WO2021128720A1 - Eddy current suppression structure and manufacturing method therefor - Google Patents

Eddy current suppression structure and manufacturing method therefor Download PDF

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Publication number
WO2021128720A1
WO2021128720A1 PCT/CN2020/091786 CN2020091786W WO2021128720A1 WO 2021128720 A1 WO2021128720 A1 WO 2021128720A1 CN 2020091786 W CN2020091786 W CN 2020091786W WO 2021128720 A1 WO2021128720 A1 WO 2021128720A1
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layer
eddy current
insulating dielectric
magnetostrictive
dielectric layer
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PCT/CN2020/091786
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French (fr)
Chinese (zh)
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彭春瑞
李君儒
陈锶
高杨
任万春
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四川爆米微纳科技有限公司
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Priority claimed from CN201911369333.0A external-priority patent/CN110970716A/en
Priority claimed from CN201922381538.2U external-priority patent/CN211376925U/en
Application filed by 四川爆米微纳科技有限公司 filed Critical 四川爆米微纳科技有限公司
Publication of WO2021128720A1 publication Critical patent/WO2021128720A1/en

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    • 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
    • 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

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  • the bulk acoustic wave magnetoelectric antenna uses the principle of bulk acoustic wave resonance and the magnetoelectric effect to radiate electromagnetic signals, which fundamentally solves the problems of impedance matching of electric small antennas and low radiation efficiency. Moreover, using the principle of acoustic wave resonance can realize the miniaturization of the device. .
  • the bulk acoustic wave magnetoelectric antenna is composed of a piezoelectric layer and a magnetostrictive layer cross composite.
  • the width of the divided strip should be equal to the thickness, so that the interrupted eddy current loop can be small enough.
  • each air gap along the y-axis direction is 0.2 ⁇ m, which accounts for 1/5 of the width of a single magnetic film strip
  • the thickness of each air gap along the z-axis direction is 0.3 ⁇ m which accounts for 1/5 of the width of a single magnetic film strip.
  • the technical problem to be solved by the present invention is to provide an eddy current suppression structure and a preparation method thereof.
  • an eddy current suppression structure including a magnetostrictive layer and an insulating medium layer disposed in the magnetostrictive layer for breaking the eddy current.
  • the present invention inserts an insulating dielectric layer in the magnetostrictive layer to reduce eddy current loss, improve the radiation efficiency of the bulk acoustic wave magnetoelectric antenna, and solve the problem of the air gap spaced magnetostrictive layer in the prior art.
  • Using an insulating medium layer as a spacer layer can improve the soft magnetic properties of the magnetostrictive layer, effectively reduce the coercivity of the magnetostrictive layer, and improve the sensitivity of the radiation area. Through simulation analysis, this solution can effectively reduce the eddy current loss by more than 65%, and greatly improve the radiation efficiency of the magnetoelectric antenna.
  • a first insulating medium layer is arranged in the magnetostrictive layer along its thickness direction and/or a second insulating medium layer is arranged in the magnetostrictive layer along its width direction.
  • the beneficial effect of adopting the above-mentioned further solution is that the present invention divides the eddy current into volume eddy current and surface eddy current according to the skin effect of the induced current in the magnetostrictive layer, and the first insulating dielectric layer can well suppress the volume eddy current, thereby reducing the eddy current loss. ; The second insulating dielectric layer can well suppress the surface eddy current, thereby reducing the eddy current loss.
  • At least one layer of the first insulating medium layer is arranged in the magnetostrictive layer along its thickness direction.
  • the beneficial effect of adopting the above-mentioned further solution is that the first insulating dielectric layer can well suppress the body eddy current, thereby reducing the eddy current loss.
  • the first insulating dielectric layer is three layers parallel to each other, each of the first insulating dielectric layer has a thickness of 5-100 nm, the magnetostrictive layer is made of FeGaB film, and the total thickness of the FeGaB film is 1 ⁇ m, the conductivity of the first insulating dielectric layer ranges from 0-100S/m, and the first insulating dielectric layer is made of any one or more of Al 2 O 3 , Si 3 N 4 and AlN .
  • the beneficial effect of adopting the above further scheme is that the simulation results show that 3 layers are sufficient to solve the problem of bulk eddy current suppression; the first insulating dielectric layer is 5-100nm, and the bulk eddy current can be well suppressed; FeGaB film is a high-quality magnetostrictive Layer material; when the insulating dielectric layer is the above material, it has a good eddy current suppression effect.
  • At least one second insulating dielectric layer is arranged in the magnetostrictive layer along its width direction.
  • the beneficial effect of adopting the above-mentioned further solution is that the second insulating dielectric layer can well suppress the surface eddy current, thereby reducing the eddy current loss.
  • the second insulating dielectric layer is three layers parallel to each other, each of the second insulating dielectric layer has a thickness of 5-30 nm, the magnetostrictive layer is made of FeGaB film, and the total thickness of the FeGaB film is 1 ⁇ m, the conductivity of the second insulating dielectric layer ranges from 0-100S/m, and the second insulating dielectric layer is made of any one or more of Al 2 O 3 , Si 3 N 4 and AlN .
  • the beneficial effect of adopting the above-mentioned further scheme is that the simulation results show that three layers are sufficient to solve the problem of surface eddy current suppression; the second insulating dielectric layer is 5-30nm, and the surface eddy current can be well suppressed; FeGaB film is a high-quality magnetostrictive Layer material; when the insulating dielectric layer is the above material, it has a good eddy current suppression effect.
  • the beneficial effect of adopting the above-mentioned further scheme is to insert insulating dielectric layers alternately spaced along the thickness and width in the magnetostrictive layer to reduce its body eddy current and surface eddy current losses, and a comprehensive consideration of body eddy current and surface eddy current insertion insulation is proposed.
  • the isolation structure of the dielectric layer minimizes the eddy current loss of the magnetostrictive layer. It solves the problem that the air gap spaced magnetostrictive layer in the prior art solution causes the stress discontinuity and the low radiation efficiency of the magnetoelectric antenna.
  • the first insulating medium layer is three layers and parallel to each other
  • the second insulating medium layer is three layers and parallel to each other
  • each layer of the first insulating medium layer has a thickness of 5-100 nm
  • each layer of the first insulating medium layer The thickness of the second insulating medium layer is 5-30 nm
  • the material of the magnetostrictive layer is FeGaB film
  • the total thickness of the FeGaB film is 1 ⁇ m
  • the conductivity ranges of the first insulating medium layer and the second insulating medium layer It is 0-100 S/m
  • both the first insulating dielectric layer and the second insulating dielectric layer are made of any one or more of Al 2 O 3 , Si 3 N 4 and AlN.
  • the beneficial effect of adopting the above-mentioned further scheme is that through simulation results, 3 layers are sufficient to solve the problem of surface eddy current suppression.
  • the thickness of the first insulating dielectric layer is 5-100nm, and the second insulating dielectric layer is 5-30nm.
  • the surface eddy current can be well obtained.
  • the above limitation suppresses the eddy current loss in the magnetic film under the premise of ensuring that the size of the insulating medium layer is as small as possible, and proposes a magnetic film structure that inserts the smallest size insulating medium to suppress the eddy current.
  • the thin film is a high-quality magnetostrictive layer material; when the insulating medium layer is the above material, it has a good eddy current suppression effect.
  • the present invention also relates to a magnetoelectric antenna, including an upper electrode, and further including the eddy current suppression structure, the eddy current suppression structure being arranged on the upper electrode.
  • the present invention also relates to a method for preparing the eddy current suppression structure, including: Step 1: Depositing a magnetostrictive layer on the body (the upper electrode of the bulk acoustic wave resonator) by magnetron sputtering; Step 2: In the step 1. Use a magnetron sputtering method to deposit a first insulating medium layer along its thickness on the magnetostrictive layer formed; Step 3: deposit a magnetostrictive layer again on the first insulating medium layer formed in step 2.
  • Step 4 Obtain the eddy current suppression structure directly, or repeat the above steps 2-3 at least once to obtain the eddy current suppression structure; or, Step a: Use on the body (the upper electrode of the bulk acoustic wave resonator) Magnetron sputtering method is used to deposit the magnetostrictive layer; Step b: Use a spinner to evenly cover a layer of photoresist on the magnetostrictive layer, and then perform pre-baking, exposure and development in sequence; Step c: Use a dry method Etching etches at least one groove in the thickness direction of the magnetostrictive layer on the structure formed in step b; step d: sputtering on the structure formed in step c by a magnetron sputtering method At least one second insulating dielectric layer is formed in the thickness direction of the magnetostrictive layer; step e: removing the photoresist on the surface of the magnetostrictive layer by a metal stripping process; step f: using chemical machinery Grinding
  • the beneficial effect of adopting the above-mentioned further solution is that the above-mentioned method can be used to realize the production of eddy current suppression structure simply, quickly and under the premise of ensuring the eddy current suppression function, thereby improving the radiation efficiency of the magnetoelectric antenna.
  • Fig. 1 is a figure 1 of a prior art eddy current loss suppression structure
  • Figure 2 is the second diagram of the prior art eddy current loss suppression structure
  • FIG. 3 is a schematic diagram of the eddy current suppression structure of the magnetostrictive layer body of the present invention.
  • Fig. 4 is a structural diagram of the magnetostrictive layer eddy current suppression structure of the present invention.
  • Fig. 5 is a 3 ⁇ 3 eddy current suppression structure of the magnetostrictive layer of the present invention.
  • Figure 6 is a process flow diagram of the eddy current suppression structure of the present invention.
  • Fig. 11 is a schematic diagram of the total loss density corresponding to different Al 2 O 3 thicknesses of the present invention.
  • Magnetostrictive layer 2. First insulating medium layer, 3. Second insulating medium layer, 4. Upper pole of bulk acoustic wave resonator, 5. Photoresist, 6. Mask, 7. Air gap.
  • the total thickness is 100nm in Figure 8 (according to the process When the condition is appropriately thickened), the change trend of the surface eddy current density corresponding to the number of Al 2 O 3 insulating layers, with the increase of the number of layers, the surface loss density is significantly reduced, but the rate of decrease after 3 layers is less than 20%, and the rate of decrease Gradually flatten out. Therefore, 3 layers are sufficient to solve the problem of surface vortex suppression.
  • the 3 ⁇ 3 cross separation method as shown in Figure 6 is used to calculate the surface eddy currents and volume eddy currents respectively.
  • the simulation results of the total loss density are shown in Figure 11. Obviously, the total loss density of the cross-space is the lowest.
  • the thickness direction (z-axis direction) and the width direction (y-axis direction) are both 10nm, the thickness direction (z-axis direction) ) into three-layer Al 2 O 3 insulating layer and the insert 3 layer Al 2 O 3 insulating layer in the width direction (y axis direction), the total loss density decreased by about 10% and 47%, while the use of cross-compartments of 3 ⁇ 3 The reduction rate is 65%, and the vortex suppression efficiency is the highest. Therefore, the use of 3 ⁇ 3 cross-spaced method is the best method for eddy current suppression.
  • an eddy current suppression structure includes a magnetostrictive layer 1, and also includes an insulating medium layer, the insulating medium layer is disposed in the magnetostrictive layer 1 for The eddy current is interrupted to suppress the eddy current loss of the bulk acoustic wave magnetoelectric antenna.
  • At least one first insulating dielectric layer 2 is provided in the magnetostrictive layer 1 along its thickness direction.
  • the first insulating dielectric layer 2 is three layers and parallel to each other, the thickness of each first insulating dielectric layer 2 is 5-100 nm, and the material of the magnetostrictive layer 1 is FeGaB film, the total thickness of the FeGaB film is 1 ⁇ m, the conductivity range of the first insulating dielectric layer 2 is 0-100 S/m, and the first insulating dielectric layer 2 is composed of Al 2 O 3 , Si 3 N 4 and Made of any one or more materials in AlN.
  • the arrow indicates the direction of the magnetic flux
  • the first insulating dielectric layer is arranged in parallel with the XOY surface (thickness direction), so as to realize its function of breaking the eddy current.
  • the second insulating dielectric layer 3 is three layers parallel to each other, the thickness of each second insulating dielectric layer 3 is 5-30 nm, and the material of the magnetostrictive layer 1 is FeGaB film, the total thickness of the FeGaB film is 1 ⁇ m, the conductivity of the second insulating dielectric layer 3 is in the range of 0-100 S/m, and the second insulating dielectric layer 3 is composed of Al 2 O 3 , Si 3 N 4 and Made of any one or more materials in AlN.
  • the arrow indicates the direction of the magnetic flux
  • the second insulating dielectric layer is arranged parallel to the XOZ surface (width direction), so as to achieve its function of breaking the eddy current; and the insulating layer is parallel to the ZOY surface (length direction)
  • the setting can not interrupt the eddy current.
  • step a use magnetron sputtering method to deposit the magnetostrictive layer 1 on the upper electrode of the body bulk acoustic wave resonator;
  • step b The magnetostrictive layer 1 is uniformly covered with a layer of photoresist 5, and then pre-baking, exposure and development are carried out in sequence;
  • Step c dry etching is used to etch the structure formed in the step b on the magnetostrictive layer 1 3 grooves in the thickness direction of the stretchable layer 1;
  • step d sputter on the structure formed in the step c by a magnetron sputtering method to form 3 layers of second insulating medium in the thickness direction of the magnetostrictive layer 1 Layer 3;
  • Step e Use a metal lift-off process to remove the photoresist 5 on the surface of the magnetostrictive layer 1;
  • Step f Use chemical mechanical polishing to remove the photoresist 5 above the surface of the magnetostrictive layer 1
  • an eddy current suppression structure includes a magnetostrictive layer 1, and also includes an insulating medium layer, the insulating medium layer is disposed in the magnetostrictive layer 1 for The eddy current is interrupted to suppress the eddy current loss of the bulk acoustic wave magnetoelectric antenna.
  • At least one first insulating dielectric layer 2 is provided in the magnetostrictive layer 1 along its thickness direction, and the magnetostrictive layer 1 is provided along its width direction.
  • the first insulating dielectric layer 2 is three layers and parallel to each other, and the second insulating dielectric layer 3 is three layers and parallel to each other.
  • the thickness of the insulating medium layer 2 is 5-100 nm
  • the thickness of each second insulating medium layer 3 is 5-30 nm
  • the material of the magnetostrictive layer 1 is FeGaB film
  • the total thickness of the FeGaB film is 1 ⁇ m.
  • the conductivity range of the first insulating dielectric layer 2 and the second insulating dielectric layer 3 is 0-100S/m, and the first insulating dielectric layer 2 and the second insulating dielectric layer 3 are made of Al 2 O 3 , It is made of any one or more materials among Si 3 N 4 and AlN.
  • the method for preparing the eddy current suppression structure includes step A: depositing a magnetostrictive layer 1 on the upper electrode of the bulk acoustic wave resonator by magnetron sputtering; step B: forming in step A The first insulating medium layer 2 in the thickness direction of the magnetostrictive layer 1 formed in the step A is deposited on the magnetostrictive layer 1 by a magnetron sputtering method; step C: the first insulating medium layer 2 formed in the step B The magnetostrictive layer 1 is deposited on the first insulating medium layer 2; Step D: Repeat the above step BC twice to obtain the first insulating medium layer structure; Step E: Use a glue spinner to apply the first insulating medium layer The layer structure is uniformly covered with a layer of photoresist 5, and then pre-baking, exposure and development are carried out in sequence; Step F: Dry etching is used to etch the magnetostrictive layer 1 on the structure formed in Step E At least one groove
  • the volume eddy current suppression method in the magnetostrictive layer adopts the thickness direction (z-axis direction) to insert the insulating medium layer, as shown in Figure 3; the middle surface eddy current suppression method of the magnetostrictive layer adopts Insert the insulating medium layer in the width direction (y-axis direction), as shown in Figure 4; the overall eddy current suppression method in the magnetostrictive layer adopts the insulating medium in the thickness direction (z-axis direction) and the width direction (y-axis direction) at the same time. Layer, as shown in Figure 5.
  • the magnetic material in the magnetostrictive layer is a FeGaB film with a thickness of 1 ⁇ m and a surface area of 100 ⁇ m ⁇ 100 ⁇ m.
  • the number of layers inserted into the insulating dielectric layer in the thickness direction and the width direction is 3 ⁇ 3, respectively.
  • the volume eddy current suppression method inserts the insulating dielectric layer along the thickness direction with a thickness of 5-30 nm, and the number of separation layers is 3 layers.
  • the surface eddy current suppression method inserts the insulating medium layer along the width direction with a width of 5-100 nm, and the number of separation layers is 3 layers. As shown in Figure 6.
  • the insertion of the insulating dielectric layer in the width direction is to etch the middle groove through a photolithography process, and then use the physical vapor deposition method to fill the insulating dielectric layer.
  • the photolithography process uses reactive ion etching.
  • Figure 6 is a process flow diagram of the eddy current suppression structure.
  • Step 1 Magnetron sputtering is used to deposit a FeGaB magnetic film on the upper electrode of the bulk acoustic wave resonator, and the thickness of the FeGaB magnetic film is 500 nm.
  • Step 3 Deposit a FeGaB magnetic film on the Al 2 O 3 insulating layer, the thickness of the magnetic film is 500 nm.
  • Step 4 Use a glue spinner to evenly cover a layer of photoresist on the FeGaB magnetic film, pre-baking, exposing, and developing.
  • the photoresist is a positive photoresist.
  • Step 5 Use dry etching to etch grooves in the magnetostrictive layer.
  • Step 6 Sputter the Al 2 O 3 insulating layer in the magnetostrictive layer by magnetron sputtering.
  • Step 7 Use a metal lift-off process to remove the photoresist on the surface of the FeGaB magnetic film.
  • Step 8 Use chemical mechanical polishing to smooth the Al 2 O 3 insulating layer 3 above the surface of the FeGaB magnetic film.
  • the present invention proposes a method and structure for suppressing the eddy current loss of a bulk acoustic wave magnetoelectric antenna.
  • This method suppresses the eddy current loss by inserting the insulating medium alternately spaced in the transverse and longitudinal directions in the magnetostrictive layer, and suppresses the eddy current loss in the magnetic film under the premise of ensuring that the size of the insulating medium layer is as small as possible. Insert the smallest size insulating medium to suppress eddy current magnetic film structure.
  • the present invention divides the eddy currents into volume eddy currents and surface eddy currents, and proposes a method for isolating the two by inserting an insulating dielectric layer, and constructs a minimum-size insulating medium for inserting
  • the magnetic film structure that suppresses eddy current ensures that the eddy current loss reaches the minimum.
  • the present invention inserts Al 2 O 3 insulating layers alternately spaced in the thickness and width directions in the magnetostrictive layer to reduce the body eddy current and surface eddy current loss, and minimize the eddy current loss of the magnetostrictive layer. It solves the problem that the air gap spaced magnetostrictive layer in the prior art solution causes the stress discontinuity and the low radiation efficiency of the magnetoelectric antenna.
  • Using the Al 2 O 3 insulating layer as the spacer layer can improve the soft magnetic properties of FeGaB, effectively reduce the coercive force of FeGaB, and improve the sensitivity of the radiation area. Through simulation analysis, this solution can effectively reduce the eddy current loss by more than 65%, and greatly improve the radiation efficiency of the magnetoelectric antenna.

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Abstract

An eddy current suppression structure, comprising a magnetostriction layer (1) and insulating dielectric layers (2, 3). The insulating dielectric layers (2, 3) are provided in the magnetostriction layer (1) and are used for breaking an eddy current so as to suppress eddy current loss of a bulk acoustic wave magnetoelectric antenna. The insulating dielectric layers (2, 3) are inserted into the magnetostriction layer (1) to reduce eddy current loss, so that the radiation efficiency of the bulk acoustic wave magnetoelectric antenna is improved, and the problems in the prior art of discontinuous stress and low radiation efficiency of a magnetoelectric antenna caused by a magnetostriction layer (1) having air gaps are solved. The insulating dielectric layers (2, 3) are used as spacer layers, so the soft magnetic characteristic of the magnetostriction layer (1) can be improved, the coercive force of the magnetostriction layer (1) is effectively reduced, and the sensitivity of a radiation region is improved. By means of simulation analysis, the solution can effectively reduce the eddy current loss by more than 65%, and greatly improve the radiation efficiency of a magnetoelectric antenna.

Description

一种涡流抑制结构及其制备方法Eddy current suppression structure and preparation method thereof 技术领域Technical field
本发明涉及射频微电子机械系统领域,具体涉及一种涡流抑制结构及其制备方法。The invention relates to the field of radio frequency microelectronic mechanical systems, in particular to an eddy current suppression structure and a preparation method thereof.
背景技术Background technique
目前智能手机、平板电脑、射频器件和雷达等设备中常用的天线是基于电流传导工作原理的电小天线,通常尺寸通常较大,难以实现小型化,还具有阻抗匹配困难、辐射效率低等缺点。体声波磁电天线利用体声波谐振原理和磁电效应来辐射电磁信号,从根本上解决了电小天线阻抗匹配困难和辐射效率过低的问题,而且利用声波谐振原理,可以实现器件的小型化。体声波磁电天线由压电层和磁致伸缩层交叉复合构成。At present, the commonly used antennas in smart phones, tablet computers, radio frequency devices and radars are electrically small antennas based on the working principle of current conduction. They are usually large in size and difficult to achieve miniaturization. They also have disadvantages such as difficulty in impedance matching and low radiation efficiency. . The bulk acoustic wave magnetoelectric antenna uses the principle of bulk acoustic wave resonance and the magnetoelectric effect to radiate electromagnetic signals, which fundamentally solves the problems of impedance matching of electric small antennas and low radiation efficiency. Moreover, using the principle of acoustic wave resonance can realize the miniaturization of the device. . The bulk acoustic wave magnetoelectric antenna is composed of a piezoelectric layer and a magnetostrictive layer cross composite.
在体声波磁电天线中,磁致伸缩层作为发射天线的辐射层,在该层内通过机磁效应产生电磁信号向外界辐射电磁波,其能量利用率直接决定发射天线的辐射效率。磁致伸缩层往往选用电导率较大的FeGaB磁性薄膜,在内部磁场的激励下,会产生较大的涡流损耗,影响发射天线辐射功率。在保证磁致伸缩层良好的软磁特性的前提下,减小涡流损耗将极大提高磁电天线的辐射效率。体声波磁电天线在射频系统中应用时,涡流损耗会造成过多的能量损耗,导致天线的辐射效率降低限制其应用范围。In the bulk acoustic wave magnetoelectric antenna, the magnetostrictive layer is used as the radiation layer of the transmitting antenna. In this layer, electromagnetic signals are generated through the electromagnetic effect to radiate electromagnetic waves to the outside. The energy utilization rate directly determines the radiation efficiency of the transmitting antenna. Magnetostrictive layer often chooses FeGaB magnetic film with higher conductivity. Under the excitation of internal magnetic field, large eddy current loss will be generated, which will affect the radiation power of transmitting antenna. On the premise of ensuring the good soft magnetic properties of the magnetostrictive layer, reducing the eddy current loss will greatly improve the radiation efficiency of the magnetoelectric antenna. When a bulk acoustic wave magnetoelectric antenna is used in a radio frequency system, the eddy current loss will cause excessive energy loss, resulting in a reduction in the antenna's radiation efficiency and limiting its application range.
Zhi Yao and Yuanxun Ethan Wang在标题为“3D ADI-FDTD Modeling of Platform Reduction with Thin Film Ferromagnetic Material”中提出了一种基于3D ADI-FDTD的涡流抑制方法,该方法利用将磁致伸缩层分割成长条状的方法打断涡流环以达到抑制涡流损耗的目的。该方法的关键技术为:Zhi Yao and Yuanxun Ethan Wang in the title "3D ADI-FDTD Modeling of Platform Reduction with Thin Film Ferromagnetic Material" proposed a 3D ADI-FDTD-based eddy current suppression method, which uses the magnetostrictive layer to be divided into long strips. The eddy current ring is broken in a way to achieve the purpose of suppressing eddy current loss. The key technologies of this method are:
(一)分割的长条宽度应该和厚度相当,这样可以使打断的涡流回路足够小。(1) The width of the divided strip should be equal to the thickness, so that the interrupted eddy current loop can be small enough.
(二)长条的纵向方向应沿着磁通方向。相邻长条之间为空气隙,由于磁致伸缩层的导电性很高,大部分电磁场都集中在空气隙中。其结构如附图1和2。(2) The longitudinal direction of the strip should be along the direction of magnetic flux. There is an air gap between adjacent strips. Because of the high conductivity of the magnetostrictive layer, most of the electromagnetic field is concentrated in the air gap. Its structure is shown in Figures 1 and 2.
上述方案提出的涡流损耗抑制方法,虽然能很好的抑制涡流损耗,但同时也会大大降低磁电天线的辐射效率,主要问题为:(一)采用空气隙作为分割长条之间的左右间隙(沿y轴方向)和上下层间隙(沿z轴方向),导致体声波磁电天线在实际工作时,应力无法在左右和上下两层之间连续传递,只有下层的磁致伸缩薄膜工作,上层磁致伸缩层中没有应力传导,无法激发出电磁波,进而使整个磁致伸缩层的辐射效率大大下降。(二)该方案中沿y轴方向的每个空气隙宽度为0.2μm占单个磁膜条宽度的1/5,沿z轴方向的每个空气隙厚度0.3μm占单个磁膜条宽度的1/2。较大尺寸的空气隙虽然可以很好的抑制涡流损耗,但会降低整个磁致伸缩层的软磁特性,导致磁电天线辐射效率过低。Although the eddy current loss suppression method proposed by the above scheme can suppress the eddy current loss very well, it will also greatly reduce the radiation efficiency of the magnetoelectric antenna. The main problems are: (1) Air gap is used as the left and right gap between the divided strips. (Along the y-axis direction) and the gap between the upper and lower layers (along the z-axis direction), the stress cannot be continuously transferred between the left and right and the upper and lower layers when the bulk acoustic wave magnetoelectric antenna is actually working. Only the lower magnetostrictive film works. There is no stress conduction in the upper magnetostrictive layer, and electromagnetic waves cannot be excited, thereby greatly reducing the radiation efficiency of the entire magnetostrictive layer. (2) In this scheme, the width of each air gap along the y-axis direction is 0.2μm, which accounts for 1/5 of the width of a single magnetic film strip, and the thickness of each air gap along the z-axis direction is 0.3μm which accounts for 1/5 of the width of a single magnetic film strip. /2. Although a larger air gap can well suppress the eddy current loss, it will reduce the soft magnetic properties of the entire magnetostrictive layer, resulting in too low radiation efficiency of the magnetoelectric antenna.
发明内容Summary of the invention
本发明所要解决的技术问题是提供一种涡流抑制结构及其制备方法。The technical problem to be solved by the present invention is to provide an eddy current suppression structure and a preparation method thereof.
本发明解决上述技术问题的技术方案如下:一种涡流抑制结构,包括磁致伸缩层,还包括绝缘介质层,所述绝缘介质层设置于所述磁致伸缩层内,用于打断涡流。The technical solution of the present invention to solve the above technical problems is as follows: an eddy current suppression structure including a magnetostrictive layer and an insulating medium layer disposed in the magnetostrictive layer for breaking the eddy current.
本发明的有益效果是:本发明在磁致伸缩层中插入绝缘介质层来减小涡流损耗,使体声波磁电天线的辐射效率提高,解决了现有技术方案中空气隙间隔磁致伸缩层导致应力不连续、磁电天线辐射效率低的问题。使用绝缘介质层作为间隔层可以改善磁致伸缩层的软磁特性,有效降低磁致伸缩层的矫顽力,提高辐射区的灵敏度。通过仿真分析,该方案可以有效减小涡流损耗65%以上,大幅地提高磁电天线的辐射效率。The beneficial effects of the present invention are: the present invention inserts an insulating dielectric layer in the magnetostrictive layer to reduce eddy current loss, improve the radiation efficiency of the bulk acoustic wave magnetoelectric antenna, and solve the problem of the air gap spaced magnetostrictive layer in the prior art. This leads to the problems of discontinuous stress and low radiation efficiency of the magnetoelectric antenna. Using an insulating medium layer as a spacer layer can improve the soft magnetic properties of the magnetostrictive layer, effectively reduce the coercivity of the magnetostrictive layer, and improve the sensitivity of the radiation area. Through simulation analysis, this solution can effectively reduce the eddy current loss by more than 65%, and greatly improve the radiation efficiency of the magnetoelectric antenna.
在上述技术方案的基础上,本发明还可以做如下改进:On the basis of the above technical solution, the present invention can also be improved as follows:
进一步,所述磁致伸缩层内沿其厚度方向设置第一绝缘介质层和/或所述磁致伸缩层内沿其宽度方向设置第二绝缘介质层。Further, a first insulating medium layer is arranged in the magnetostrictive layer along its thickness direction and/or a second insulating medium layer is arranged in the magnetostrictive layer along its width direction.
采用上述进一步方案的有益效果是本发明根据磁致伸缩层中感应电流的趋肤效应将涡流分为体涡流和面涡流,第一绝缘介质层能够很好的抑制体涡流,从而减小涡流损耗;第二绝缘介质层能够很好的抑制面涡流,从而减小涡流损耗。The beneficial effect of adopting the above-mentioned further solution is that the present invention divides the eddy current into volume eddy current and surface eddy current according to the skin effect of the induced current in the magnetostrictive layer, and the first insulating dielectric layer can well suppress the volume eddy current, thereby reducing the eddy current loss. ; The second insulating dielectric layer can well suppress the surface eddy current, thereby reducing the eddy current loss.
进一步,所述磁致伸缩层内沿其厚度方向设置至少一层所述第一绝缘介质层。Further, at least one layer of the first insulating medium layer is arranged in the magnetostrictive layer along its thickness direction.
采用上述进一步方案的有益效果是第一绝缘介质层能够很好的抑制体涡流,从而减小涡流损耗。The beneficial effect of adopting the above-mentioned further solution is that the first insulating dielectric layer can well suppress the body eddy current, thereby reducing the eddy current loss.
进一步,所述第一绝缘介质层为三层且相互平行,每层所述第一绝缘介质层的厚度为5-100nm,所述磁致伸缩层的材料为FeGaB薄膜,所述FeGaB薄膜总厚度为1μm,所述第一绝缘介质层的电导率范围为0-100S/m,所述第一绝缘介质层由Al 2O 3、Si 3N 4和AlN中任一种或者多种材料制成。 Further, the first insulating dielectric layer is three layers parallel to each other, each of the first insulating dielectric layer has a thickness of 5-100 nm, the magnetostrictive layer is made of FeGaB film, and the total thickness of the FeGaB film is 1μm, the conductivity of the first insulating dielectric layer ranges from 0-100S/m, and the first insulating dielectric layer is made of any one or more of Al 2 O 3 , Si 3 N 4 and AlN .
采用上述进一步方案的有益效果是经过模拟结果可知,3层已足以解决体涡流抑制问题;第一绝缘介质层在5-100nm,体涡流可以得到很好的抑制;FeGaB薄膜是优质的磁致伸缩层材料;绝缘介质层为上述材料时,具有很好的涡流抑制效果。The beneficial effect of adopting the above further scheme is that the simulation results show that 3 layers are sufficient to solve the problem of bulk eddy current suppression; the first insulating dielectric layer is 5-100nm, and the bulk eddy current can be well suppressed; FeGaB film is a high-quality magnetostrictive Layer material; when the insulating dielectric layer is the above material, it has a good eddy current suppression effect.
进一步,所述磁致伸缩层内沿其宽度方向设置至少一层所述第二绝缘介质层。Further, at least one second insulating dielectric layer is arranged in the magnetostrictive layer along its width direction.
采用上述进一步方案的有益效果是第二绝缘介质层能够很好的抑制面涡流,从而减小涡流损耗。The beneficial effect of adopting the above-mentioned further solution is that the second insulating dielectric layer can well suppress the surface eddy current, thereby reducing the eddy current loss.
进一步,所述第二绝缘介质层为三层且相互平行,每层所述第二绝缘介质层的厚度为5-30nm,所述磁致伸缩层的材料为FeGaB薄膜,所述FeGaB 薄膜总厚度为1μm,所述第二绝缘介质层的电导率范围为0-100S/m,所述第二绝缘介质层由Al 2O 3、Si 3N 4和AlN中任一种或者多种材料制成。 Further, the second insulating dielectric layer is three layers parallel to each other, each of the second insulating dielectric layer has a thickness of 5-30 nm, the magnetostrictive layer is made of FeGaB film, and the total thickness of the FeGaB film is 1μm, the conductivity of the second insulating dielectric layer ranges from 0-100S/m, and the second insulating dielectric layer is made of any one or more of Al 2 O 3 , Si 3 N 4 and AlN .
采用上述进一步方案的有益效果是经过模拟结果可知,3层已足以解决面涡流抑制问题;第二绝缘介质层在5-30nm,面涡流可以得到很好的抑制;FeGaB薄膜是优质的磁致伸缩层材料;绝缘介质层为上述材料时,具有很好的涡流抑制效果。The beneficial effect of adopting the above-mentioned further scheme is that the simulation results show that three layers are sufficient to solve the problem of surface eddy current suppression; the second insulating dielectric layer is 5-30nm, and the surface eddy current can be well suppressed; FeGaB film is a high-quality magnetostrictive Layer material; when the insulating dielectric layer is the above material, it has a good eddy current suppression effect.
进一步,所述磁致伸缩层内沿其厚度方向设置至少一层第一绝缘介质层,所述磁致伸缩层内沿其宽度方向设置至少一层第二绝缘介质层,所述第一绝缘介质层和所述第二绝缘介质层交叉间隔设置。Further, at least one first insulating medium layer is arranged in the magnetostrictive layer along its thickness direction, at least one second insulating medium layer is arranged in the magnetostrictive layer along its width direction, and the first insulating medium The layer and the second insulating dielectric layer are intersected and arranged at intervals.
采用上述进一步方案的有益效果是在磁致伸缩层中插入沿厚度和沿宽度方向交替间隔的绝缘介质层来减小其体涡流和面涡流损耗,提出了综合考虑体涡流和面涡流的插入绝缘介质层隔离结构,使磁致伸缩层的涡流损耗最小。解决了现有技术方案中空气隙间隔磁致伸缩层导致应力不连续、磁电天线辐射效率低的问题。使用绝缘介质层作为间隔层可以改善磁致伸缩层的软磁特性,有效降低磁致伸缩层的矫顽力,提高辐射区的灵敏度。通过仿真分析,该方案可以有效减小涡流损耗65%以上,大幅地提高磁电天线的辐射效率。The beneficial effect of adopting the above-mentioned further scheme is to insert insulating dielectric layers alternately spaced along the thickness and width in the magnetostrictive layer to reduce its body eddy current and surface eddy current losses, and a comprehensive consideration of body eddy current and surface eddy current insertion insulation is proposed. The isolation structure of the dielectric layer minimizes the eddy current loss of the magnetostrictive layer. It solves the problem that the air gap spaced magnetostrictive layer in the prior art solution causes the stress discontinuity and the low radiation efficiency of the magnetoelectric antenna. Using an insulating medium layer as a spacer layer can improve the soft magnetic properties of the magnetostrictive layer, effectively reduce the coercivity of the magnetostrictive layer, and improve the sensitivity of the radiation area. Through simulation analysis, this solution can effectively reduce the eddy current loss by more than 65%, and greatly improve the radiation efficiency of the magnetoelectric antenna.
进一步,所述第一绝缘介质层为三层且相互平行,所述第二绝缘介质层为三层且相互平行,每层所述第一绝缘介质层厚度为5-100nm,每层所述第二绝缘介质层厚度为5-30nm,所述磁致伸缩层的材料为FeGaB薄膜,所述FeGaB薄膜总厚度为1μm,所述第一绝缘介质层和所述第二绝缘介质层的电导率范围为0-100S/m,所述第一绝缘介质层和所述第二绝缘介质层均由Al 2O 3、Si 3N 4和AlN中任一种或者多种材料制成。 Further, the first insulating medium layer is three layers and parallel to each other, the second insulating medium layer is three layers and parallel to each other, each layer of the first insulating medium layer has a thickness of 5-100 nm, and each layer of the first insulating medium layer The thickness of the second insulating medium layer is 5-30 nm, the material of the magnetostrictive layer is FeGaB film, the total thickness of the FeGaB film is 1 μm, and the conductivity ranges of the first insulating medium layer and the second insulating medium layer It is 0-100 S/m, and both the first insulating dielectric layer and the second insulating dielectric layer are made of any one or more of Al 2 O 3 , Si 3 N 4 and AlN.
采用上述进一步方案的有益效果是经过模拟结果可知,3层已足以解决面涡流抑制问题,第一绝缘介质层厚度为5-100nm,第二绝缘介质层在 5-30nm,面涡流可以得到很好的抑制,上述限定在保证绝缘介质层尺寸尽可能小的前提下对磁膜中的涡流损耗进行抑制,并提出了一种插入最小尺寸绝缘介质用于抑制涡流的磁膜结构,该结构能够在有效抑制磁致伸缩层中涡流损耗的同时,可以有效的保证磁致伸缩层良好的软磁特性,提高磁电天线辐射效率,使体声波磁电天线更适用于无线通信中的应用场合;FeGaB薄膜是优质的磁致伸缩层材料;绝缘介质层为上述材料时,具有很好的涡流抑制效果。The beneficial effect of adopting the above-mentioned further scheme is that through simulation results, 3 layers are sufficient to solve the problem of surface eddy current suppression. The thickness of the first insulating dielectric layer is 5-100nm, and the second insulating dielectric layer is 5-30nm. The surface eddy current can be well obtained. The above limitation suppresses the eddy current loss in the magnetic film under the premise of ensuring that the size of the insulating medium layer is as small as possible, and proposes a magnetic film structure that inserts the smallest size insulating medium to suppress the eddy current. While effectively suppressing the eddy current loss in the magnetostrictive layer, it can effectively ensure the good soft magnetic properties of the magnetostrictive layer, improve the radiation efficiency of the magnetoelectric antenna, and make the bulk acoustic wave magnetoelectric antenna more suitable for wireless communication applications; FeGaB The thin film is a high-quality magnetostrictive layer material; when the insulating medium layer is the above material, it has a good eddy current suppression effect.
本发明还涉及一种磁电天线,包括上电极,还包括所述涡流抑制结构,所述涡流抑制结构设置在所述上电极上。The present invention also relates to a magnetoelectric antenna, including an upper electrode, and further including the eddy current suppression structure, the eddy current suppression structure being arranged on the upper electrode.
本发明还涉及一种所述涡流抑制结构的制备方法,包括,步骤1:在机体(体声波谐振器上电极)上利用磁控溅射法沉积磁致伸缩层;步骤2:在所述步骤1形成的所述磁致伸缩层上利用磁控溅射法沉积沿其厚度方向的第一绝缘介质层;步骤3:在所述步骤2形成的所述第一绝缘介质层上再次沉积磁致伸缩层;步骤4:直接得到所述涡流抑制结构,或者再重复进行上述步骤2-3至少一次,得到所述涡流抑制结构;或者,步骤a:在机体(体声波谐振器上电极)上利用磁控溅射法沉积磁致伸缩层;步骤b:用甩胶机在所述磁致伸缩层上均匀覆盖一层光刻胶,然后依次进行前烘、曝光和显影;步骤c:用干法刻蚀在所述步骤b形成的结构上刻蚀出在所述磁致伸缩层厚度方向的至少一个凹槽;步骤d:用磁控溅射法在所述步骤c形成的结构上溅射以形成在所述磁致伸缩层厚度方向的至少一层第二绝缘介质层;步骤e:采用金属剥离工艺去除所述所述磁致伸缩层表面的所述光刻胶;步骤f:利用化学机械研磨将高出所述磁致伸缩层表面的所述第二绝缘介质层磨平;或者,步骤A:在(体声波谐振器上电极)机体上利用磁控溅射法沉积磁致伸缩层;步骤B:在所述步骤A形成的所述磁致伸缩层上利用磁控溅射法沉积所述步骤A形成的所述磁致伸缩层厚度方向的第一绝缘介质层;步骤C:在所 述步骤B形成的所述第一绝缘介质层上沉积磁致伸缩层;步骤D:直接得到第一绝缘介质层结构,或者再重复进行上述步骤B-C至少一次,得到所述第一绝缘介质层结构;步骤E:用甩胶机在所述第一绝缘介质层结构上均匀覆盖一层光刻胶,然后依次进行前烘,曝光和显影;步骤F:用干法刻蚀在所述步骤E形成的结构上刻蚀出在所述磁致伸缩层宽度方向的至少一个凹槽;步骤G:用磁控溅射法在所述步骤F形成的结构上溅射以形成在所述磁致伸缩层宽度方向的至少一层所述第二绝缘介质层;步骤H:采用金属剥离工艺去除所述步骤D形成的所述第一绝缘介质层结构表面的所述光刻胶;步骤I:利用化学机械研磨将高出所述步骤D形成的所述第一绝缘介质层结构表面的所述第二绝缘介质层磨平。The present invention also relates to a method for preparing the eddy current suppression structure, including: Step 1: Depositing a magnetostrictive layer on the body (the upper electrode of the bulk acoustic wave resonator) by magnetron sputtering; Step 2: In the step 1. Use a magnetron sputtering method to deposit a first insulating medium layer along its thickness on the magnetostrictive layer formed; Step 3: deposit a magnetostrictive layer again on the first insulating medium layer formed in step 2. Stretching layer; Step 4: Obtain the eddy current suppression structure directly, or repeat the above steps 2-3 at least once to obtain the eddy current suppression structure; or, Step a: Use on the body (the upper electrode of the bulk acoustic wave resonator) Magnetron sputtering method is used to deposit the magnetostrictive layer; Step b: Use a spinner to evenly cover a layer of photoresist on the magnetostrictive layer, and then perform pre-baking, exposure and development in sequence; Step c: Use a dry method Etching etches at least one groove in the thickness direction of the magnetostrictive layer on the structure formed in step b; step d: sputtering on the structure formed in step c by a magnetron sputtering method At least one second insulating dielectric layer is formed in the thickness direction of the magnetostrictive layer; step e: removing the photoresist on the surface of the magnetostrictive layer by a metal stripping process; step f: using chemical machinery Grinding to smooth the second insulating medium layer higher than the surface of the magnetostrictive layer; or, step A: depositing the magnetostrictive layer on the body (the upper electrode of the bulk acoustic wave resonator) by magnetron sputtering; Step B: Depositing a first insulating medium layer in the thickness direction of the magnetostrictive layer formed in Step A on the magnetostrictive layer formed in Step A by using a magnetron sputtering method; Step C: Depositing a magnetostrictive layer on the first insulating dielectric layer formed in step B; Step D: directly obtaining the first insulating dielectric layer structure, or repeating the above step BC at least once to obtain the first insulating dielectric layer structure Step E: Use a spinner to uniformly cover a layer of photoresist on the first insulating dielectric layer structure, and then perform pre-baking, exposure and development in sequence; Step F: Use dry etching to form in Step E At least one groove in the width direction of the magnetostrictive layer is etched on the structure; Step G: Sputter the structure formed in the step F using a magnetron sputtering method to form the magnetostrictive layer At least one layer of the second insulating dielectric layer in the width direction; Step H: Use a metal lift-off process to remove the photoresist on the surface of the first insulating dielectric layer structure formed in Step D; Step I: Use chemical machinery Grinding smoothes the second insulating dielectric layer higher than the surface of the first insulating dielectric layer structure formed in the step D.
采用上述进一步方案的有益效果是利用上述方法能够简单、快速且保证涡流抑制功能的前提下实现涡流抑制结构的生产,从而提高磁电天线辐射效率。The beneficial effect of adopting the above-mentioned further solution is that the above-mentioned method can be used to realize the production of eddy current suppression structure simply, quickly and under the premise of ensuring the eddy current suppression function, thereby improving the radiation efficiency of the magnetoelectric antenna.
附图说明Description of the drawings
图1为现有技术涡流损耗抑制结构之图一;Fig. 1 is a figure 1 of a prior art eddy current loss suppression structure;
图2为现有技术涡流损耗抑制结构之图二;Figure 2 is the second diagram of the prior art eddy current loss suppression structure;
图3为本发明磁致伸缩层体涡流抑制结构示意图;3 is a schematic diagram of the eddy current suppression structure of the magnetostrictive layer body of the present invention;
图4为本发明磁致伸缩层面涡流抑制结构图;Fig. 4 is a structural diagram of the magnetostrictive layer eddy current suppression structure of the present invention;
图5为本发明磁致伸缩层3×3涡流抑制结构;Fig. 5 is a 3×3 eddy current suppression structure of the magnetostrictive layer of the present invention;
图6为本发明涡流抑制结构工艺流程图;Figure 6 is a process flow diagram of the eddy current suppression structure of the present invention;
图7为本发明Al 2O 3薄膜厚度对表面损耗的影响示意图; 7 is a schematic diagram of the influence of the thickness of the Al 2 O 3 film of the present invention on the surface loss;
图8为本发明Al 2O 3薄膜层数对表面损耗的影响示意图; 8 is a schematic diagram of the influence of the number of Al 2 O 3 film layers on the surface loss of the present invention;
图9为本发明Al 2O 3薄膜厚度对体内损耗的影响示意图; 9 is a schematic diagram of the influence of the thickness of the Al 2 O 3 film of the present invention on the body loss;
图10为本发明Al 2O 3薄膜层数对体内损耗的影响示意图; 10 is a schematic diagram of the influence of the number of Al 2 O 3 film layers of the present invention on the body loss;
图11为本发明不同Al 2O 3厚度对应的总损耗密度示意图。 Fig. 11 is a schematic diagram of the total loss density corresponding to different Al 2 O 3 thicknesses of the present invention.
附图中,各标号所代表的部件列表如下:In the drawings, the list of parts represented by each number is as follows:
1、磁致伸缩层,2、第一绝缘介质层,3、第二绝缘介质层,4、体声波谐振器上极,5、光刻胶,6、掩膜板,7、空气隙。1. Magnetostrictive layer, 2. First insulating medium layer, 3. Second insulating medium layer, 4. Upper pole of bulk acoustic wave resonator, 5. Photoresist, 6. Mask, 7. Air gap.
具体实施方式Detailed ways
以下结合附图对本发明的原理和特征进行描述,所举实例只用于解释本发明,并非用于限定本发明的范围。The principles and features of the present invention will be described below in conjunction with the accompanying drawings. The examples cited are only used to explain the present invention, and not used to limit the scope of the present invention.
利用Comsol仿真软件分别对磁致伸缩层的面涡流和体涡流进行仿真,其验证结果分别如图所示。Use Comsol simulation software to simulate the surface eddy current and volume eddy current of the magnetostrictive layer, and the verification results are shown in the figure.
如图7所示,Al 2O 3厚度(绝缘介质层)在5nm以内的表面损耗密度明显降低,之后虽有逐渐减小的趋势,但降低速率基本维持在5%以内,使表面涡流得到了很好的抑制。因此,Al 2O 3厚度在5nm以内面涡流损耗得到很好的抑制,可根据工艺条件适当加厚Al 2O 3厚度。在保持插入的Al 2O 3绝缘层总厚度不变的情况下,将其分隔为2、3、4、5层,均匀间隔在FeGaB金属层中,图8中取总厚度100nm(可根据工艺条件适当加厚)时,不同Al 2O 3绝缘层数对应的面涡流密度变化趋势,随层数的增加,表面损耗密度明显降低,但3层之后的降低速率低于20%,且降低速率逐渐趋于平缓。因此,3层已足以解决面涡流抑制的问题。 As shown in Figure 7, the surface loss density of the Al 2 O 3 thickness (insulating dielectric layer) within 5 nm is significantly reduced, and although there is a gradual decrease thereafter, the reduction rate is basically maintained within 5%, so that the surface eddy current is obtained Very good suppression. Therefore, the eddy current loss on the inner surface of the Al 2 O 3 thickness of 5 nm is well suppressed, and the Al 2 O 3 thickness can be appropriately thickened according to the process conditions. While keeping the total thickness of the inserted Al 2 O 3 insulating layer unchanged, divide it into 2, 3, 4, and 5 layers, evenly spaced in the FeGaB metal layer. The total thickness is 100nm in Figure 8 (according to the process When the condition is appropriately thickened), the change trend of the surface eddy current density corresponding to the number of Al 2 O 3 insulating layers, with the increase of the number of layers, the surface loss density is significantly reduced, but the rate of decrease after 3 layers is less than 20%, and the rate of decrease Gradually flatten out. Therefore, 3 layers are sufficient to solve the problem of surface vortex suppression.
根据仿真结果,不同Al 2O 3厚度对应的体内损耗密度的变化趋势如图9所示。在加入5nm厚度的Al 2O 3后,体内损耗密度降低了60%以上,在Al 2O 3厚度为30nm左右时,涡流损耗密度最小,之后有微小的增长趋势,增长速率小于1%。因此,对于Al 2O 3绝缘层厚度在5-30nm体涡流可以得到很好的抑制。将Al 2O 3层总厚度设定为体涡流损耗密度最小值处30nm,将其分隔为2、3、4、5层,结果如图10所示。随Al 2O 3绝缘层数的增加,体涡流损耗密度明显降低,同表面损耗密度一样,3层之后的降低速率逐渐趋缓。 According to the simulation results, the changing trend of the body loss density corresponding to different Al 2 O 3 thicknesses is shown in Fig. 9. After Al 2 O 3 with a thickness of 5 nm is added, the internal loss density is reduced by more than 60%. When the thickness of Al 2 O 3 is about 30 nm, the eddy current loss density is the smallest, and then there is a slight growth trend, with a growth rate of less than 1%. Therefore, the eddy current of the Al 2 O 3 insulating layer with a thickness of 5-30 nm can be well suppressed. The total thickness of the Al 2 O 3 layer was set to 30 nm at the minimum volume eddy current loss density, and it was divided into 2, 3, 4, and 5 layers. The results are shown in FIG. 10. With the increase of the number of Al 2 O 3 insulating layers, the bulk eddy current loss density decreases significantly. Like the surface loss density, the rate of decrease gradually slows down after 3 layers.
综合考虑面涡流和体涡流各自最优的隔法,采用了如图6的3×3交叉隔法分别计算了面涡流和体涡流,其总损耗密度的仿真结果如图11所示。很明显,采用交叉隔的总损耗密度最低,在沿厚度方向(z轴方向)和宽度方向(y轴方向)加入的Al 2O 3厚度均为10nm时,分别采用沿厚度方向(z轴方向)插入3层Al 2O 3绝缘层和沿宽度方向(y轴方向)插入3层Al 2O 3绝缘层,总损耗密度分别降低了10%和47%左右,而采用交叉隔3×3的降低率为65%,对涡流抑制效率最高。因此,采用3×3交叉隔法是涡流抑制的最优方法。 Considering the optimal separation methods of surface eddy currents and volume eddy currents, the 3×3 cross separation method as shown in Figure 6 is used to calculate the surface eddy currents and volume eddy currents respectively. The simulation results of the total loss density are shown in Figure 11. Obviously, the total loss density of the cross-space is the lowest. When the thickness of Al 2 O 3 added in the thickness direction (z-axis direction) and the width direction (y-axis direction) are both 10nm, the thickness direction (z-axis direction) ) into three-layer Al 2 O 3 insulating layer and the insert 3 layer Al 2 O 3 insulating layer in the width direction (y axis direction), the total loss density decreased by about 10% and 47%, while the use of cross-compartments of 3 × 3 The reduction rate is 65%, and the vortex suppression efficiency is the highest. Therefore, the use of 3×3 cross-spaced method is the best method for eddy current suppression.
实施例1Example 1
如图3-11,作为本发明的基础方案,一种涡流抑制结构,包括磁致伸缩层1,还包括绝缘介质层,所述绝缘介质层设置于所述磁致伸缩层1内,用于打断涡流从而抑制体声波磁电天线涡流损耗。As shown in Figure 3-11, as the basic solution of the present invention, an eddy current suppression structure includes a magnetostrictive layer 1, and also includes an insulating medium layer, the insulating medium layer is disposed in the magnetostrictive layer 1 for The eddy current is interrupted to suppress the eddy current loss of the bulk acoustic wave magnetoelectric antenna.
如图3,作为本实施例进一步的方案,所述磁致伸缩层1内沿其厚度方向设置至少一层所述第一绝缘介质层2。As shown in Fig. 3, as a further solution of this embodiment, at least one first insulating dielectric layer 2 is provided in the magnetostrictive layer 1 along its thickness direction.
作为本实施例进一步的方案,所述第一绝缘介质层2为三层且相互平行,每层所述第一绝缘介质层2的厚度为5-100nm,所述磁致伸缩层1的材料为FeGaB薄膜,所述FeGaB薄膜总厚度为1μm,所述第一绝缘介质层2的电导率范围为0-100S/m,所述第一绝缘介质层2由Al 2O 3、Si 3N 4和AlN中任一种或者多种材料制成。 As a further solution of this embodiment, the first insulating dielectric layer 2 is three layers and parallel to each other, the thickness of each first insulating dielectric layer 2 is 5-100 nm, and the material of the magnetostrictive layer 1 is FeGaB film, the total thickness of the FeGaB film is 1 μm, the conductivity range of the first insulating dielectric layer 2 is 0-100 S/m, and the first insulating dielectric layer 2 is composed of Al 2 O 3 , Si 3 N 4 and Made of any one or more materials in AlN.
具体的,如图3,箭头指示磁通方向,第一绝缘介质层与XOY面(厚度方向)平行设置,从而实现其打断涡流的功能。Specifically, as shown in FIG. 3, the arrow indicates the direction of the magnetic flux, and the first insulating dielectric layer is arranged in parallel with the XOY surface (thickness direction), so as to realize its function of breaking the eddy current.
如图3和6,所述涡流抑制结构的制备方法,步骤1:在机体体声波谐振器上电极上利用磁控溅射法沉积磁致伸缩层1;步骤2:在所述步骤1形成的所述磁致伸缩层1上利用磁控溅射法沉积沿其厚度方向的第一绝缘介质层2;步骤3:在所述步骤2形成的所述第一绝缘介质层2上再次沉积磁致伸缩 层1;步骤4:再重复进行上述步骤2次,得到所述涡流抑制结构。As shown in Figures 3 and 6, the method for preparing the eddy current suppression structure, Step 1: Use magnetron sputtering to deposit the magnetostrictive layer 1 on the upper electrode of the body's bulk acoustic wave resonator; Step 2: Formed in the step 1 The magnetron sputtering method is used to deposit the first insulating medium layer 2 along its thickness on the magnetostrictive layer 1; step 3: the magnetostrictive layer 2 is again deposited on the first insulating medium layer 2 formed in the step 2. Stretching layer 1; Step 4: Repeat the above steps twice to obtain the eddy current suppression structure.
实施例2Example 2
如图3-11,作为本发明的基础方案,一种涡流抑制结构,包括磁致伸缩层1,还包括绝缘介质层,所述绝缘介质层设置于所述磁致伸缩层1内,用于打断涡流从而抑制体声波磁电天线涡流损耗。As shown in Figure 3-11, as the basic solution of the present invention, an eddy current suppression structure includes a magnetostrictive layer 1, and also includes an insulating medium layer, the insulating medium layer is disposed in the magnetostrictive layer 1 for The eddy current is interrupted to suppress the eddy current loss of the bulk acoustic wave magnetoelectric antenna.
如图4,作为本实施例进一步的方案,所述磁致伸缩层1内沿其宽度方向设置至少一层所述第二绝缘介质层3。As shown in Fig. 4, as a further solution of this embodiment, at least one second insulating dielectric layer 3 is provided in the magnetostrictive layer 1 along its width direction.
作为本实施例进一步的方案,所述第二绝缘介质层3为三层且相互平行,每层所述第二绝缘介质层3的厚度为5-30nm,所述磁致伸缩层1的材料为FeGaB薄膜,所述FeGaB薄膜总厚度为1μm,所述第二绝缘介质层3的电导率范围为0-100S/m,所述第二绝缘介质层3由Al 2O 3、Si 3N 4和AlN中任一种或者多种材料制成。 As a further solution of this embodiment, the second insulating dielectric layer 3 is three layers parallel to each other, the thickness of each second insulating dielectric layer 3 is 5-30 nm, and the material of the magnetostrictive layer 1 is FeGaB film, the total thickness of the FeGaB film is 1 μm, the conductivity of the second insulating dielectric layer 3 is in the range of 0-100 S/m, and the second insulating dielectric layer 3 is composed of Al 2 O 3 , Si 3 N 4 and Made of any one or more materials in AlN.
具体的,如图4所述,箭头指示磁通方向,第二绝缘介质层与XOZ面(宽度方向)平行设置,从而实现其打断涡流的功能;而绝缘层与ZOY面(长度方向)平行设置则不能打断涡流。Specifically, as shown in Figure 4, the arrow indicates the direction of the magnetic flux, and the second insulating dielectric layer is arranged parallel to the XOZ surface (width direction), so as to achieve its function of breaking the eddy current; and the insulating layer is parallel to the ZOY surface (length direction) The setting can not interrupt the eddy current.
如图4和6,所述涡流抑制结构的制备方法,步骤a:在机体体声波谐振器上电极上利用磁控溅射法沉积磁致伸缩层1;步骤b:用甩胶机在所述磁致伸缩层1上均匀覆盖一层光刻胶5,然后依次进行前烘、曝光和显影;步骤c:用干法刻蚀在所述步骤b形成的结构上刻蚀出在所述磁致伸缩层1厚度方向的3个凹槽;步骤d:用磁控溅射法在所述步骤c形成的结构上溅射以形成在所述磁致伸缩层1厚度方向的3层第二绝缘介质层3;步骤e:采用金属剥离工艺去除所述所述磁致伸缩层1表面的所述光刻胶5;步骤f:利用化学机械研磨将高出所述磁致伸缩层1表面的所述第二绝缘介质层3磨平。本方法中刻蚀前在光刻胶上放置掩膜板6,是保证非凹槽部分不被刻蚀。4 and 6, the preparation method of the eddy current suppression structure, step a: use magnetron sputtering method to deposit the magnetostrictive layer 1 on the upper electrode of the body bulk acoustic wave resonator; step b: The magnetostrictive layer 1 is uniformly covered with a layer of photoresist 5, and then pre-baking, exposure and development are carried out in sequence; Step c: dry etching is used to etch the structure formed in the step b on the magnetostrictive layer 1 3 grooves in the thickness direction of the stretchable layer 1; step d: sputter on the structure formed in the step c by a magnetron sputtering method to form 3 layers of second insulating medium in the thickness direction of the magnetostrictive layer 1 Layer 3; Step e: Use a metal lift-off process to remove the photoresist 5 on the surface of the magnetostrictive layer 1; Step f: Use chemical mechanical polishing to remove the photoresist 5 above the surface of the magnetostrictive layer 1 The second insulating dielectric layer 3 is ground flat. In this method, the mask 6 is placed on the photoresist before etching to ensure that the non-groove part is not etched.
实施例3Example 3
如图3-11,作为本发明的基础方案,一种涡流抑制结构,包括磁致伸缩层1,还包括绝缘介质层,所述绝缘介质层设置于所述磁致伸缩层1内,用于打断涡流从而抑制体声波磁电天线涡流损耗。As shown in Figure 3-11, as the basic solution of the present invention, an eddy current suppression structure includes a magnetostrictive layer 1, and also includes an insulating medium layer, the insulating medium layer is disposed in the magnetostrictive layer 1 for The eddy current is interrupted to suppress the eddy current loss of the bulk acoustic wave magnetoelectric antenna.
如图5和6,作为本实施例进一步的方案,所述磁致伸缩层1内沿其厚度方向设置至少一层第一绝缘介质层2,所述磁致伸缩层1内沿其宽度方向设置至少一层第二绝缘介质层3,所述第一绝缘介质层2和所述第二绝缘介质层3交叉间隔设置。As shown in Figures 5 and 6, as a further solution of this embodiment, at least one first insulating dielectric layer 2 is provided in the magnetostrictive layer 1 along its thickness direction, and the magnetostrictive layer 1 is provided along its width direction. There is at least one second insulating dielectric layer 3, and the first insulating dielectric layer 2 and the second insulating dielectric layer 3 are arranged at intervals and crossing each other.
如图5和6,作为本实施例进一步的方案,所述第一绝缘介质层2为三层且相互平行,所述第二绝缘介质层3为三层且相互平行,每层所述第一绝缘介质层2厚度为5-100nm,每层所述第二绝缘介质层3厚度为5-30nm,所述磁致伸缩层1的材料为FeGaB薄膜,所述FeGaB薄膜总厚度为1μm,所述第一绝缘介质层2和所述第二绝缘介质层3的电导率范围为0-100S/m,所述第一绝缘介质层2和所述第二绝缘介质层3均由Al 2O 3、Si 3N 4和AlN中任一种或者多种材料制成。 As shown in Figures 5 and 6, as a further solution of this embodiment, the first insulating dielectric layer 2 is three layers and parallel to each other, and the second insulating dielectric layer 3 is three layers and parallel to each other. The thickness of the insulating medium layer 2 is 5-100 nm, the thickness of each second insulating medium layer 3 is 5-30 nm, the material of the magnetostrictive layer 1 is FeGaB film, and the total thickness of the FeGaB film is 1 μm. The conductivity range of the first insulating dielectric layer 2 and the second insulating dielectric layer 3 is 0-100S/m, and the first insulating dielectric layer 2 and the second insulating dielectric layer 3 are made of Al 2 O 3 , It is made of any one or more materials among Si 3 N 4 and AlN.
具体的,如图5所述,箭头指示磁通方向,第一绝缘介质层与XOY面(厚度方向)平行设置,从而实现其打断涡流的功能;第二绝缘层与ZOX面(宽度方向)平行设置,从而实现其打断涡流的功能,而绝缘层与ZOY面(长度方向)平行则不能打断涡流。Specifically, as shown in Figure 5, the arrow indicates the direction of the magnetic flux, the first insulating dielectric layer is arranged parallel to the XOY surface (thickness direction), so as to achieve its function of breaking the eddy current; the second insulating layer and the ZOX surface (width direction) It is arranged in parallel to realize the function of breaking the eddy current, and the insulating layer is parallel to the ZOY surface (length direction), and the eddy current cannot be interrupted.
如图5和6,所述涡流抑制结构的制备方法,包括步骤A:在体声波谐振器上电极上利用磁控溅射法沉积磁致伸缩层1;步骤B:在所述步骤A形成的所述磁致伸缩层1上利用磁控溅射法沉积所述步骤A形成的所述磁致伸缩层1厚度方向的第一绝缘介质层2;步骤C:在所述步骤B形成的所述第一绝缘介质层2上沉积磁致伸缩层1;步骤D:再重复进行上述步骤B-C两次, 得到所述第一绝缘介质层结构;步骤E:用甩胶机在所述第一绝缘介质层结构上均匀覆盖一层光刻胶5,然后依次进行前烘,曝光和显影;步骤F:用干法刻蚀在所述步骤E形成的结构上刻蚀出在所述磁致伸缩层1宽度方向的至少一个凹槽;步骤G:用磁控溅射法在所述步骤F形成的结构上溅射以形成在所述磁致伸缩层1宽度方向的至少一层所述第二绝缘介质层4;步骤H:采用金属剥离工艺去除所述步骤D形成的所述第一绝缘介质层结构表面的所述光刻胶5;步骤I:利用化学机械研磨将高出所述步骤D形成的所述第一绝缘介质层结构表面的所述第二绝缘介质层3磨平。本方法中刻蚀前在光刻胶上放置掩膜板6,是保证非凹槽部分不被刻蚀。As shown in Figures 5 and 6, the method for preparing the eddy current suppression structure includes step A: depositing a magnetostrictive layer 1 on the upper electrode of the bulk acoustic wave resonator by magnetron sputtering; step B: forming in step A The first insulating medium layer 2 in the thickness direction of the magnetostrictive layer 1 formed in the step A is deposited on the magnetostrictive layer 1 by a magnetron sputtering method; step C: the first insulating medium layer 2 formed in the step B The magnetostrictive layer 1 is deposited on the first insulating medium layer 2; Step D: Repeat the above step BC twice to obtain the first insulating medium layer structure; Step E: Use a glue spinner to apply the first insulating medium layer The layer structure is uniformly covered with a layer of photoresist 5, and then pre-baking, exposure and development are carried out in sequence; Step F: Dry etching is used to etch the magnetostrictive layer 1 on the structure formed in Step E At least one groove in the width direction; step G: sputtering on the structure formed in step F by a magnetron sputtering method to form at least one layer of the second insulating medium in the width direction of the magnetostrictive layer 1 Layer 4; Step H: Use a metal lift-off process to remove the photoresist 5 on the surface of the first insulating dielectric layer structure formed in Step D; Step I: Use chemical mechanical polishing to be higher than that formed in Step D The second insulating dielectric layer 3 on the surface of the first insulating dielectric layer structure is ground flat. In this method, the mask 6 is placed on the photoresist before etching to ensure that the non-groove part is not etched.
实施例1-3中所用方法均为本领域内现有技术。The methods used in Examples 1-3 are all existing technologies in the field.
体声波磁电天线涡流损耗抑制方法:磁致伸缩层中体涡流抑制方法采用沿厚度方向(z轴方向)插入绝缘介质层,如附图3所示;磁致伸缩层中面涡流抑制方法采用沿宽度方向(y轴方向)插入绝缘介质层,如附图4所示;磁致伸缩层中整体涡流抑制方法采用同时沿厚度方向(z轴方向)和宽度方向(y轴方向)插入绝缘介质层,如附图5所示。Bulk acoustic wave magnetoelectric antenna eddy current loss suppression method: the volume eddy current suppression method in the magnetostrictive layer adopts the thickness direction (z-axis direction) to insert the insulating medium layer, as shown in Figure 3; the middle surface eddy current suppression method of the magnetostrictive layer adopts Insert the insulating medium layer in the width direction (y-axis direction), as shown in Figure 4; the overall eddy current suppression method in the magnetostrictive layer adopts the insulating medium in the thickness direction (z-axis direction) and the width direction (y-axis direction) at the same time. Layer, as shown in Figure 5.
所述磁致伸缩层中磁性材料为FeGaB薄膜,厚度为1μm,表面积为100μm×100μm。The magnetic material in the magnetostrictive layer is a FeGaB film with a thickness of 1 μm and a surface area of 100 μm×100 μm.
所述绝缘介质层电导率范围为0-100S/m,如Al 2O 3、Si 3N 4、AlN。 The conductivity range of the insulating dielectric layer is 0-100 S/m, such as Al 2 O 3 , Si 3 N 4 , and AlN.
所述沿厚度方向和宽度方向插入绝缘介质层的层数分别为3×3。The number of layers inserted into the insulating dielectric layer in the thickness direction and the width direction is 3×3, respectively.
所述体涡流抑制方法沿厚度方向插入绝缘介质层厚度为5-30nm,分隔层数为3层。The volume eddy current suppression method inserts the insulating dielectric layer along the thickness direction with a thickness of 5-30 nm, and the number of separation layers is 3 layers.
所述面涡流抑制方法沿宽度方向插入绝缘介质层宽度为5-100nm,分隔层数为3层。如附图6所示。The surface eddy current suppression method inserts the insulating medium layer along the width direction with a width of 5-100 nm, and the number of separation layers is 3 layers. As shown in Figure 6.
所述沿宽度方向插入绝缘介质层是通过光刻工艺刻蚀中间凹槽,然后利 用物理气相沉积法填充绝缘介质层。所述光刻工艺采用反应离子刻蚀。The insertion of the insulating dielectric layer in the width direction is to etch the middle groove through a photolithography process, and then use the physical vapor deposition method to fill the insulating dielectric layer. The photolithography process uses reactive ion etching.
下面结合附图6对本发明实施方案详细说明:The following describes the embodiments of the present invention in detail with reference to FIG. 6:
图6为涡流抑制结构工艺流程图。Figure 6 is a process flow diagram of the eddy current suppression structure.
步骤1:在体声波谐振器上电极上利用磁控溅射沉积FeGaB磁性薄膜,所述FeGaB磁性薄膜厚度为500nm。Step 1: Magnetron sputtering is used to deposit a FeGaB magnetic film on the upper electrode of the bulk acoustic wave resonator, and the thickness of the FeGaB magnetic film is 500 nm.
步骤2:在FeGaB磁性薄膜上利用磁控溅射法沉积Al 2O 3绝缘层,所述Al 2O 3绝缘层厚度为5-30nm。 Step 2: Depositing an Al 2 O 3 insulating layer on the FeGaB magnetic film by magnetron sputtering , the thickness of the Al 2 O 3 insulating layer being 5-30 nm.
步骤3:在Al 2O 3绝缘层沉积FeGaB磁性薄膜,所述磁性薄膜厚度为500nm。 Step 3: Deposit a FeGaB magnetic film on the Al 2 O 3 insulating layer, the thickness of the magnetic film is 500 nm.
步骤4:用甩胶机在FeGaB磁性薄膜上均匀覆盖一层光刻胶,前烘,曝光,显影。所述光刻胶为正胶。Step 4: Use a glue spinner to evenly cover a layer of photoresist on the FeGaB magnetic film, pre-baking, exposing, and developing. The photoresist is a positive photoresist.
步骤5:用干法刻蚀在磁致伸缩层刻蚀出凹槽。Step 5: Use dry etching to etch grooves in the magnetostrictive layer.
步骤6:用磁控溅射法在磁致伸缩层中溅射Al 2O 3绝缘层。 Step 6: Sputter the Al 2 O 3 insulating layer in the magnetostrictive layer by magnetron sputtering.
步骤7:采用金属剥离工艺去除FeGaB磁性薄膜表面的光刻胶。Step 7: Use a metal lift-off process to remove the photoresist on the surface of the FeGaB magnetic film.
步骤8:利用化学机械研磨将高出FeGaB磁性薄膜表面的Al 2O 3绝缘层3磨平。 Step 8: Use chemical mechanical polishing to smooth the Al 2 O 3 insulating layer 3 above the surface of the FeGaB magnetic film.
本发明为解决上述技术缺陷,提出了一种体声波磁电天线涡流损耗抑制方法和结构。该方法通过在磁致伸缩层中插入横向和纵向交替间隔的绝缘介质来抑制涡流损耗,在保证绝缘介质层尺寸尽可能小的前提下对磁膜中的涡流损耗进行抑制,并提出了一种插入最小尺寸绝缘介质用于抑制涡流的磁膜结构。该结构能够在有效抑制磁致伸缩层中涡流损耗的同时,可以有效的保证磁致伸缩层良好的软磁特性,提高磁电天线辐射效率,使体声波磁电天线更适用于无线通信中的应用场合。本发明根据磁致伸缩层中感应电流的趋肤效应将涡流分为体涡流和面涡流,提出了综合考虑二者的插入绝缘介质层隔离方法,并且构造了一种插入最小尺寸绝缘介质用于抑制涡流的磁膜结构, 保证涡流损耗达到最小值。In order to solve the above technical defects, the present invention proposes a method and structure for suppressing the eddy current loss of a bulk acoustic wave magnetoelectric antenna. This method suppresses the eddy current loss by inserting the insulating medium alternately spaced in the transverse and longitudinal directions in the magnetostrictive layer, and suppresses the eddy current loss in the magnetic film under the premise of ensuring that the size of the insulating medium layer is as small as possible. Insert the smallest size insulating medium to suppress eddy current magnetic film structure. This structure can effectively suppress the eddy current loss in the magnetostrictive layer, and can effectively ensure the good soft magnetic properties of the magnetostrictive layer, improve the radiation efficiency of the magnetoelectric antenna, and make the bulk acoustic wave magnetoelectric antenna more suitable for wireless communication. Application occasions. According to the skin effect of the induced current in the magnetostrictive layer, the present invention divides the eddy currents into volume eddy currents and surface eddy currents, and proposes a method for isolating the two by inserting an insulating dielectric layer, and constructs a minimum-size insulating medium for inserting The magnetic film structure that suppresses eddy current ensures that the eddy current loss reaches the minimum.
本发明在磁致伸缩层中插入沿厚度和沿宽度方向交替间隔的Al 2O 3绝缘层来减小其体涡流和面涡流损耗,使磁致伸缩层的涡流损耗最小。解决了现有技术方案中空气隙间隔磁致伸缩层导致应力不连续、磁电天线辐射效率低的问题。使用Al 2O 3绝缘层作为间隔层可以改善FeGaB的软磁特性,有效降低FeGaB的矫顽力,提高辐射区的灵敏度。通过仿真分析,该方案可以有效减小涡流损耗65%以上,大幅地提高磁电天线的辐射效率。 The present invention inserts Al 2 O 3 insulating layers alternately spaced in the thickness and width directions in the magnetostrictive layer to reduce the body eddy current and surface eddy current loss, and minimize the eddy current loss of the magnetostrictive layer. It solves the problem that the air gap spaced magnetostrictive layer in the prior art solution causes the stress discontinuity and the low radiation efficiency of the magnetoelectric antenna. Using the Al 2 O 3 insulating layer as the spacer layer can improve the soft magnetic properties of FeGaB, effectively reduce the coercive force of FeGaB, and improve the sensitivity of the radiation area. Through simulation analysis, this solution can effectively reduce the eddy current loss by more than 65%, and greatly improve the radiation efficiency of the magnetoelectric antenna.
以上所述仅为本发明的较佳实施例,并不用以限制本发明,凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above are only the preferred embodiments of the present invention and are not intended to limit the present invention. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included in the protection of the present invention. Within range.

Claims (10)

  1. 一种涡流抑制结构,包括磁致伸缩层(1),其特征在于,还包括绝缘介质层,所述绝缘介质层设置于所述磁致伸缩层(1)内,用于打断涡流。An eddy current suppression structure includes a magnetostrictive layer (1), and is characterized in that it also includes an insulating medium layer disposed in the magnetostrictive layer (1) for breaking the eddy current.
  2. 根据权利要求1所述一种涡流抑制结构,其特征在于,所述磁致伸缩层(1)内沿其厚度方向设置第一绝缘介质层(2)和/或所述磁致伸缩层(1)内沿其宽度方向设置第二绝缘介质层(3)。The eddy current suppression structure according to claim 1, wherein the magnetostrictive layer (1) is provided with a first insulating medium layer (2) and/or the magnetostrictive layer (1) along its thickness direction. A second insulating dielectric layer (3) is arranged in the width direction thereof.
  3. 根据权利要求2所述一种涡流抑制结构,其特征在于,所述磁致伸缩层(1)内沿其厚度方向设置至少一层所述第一绝缘介质层(2)。The eddy current suppression structure according to claim 2, wherein at least one layer of the first insulating dielectric layer (2) is arranged in the magnetostrictive layer (1) along its thickness direction.
  4. 根据权利要求3所述一种涡流抑制结构,其特征在于,所述第一绝缘介质层(2)为三层且相互平行,每层所述第一绝缘介质层(2)的厚度为5-100nm,所述磁致伸缩层(1)的材料为FeGaB薄膜,所述FeGaB薄膜总厚度为1μm,所述第一绝缘介质层(2)的电导率范围为0-100S/m,所述第一绝缘介质层(2)由Al 2O 3、Si 3N 4和AlN中任一种或者多种材料制成。 The eddy current suppression structure according to claim 3, characterized in that, the first insulating dielectric layer (2) is three layers parallel to each other, and the thickness of each first insulating dielectric layer (2) is 5- 100nm, the material of the magnetostrictive layer (1) is FeGaB film, the total thickness of the FeGaB film is 1μm, the conductivity range of the first insulating dielectric layer (2) is 0-100S/m, the first An insulating dielectric layer (2) is made of any one or more of Al 2 O 3 , Si 3 N 4 and AlN.
  5. 根据权利要求2所述一种涡流抑制结构,其特征在于,所述磁致伸缩层(1)内沿其宽度方向设置至少一层所述第二绝缘介质层(3)。The eddy current suppression structure according to claim 2, wherein at least one second insulating dielectric layer (3) is arranged in the magnetostrictive layer (1) along its width direction.
  6. 根据权利要求5所述一种涡流抑制结构,其特征在于,所述第二绝缘介质层(3)为三层且相互平行,每层所述第二绝缘介质层(3)的厚度为5-30nm,所述磁致伸缩层(1)的材料为FeGaB薄膜,所述FeGaB薄膜总厚度为1μm,所述第二绝缘介质层(3)的电导率范围为0-100S/m,所述第二绝缘介质层(3)由Al 2O 3、Si 3N 4和AlN中任一种或者多种材料制成。 The eddy current suppression structure according to claim 5, characterized in that the second insulating dielectric layer (3) is three layers parallel to each other, and the thickness of each second insulating dielectric layer (3) is 5- 30nm, the material of the magnetostrictive layer (1) is FeGaB film, the total thickness of the FeGaB film is 1μm, the conductivity of the second insulating dielectric layer (3) ranges from 0-100S/m, and the first The second insulating dielectric layer (3) is made of any one or more of Al 2 O 3 , Si 3 N 4 and AlN.
  7. 根据权利要求2所述一种涡流抑制结构,其特征在于,所述磁致伸缩层(1)内沿其厚度方向设置至少一层第一绝缘介质层(2),所述磁致伸缩层(1)内沿其宽度方向设置至少一层第二绝缘介质层(3),所述第一绝缘介质层(2)和所述第二绝缘介质层(3)交叉间隔设置。The eddy current suppression structure according to claim 2, wherein at least one first insulating medium layer (2) is arranged in the magnetostrictive layer (1) along its thickness direction, and the magnetostrictive layer (1) 1) At least one second insulating medium layer (3) is arranged in the inner portion along its width direction, and the first insulating medium layer (2) and the second insulating medium layer (3) are arranged at intervals and crossing each other.
  8. 根据权利要求7所述一种涡流抑制结构,其特征在于,所述第一绝缘介质层(2)为三层且相互平行,所述第二绝缘介质层(3)为三层且相互平行,每层所述第一绝缘介质层(2)厚度为5-100nm,每层所述第二绝缘介质层(3)厚度为5-30nm,所述磁致伸缩层(1)的材料为FeGaB薄膜,所述FeGaB薄膜总厚度为1μm,所述第一绝缘介质层(2)和所述第二绝缘介质层(3)的电导率范围为0-100S/m,所述第一绝缘介质层(2)和所述第二绝缘介质层(3)均由Al 2O 3、Si 3N 4和AlN中任一种或者多种材料制成。 The eddy current suppression structure according to claim 7, wherein the first insulating dielectric layer (2) is three layers and parallel to each other, and the second insulating dielectric layer (3) is three layers and parallel to each other, The thickness of each layer of the first insulating medium layer (2) is 5-100 nm, the thickness of each layer of the second insulating medium layer (3) is 5-30 nm, and the material of the magnetostrictive layer (1) is FeGaB thin film , The total thickness of the FeGaB film is 1 μm, the conductivity range of the first insulating dielectric layer (2) and the second insulating dielectric layer (3) is 0-100S/m, and the first insulating dielectric layer ( 2) and the second insulating dielectric layer (3) are made of any one or more of Al 2 O 3 , Si 3 N 4 and AlN.
  9. 一种磁电天线,包括上电极,其特征在于,还包括权利要求1-7任一项所述涡流抑制结构,所述涡流抑制结构设置在所述上电极上。A magnetoelectric antenna, comprising an upper electrode, characterized in that it further comprises the eddy current suppression structure according to any one of claims 1-7, and the eddy current suppression structure is arranged on the upper electrode.
  10. 一种如权利要求2-9任一项所述涡流抑制结构的制备方法,其特征在于,包括以下步骤:A method for preparing the eddy current suppression structure according to any one of claims 2-9, characterized in that it comprises the following steps:
    步骤1:在机体上利用磁控溅射法沉积磁致伸缩层(1);Step 1: Use magnetron sputtering to deposit a magnetostrictive layer (1) on the body;
    步骤2:在所述步骤1形成的所述磁致伸缩层(1)上利用磁控溅射法沉积沿其厚度方向的第一绝缘介质层(2);Step 2: Depositing a first insulating dielectric layer (2) along the thickness direction of the magnetron sputtering method on the magnetostrictive layer (1) formed in the step 1;
    步骤3:在所述步骤2形成的所述第一绝缘介质层(2)上再次沉积磁致伸缩层(1);Step 3: Depositing a magnetostrictive layer (1) again on the first insulating dielectric layer (2) formed in the step 2;
    步骤4:直接得到所述涡流抑制结构,或者再重复进行上述步骤2-3至少一次,得到所述涡流抑制结构;Step 4: Obtain the vortex suppression structure directly, or repeat the above steps 2-3 at least once to obtain the vortex suppression structure;
    或者,or,
    步骤a:在机体上利用磁控溅射法沉积磁致伸缩层(1);Step a: Depositing a magnetostrictive layer (1) on the body by magnetron sputtering;
    步骤b:用甩胶机在所述磁致伸缩层(1)上均匀覆盖一层光刻胶(5),然后依次进行前烘、曝光和显影;Step b: Use a glue spinner to evenly cover a layer of photoresist (5) on the magnetostrictive layer (1), and then perform pre-baking, exposure and development in sequence;
    步骤c:用干法刻蚀在所述步骤b形成的结构上刻蚀出在所述磁致伸缩层(1)厚度方向的至少一个凹槽;Step c: Use dry etching to etch at least one groove in the thickness direction of the magnetostrictive layer (1) on the structure formed in step b;
    步骤d:用磁控溅射法在所述步骤c形成的结构上溅射以形成在所述磁 致伸缩层(1)厚度方向的至少一层第二绝缘介质层(3);Step d: Sputtering on the structure formed in step c by a magnetron sputtering method to form at least one second insulating medium layer (3) in the thickness direction of the magnetostrictive layer (1);
    步骤e:采用金属剥离工艺去除所述所述磁致伸缩层(1)表面的所述光刻胶(5);Step e: removing the photoresist (5) on the surface of the magnetostrictive layer (1) by using a metal stripping process;
    步骤f:利用化学机械研磨将高出所述磁致伸缩层(1)表面的所述第二绝缘介质层(3)磨平;Step f: Use chemical mechanical polishing to smooth the second insulating dielectric layer (3) higher than the surface of the magnetostrictive layer (1);
    或者,or,
    步骤A:在机体上利用磁控溅射法沉积磁致伸缩层(1);Step A: Depositing a magnetostrictive layer on the body by magnetron sputtering (1);
    步骤B:在所述步骤A形成的所述磁致伸缩层(1)上利用磁控溅射法沉积所述步骤A形成的所述磁致伸缩层(1)厚度方向的第一绝缘介质层(2);Step B: Depositing the first insulating medium layer in the thickness direction of the magnetostrictive layer (1) formed in the step A by using a magnetron sputtering method on the magnetostrictive layer (1) formed in the step A (2);
    步骤C:在所述步骤B形成的所述第一绝缘介质层(2)上沉积磁致伸缩层(1);Step C: Depositing a magnetostrictive layer (1) on the first insulating dielectric layer (2) formed in the step B;
    步骤D:直接得到第一绝缘介质层结构,或者再重复进行上述步骤B-C至少一次,得到所述第一绝缘介质层结构;Step D: Obtain the first insulating dielectric layer structure directly, or repeat the above steps B-C at least once to obtain the first insulating dielectric layer structure;
    步骤E:用甩胶机在所述第一绝缘介质层结构上均匀覆盖一层光刻胶(5),然后依次进行前烘,曝光和显影;Step E: Use a glue spinner to uniformly cover a layer of photoresist (5) on the first insulating dielectric layer structure, and then perform pre-baking, exposure and development in sequence;
    步骤F:用干法刻蚀在所述步骤E形成的结构上刻蚀出在所述磁致伸缩层(1)宽度方向的至少一个凹槽;Step F: Use dry etching to etch at least one groove in the width direction of the magnetostrictive layer (1) on the structure formed in Step E;
    步骤G:用磁控溅射法在所述步骤F形成的结构上溅射以形成在所述磁致伸缩层(1)宽度方向的至少一层所述第二绝缘介质层(4);Step G: Sputter the structure formed in step F by using a magnetron sputtering method to form at least one second insulating medium layer (4) in the width direction of the magnetostrictive layer (1);
    步骤H:采用金属剥离工艺去除所述步骤D形成的所述第一绝缘介质层结构表面的所述光刻胶(5);Step H: Use a metal lift-off process to remove the photoresist (5) on the surface of the first insulating dielectric layer structure formed in Step D;
    步骤I:利用化学机械研磨将高出所述步骤D形成的所述第一绝缘介质层结构表面的所述第二绝缘介质层(3)磨平。Step I: Use chemical mechanical polishing to smooth the second insulating dielectric layer (3) that is higher than the surface of the first insulating dielectric layer structure formed in Step D.
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