TWI784580B - Piezoelectric mems accelerometer and method for manufacturing the same - Google Patents
Piezoelectric mems accelerometer and method for manufacturing the same Download PDFInfo
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本發明是有關於一種加速規及其製造方法,且特別是有關於一種壓電式微機電加速規及其製造方法。 The present invention relates to an accelerometer and its manufacturing method, and in particular to a piezoelectric micro-electromechanical accelerometer and its manufacturing method.
加速規(Accelerometer)是藉由量測加速度來獲得物體受力程度的慣性感測器。隨著微機電(Micro Electro-Mechanical Systems,MEMS)製程的發展,加速規的尺寸可大幅縮小且可大量製造,而被廣泛應用於各個領域。 An accelerometer is an inertial sensor that obtains the degree of force on an object by measuring acceleration. With the development of micro-electro-mechanical systems (MEMS) manufacturing processes, the size of accelerometers can be greatly reduced and mass-manufactured, and are widely used in various fields.
然而,當使用MEMS製程製造加速規時,需要經過複數道微影製程(photolithography),曝光顯影時容易因為曝光機對準誤差、光罩圖形誤差等因素,而導致加速規短路損壞,降低製作良率。 However, when using the MEMS process to manufacture accelerometers, it needs to go through multiple photolithography processes. During exposure and development, it is easy to cause short-circuit damage to accelerometers due to factors such as exposure machine alignment errors and mask pattern errors, reducing the production quality. Rate.
本發明之目的在於提供一種壓電式微機電加速規及其製造方法,以解決上述問題。 The object of the present invention is to provide a piezoelectric MEMS accelerometer and its manufacturing method to solve the above problems.
依據本發明之一實施方式是提供一種壓電式微機電加速規,包含一 載體、一第一電極層、一壓電層及一第二電極層。載體包含一第一表面及一第二表面相對於第一表面。第一表面包含一第一突塊部及一第二突塊部,第一突塊部突出於第一表面,第二突塊部突出於第一表面,且與第一突塊部間隔設置。第一電極層設置於第二表面上,壓電層設置於第一電極層上,第二電極層設置於壓電層上。第一電極層及第二電極層的分布範圍皆位於壓電層的分布範圍內。第一突塊部是壓電式微機電加速規的質量塊的主要構成物,第二突塊部是壓電式微機電加速規的連接部的主要構成物。 According to one embodiment of the present invention, a piezoelectric MEMS accelerometer is provided, comprising a Carrier, a first electrode layer, a piezoelectric layer and a second electrode layer. The carrier includes a first surface and a second surface opposite to the first surface. The first surface includes a first protrusion and a second protrusion, the first protrusion protrudes from the first surface, and the second protrusion protrudes from the first surface and is spaced apart from the first protrusion. The first electrode layer is arranged on the second surface, the piezoelectric layer is arranged on the first electrode layer, and the second electrode layer is arranged on the piezoelectric layer. The distribution ranges of the first electrode layer and the second electrode layer are both within the distribution range of the piezoelectric layer. The first protruding part is the main component of the mass block of the piezoelectric microelectromechanical accelerometer, and the second protruding part is the main component of the connection part of the piezoelectric microelectromechanical accelerometer.
依據本發明之另一實施方式是提供一種壓電式微機電加速規的製造方法,包含以下步驟。提供一基板,基板包含一頂面及一底面相對於頂面。形成一第一電極層,使第一電極層位於頂面上且局部覆蓋頂面。形成一壓電層,使壓電層位於第一電極層上。形成一第二電極層,使第二電極層位於壓電層上。進行一蝕刻步驟,移除基板的一部份,使基板形成一載體,其中載體包含一第一表面及一第二表面相對於第一表面,第一表面包含一第一突塊部及一第二突塊部,第一突塊部突出於第一表面,第二突塊部突出於第一表面且與第一突塊部間隔設置,第一表面、第一突塊部及第二突塊部係底面受蝕刻後往內凹陷所形成,第二表面係頂面經蝕刻後所餘留的部分。壓電式微機電加速規中,第一電極層及第二電極層皆位於壓電層的分布範圍內。第一突塊部是壓電式微機電加速規的質量塊的主要構成物,第二突塊部是壓電式微機電加速規的連接部的主要構成物。 Another embodiment of the present invention provides a method for manufacturing a piezoelectric MEMS accelerometer, which includes the following steps. A substrate is provided, and the substrate includes a top surface and a bottom surface opposite to the top surface. A first electrode layer is formed so that the first electrode layer is located on the top surface and partially covers the top surface. A piezoelectric layer is formed such that the piezoelectric layer is located on the first electrode layer. A second electrode layer is formed so that the second electrode layer is located on the piezoelectric layer. An etching step is performed to remove a portion of the substrate so that the substrate forms a carrier, wherein the carrier includes a first surface and a second surface opposite to the first surface, the first surface includes a first bump portion and a first surface Two protrusions, the first protrusion protrudes from the first surface, the second protrusion protrudes from the first surface and is spaced apart from the first protrusion, the first surface, the first protrusion and the second protrusion The part is formed by inward depression after the bottom surface is etched, and the second surface is the remaining part after the top surface is etched. In the piezoelectric MEMS accelerometer, both the first electrode layer and the second electrode layer are located within the distribution range of the piezoelectric layer. The first protruding part is the main component of the mass block of the piezoelectric microelectromechanical accelerometer, and the second protruding part is the main component of the connection part of the piezoelectric microelectromechanical accelerometer.
相較於先前技術,本發明的壓電式微機電加速規藉由第一電極層及第二電極層皆位於壓電層的分布範圍內,可通過壓電層有效分隔第一電極層及第二電極層,可降低第一電極層及第二電極層發生短路的情況,而有利於提升 壓電式微機電加速規的良率。 Compared with the prior art, the piezoelectric MEMS accelerometer of the present invention can effectively separate the first electrode layer and the second electrode layer through the piezoelectric layer because the first electrode layer and the second electrode layer are located within the distribution range of the piezoelectric layer. The electrode layer can reduce the short circuit of the first electrode layer and the second electrode layer, which is conducive to improving the Yield of piezoelectric MEMS accelerometers.
100:壓電式微機電加速規 100: Piezoelectric MEMS Acceleration Gauge
110:載體 110: carrier
110a:本體 110a: Ontology
110b:絕緣層 110b: insulating layer
111:第一表面 111: first surface
112:第一突塊部 112: the first protrusion
113:第二突塊部 113: the second protrusion
115:第二表面 115: second surface
116:第一區域 116: The first area
117:第二區域 117: Second area
130:第一電極層 130: the first electrode layer
140:電極黏著層 140: electrode adhesive layer
150:壓電層 150: piezoelectric layer
170:第二電極層 170: second electrode layer
190:蝕刻保護層 190: etching protective layer
210:基板 210: Substrate
211:底面 211: Bottom
215:頂面 215: top surface
221,222,223:凹槽 221,222,223: Groove
300:光阻層 300: photoresist layer
900:壓電式微機電加速規的製造方法 900: Manufacturing method of piezoelectric MEMS accelerometer
910~980:步驟 910~980: steps
A:連接部 A: Connecting part
B:懸臂樑 B: cantilever beam
C:質量塊 C: mass block
P:部位 P: part
D1:縱向方向 D1: Portrait direction
D2:橫向方向 D2: Horizontal direction
E1,E2,L1,L2:長度 E1, E2, L1, L2: Length
H1,H2:高度 H1, H2: Height
X1:第一長度 X1: first length
X2:第二長度 X2: second length
X3:距離 X3: Distance
W1,W2:寬度 W1, W2: width
X,Y,Z:坐標軸 X, Y, Z: coordinate axes
第1圖是依據本發明一實施方式的壓電式微機電加速規的外觀立體示意圖。 FIG. 1 is a schematic perspective view of the appearance of a piezoelectric MEMS accelerometer according to an embodiment of the present invention.
第2圖是第1圖中壓電式微機電加速規的俯視示意圖。 Fig. 2 is a schematic top view of the piezoelectric MEMS accelerometer in Fig. 1.
第3圖是第1圖中壓電式微機電加速規的側視示意圖。 Fig. 3 is a schematic side view of the piezoelectric MEMS accelerometer in Fig. 1.
第4圖是第1圖中壓電式微機電加速規的剖視示意圖。 Figure 4 is a schematic cross-sectional view of the piezoelectric MEMS accelerometer in Figure 1 .
第5圖是第4圖中壓電式微機電加速規的局部俯視示意圖。 Fig. 5 is a schematic partial top view of the piezoelectric MEMS accelerometer in Fig. 4.
第6圖至第8圖是第4圖中壓電式微機電加速規的製造流程示意圖。 Figures 6 to 8 are schematic diagrams of the manufacturing process of the piezoelectric MEMS accelerometer in Figure 4 .
第9圖是依據本發明另一實施方式的壓電式微機電加速規的製造方法的步驟流程圖。 FIG. 9 is a flow chart of the steps of the manufacturing method of the piezoelectric MEMS accelerometer according to another embodiment of the present invention.
有關本發明之前述及其它技術內容、特點與功效,在以下配合參考圖式之較佳實施方式的詳細說明中,將可清楚地呈現。以下實施方式所提到的方向用語,例如:上、下、左、右、前、後、頂、底等,僅是參考附加圖式的方向。因此,使用的方向用語是用以說明,而非對本發明加以限制。圖式各元件的尺寸僅為相對位置或配置的示意,並非對本發明元件之尺寸加以限制。在下列各實施方式中,相同或相似的元件將採用相同或相似的標號。 The aforementioned and other technical contents, features and effects of the present invention will be clearly presented in the following detailed description of preferred embodiments with reference to the drawings. The directional terms mentioned in the following embodiments, such as: up, down, left, right, front, back, top, bottom, etc., are only directions referring to the attached drawings. Accordingly, the directional terms used are illustrative rather than limiting of the invention. The dimensions of the components in the drawings are only indicative of relative positions or configurations, and do not limit the dimensions of the components of the present invention. In each of the following embodiments, the same or similar components will use the same or similar symbols.
本發明中,一元件設置於/位於另一元件的上方,可指所述元件直接設置於/位於所述另一元件的上方,二者之間不存在其他元件,也可指所述元件間接設置於/位於所述另一元件的上方,二者之間可存在有其他元件。 In the present invention, an element is arranged/located on another element, may mean that said element is directly arranged/located on said another element, there is no other element between them, and it may also mean that said element is indirectly Disposed/located above said another element, with other elements interposed therebetween.
下文中,為便於說明各元件的方向,係配合XYZ直角坐標系進行描述。 In the following, for the convenience of explaining the directions of each element, the description is made in conjunction with the XYZ rectangular coordinate system.
下文中,為了簡潔的緣故,可將第一電極層、壓電層、第二電極層、電極黏著層、蝕刻保護層、絕緣層等膜層簡稱為「膜層」,「膜層」實際代表的意義係配合上、下文及圖式。 Hereinafter, for the sake of brevity, the first electrode layer, the piezoelectric layer, the second electrode layer, the electrode adhesion layer, the etching protection layer, the insulating layer and other film layers may be referred to as "film layers" for short, and "film layers" actually represent The meaning of "coordinates" with upper, lower and schema.
<壓電式微機電加速規> <Piezoelectric MEMS accelerometer>
請參照第1圖至第3圖,第1圖是依據本發明一實施方式的壓電式微機電加速規100的外觀立體示意圖,第2圖是第1圖中壓電式微機電加速規100的俯視示意圖,第3圖是第1圖中壓電式微機電加速規100的側視示意圖。壓電式微機電加速規100包含一連接部A、一懸臂樑(Cantilever beam)B以及一質量塊(Proof mass)C,懸臂樑B連接於連接部A以及質量塊C之間,其中當質量塊C受到外力產生運動,可將能量傳遞至懸臂樑B,並藉由位於懸臂樑B的壓電層(可參照第4圖的壓電層150)可將能量轉變為電訊號,而連接部A係用於將壓電式微機電加速規100連接至一目的物,例如,目的物可為電路板,而使壓電式微機電加速規100可整合至電子電路中,並可將前述電訊號傳送至電子電路中以換算成加速度。換句話說,壓電式微機電加速規100在此例示為懸臂樑加速規,然而,本發明不以此為限,在其他實施方式中,壓電式微機電加速規100可為高頻寬圓盤型加速規或三軸加速規。
Please refer to Figures 1 to 3, Figure 1 is a schematic perspective view of the appearance of a
請參照第4圖,其是第1圖中壓電式微機電加速規100的剖視示意圖。壓電式微機電加速規100包含一載體110、一第一電極層130、一壓電層150及一第二電極層170,且可選擇第包含二電極黏著層140以及一蝕刻保護層190。
Please refer to FIG. 4 , which is a schematic cross-sectional view of the
載體110包含一第一表面111及一第二表面115,第二表面115與第一表面111相對。第一表面111包含一第一突塊部112及一第二突塊部113,第一突塊部112突出於第一表面111,第二突塊部113突出於第一表面111,且與第一突塊部112間隔設置。第一電極層130設置於第二表面115上,壓電層150設置於第一電極層130上,第二電極層170設置於壓電層150上。
The
質量塊C包含第一突塊部112與其下方的蝕刻保護層190及其上方的壓電層150,連接部A包含第二突塊部113與其下方的蝕刻保護層190及其上方的二電極黏著層140、第一電極層130、壓電層150、第二電極層170。實務上,各膜層的厚度(約0.2μm~1.0μm)遠低於第一突塊部112及第二突塊部113的厚度(約400μm),因此,第一突塊部112是壓電式微機電加速規100的質量塊C的主要構成物,第二突塊部113是壓電式微機電加速規100的連接部A的主要構成物。第4圖中為了清楚表示各膜層,因此放大各膜層的厚度,即各膜層、第一突塊部112及第二突塊部113的厚度並未依據實際比例繪製。另外,由於各膜層的厚度很薄,因此,第1圖至第3圖中並未繪示出各膜層於壓電式微機電加速規100所造成的表面高度差。
The proof mass C includes the
第一電極層130及第二電極層170的分布範圍皆位於壓電層150的分布範圍內,前述「第一電極層130及第二電極層170的分布範圍皆位於壓電層150的分布範圍內」是指第一電極層130於第二表面115上具有一覆蓋面積(未另標號),第二電極層170於第二表面115上具有一覆蓋面積(未另標號),壓電層150於第二表面115上具有一覆蓋面積(未另標號),第一電極層130及第二電極層170於第二表面115上的覆蓋面積皆小於壓電層150於第二表面115的覆蓋面積,且皆位
於壓電層150於第二表面115的覆蓋面積內,如第4圖所示,第一電極層130於X軸上的長度E1等於第二電極層170於X軸上的長度E1,壓電層150於X軸上的長度E2大於第一電極層130及第二電極層170的長度E1。藉此,壓電層150可有效分隔第一電極層130及第二電極層170,可降低第一電極層130及第二電極層170發生短路的情況,而有利於提升壓電式微機電加速規100的良率。
The distribution ranges of the
第2圖中,懸臂樑B具有一長度L1,質量塊C具有一長度L2,長度L1、L2皆平行於X軸,其可滿足下列條件:L1/L2=5。懸臂樑B具有一寬度W1,質量塊C具有一寬度W2,長度W1、W2皆平行於Y軸,其可滿足下列條件:1/3W1/W22。第3圖中,懸臂樑B具有一高度H1,質量塊C具有一高度H2,高度H1、H2皆平行於Z軸,其可滿足下列條件:1/40H1/H23/20。藉此尺寸配置,有利於提升壓電式微機電加速規100的靈敏度。
In Fig. 2 , the cantilever beam B has a length L1, and the proof mass C has a length L2. The lengths L1 and L2 are both parallel to the X-axis, which can satisfy the following condition: L1/L2=5. The cantilever beam B has a width W1, the proof mass C has a width W2, and the lengths W1 and W2 are both parallel to the Y axis, which can satisfy the following conditions: 1/3 W1/W2 2. In Figure 3, the cantilever beam B has a height H1, and the mass block C has a height H2. The heights H1 and H2 are both parallel to the Z-axis, which can satisfy the following conditions: 1/40 H1/H2 3/20. This size configuration is beneficial to improve the sensitivity of the
請同時參照第4圖及第5圖,第5圖是第4圖中壓電式微機電加速規100的局部俯視示意圖。第5圖中為了表示第一電極層130及壓電層150的關係,因此省略電極黏著層140及第二電極層170,並將第一電極層130用撒點表示,將壓電層150用斜線表示。第二表面115包含一第一區域116及一第二區域117,第二區域117與第一區域116相連,第一區域116對應第一突塊部112,第一電極層130設置於第二區域117上。壓電層150設置於第一電極層130上並完整覆蓋第二區域117,同時,壓電層150延伸至第一區域116並完整覆蓋第一區域116。藉此,設置於第一區域116上方的壓電層150,在製造壓電式微機電加速規100的過程中可作為載體110的保護層,而有利於減少一次濺鍍步驟、一次微影步驟,而可提升製程效率及降低成本。此外,第二區域117具有一縱向方向D1平行於X軸,第二區域117具有一橫向方向D2平行於Y軸,縱向方向D1與橫向方向D2互相垂直,第一
電極層130的分布範圍沿著橫向方向D2具有一第一長度X1,壓電層150的分布範圍沿著橫向方向D2具有一第二長度X2,第二長度X2平行於第一長度X1,第二長度X2大於第一長度X1,優選地,第一長度X1為第二長度X2的85%至95%,藉此,有利於在壓電層150的邊緣及第一電極層130的邊緣之間的預留足夠的距離X3,有利於提升壓電層150分隔第一電極層130及第二電極層170的效果。
Please refer to FIG. 4 and FIG. 5 at the same time. FIG. 5 is a partial top view of the
詳細來說,載體110可包含本體110a以及二絕緣層110b分別設置於本體110a的上、下表面。本體110a可為矽晶圓,或其他具有高阻抗、耐高溫及抗蝕刻的材料,例如,電阻率大於或等於0.5Ωcm,可承受600℃以上高溫,以及可抵抗丙酮、異丙醇及顯影劑腐蝕的材料。絕緣層110b可為二氧化矽,或其他絕緣可降低導線漏電流影響的材質,例如氮化矽(Si3N4)或氮氧化摻雜物。當本體110a本身的絕緣能力優良且足以降低導線漏電流影響時,可省略絕緣層110b。
In detail, the
第一電極層130及第二電極層170的材質可為鉑,或其他適於作為電極且具有導電能力的材質,例如銀、鋁、金、氮化鈦(TiN)、鎳、銅、錫等。
The material of the
電極黏著層140可設置於第二表面115及第一電極層130之間,電極黏著層140係用於提升第一電極層130與第二表面115之間的附著力,因此,當一電極層130與載體110的材質可提供彼此足夠的附著力時,第一電極層130與第二表面115之間可省略電極黏著層140。相似地,電極黏著層140係用於提升第二電極層170與壓電層150之間的附著力,當第二電極層170與壓電層150的材質可提供彼此足夠的附著力時,第二電極層170與壓電層150之間可省略電極黏著層140。電極黏著層140的材質可為鈦、氧化鋅、氮化鋁、氧化鋁、氮化鈦或二氧化鈦等。
The
壓電層150的材料可為壓電材料,優選地,壓電層150的材料可為Li:ZnO,其中Li的比例為1莫耳百分率~10莫耳百分率,藉此,壓電層150的成分不含鉛,可避免環境污染。
The material of the
蝕刻保護層190設置於第一突塊部112遠離第一表面111的一側,且設置於第二突塊部113遠離第一表面111的一側,蝕刻保護層190是用於進行蝕刻步驟時,保護第一突塊部112及第二突塊部113免於被蝕刻,蝕刻保護層190的材質可為金屬或無機物,例如氧化鋅、氮化鋁、氧化鋁、銀、鋁、金、氮化鈦、鎳、銅、錫等。在其他實施方式中,進行完蝕刻步驟後,可將蝕刻保護層190予以移除,因此蝕刻保護層190為選擇性膜層。
The
<壓電式微機電加速規的製造方法> <Manufacturing method of piezoelectric MEMS accelerometer>
請參照第9圖,其是依據本發明另一實施方式的壓電式微機電加速規的製造方法900的步驟流程圖。壓電式微機電加速規的製造方法900包含步驟910至步驟980,其中步驟920及950為選擇性步驟。請同時參照第6圖至第8圖,其是第4圖中壓電式微機電加速規100的製造流程示意圖,在此以第6圖至第8圖例示說明壓電式微機電加速規的製造方法900。
Please refer to FIG. 9 , which is a flowchart of steps of a
步驟910是提供一基板。如第6圖(a)子圖所示,基板210包含一頂面215及一底面211相對於頂面215,基板210可包含本體110a以及二絕緣層110b。
Step 910 is to provide a substrate. As shown in the sub-figure of FIG. 6( a ), the
步驟920是形成一電極黏著層。步驟930是形成一第一電極層。如第6圖(b)子圖所示,為了定義電極黏著層140及第一電極層130的圖案,先於頂面215形成圖案化的光阻層300,再依序形成電極黏著層140及第一電極層130。之後利
用舉離(lift-off)製程除去光阻層300及其上方的膜層,結果如第6圖(c)子圖所示,電極黏著層140及第一電極層130位於頂面215上且局部覆蓋頂面215。
Step 920 is to form an electrode adhesive layer. Step 930 is to form a first electrode layer. As shown in the sub-figure of FIG. 6 (b), in order to define the patterns of the
步驟940是形成一壓電層。如第6圖(d)子圖所示,依序形成壓電層150及圖案化的光阻層300,再利用濕式蝕刻(wet etch)製程除去光阻層300及部分壓電層150,結果如第7圖(a)子圖所示,其中壓電層150位於第一電極層130上,且第一電極層130位於壓電層150的分布範圍內。
Step 940 is to form a piezoelectric layer. As shown in the sub-figure of FIG. 6 (d), the
步驟950是形成一電極黏著層。步驟960是形成一第二電極層。如第7圖(b)子圖所示,為了定義電極黏著層140及第二電極層170的圖案,先形成圖案化的光阻層300,再依序形成電極黏著層140及第二電極層170。之後利用舉離製程除去光阻層300及其上方的膜層,結果如第7圖(c)子圖所示,電極黏著層140及第二電極層170位於壓電層150上,且第二電極層170位於壓電層150的分布範圍內。
Step 950 is to form an electrode adhesive layer. Step 960 is to form a second electrode layer. As shown in the sub-figure of Figure 7 (b), in order to define the pattern of the
步驟970是形成一蝕刻阻擋層。如第7圖(d)子圖所示,為了定義蝕刻阻擋層190的圖案,先形成圖案化的光阻層300,再形成蝕刻阻擋層190,之後利用舉離製程除去光阻層300及附著其上的蝕刻阻擋層190,結果如第8圖(a)子圖所示,以獲得圖案化的蝕刻阻擋層190,蝕刻阻擋層190位於底面211上。
Step 970 is to form an etch stop layer. As shown in the sub-figure of Figure 7 (d), in order to define the pattern of the
步驟980是進行一蝕刻步驟,移除基板210的一部份,使基板210形成載體110。如第8圖(b)子圖所示,先除去部分位於上方的絕緣層110b,以形成凹槽221。並除去部分位於下方的絕緣層110b,以形成凹槽222、223。續於凹槽221處蝕刻掉部分本體110a,使凹槽221加深,結果如第8圖(c)子圖所示。再由凹槽
222、223蝕刻掉部分本體110a,以切除多餘的部位P,並使凹槽223加深,結果如第8圖(d)子圖所示。基板210受蝕刻後變成載體110,載體110的第一表面111、第一突塊部112及第二突塊部113係底面211受蝕刻後往內凹陷所形成,第二表面115係頂面215經蝕刻後所餘留的部分。蝕刻步驟可採用乾式蝕刻,例如,可使用感應耦合式電漿蝕刻系統(Inductive Couple Plasma Etcher,ICP Etcher)進行反應離子刻蝕(Reactive-Ion Etching,RIE)。
Step 980 is to perform an etching step to remove a part of the
前述步驟中,各膜層可使用射頻磁控濺鍍系統沉積而得。圖案化的光阻層300可利用微影製程所形成,光阻層300可使用市售產品,如AZ 1500。濕式蝕刻所使用的蝕刻液可為鋁蝕刻液,舉離製程所使用的浸泡溶液可為丙酮。然而,本發明不以此為限,各膜層可採用其他製程形成。關於各膜層的細節可參照上文,在此不予贅述。
In the foregoing steps, each film layer can be deposited using a radio frequency magnetron sputtering system. The patterned
<壓電式微機電加速規的性質量測> <Measurement of Properties of Piezoelectric MEMS Accelerometer>
實施例1:依據前述壓電式微機電加速規的製造方法900獲得實施例1的壓電式微機電加速規,實施例1的壓電式微機電加速規為懸臂樑加速規。其尺寸及各膜層的成分如表一、表二所示,其中長度L1、L2、高度H1、H2及寬度W1、W2的定義請參照第2圖及第3圖。
Embodiment 1: According to the
將實施例1的壓電式微機電加速規進行靈敏度測試以及共振頻率測試,係使用振盪系統(THE MPDAL SHOP 9100D)提供一振動源,使實施例1的壓電式微機電加速規產生訊號,並透過軟體(m+p加速規量測軟體)分析訊號,得到實施例1的壓電式微機電加速規的靈敏度為2mV/g~8mV/g,共振頻率為200Hz~1000Hz,其中mV為毫伏特,g為重力加速度,1g=9.8m/s2,顯示依據本發明的壓電式微機電加速規具有優良的靈敏度及共振頻率。 The sensitivity test and resonance frequency test of the piezoelectric MEMS accelerometer in Example 1 is performed by using an oscillation system (THE MPDAL SHOP 9100D) to provide a vibration source, so that the piezoelectric MEMS accelerometer in Example 1 generates a signal, and through Software (m+p accelerometer measuring software) analyzes the signal, and the sensitivity of the piezoelectric MEMS accelerometer in Example 1 is 2mV/g~8mV/g, and the resonance frequency is 200Hz~1000Hz, where mV is millivolts, g is the acceleration of gravity, 1g=9.8m/s 2 , which shows that the piezoelectric MEMS accelerometer according to the present invention has excellent sensitivity and resonance frequency.
相較於先前技術,本發明的壓電式微機電加速規藉由第一電極層及第二電極層皆位於壓電層的分布範圍內,可通過壓電層有效分隔第一電極層及第二電極層,可降低第一電極層及第二電極層發生短路的情況,而有利於提升壓電式微機電加速規的良率。優選地,藉由壓電層延伸至第一區域並完整覆蓋第一區域,在製造壓電式微機電加速規時,有利於減少一次濺鍍步驟、一次微影步驟,而可提升製程效率及降低成本。 Compared with the prior art, the piezoelectric MEMS accelerometer of the present invention can effectively separate the first electrode layer and the second electrode layer through the piezoelectric layer because the first electrode layer and the second electrode layer are located within the distribution range of the piezoelectric layer. The electrode layer can reduce the short circuit between the first electrode layer and the second electrode layer, and is beneficial to improve the yield rate of the piezoelectric MEMS accelerometer. Preferably, by extending the piezoelectric layer to the first region and completely covering the first region, when manufacturing a piezoelectric MEMS accelerometer, it is beneficial to reduce one sputtering step and one lithography step, thereby improving process efficiency and reducing cost.
以上所述僅為本發明之較佳實施例,凡依本發明申請專利範圍所做之均等變化與修飾,皆應屬本發明之涵蓋範圍。 The above descriptions are only preferred embodiments of the present invention, and all equivalent changes and modifications made according to the scope of the patent application of the present invention shall fall within the scope of the present invention.
100:壓電式微機電加速規 100: Piezoelectric MEMS Acceleration Gauge
110:載體 110: carrier
110a:本體 110a: Ontology
110b:絕緣層 110b: insulating layer
111:第一表面 111: first surface
112:第一突塊部 112: the first protrusion
113:第二突塊部 113: the second protrusion
115:第二表面 115: second surface
116:第一區域 116: The first area
117:第二區域 117: Second area
130:第一電極層 130: the first electrode layer
140:電極黏著層 140: electrode adhesive layer
150:壓電層 150: piezoelectric layer
170:第二電極層 170: second electrode layer
190:蝕刻保護層 190: etching protective layer
A:連接部 A: Connecting part
B:懸臂樑 B: cantilever beam
C:質量塊 C: mass block
E1,E2:長度 E1, E2: Length
X,Z:坐標軸 X, Z: coordinate axis
Claims (11)
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TW200829919A (en) * | 2007-01-02 | 2008-07-16 | Polstar Technologies Inc | Calibration system for accelerometer and the method of using the same |
TW200923369A (en) * | 2007-11-19 | 2009-06-01 | Univ Nat Yunlin Sci & Tech | High performance acceleration gauge |
JP2012159494A (en) * | 2011-02-02 | 2012-08-23 | Honeywell Internatl Inc | Mems vibrating-beam accelerometer with piezoelectric drive |
US20180335443A1 (en) * | 2016-03-18 | 2018-11-22 | Rosemount Aerospace Inc. | Symmetric mems piezoelectric accelerometer for lateral noise reduction |
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TW200829919A (en) * | 2007-01-02 | 2008-07-16 | Polstar Technologies Inc | Calibration system for accelerometer and the method of using the same |
TW200923369A (en) * | 2007-11-19 | 2009-06-01 | Univ Nat Yunlin Sci & Tech | High performance acceleration gauge |
JP2012159494A (en) * | 2011-02-02 | 2012-08-23 | Honeywell Internatl Inc | Mems vibrating-beam accelerometer with piezoelectric drive |
US20180335443A1 (en) * | 2016-03-18 | 2018-11-22 | Rosemount Aerospace Inc. | Symmetric mems piezoelectric accelerometer for lateral noise reduction |
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