, it is not necessary to increase the length of the first feeder 2, and the area of the second metal sheet 3 coupled with the feeding is easy to adjust, and the second metal sheet 3 is coupled and fed only for the different working frequency bands. The area is fine.
值得注意的是, 在第四实施例中, 如图 7所示, 在天线上亦设置有供电子 元件嵌入的预留空间(未标示), 通过在预留空间中加入不同参数(电感值、 电阻 值、 电容值) 的电子元件, 可实现天线性能参数的可调, 由此提高天线的通用 性。 其中, 预留空间例如可以设置于馈线上、 馈线与金属片之间、 金属走线上 或是第一微槽结构上。 换而言之, 在第四实施例中, 供电子元件嵌入的预留空 间的设置原理与设置方式与前述第一实施例中描述的相同, 因而在此不再赘述。 以下将参见图 8对本发明第五实施例作出详细介绍, 其中, 图 8是本发明 的天线第五实施例的立体结构图。 It should be noted that, in the fourth embodiment, as shown in FIG. 7, a reserved space (not labeled) for embedding an electronic component is also disposed on the antenna, by adding different parameters (inductance value, The electronic components of the resistance value and the capacitance value can adjust the antenna performance parameters, thereby improving the versatility of the antenna. The reserved space may be disposed, for example, on the feeder, between the feeder and the metal sheet, on the metal trace, or on the first microgroove structure. In other words, in the fourth embodiment, the setting principle and setting manner of the reserved space for embedding the electronic component are the same as those described in the foregoing first embodiment, and thus will not be described herein. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, a fifth embodiment of the present invention will be described in detail with reference to FIG. 8, which is a perspective structural view of a fifth embodiment of the antenna of the present invention.
第五实施例与第一实施例的主要区别在于, 在本实施例中, 天线 100进一 步包括第二介质基板 5 , 第二介质基板 5覆盖第一金属片 4。  The main difference between the fifth embodiment and the first embodiment is that, in the embodiment, the antenna 100 further includes a second dielectric substrate 5 covering the first metal piece 4.
在本实施例中, 由于金属片 4位于第一介质基板 1与第二介质基板 5之间, 使得天线 100在接收或者发射电磁波时均需要通过该第二介质基板 5 ,从而令天 线 100整体的分布电容增大, 分布电容的增大能有效降低天线工作频率, 因此 可在不改变馈线长度的情况下使得天线在低频时仍然工作良好, 满足天线小体 积、 低工作频率及宽带多模的要求。  In this embodiment, since the metal piece 4 is located between the first dielectric substrate 1 and the second dielectric substrate 5, the antenna 100 needs to pass through the second dielectric substrate 5 when receiving or transmitting electromagnetic waves, thereby making the antenna 100 as a whole. The distributed capacitance increases, and the increase of the distributed capacitance can effectively reduce the operating frequency of the antenna. Therefore, the antenna can still work well at low frequencies without changing the length of the feeder, satisfying the requirements of small antenna size, low operating frequency and wideband multimode. .
值得注意的是, 在第五实施例中, 如图 8所示, 在天线上亦设置有供电子 元件嵌入的预留空间(未标示), 通过在预留空间中加入不同参数(电感值、 电阻 值、 电容值) 的电子元件, 可实现天线性能参数的可调, 由此提高天线的通用 性。 其中, 预留空间例如可以设置于馈线上、 馈线与金属片之间、 金属走线上 或是第一微槽结构上。 换而言之, 在第五实施例中, 供电子元件嵌入的预留空 间的设置原理与设置方式与前述第一实施例中描述的相同, 因而在此不再赘述。  It should be noted that, in the fifth embodiment, as shown in FIG. 8, a reserved space (not labeled) for embedding the electronic component is also disposed on the antenna, by adding different parameters (inductance value, The electronic components of the resistance value and the capacitance value can adjust the antenna performance parameters, thereby improving the versatility of the antenna. The reserved space may be disposed, for example, on the feeder, between the feeder and the metal sheet, on the metal trace, or on the first microgroove structure. In other words, in the fifth embodiment, the setting principle and setting manner of the reserved space for embedding the electronic component are the same as those described in the foregoing first embodiment, and thus will not be described herein.
以下将参见图 9-10对本发明第六实施例作出详细介绍, 其中, 图 9是本发 明的天线第五实施例的正面立体结构图, 图 10是本发明的天线第五实施例的背 面立体结构图。  9 is a detailed front view of a fifth embodiment of the antenna of the present invention, and FIG. 10 is a front perspective view of the fifth embodiment of the antenna of the present invention. Structure diagram.
请参见图 9-10, 第六实施例与第一实施例的区别在于, 在本实施例中, 天 线 100进一步包括第二金属片 7,第二金属片 7附着在第一介质基板 1另一表面 (b表面), 围绕第二金属片 7设置有第二馈线 8, 第二馈线 8通过耦合方式馈入 第二金属片 7, 第二金属片 7上镂空有第二微槽结构 71以在第二金属片 7上形 成第二金属走线 72 , 第一馈线 2与第二馈线 8电连接。  Referring to FIG. 9-10, the sixth embodiment is different from the first embodiment in that, in this embodiment, the antenna 100 further includes a second metal piece 7, and the second metal piece 7 is attached to the first dielectric substrate 1 and a surface (b surface), a second feed line 8 is disposed around the second metal piece 7, the second feed line 8 is fed into the second metal piece 7 by coupling, and the second metal piece 7 is hollowed out with the second micro groove structure 71 to A second metal trace 72 is formed on the second metal piece 7, and the first feed line 2 is electrically connected to the second feed line 8.
如图 9及图 10所示, 第一馈线 2与第二馈线 8通过在第一介质基板 1上开 的金属化通孔 10电连接。 本实施例中, 在第一实施例的基础上增设了设置有第二馈线 8 以及设置于 第一介质基板 1另一表面的第二金属片 7,这种设计等效于增加了天线物理长度 (实际长度尺寸不增加;), 这样就可以在极小的空间内设计出工作在极低工作频 率下的射频天线。 解决传统天线在低频工作时天线受控空间面积的物理局限。 As shown in FIGS. 9 and 10, the first feed line 2 and the second feed line 8 are electrically connected by a metallized through hole 10 opened in the first dielectric substrate 1. In this embodiment, a second metal strip 7 disposed on the other surface of the first dielectric substrate 1 and a second metal strip 7 disposed on the other surface of the first dielectric substrate 1 are added to the first embodiment. This design is equivalent to increasing the physical length of the antenna. (The actual length does not increase;), so that the RF antenna operating at very low operating frequencies can be designed in a very small space. Solve the physical limitation of the controlled space area of the antenna when the traditional antenna operates at low frequencies.
值得注意的是, 在本实施例中, 综合图 9和图 10可以看出, 第一介质基板 1的 a表面及 b表面上附着的结构相同, 即第一馈线 2、 第一金属片 4在 b表面 的投影分别与第二馈线 8、 第二金属片 7重合。 当然, 这只是一个优选的方案, a表面与 b表面的结构根据需要也可以不同。  It should be noted that, in this embodiment, as can be seen from FIG. 9 and FIG. 10, the structures attached to the a surface and the b surface of the first dielectric substrate 1 are the same, that is, the first feed line 2 and the first metal piece 4 are The projection of the b surface coincides with the second feed line 8 and the second metal piece 7, respectively. Of course, this is only a preferred solution, and the structure of the a surface and the b surface may be different as needed.
值得注意的是, 在第六实施例中, 如图 9至图 10所示, 在天线上亦设置有 供电子元件嵌入的预留空间(未标示),通过在预留空间中加入不同参数(电感值、 电阻值、 电容值) 的电子元件, 可实现天线性能参数的可调, 由此提高天线的 通用性。 其中, 预留空间例如可以设置于馈线上、 馈线与金属片之间、 金属走 线上或是第一微槽结构上。 换而言之, 在第六实施例中, 供电子元件嵌入的预 留空间的设置原理与设置方式与前述第一实施例中描述的相同, 因而在此不再 赘述。  It should be noted that, in the sixth embodiment, as shown in FIG. 9 to FIG. 10, a reserved space (not labeled) for embedding the electronic component is also disposed on the antenna, by adding different parameters in the reserved space ( The electronic components of the inductance value, the resistance value, and the capacitance value can adjust the antenna performance parameters, thereby improving the versatility of the antenna. The reserved space may be disposed, for example, on the feeder, between the feeder and the metal sheet, on the metal trace, or on the first microgroove structure. In other words, in the sixth embodiment, the arrangement principle and arrangement manner of the reserved space for embedding the electronic component are the same as those described in the foregoing first embodiment, and thus will not be described herein.
以下将参见图 11-13对本发明第七实施例作出详细介绍, 其中, 图 11是本 发明的天线第七实施例的第一介质基板的 A面视角结构图,图 12是本发明的天 线第七实施例的第一介质基板的 B面视角结构图, 图 13是本发明的天线第七实 施例的第二介质基板 2的结构图。  The seventh embodiment of the present invention will be described in detail with reference to FIGS. 11-13. FIG. 11 is a perspective view of the first dielectric substrate of the seventh embodiment of the antenna of the present invention, and FIG. 12 is the antenna of the present invention. FIG. 13 is a structural view of a second dielectric substrate 2 of a seventh embodiment of the antenna of the present invention. FIG.
如图 11-13 , 本实施例在上述的第六实施例的基础上作出如下改进: 增设一 第二介质基板 2, 第二介质基板 2—表面与第一介质基板 1的 A表面重合, 第 二介质基板 2未与第一介质基板 1重合的另一表面设置有第三金属片 30。  As shown in FIG. 11-13, the present embodiment provides the following improvements on the basis of the sixth embodiment: a second dielectric substrate 2 is disposed, and the surface of the second dielectric substrate 2 coincides with the surface A of the first dielectric substrate 1, The other surface of the two dielectric substrates 2 that is not overlapped with the first dielectric substrate 1 is provided with a third metal piece 30.
第二介质基板 2上形成有金属化通孔 23 , 金属化通孔 23电连接第二馈线 2 与第三金属片 30。 由于第三金属片 30耦合馈电的面积易于调节, 因此针对不同 那个的工作频段只需筒单的调整第三金属片 30的耦合馈电面积即可。  A metallized via 23 is formed on the second dielectric substrate 2, and the metal via 23 electrically connects the second feed line 2 and the third metal piece 30. Since the area of the coupling feeding of the third metal piece 30 is easy to adjust, it is only necessary to adjust the coupling feeding area of the third metal piece 30 for the different working frequency bands.
值得注意的是, 在第七实施例中, 如图 11至图 13所示, 在天线上亦设置 有供电子元件嵌入的预留空间(未标示), 通过在预留空间中加入不同参数 (电感 值、 电阻值、 电容值) 的电子元件, 可实现天线性能参数的可调, 由此提高天 线的通用性。 其中, 预留空间例如可以设置于馈线上、 馈线与金属片之间、 金 属走线上或是第一微槽结构上。 换而言之, 在第七实施例中, 供电子元件嵌入 的预留空间的设置原理与设置方式与前述第一实施例中描述的相同, 因而在此 不再赘述。 It should be noted that in the seventh embodiment, as shown in FIG. 11 to FIG. 13, the antenna is also disposed. There is a reserved space for electronic components (not shown). By adding electronic components with different parameters (inductance value, resistance value, capacitance value) in the reserved space, the antenna performance parameters can be adjusted, thereby improving the antenna. Universality. The reserved space may be disposed, for example, on the feeder, between the feeder and the metal sheet, on the metal trace, or on the first microgroove structure. In other words, in the seventh embodiment, the setting principle and setting manner of the reserved space for embedding the electronic component are the same as those described in the foregoing first embodiment, and thus will not be described herein.
以下将参见图 14-15对本发明第八实施例作出详细介绍, 其中, 图 14是本 发明的天线第八实施例的正面立体结构图, 图 15是本发明的天线第八实施例的 背面立体结构图。  The eighth embodiment of the present invention will be described in detail with reference to Figs. 14-15, wherein Fig. 14 is a front perspective view of the eighth embodiment of the antenna of the present invention, and Fig. 15 is a rear perspective view of the eighth embodiment of the antenna of the present invention. Structure diagram.
如图 14-15 , 第八实施例在上述的第七实施例的基础上作出如下改进: 在第 一金属片 4上进一步镂空有第三微槽结构 43 ,第三微槽结构 43与第一微槽结构 41非对称设置, 第一微槽结构 41和第三微槽结构 43在第一金属片 4上形成第 一金属走线 42, 第二金属片 7上进一步镂空有第四微槽结构 73 , 第二微槽结构 71和第四微槽结构 73在第二金属片 7上形成第二金属走线 72。  14-15, the eighth embodiment is improved on the basis of the seventh embodiment described above: further recessed on the first metal piece 4 has a third microgroove structure 43, the third microgroove structure 43 and the first The microgroove structure 41 is asymmetrically disposed. The first microgroove structure 41 and the third microgroove structure 43 form a first metal trace 42 on the first metal piece 4, and the second metal strip 7 is further hollowed out to have a fourth microgroove structure. 73. The second microgroove structure 71 and the fourth microgroove structure 73 form a second metal trace 72 on the second metal piece 7.
其中, 上述的非对称设置方式在本发明的第二实施例中得到具体描述, 于 此不再赘述, 其所产生的技术效果是, 可产生至少两个不同的谐振点, 而且谐 振点不易抵消, 有利于实现天线丰富的多模化。  The asymmetrical arrangement described above is specifically described in the second embodiment of the present invention, and is not described herein again. The technical effect is that at least two different resonance points can be generated, and the resonance point is not easily offset. , is conducive to the rich multi-mode of the antenna.
值得注意的是, 在第八实施例中, 如图 14至图 15所示, 在天线上亦设置 有供电子元件嵌入的预留空间(未标示), 通过在预留空间中加入不同参数 (电感 值、 电阻值、 电容值) 的电子元件, 可实现天线性能参数的可调, 由此提高天 线的通用性。 其中, 预留空间例如可以设置于馈线上、 馈线与金属片之间、 金 属走线上或是第一微槽结构上。 换而言之, 在第八实施例中, 供电子元件嵌入 的预留空间的设置原理与设置方式与前述第一实施例中描述的相同, 因而在此 不再赘述。  It should be noted that, in the eighth embodiment, as shown in FIG. 14 to FIG. 15, a reserved space (not labeled) for embedding an electronic component is also disposed on the antenna, by adding different parameters in the reserved space ( The electronic components of the inductance value, the resistance value, and the capacitance value can adjust the antenna performance parameters, thereby improving the versatility of the antenna. The reserved space may be disposed, for example, on the feeder, between the feeder and the metal sheet, on the metal trace, or on the first microgroove structure. In other words, in the eighth embodiment, the setting principle and setting manner of the reserved space for embedding the electronic component are the same as those described in the foregoing first embodiment, and thus will not be described herein.
值得注意的是, 在本发明的所有实施例中, 微槽结构可以是图 16所示的互 补式开口谐振环结构、 图 17所示的互补式螺旋线结构、 图 18所示的开口螺旋 环结构、 图 19所示的双开口螺旋环结构、 图 20所示的互补式弯折线结构中的 一种或者是通过前面几种结构中的其中一种结构衍生、 多种结构复合或一种结 构组阵得到的微槽结构。 It should be noted that in all embodiments of the present invention, the microgroove structure may be the complementary open resonant ring structure shown in FIG. 16, the complementary spiral structure shown in FIG. 17, and the open spiral shown in FIG. One of the ring structure, the double-open spiral ring structure shown in FIG. 19, and the complementary bent line structure shown in FIG. 20 is derived from one of the foregoing structures, a plurality of structural composites or a The microgroove structure obtained by the structural array.
其中, 衍生分为两种, 一种是几何形状衍生, 另一种是扩展衍生, 此处的 几何形状衍生是指功能类似、 形状不同的结构衍生, 例如由方框类结构衍生到 曲线类结构、 三角形类结构及其它不同的多边形类结构。  Among them, there are two kinds of derivatives, one is geometric shape derivation, and the other is extended derivation. Here, geometric derivation refers to structural derivation with similar functions and different shapes, for example, derived from a box-like structure to a curve-like structure. , triangle class structure and other different polygon class structures.
此处的扩展衍生即在图 16至图 20的基础上开设新的槽以形成新的 槽结 构; 以图 16所示的互补式开口谐振环结构为例, 图 21为其几何形状衍生示意 图, 图 22为其几何形状衍生示意图。  The extended derivative here is to open a new groove on the basis of FIG. 16 to FIG. 20 to form a new groove structure; taking the complementary open resonant ring structure shown in FIG. 16 as an example, FIG. 21 is a schematic diagram of the geometrical derivative thereof. Figure 22 is a schematic representation of its geometry.
此处的复合是指, 图 16至图 20的微槽结构多个叠加形成一个新的微槽结 构, 如图 23所示, 为三个图 16所示的互补式开口谐振环结构复合后的结构示 意图; 如图 24所示, 为两个图 16所示的互补式开口谐振环结构与图 17所示为 互补式螺旋线结构共同复合后的结构示意图。  The composite here means that the microgroove structures of FIGS. 16 to 20 are superposed to form a new microgroove structure, as shown in FIG. 23, after the composite of the complementary open resonant ring structures shown in FIG. Schematic diagram of the structure; as shown in FIG. 24, a schematic structural view of the complementary open resonant ring structure shown in FIG. 16 and the complementary spiral structure shown in FIG.
此处的组阵是指由多个图 16至图 20所示的 槽结构在同一金属片上阵列 形成一个整体的 槽结构, 如图 25所示, 为多个如图 16所示的互补式开口谐 振环结构组阵后的结构示意图。 以上各实施例中均以图 18所示的开口螺旋环结 构为例阐述本发明。  The array here refers to a plurality of groove structures formed on the same metal sheet by a plurality of groove structures shown in FIG. 16 to FIG. 20, and as shown in FIG. 25, a plurality of complementary openings as shown in FIG. Schematic diagram of the structure after the resonant ring structure array. In the above embodiments, the invention has been described by taking the open spiral ring structure shown in Fig. 18 as an example.
本发明还提供了一种 MIMO天线,所述的 MIMO天线由多个上述一至七任 意一个实施例所揭示的天线组成。 在 MIMO天线上, 每一天线同时发射, 同时 接收。 MIMO 天线可以在不需要增加带宽或总发送功率损耗的前提下大幅度增 加系统的信息吞吐量及传输距离。 另外本发明的 MIMO天线还具有很高的隔离 度, 多个天线之间的抗干扰能力强。 并且, 本发明的 MIMO天线, 其每个天线 的第一馈线与第二馈线电连接后再与一个接收 /发射机连接, 所有的接收 /发射机 均连接到一个基带信号处理器上。 下有益效果: 通过天线上设置供电子元件嵌入的空间, 可以通过改变嵌入的电 子元件的性能对天线的性能进行微调, 设计出满足适应性及通用性的要求的天 线。 The present invention also provides a MIMO antenna, which is composed of a plurality of antennas disclosed in any one of the above one to seven embodiments. On a MIMO antenna, each antenna is simultaneously transmitted and received simultaneously. The MIMO antenna can greatly increase the information throughput and transmission distance of the system without increasing the bandwidth or total transmission power loss. In addition, the MIMO antenna of the present invention also has high isolation and strong anti-interference ability between multiple antennas. Moreover, in the MIMO antenna of the present invention, the first feeder of each antenna is electrically connected to the second feeder and then connected to a receiver/transmitter, and all the receivers/transmitters are connected to a baseband signal processor. The following beneficial effects: By embedding the space for the electronic component to be embedded on the antenna, the embedded electric power can be changed The performance of the sub-components fine-tunes the performance of the antenna to design an antenna that meets the requirements of adaptability and versatility.
上面结合附图对本发明的实施例进行了描述, 但是本发明并不局限于上述 的具体实施方式, 上述的具体实施方式仅仅是示意性的, 而不是限制性的, 本 领域的普通技术人员在本发明的启示下, 在不脱离本发明宗旨和权利要求所保 护的范围情况下, 还可做出很多形式, 这些均属于本发明的保护之内。  The embodiments of the present invention have been described above with reference to the drawings, but the present invention is not limited to the specific embodiments described above, and the specific embodiments described above are merely illustrative and not restrictive, and those skilled in the art In the light of the present invention, many forms may be made without departing from the spirit and scope of the invention as claimed.

Claims

权利要求 Rights request
1、 一种天线, 其特征在于, 所述天线包括第一介质基板、 第一馈线、 附着 在所述第一介质基板一表面的第一金属片, 所述第一馈线通过耦合方式馈入所 述第一金属片, 所述第一金属片上镂空有第一微槽结构以在所述第一金属片上 形成第一金属走线, 所述天线预设有供电子元件嵌入的空间。  An antenna, comprising: a first dielectric substrate, a first feed line, and a first metal piece attached to a surface of the first dielectric substrate, wherein the first feed line is fed through a coupling manner The first metal piece is hollowed out with a first micro-groove structure to form a first metal trace on the first metal piece, and the antenna is pre-configured with a space for electronic components to be embedded.
2、 根据权利要求 1所述的天线, 其特征在于, 所述第一金属片上进一步镂 空有第二微槽结构, 其中所述第一微槽结构与所述第二微槽结构非对称设置。  The antenna according to claim 1, wherein the first metal piece is further hollowed out with a second micro groove structure, wherein the first micro groove structure and the second micro groove structure are asymmetrically disposed.
3、 根据权利要求 1所述的天线, 其特征在于, 所述天线进一步包括第二金 属片, 所述第二金属片与所述第一金属片相对设置且与所述第一馈线电连接。  The antenna according to claim 1, wherein the antenna further comprises a second metal piece, and the second metal piece is disposed opposite to the first metal piece and electrically connected to the first feed line.
4、 根据权利要求 1所述的天线, 其特征在于, 所述天线进一步包括第二介 质基板, 所述第二介质基板覆盖所述第一金属片。  The antenna according to claim 1, wherein the antenna further comprises a second dielectric substrate, and the second dielectric substrate covers the first metal piece.
5、 根据权利要求 1所述的天线, 其特征在于, 所述天线进一步包括第二金 属片, 所述第二金属片附着在所述第一介质基板另一表面, 围绕所述第二金属 片设置有第二馈线, 所述第二馈线通过耦合方式馈入所述第二金属片, 所述第 二金属片上镂空有第二微槽结构以在所述第二金属片上形成第二金属走线, 所 述第一馈线与所述第二馈线电连接。  The antenna according to claim 1, wherein the antenna further comprises a second metal piece, the second metal piece is attached to another surface of the first dielectric substrate, surrounding the second metal piece a second feed line is provided, the second feed line is fed into the second metal piece by coupling, and the second metal piece is hollowed out with a second micro groove structure to form a second metal trace on the second metal piece The first feed line is electrically connected to the second feed line.
6、 根据权利要求 5所述的天线, 其特征在于, 所述第一微槽结构、 所述第 二 槽结构、 所述第三 槽结构和所述第四 槽结构中的任意一种为互补式开 口谐振环结构、 互补式螺旋线结构、 开口螺旋环结构、 双开口螺旋环结构以及 互补式弯折线结构中的一种或者是通过前面五种结构的其中一种结构衍生、 其 中多种结构复合或其中一种结构组阵得到的结构。  The antenna according to claim 5, wherein any one of the first microgroove structure, the second trough structure, the third trough structure, and the fourth trough structure is complementary One of the open-loop resonant ring structure, the complementary spiral structure, the open spiral ring structure, the double-open spiral ring structure, and the complementary bent line structure or derived from one of the first five structures, and various structures thereof A composite or a structure obtained by one of the structural arrays.
7、 根据权利要求 5所述的天线, 其特征在于, 所述第一金属片上进一步镂 空有第三微槽结构, 所述第一微槽结构和所述第三微槽结构设置为非对称, 所 述第一微槽结构和所述第三微槽结构在所述第一金属片上形成所述第一金属走 线, 所述第二金属片上进一步镂空有第四微槽结构, 所述第二微槽结构和所述 第四微槽结构设置为非对称, 所述第二微槽结构和所述第四微槽结构在所述第 二金属片上形成所述第二金属走线。 The antenna according to claim 5, wherein the first metal piece is further hollowed out with a third micro groove structure, and the first micro groove structure and the third micro groove structure are asymmetrically arranged. The first microgroove structure and the third microgroove structure form the first metal trace on the first metal piece, and the second metal strip is further hollowed out to have a fourth microgroove structure, the second The microgroove structure and the fourth microgroove structure are disposed asymmetrically, and the second microgroove structure and the fourth microgroove structure are in the The second metal trace is formed on the two metal sheets.
8、 根据权利要求 5所述的天线, 其特征在于, 所述天线进一步包括第二介 质基板, 所述第二介质基板一表面与所述第一介质基板另一表面重合, 所述第 二介质基板另一表面设置有第三金属片。  The antenna according to claim 5, wherein the antenna further includes a second dielectric substrate, a surface of the second dielectric substrate coincides with another surface of the first dielectric substrate, and the second medium The other surface of the substrate is provided with a third metal piece.
9、 根据权利要求 8所述的天线, 其特征在于, 所述第一金属片上进一步镂 空有第三微槽结构, 所述第三微槽结构与所述第一微槽结构非对称设置, 所述 第一微槽结构和所述第三微槽结构在所述第一金属片上形成第一金属走线, 所 述第二金属片上进一步镂空有第四微槽结构, 所述第二微槽结构和所述第四微 槽结构在所述第二金属片上形成第二金属走线。  The antenna according to claim 8, wherein the first metal piece is further hollowed out with a third micro groove structure, and the third micro groove structure and the first micro groove structure are asymmetrically arranged. The first microgroove structure and the third microgroove structure form a first metal trace on the first metal piece, and the second metal strip is further hollowed out to have a fourth microgroove structure, and the second microgroove structure Forming a second metal trace on the second metal sheet and the fourth microgroove structure.
10、 根据权利要求 1 所述的天线, 其特征在于, 所述空间设置在所述第一 馈线上、 所述第一馈线与所述第一金属片之间、 所述金属片的金属走线上或在 所述第一微槽结构上且连接所述第一微槽结构两侧的金属走线上。  The antenna according to claim 1, wherein the space is disposed on the first feed line, between the first feed line and the first metal piece, and the metal trace of the metal piece On or on the first microgroove structure and connecting the metal traces on both sides of the first microgroove structure.
11、 根据权利要求 1 所述的天线, 其特征在于, 所述电子元件为感性电子 元件、 容性电子元件或电阻。  The antenna according to claim 1, wherein the electronic component is an inductive electronic component, a capacitive electronic component, or a resistor.
12、 根据权利要求 11所述的天线, 其特征在于, 所述空间为形成在所述天 线上的焊盘。  The antenna according to claim 11, wherein the space is a pad formed on the antenna.
13、 根据权利要求 11所述的天线, 其特征在于, 所述感性电子元件电感值 的范围在 0-5uH之间, 所述容性电子元件电容值的范围在 0-2pF之间。  The antenna according to claim 11, wherein the inductive electronic component inductance value ranges from 0 to 5 uH, and the capacitive electronic component capacitance value ranges from 0 to 2 pF.
14、 根据权利要求 1 所述的天线, 其特征在于, 所述第一微槽结构为互补 式开口谐振环结构、 互补式螺旋线结构、 开口螺旋环结构、 双开口螺旋环结构 以及互补式弯折线结构中的一种或者是通过前面几种结构衍生、 复合或组阵得 到的微槽结构。  The antenna according to claim 1, wherein the first microgroove structure is a complementary open resonant ring structure, a complementary spiral structure, an open spiral ring structure, a double open spiral ring structure, and a complementary bend. One of the fold line structures is a microgroove structure obtained by deriving, compounding or arraying the foregoing structures.
15、 一种 MIMO天线, 其特征在于, 所述 MIMO天线包括多个天线, 每一 所述天线包括第一介质基板、 第一馈线、 附着在所述第一介质基板一表面的第 一金属片, 所述第一馈线通过耦合方式馈入所述第一金属片, 所述第一金属片 上镂空有第一微槽结构以在所述第一金属片上形成金属走线, 所述天线预设有 供电子元件嵌入的空间。 A MIMO antenna, wherein the MIMO antenna includes a plurality of antennas, each of the antennas includes a first dielectric substrate, a first feed line, and a first metal piece attached to a surface of the first dielectric substrate The first feed line is fed into the first metal piece by a coupling manner, and the first metal piece is hollowed out with a first micro groove structure to form a metal trace on the first metal piece, and the antenna is pre-equipped A space for electronic components to be embedded.
16、根据权利要求 15所述的 MIMO天线, 其特征在于, 所述第一金属片上 进一步镂空有第二微槽结构, 其中所述第一微槽结构与所述第二微槽结构非对 称设置。  The MIMO antenna according to claim 15, wherein the first metal piece is further hollowed out with a second micro groove structure, wherein the first micro groove structure and the second micro groove structure are asymmetrically arranged. .
17、根据权利要求 15所述的 MIMO天线, 其特征在于, 所述天线进一步包 括第二金属片, 所述第二金属片与所述第一金属片相对设置且与所述第一馈线 电连接。  The MIMO antenna according to claim 15, wherein the antenna further comprises a second metal piece, the second metal piece being disposed opposite to the first metal piece and electrically connected to the first feed line .
18、 根据权利要求 15所述的 MIMO天线, 其特征在于, 其特征在于, 所述 天线进一步包括第二介质基板, 所述第二介质基板覆盖所述第一金属片。  The MIMO antenna according to claim 15, wherein the antenna further comprises a second dielectric substrate, and the second dielectric substrate covers the first metal piece.
19、根据权利要求 15所述的 MIMO天线, 其特征在于, 所述天线进一步包 括第二金属片, 所述第二金属片附着在所述第一介质基板另一表面, 围绕所述 第二金属片设置有第二馈线, 所述第二馈线通过耦合方式馈入所述第二金属片, 所述第二金属片上镂空有第二微槽结构以在所述第二金属片上形成金属走线, 所述第一馈线与所述第二馈线电连接。  The MIMO antenna according to claim 15, wherein the antenna further comprises a second metal piece, the second metal piece is attached to another surface of the first dielectric substrate, surrounding the second metal The sheet is provided with a second feed line, the second feed line is fed into the second metal piece by coupling, and the second metal piece is hollowed out with a second micro groove structure to form a metal trace on the second metal piece. The first feed line is electrically connected to the second feed line.
20、根据权利要求 19所述的 MIMO天线, 其特征在于, 所述第一金属片上 进一步镂空有第三微槽结构, 所述第一微槽结构和所述第三微槽结构设置为非 对称, 所述第一微槽结构和所述第三微槽结构在所述第一金属片上形成所述第 一金属走线, 所述第二金属片上进一步镂空有第四微槽结构, 所述第二微槽结 构和所述第四 槽结构设置为非对称, 所述第二 槽结构和所述第四 槽结构 在所述第二金属片上形成所述第二金属走线。  The MIMO antenna according to claim 19, wherein the first metal piece is further hollowed out with a third micro groove structure, and the first micro groove structure and the third micro groove structure are set to be asymmetric The first microgroove structure and the third microgroove structure form the first metal trace on the first metal piece, and the second metal strip is further hollowed out to have a fourth microgroove structure, the first The second micro-slot structure and the fourth groove structure are disposed asymmetrically, and the second groove structure and the fourth groove structure form the second metal trace on the second metal piece.
PCT/CN2011/080437 2011-03-14 2011-09-30 Antenna and mimo antenna having the antenna WO2012122794A1 (en)

Applications Claiming Priority (18)

Application Number Priority Date Filing Date Title
CN201110062188.9 2011-03-14
CN201110062188.9A CN102683805B (en) 2011-03-14 2011-03-14 A kind of adjustable radio-frequency antenna
CN2011101451457A CN102810734A (en) 2011-05-31 2011-05-31 Antenna and multiple-input and multiple-output (MIMO) antenna with same
CN2011101449372A CN102800936A (en) 2011-05-31 2011-05-31 Antenna and multiple input multiple output (MIMO) antenna with same
CN201110145107.1 2011-05-31
CN201110144937.2 2011-05-31
CN201110145005.XA CN102800939B (en) 2011-05-31 2011-05-31 A kind of antenna and there is the mimo antenna of this antenna
CN2011101451993A CN102800945A (en) 2011-05-31 2011-05-31 Antenna and multiple input multiple output (MIMO) antenna with same
CN201110144982.8 2011-05-31
CN201110145167.3 2011-05-31
CN201110145181.3 2011-05-31
CN201110145107.1A CN103036015B (en) 2011-05-31 2011-05-31 Antenna and multiple input multiple output (MIMO) antenna with same
CN2011101451673A CN102800942A (en) 2011-05-31 2011-05-31 Antenna and multiple input multiple output (MIMO) antenna with same
CN201110144982.8A CN102800937B (en) 2011-05-31 2011-05-31 A kind of antenna and there is the mimo antenna of this antenna
CN201110145181.3A CN102891355B (en) 2011-05-31 2011-05-31 A kind of antenna and there is the mimo antenna of this antenna
CN201110145005.X 2011-05-31
CN201110145199.3 2011-05-31
CN201110145145.7 2011-05-31

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