TWI395844B - Silicon wafer and fabrication method thereof - Google Patents

Silicon wafer and fabrication method thereof Download PDF

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TWI395844B
TWI395844B TW098130435A TW98130435A TWI395844B TW I395844 B TWI395844 B TW I395844B TW 098130435 A TW098130435 A TW 098130435A TW 98130435 A TW98130435 A TW 98130435A TW I395844 B TWI395844 B TW I395844B
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wafer
approximately
temperature
annealing process
body region
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TW201026914A (en
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Jung-Goo Park
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Magnachip Semiconductor Ltd
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L21/00Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
    • H01L21/02Manufacture or treatment of semiconductor devices or of parts thereof
    • H01L21/02104Forming layers
    • H01L21/02365Forming inorganic semiconducting materials on a substrate
    • H01L21/02367Substrates
    • H01L21/0237Materials
    • H01L21/02373Group 14 semiconducting materials
    • H01L21/02381Silicon, silicon germanium, germanium
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L21/00Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
    • H01L21/02Manufacture or treatment of semiconductor devices or of parts thereof
    • H01L21/02104Forming layers
    • H01L21/02107Forming insulating materials on a substrate
    • H01L21/02225Forming insulating materials on a substrate characterised by the process for the formation of the insulating layer
    • H01L21/0226Forming insulating materials on a substrate characterised by the process for the formation of the insulating layer formation by a deposition process
    • H01L21/02293Forming insulating materials on a substrate characterised by the process for the formation of the insulating layer formation by a deposition process formation of epitaxial layers by a deposition process
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L21/00Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
    • H01L21/02Manufacture or treatment of semiconductor devices or of parts thereof
    • H01L21/02104Forming layers
    • H01L21/02365Forming inorganic semiconducting materials on a substrate
    • H01L21/02436Intermediate layers between substrates and deposited layers
    • H01L21/02439Materials
    • H01L21/02469Group 12/16 materials
    • H01L21/02472Oxides
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L21/00Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
    • H01L21/02Manufacture or treatment of semiconductor devices or of parts thereof
    • H01L21/04Manufacture or treatment of semiconductor devices or of parts thereof the devices having at least one potential-jump barrier or surface barrier, e.g. PN junction, depletion layer or carrier concentration layer
    • H01L21/18Manufacture or treatment of semiconductor devices or of parts thereof the devices having at least one potential-jump barrier or surface barrier, e.g. PN junction, depletion layer or carrier concentration layer the devices having semiconductor bodies comprising elements of Group IV of the Periodic System or AIIIBV compounds with or without impurities, e.g. doping materials
    • H01L21/30Treatment of semiconductor bodies using processes or apparatus not provided for in groups H01L21/20 - H01L21/26
    • H01L21/322Treatment of semiconductor bodies using processes or apparatus not provided for in groups H01L21/20 - H01L21/26 to modify their internal properties, e.g. to produce internal imperfections
    • H01L21/3221Treatment of semiconductor bodies using processes or apparatus not provided for in groups H01L21/20 - H01L21/26 to modify their internal properties, e.g. to produce internal imperfections of silicon bodies, e.g. for gettering
    • H01L21/3225Thermally inducing defects using oxygen present in the silicon body for intrinsic gettering
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L21/00Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
    • H01L21/02Manufacture or treatment of semiconductor devices or of parts thereof
    • H01L21/04Manufacture or treatment of semiconductor devices or of parts thereof the devices having at least one potential-jump barrier or surface barrier, e.g. PN junction, depletion layer or carrier concentration layer
    • H01L21/18Manufacture or treatment of semiconductor devices or of parts thereof the devices having at least one potential-jump barrier or surface barrier, e.g. PN junction, depletion layer or carrier concentration layer the devices having semiconductor bodies comprising elements of Group IV of the Periodic System or AIIIBV compounds with or without impurities, e.g. doping materials
    • H01L21/30Treatment of semiconductor bodies using processes or apparatus not provided for in groups H01L21/20 - H01L21/26
    • H01L21/324Thermal treatment for modifying the properties of semiconductor bodies, e.g. annealing, sintering
    • HELECTRICITY
    • H10SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10BELECTRONIC MEMORY DEVICES
    • H10B10/00Static random access memory [SRAM] devices

Description

矽晶圓及其製造方法Silicon wafer and its manufacturing method

本發明係關於半導體製造技術,且更特定言之,係關於矽晶圓及其製造方法。The present invention relates to semiconductor fabrication techniques and, more particularly, to germanium wafers and methods of fabricating the same.

本發明主張2008年9月29日及2009年1月16日向韓國智慧財產局申請之韓國專利申請案第10-2008-0095462號及第10-2009-0003697號之優先權,該等專利申請案以引用之方式併入本文中。The present invention claims priority to Korean Patent Application No. 10-2008-0095462 and No. 10-2009-0003697, filed on Sep. 29, 2008, and Jan. 16, 2009, to the Korean Intellectual Property Office. This is incorporated herein by reference.

在諸如NMOS電晶體及PMOS電晶體之大多數高壓器件中,通常自一基板之一表面形成一井至大致5微米至10微米之深度。僅使用離子植入製程難以達成具有5微米至10微米深度之井的摻雜分布。為此,在離子植入製程後應必需使用高溫熱處理執行摻雜劑擴散過程。In most high voltage devices, such as NMOS transistors and PMOS transistors, a well is typically formed from the surface of one of the substrates to a depth of approximately 5 microns to 10 microns. It is difficult to achieve a doping profile of a well having a depth of 5 microns to 10 microns using only an ion implantation process. For this reason, it is necessary to perform a dopant diffusion process using a high temperature heat treatment after the ion implantation process.

然而,歸因於高溫熱處理,在矽本體中不能完全達成氧析出。此引起在用於淺渠溝隔離(STI)之刻蝕製程後在矽基板中出現諸如環狀位錯之晶體缺陷。However, due to the high temperature heat treatment, oxygen evolution cannot be completely achieved in the crucible body. This causes crystal defects such as ring dislocations to occur in the germanium substrate after the etching process for shallow trench isolation (STI).

此外,此等晶體缺陷降低生產良率,且亦惡化諸如高壓器件之臨限電壓及靜態隨機存取記憶體(SRAM)之待用模式期間的漏電流均一性之電參數特性。此外,此等晶體缺陷增加在雜質檢驗過程(其為製造半導體器件所必需執行之過程)期間用以檢驗及分析大量缺陷的時間,從而導致製造半導體器件之總處理時間的增加。In addition, such crystal defects reduce production yield and also deteriorate electrical parameter characteristics such as the threshold voltage of the high voltage device and the leakage current uniformity during the standby mode of the static random access memory (SRAM). Moreover, such crystal defects increase the time to inspect and analyze a large number of defects during the impurity inspection process, which is a process that must be performed to fabricate a semiconductor device, resulting in an increase in the total processing time for fabricating the semiconductor device.

本發明之實施例係針對一種用於藉由充分地增加吸氣位點來防止晶體缺陷歸因於由後繼高溫熱處理製程引起之熱預算而產生的矽晶圓。Embodiments of the present invention are directed to a germanium wafer for preventing crystal defects from being caused by a thermal budget caused by a subsequent high temperature heat treatment process by substantially increasing the gettering sites.

本發明之另一實施例係針對一種在本體區域中具有高且均勻之本體微觀缺陷(BMD)密度之矽晶圓。Another embodiment of the present invention is directed to a germanium wafer having a high and uniform bulk microscopic defect (BMD) density in the body region.

本發明之另一實施例係針對一種用於製造藉由充分地增加吸取位點來防止晶體缺陷歸因於由後繼高溫熱處理製程引起之熱預算而產生的矽晶圓的方法。Another embodiment of the present invention is directed to a method for fabricating a tantalum wafer that is produced by substantially increasing the gettering sites to prevent crystal defects from being attributed to thermal budgets caused by subsequent high temperature heat treatment processes.

本發明之另一實施例係針對一種用於製造在本體區域中具有高且均勻之本體微觀缺陷(BMD)密度之矽晶圓的方法。Another embodiment of the present invention is directed to a method for fabricating a tantalum wafer having a high and uniform bulk microscopic defect (BMD) density in a body region.

本發明之另一實施例係針對一種藉由使用以上描述之矽晶圓製造之半導體器件。Another embodiment of the present invention is directed to a semiconductor device fabricated by using the germanium wafer described above.

本發明之另一實施例係針對一種用於藉由使用以上描述之用於製造矽晶圓之方法製造半導體器件的方法。Another embodiment of the present invention is directed to a method for fabricating a semiconductor device by using the method described above for fabricating a germanium wafer.

根據本發明之一態樣,提供一種矽晶圓,其包括:一第一剝蝕區,其經形成具有始於該矽晶圓之一頂面的一預定深度;及一本體區域,其形成於該第一剝蝕區與矽晶圓之一背面之間,其中該第一剝蝕區經形成具有範圍為始於該頂面的大致20微米至大致80微米之一深度,且其中本體區域中氧之濃度遍及本體區域以10%內之變化均勻分布。According to an aspect of the present invention, a germanium wafer is provided, comprising: a first ablation region formed to have a predetermined depth starting from a top surface of the germanium wafer; and a body region formed on Between the first ablation region and a back surface of the germanium wafer, wherein the first ablation region is formed to have a depth ranging from approximately 20 micrometers to approximately 80 micrometers from the top surface, and wherein oxygen is present in the body region The concentration is evenly distributed throughout the body region within 10% of the change.

根據本發明之又一態樣,提供一種用於製造一矽晶圓之方法,其包括:提供具有一剝蝕區及一本體區域之矽晶圓;在一第一溫度下對該矽晶圓執行第一退火製程以在本體區域中補充產生氧析出物核及氧析出物;及在高於第一溫度之第二溫度下對矽晶圓執行第二退火製程以增大本體區域中之氧析出物。According to still another aspect of the present invention, a method for fabricating a germanium wafer is provided, comprising: providing a germanium wafer having a denuded region and a body region; performing the germanium wafer at a first temperature a first annealing process to supplement an oxygen precipitate core and an oxygen precipitate in the body region; and performing a second annealing process on the germanium wafer at a second temperature higher than the first temperature to increase oxygen deposition in the body region Things.

根據本發明之又一態樣,提供一種用於製造一矽晶圓之方法,其包括:提供該矽晶圓;在一裝載溫度下將矽晶圓裝載至加熱裝置內部;執行一將矽晶圓自裝載溫度加熱至第一溫度之第一加熱製程;在該第一溫度下執行使該矽晶圓退火之一第一退火製程以產生氧析出物;執行一將該矽晶圓自該第一溫度加熱至高於該第一溫度之一第二溫度的第二加熱過程;在該第二溫度下執行使該矽晶圓退火之一第二退火製程以增大氧析出物以用於增加其密度;執行一將該矽晶圓自該第二溫度冷卻至一卸載溫度之冷卻製程;及將該矽晶圓自該加熱裝置卸載至外部。According to still another aspect of the present invention, a method for fabricating a germanium wafer is provided, comprising: providing the germanium wafer; loading the germanium wafer into the interior of the heating device at a loading temperature; performing a twinning a first heating process for heating the temperature from the loading temperature to the first temperature; performing a first annealing process for annealing the germanium wafer to generate oxygen precipitates at the first temperature; performing a silicon wafer from the first Heating a temperature to a second heating process that is higher than a second temperature of the first temperature; performing a second annealing process for annealing the germanium wafer to increase oxygen precipitates for use in the second temperature Density; performing a cooling process for cooling the germanium wafer from the second temperature to an unloading temperature; and unloading the germanium wafer from the heating device to the outside.

本發明之其他目標及優點可藉由以下描述來理解,且參考本發明之實施例變得顯而易見。又,本發明之目標及優點可藉由如所主張之構件及其組合實現對於熟悉本發明所屬之相關技術者為顯然的。The other objects and advantages of the invention will be apparent from the description and appended claims. Further, the objects and advantages of the invention will be apparent to those skilled in the <RTIgt;

本發明之優點、特徵及態樣將自參看隨附圖式之下文所闡述的實施例之以下描述變得顯而易見。The advantages, features, and aspects of the invention will be apparent from the description of the embodiments described herein.

在諸圖中,為說明清楚,誇示層及區域之尺寸。亦應理解,當一層(或膜)被稱為「在另一層或基板上」時,其可直接在另一層或基板上,或亦可存在插入層。此外,應理解,當一層被稱為「在另一層下方」時,其可直接在另一層下方,且亦可存在一或多個插入層。此外,亦應理解,當一層被稱為「在兩個層之間」時,其可為兩個層之間的唯一層,或亦可存在一或多個插入層。In the figures, the dimensions of layers and regions are exaggerated for clarity of illustration. It will also be understood that when a layer (or film) is referred to as "on another layer or substrate", it can be directly on the other layer or substrate, or an intervening layer can also be present. In addition, it should be understood that when a layer is referred to as "below another layer", it may be directly below the other layer, and one or more intervening layers may also be present. In addition, it should also be understood that when a layer is referred to as "between two layers," it may be a single layer between two layers, or one or more intervening layers may be present.

本發明可藉由對晶圓矽使用兩步驟退火製程來實現本體區域中高且均勻之BMD密度。結果,本發明可藉由充分地增加吸取位點(gettering site)來防止晶體缺陷歸因於由後繼高溫熱處理製程引起之熱預算而產生。The present invention achieves a high and uniform BMD density in the body region by using a two-step annealing process for the wafer crucible. As a result, the present invention can prevent crystal defects from being generated due to a thermal budget caused by a subsequent high-temperature heat treatment process by sufficiently increasing a gettering site.

圖1為根據本發明之一實施例的矽晶圓之橫截面圖。1 is a cross-sectional view of a tantalum wafer in accordance with an embodiment of the present invention.

如圖1所展示,矽晶圓100包括:一第一剝蝕區DZ1,該第一剝蝕區DZ1經形成具有始於該矽晶圓之一頂面101的一預定深度;及一本體區域區塊,該本體區域BK形成於該第一剝蝕區DZ1與一背面102之間。矽晶圓100進一步包括一第二剝蝕區DZ2,該第二剝蝕區DZ2經形成具有自該背面102朝向該頂面101之方向的預定深度。As shown in FIG. 1, the germanium wafer 100 includes: a first ablation region DZ1 formed to have a predetermined depth starting from a top surface 101 of the germanium wafer; and a body region block The body region BK is formed between the first ablation region DZ1 and a back surface 102. The germanium wafer 100 further includes a second ablated region DZ2 that is formed to have a predetermined depth from the back surface 102 toward the top surface 101.

經形成具有自頂面101朝向背面102之方向的預定深度之第一剝蝕區DZ1為無缺陷區域(DFZ),其不存在諸如空位及位錯之晶體缺陷。較佳地,第一剝蝕區DZ1經形成具有自頂面101朝向背面102之方向的範圍為大致20微米至大致80微米的深度。The first ablation region DZ1 formed to have a predetermined depth from the top surface 101 toward the back surface 102 is a defect-free region (DFZ) which does not have crystal defects such as vacancies and dislocations. Preferably, the first ablation zone DZ1 is formed to have a depth ranging from about 20 micrometers to about 80 micrometers from the direction of the top surface 101 toward the back surface 102.

第二剝蝕區DZ2亦為DFZ且經形成具有自背面102朝向頂面101之方向的與第一剝蝕區DZ1之深度相同的深度,或根據對背面102之拋光製程,第二剝蝕區DZ2經形成具有小於第一剝蝕區DZ1之深度的深度。亦即,當對矽晶圓100之頂面101及背面102兩者無差別地進行鏡面拋光時,相同深度形成具有相同深度的第一剝蝕區DZ1及第二剝蝕區DZ2。相反,當對頂面101進行鏡面拋光且不對背面102進行鏡面拋光時,形成具有小於第一剝蝕區DZ1深度之深度的第二剝蝕區DZ2,因為根據背面102之粗糙度緊接於背面102形成氧析出物。The second ablation zone DZ2 is also DFZ and formed to have the same depth as the depth of the first ablation zone DZ1 from the back surface 102 toward the top surface 101, or according to the polishing process for the back surface 102, the second ablation zone DZ2 is formed. It has a depth smaller than the depth of the first ablation zone DZ1. That is, when the top surface 101 and the back surface 102 of the wafer 100 are mirror-polished without difference, the first ablation region DZ1 and the second ablation region DZ2 having the same depth are formed at the same depth. In contrast, when the top surface 101 is mirror-polished and the back surface 102 is not mirror-polished, a second ablation region DZ2 having a depth smaller than the depth of the first ablation region DZ1 is formed because the roughness of the back surface 102 is formed next to the back surface 102. Oxygen precipitates.

在第一剝蝕區DZ1與第二剝蝕區DZ2之間形成的本體區域BK包括本體微觀缺陷(BMD)103。BMD 103在整個本體區域中保持均勻。BMD 103包括析出物及本體疊差。此外,可控制本體區域BK中之BMD 103以具有足夠密度,藉此吸取經由後繼高溫熱處理製程或熱製程待在矽晶圓之表面上擴散之金屬污染物。本體區域BK中之BMD 103較佳可保持自大致1×105 ea/cm2 至大致1×107 ea/cm2 之密度,且更佳自大致1×106 ea/cm2 至1×107 ea/cm2 。本體區域BK中氧之濃度(以下稱為「氧濃度」)與氧析出物緊密相關,且氧濃度較佳遍及本體區域BK以10%內之變化分布且保持自大致10.5至大致13PPMA(原子百萬分率)。The body region BK formed between the first ablation region DZ1 and the second ablation region DZ2 includes a bulk microscopic defect (BMD) 103. The BMD 103 remains uniform throughout the body area. BMD 103 includes precipitates and bulk stacks. In addition, the BMD 103 in the body region BK can be controlled to have a sufficient density to draw metal contaminants to be diffused on the surface of the germanium wafer via a subsequent high temperature heat treatment process or thermal process. The BMD 103 in the body region BK preferably maintains a density of from about 1 x 10 5 ea/cm 2 to about 1 × 10 7 ea/cm 2 , and more preferably from about 1 × 10 6 ea/cm 2 to 1 ×. 10 7 ea/cm 2 . The concentration of oxygen in the body region BK (hereinafter referred to as "oxygen concentration") is closely related to the oxygen precipitate, and the oxygen concentration is preferably distributed throughout the body region BK within 10% and is maintained from approximately 10.5 to approximately 13 PPMA (atoms Ten thousand points).

圖2為說明根據本發明之第一實施例的用於製造矽晶圓之方法的橫截面圖。2 is a cross-sectional view illustrating a method for fabricating a germanium wafer in accordance with a first embodiment of the present invention.

參看圖2,製備矽晶圓200。此時,矽晶圓200可為裸晶圓。可按照以下步驟形成矽晶圓200。首先,在成長單晶矽後,將單晶矽切割成晶圓形狀。在執行刻蝕製程以蝕刻經切割晶圓之表面或使經切割晶圓之側面變圓之後,對矽晶圓200之頂面201及背面202進行鏡面拋光。此時,使用柴氏(Czochralski,CZ)晶體成長法來使單晶矽成長。此外,可在後續熱製程後執行對矽晶圓200之鏡面拋光製程。Referring to Figure 2, a germanium wafer 200 is prepared. At this time, the germanium wafer 200 may be a bare wafer. The germanium wafer 200 can be formed in the following steps. First, after the single crystal germanium is grown, the single crystal germanium is cut into a wafer shape. After performing an etching process to etch the surface of the diced wafer or rounding the sides of the diced wafer, the top surface 201 and the back surface 202 of the ruthenium wafer 200 are mirror polished. At this time, a single crystal crucible was grown using a Czochralski (CZ) crystal growth method. In addition, the mirror polishing process for the germanium wafer 200 can be performed after the subsequent thermal process.

執行對矽晶圓200之第一熱製程,使得矽晶圓200之頂面201與背面202之間的氧化物元素203向內部擴散。結果,形成第一剝蝕區DZ1及第二剝蝕區DZ2以及本體區域BK。第一熱製程可為RTP(快速熱製程)或使用爐裝置之退火製程。較佳地,第一熱製程包括RTP。The first thermal process of the wafer 200 is performed such that the oxide element 203 between the top surface 201 and the back surface 202 of the germanium wafer 200 diffuses internally. As a result, the first ablation zone DZ1 and the second ablation zone DZ2 and the body region BK are formed. The first thermal process can be an RTP (rapid thermal process) or an annealing process using a furnace apparatus. Preferably, the first thermal process comprises RTP.

為快速擴散矽晶圓200之頂面201及背面202中之氧化物元素203,使用氬(Ar)氣、氮(N2 )氣、氨(NH3 )氣或其組合在高溫下執行第一熱製程。當第一熱製程為RTP時,在範圍為1050℃至大致1150℃之溫度下執行第一熱製程歷時大致10秒至大致30秒。當第一熱製程為退火製程時,在範圍為1050℃至大致1150℃之溫度下執行第一熱製程歷時大致100分鐘至大致300分鐘。To rapidly diffuse the oxide element 203 in the top surface 201 and the back surface 202 of the germanium wafer 200, the first step is performed at a high temperature using argon (Ar) gas, nitrogen (N 2 ) gas, ammonia (NH 3 ) gas, or a combination thereof. Hot process. When the first thermal process is RTP, the first thermal process is performed for a period of from about 10 seconds to about 30 seconds at a temperature ranging from 1050 ° C to approximately 1150 ° C. When the first thermal process is an annealing process, the first thermal process is performed for a period of from about 100 minutes to about 300 minutes at a temperature ranging from 1050 ° C to about 1150 ° C.

接著,執行對矽晶圓200之第二熱製程,使得本體區域BK中之氧化物元素203結合。結果,產生氧析出物核204。與第一熱製程類似,第二熱製程可為RTP或使用爐裝置之退火製程。第二熱製程較佳包括RTP。Next, a second thermal process for the germanium wafer 200 is performed such that the oxide elements 203 in the body region BK are bonded. As a result, an oxygen precipitate core 204 is produced. Similar to the first thermal process, the second thermal process can be an RTP or an annealing process using a furnace apparatus. The second thermal process preferably includes RTP.

為易於形成氧析出物核204,使用氬(Ar)氣、氮(N2 )氣、氨(NH3 )氣或其組合在低於第一熱製程之溫度的溫度下執行第二熱製程。當第二熱製程為RTP時,在範圍為大致950℃至大致1000℃之溫度下執行第二熱製程歷時大致10秒至大致30秒。當第二熱製程為退火製程時,在範圍為大致950℃至大致1000℃之溫度下執行第二熱製程歷時大致100分鐘至大致200分鐘。To facilitate the formation of the oxygen precipitate core 204, a second thermal process is performed at a temperature lower than the temperature of the first thermal process using argon (Ar) gas, nitrogen (N 2 ) gas, ammonia (NH 3 ) gas, or a combination thereof. When the second thermal process is RTP, the second thermal process is performed for a period of time from about 10 seconds to about 30 seconds at a temperature ranging from about 950 ° C to about 1000 ° C. When the second thermal process is an annealing process, the second thermal process is performed for a period of from about 100 minutes to about 200 minutes at a temperature ranging from about 950 ° C to about 1000 ° C.

隨後,在完成第二熱製程後對矽晶圓200執行第一退火製程。使用爐裝置執行第一退火製程。藉由在低於第二熱製程之溫度的預定溫度下加熱矽晶圓200,補充產生本體區域BK中之氧析出物核204,且同時,產生氧析出物205A。較佳地,在範圍為大致750℃至大致800℃之溫度下執行第一退火製程歷時大致100分鐘至大致180分鐘。此外,在氧(O2 )氣氛圍下執行第一退火製程。Subsequently, a first annealing process is performed on the germanium wafer 200 after the second thermal process is completed. The first annealing process is performed using a furnace device. The oxygen precipitates core 204 in the body region BK is replenished by heating the tantalum wafer 200 at a predetermined temperature lower than the temperature of the second heat process, and at the same time, the oxygen precipitates 205A are generated. Preferably, the first annealing process is performed for a period of from about 100 minutes to about 180 minutes at a temperature ranging from about 750 ° C to about 800 ° C. Further, the first annealing process is performed under an oxygen (O 2 ) gas atmosphere.

在完成第一退火製程後對矽晶圓200執行第二退火製程。亦使用爐裝置執行第二退火製程。藉由在高於第一退火製程之溫度的預定溫度下加熱矽晶圓200,增大氧析出物205A。結果,產生經增大之氧析出物205B。較佳地,在範圍為大致1000℃至大致1150℃之溫度下執行第二退火製程歷時大致100分鐘至大致180分鐘。此外,在氧(O2 )氣氛圍下執行第二退火製程。A second annealing process is performed on the germanium wafer 200 after the first annealing process is completed. A second annealing process is also performed using the furnace apparatus. The oxygen precipitate 205A is enlarged by heating the tantalum wafer 200 at a predetermined temperature higher than the temperature of the first annealing process. As a result, an enlarged oxygen precipitate 205B is produced. Preferably, the second annealing process is performed at a temperature ranging from approximately 1000 ° C to approximately 1150 ° C for a period of from about 100 minutes to about 180 minutes. Further, a second annealing process is performed under an oxygen (O 2 ) gas atmosphere.

在下文中,詳細描述第一退火製程及第二退火製程。在下文中,將第一退火製程及第二退火製程稱為兩步驟退火製程。Hereinafter, the first annealing process and the second annealing process are described in detail. Hereinafter, the first annealing process and the second annealing process are referred to as a two-step annealing process.

圖6為說明根據本發明之一實施例的兩步驟退火製程之曲線圖。6 is a graph illustrating a two-step annealing process in accordance with an embodiment of the present invention.

參看圖6,使用爐裝置之退火製程包括使用氧(O2 )氣在第一溫度下使矽晶圓200退火之第一退火製程(II)及在高於第一溫度之第二溫度下執行使矽晶圓200退火的第二退火製程(IV)。執行第一退火製程(II)及第二退火製程(IV)中之每一者歷時大致100分鐘至大致180分鐘。第一退火製程(II)之第一溫度的範圍為大致750℃至大致800℃,且第二退火製程(IV)之第二溫度的範圍為大致1000℃至大致1150℃。Referring to FIG. 6, the annealing process using the furnace apparatus includes performing a first annealing process (II) for annealing the tantalum wafer 200 at a first temperature using oxygen (O 2 ) gas and performing a second temperature higher than the first temperature. A second annealing process (IV) for annealing the tantalum wafer 200. Each of the first annealing process (II) and the second annealing process (IV) is performed for approximately 100 minutes to approximately 180 minutes. The first temperature of the first annealing process (II) ranges from approximately 750 ° C to approximately 800 ° C, and the second temperature of the second annealing process (IV) ranges from approximately 1000 ° C to approximately 1150 ° C.

為改良氧化製程及熱處理製程之效應,在第一退火製程(II)前,根據本發明之實施例的兩步驟退火製程可進一步包括將矽晶圓200裝載至爐裝置內部且接著將矽晶圓200保持至裝載溫度歷時一預定持續時間的裝載過程(L)。又,在第二退火製程(IV)後,根據本發明之實施例的兩步驟退火製程可進一步包括在將矽晶圓200卸載至爐裝置外部前將矽晶圓200保持至卸載溫度歷時一預定持續時間的卸載過程(UL)。To improve the effects of the oxidation process and the heat treatment process, prior to the first annealing process (II), the two-step annealing process according to an embodiment of the present invention may further include loading the germanium wafer 200 into the furnace device and then transferring the germanium wafer 200 is maintained until the loading temperature (L) for a predetermined duration. Moreover, after the second annealing process (IV), the two-step annealing process according to an embodiment of the present invention may further include maintaining the germanium wafer 200 to the unloading temperature for a predetermined time before unloading the germanium wafer 200 to the outside of the furnace device. The duration of the uninstall process (UL).

裝載過程(L)之裝載溫度低於第一溫度。較佳地,裝載溫度之範圍為大致600℃至大致700℃。在裝載過程(L)期間不將氧氣供應至爐裝置中。結果,在裝載過程(L)期間矽晶圓200未受到氧化。卸載過程(UL)之卸載溫度大體上等於第一溫度。較佳地,卸載溫度之範圍為大致750℃至大致800℃。在卸載過程(UL)期間,不供應氧氣而僅供應氮氣。氮氣之流動速率的範圍為大致9slm至大致11slm。The loading temperature of the loading process (L) is lower than the first temperature. Preferably, the loading temperature ranges from approximately 600 ° C to approximately 700 ° C. No oxygen is supplied to the furnace unit during the loading process (L). As a result, the wafer 200 is not oxidized during the loading process (L). The unloading temperature of the unloading process (UL) is substantially equal to the first temperature. Preferably, the unloading temperature ranges from approximately 750 ° C to approximately 800 ° C. During the unloading process (UL), no oxygen is supplied and only nitrogen is supplied. The flow rate of nitrogen ranges from approximately 9 slm to approximately 11 slm.

此外,根據本發明之實施例的兩步驟退火製程可進一步包括在裝載過程(L)與第一退火製程(II)之間的用於將裝載溫度加熱至第一溫度的第一加熱製程(I)及在第一退火製程(II)與第二退火製程(IV)之間的用於將第一溫度加熱至第二溫度的第二加熱製程(III)。當在第一加熱製程(I)及第二加熱製程(III)期間每分鐘升溫速率過高時,晶圓結構可能變形。因此,可將第一加熱製程(I)及第二加熱製程(III)中之升溫速率設定為大致5℃/分鐘至大致8℃/分鐘之範圍。Further, the two-step annealing process according to an embodiment of the present invention may further include a first heating process for heating the loading temperature to the first temperature between the loading process (L) and the first annealing process (II) (I And a second heating process (III) for heating the first temperature to the second temperature between the first annealing process (II) and the second annealing process (IV). When the rate of temperature increase per minute during the first heating process (I) and the second heating process (III) is too high, the wafer structure may be deformed. Therefore, the rate of temperature rise in the first heating process (I) and the second heating process (III) can be set to a range of approximately 5 ° C / min to approximately 8 ° C / min.

又,根據本發明之實施例的兩步驟退火製程可進一步包括在第二退火製程(IV)與卸載過程(UL)之間的用於將第二溫度冷卻至卸載溫度的冷卻製程(V)。冷卻製程(V)之降溫速率的範圍可為大致2℃/分鐘至大致4℃/分鐘。Further, the two-step annealing process according to an embodiment of the present invention may further include a cooling process (V) for cooling the second temperature to the unloading temperature between the second annealing process (IV) and the unloading process (UL). The cooling rate of the cooling process (V) can range from approximately 2 ° C/min to approximately 4 ° C/min.

在根據本發明之實施例的兩步驟退火製程中,矽晶圓200之退火大體上主要在第一退火製程及第二退火製程(II、IV)期間達成,因為僅在此等製程期間供應氧氣。第一退火製程及第二退火製程(II、IV)期間所供應之氧氣之流動速率的範圍可為大致50sccm至大致120sccm。可執行第一退火製程及第二退火製程(II、IV)中之每一者歷時大致100分鐘至大致180分鐘。In the two-step annealing process according to an embodiment of the present invention, the annealing of the germanium wafer 200 is substantially achieved primarily during the first annealing process and the second annealing process (II, IV) because oxygen is supplied only during such processes. . The flow rate of oxygen supplied during the first annealing process and the second annealing process (II, IV) may range from approximately 50 sccm to approximately 120 sccm. Each of the first annealing process and the second annealing process (II, IV) may be performed for approximately 100 minutes to approximately 180 minutes.

如圖6中描述之兩步驟退火製程可應用於圖3至圖5中展示之根據本發明之以下實施例的用於製造矽晶圓之方法的第一退火製程及第二退火製程。The two-step annealing process as described in FIG. 6 can be applied to the first annealing process and the second annealing process of the method for fabricating a germanium wafer according to the following embodiments of the present invention shown in FIGS. 3 through 5.

圖3為說明根據本發明之第二實施例的用於製造矽晶圓之方法的橫截面圖。3 is a cross-sectional view illustrating a method for fabricating a germanium wafer in accordance with a second embodiment of the present invention.

參看圖3,執行對矽晶圓300之熱製程,使得矽晶圓300之頂面301與背面302之間的氧化物元素303向內部擴散。結果,形成第一剝蝕區DZ1及第二剝蝕區DZ2以及本體區域BK。熱製程可為RTP或使用爐裝置之退火製程。較佳地,第一熱製程包括RTP。Referring to FIG. 3, a thermal process for the germanium wafer 300 is performed such that the oxide element 303 between the top surface 301 and the back surface 302 of the germanium wafer 300 is diffused internally. As a result, the first ablation zone DZ1 and the second ablation zone DZ2 and the body region BK are formed. The thermal process can be RTP or an annealing process using a furnace unit. Preferably, the first thermal process comprises RTP.

為快速擴散矽晶圓300之頂面301及背面302之氧化物元素303,在高溫下執行熱製程。當熱製程為RTP時,在範圍為1050℃至大致1150℃之溫度下執行熱製程歷時大致10秒至大致30秒。當熱製程為退火製程時,在範圍為1050℃至大致1150℃之溫度下執行熱製程歷時大致100分鐘至大致200分鐘。In order to rapidly diffuse the oxide element 303 of the top surface 301 and the back surface 302 of the tantalum wafer 300, a thermal process is performed at a high temperature. When the thermal process is RTP, the thermal process is performed for a period of approximately 10 seconds to approximately 30 seconds at a temperature ranging from 1050 ° C to approximately 1150 ° C. When the thermal process is an annealing process, the thermal process is performed at a temperature ranging from 1050 ° C to approximately 1150 ° C for approximately 100 minutes to approximately 200 minutes.

隨後,對矽晶圓300執行第一退火製程,使得本體區域BK中之氧化物元素203結合。結果,形成氧析出物核304。在低於熱製程之溫度的預定溫度下使用爐裝置執行第一退火製程。較佳地,在範圍為大致750℃至大致800℃之溫度下執行第一退火製程歷時大致100分鐘至大致180分鐘。此外,在氧(O2 )氣氛圍下執行第一退火製程。Subsequently, a first annealing process is performed on the germanium wafer 300 such that the oxide elements 203 in the body region BK are bonded. As a result, an oxygen precipitate core 304 is formed. The first annealing process is performed using a furnace apparatus at a predetermined temperature lower than the temperature of the hot process. Preferably, the first annealing process is performed for a period of from about 100 minutes to about 180 minutes at a temperature ranging from about 750 ° C to about 800 ° C. Further, the first annealing process is performed under an oxygen (O 2 ) gas atmosphere.

對矽晶圓300執行第二退火製程。亦使用爐裝置執行第二退火製程。藉由在高於第一退火製程之溫度的預定溫度下加熱矽晶圓300,產生氧析出物305。較佳地,在範圍為大致1000℃至大致1150℃之溫度下執行第二退火製程歷時大致100分鐘至大致180分鐘。此外,在氧(O2 )氣氛圍下執行第二退火製程。A second annealing process is performed on the germanium wafer 300. A second annealing process is also performed using the furnace apparatus. The oxygen precipitates 305 are produced by heating the tantalum wafer 300 at a predetermined temperature higher than the temperature of the first annealing process. Preferably, the second annealing process is performed at a temperature ranging from approximately 1000 ° C to approximately 1150 ° C for a period of from about 100 minutes to about 180 minutes. Further, a second annealing process is performed under an oxygen (O 2 ) gas atmosphere.

圖4為說明根據本發明之第三實施例的用於製造矽晶圓之方法的橫截面圖。4 is a cross-sectional view illustrating a method for fabricating a germanium wafer in accordance with a third embodiment of the present invention.

在圖4中,在低於圖3之熱製程之溫度的溫度下執行第一退火製程之前的熱製程。In FIG. 4, the thermal process prior to the first annealing process is performed at a temperature lower than the temperature of the thermal process of FIG.

參看圖4,在低於圖3之熱製程之溫度的溫度下執行對矽晶圓400之熱製程。因此,產生氧析出物核404。因為在低溫下執行熱製程,所以在第一剝蝕區DZ1及第二剝蝕區DZ2以及本體區域BK中形成氧析出物核404。熱製程可為RTP或退火製程。較佳地,第一熱製程包括RTP。當熱製程為RTP時,在範圍為大致950℃至大致1000℃之溫度下執行熱製程歷時大致10秒至大致30秒。當熱製程為退火製程時,在範圍為大致950℃至大致1000℃之溫度下執行熱製程歷時大致100分鐘至大致200分鐘。Referring to FIG. 4, a thermal process for the germanium wafer 400 is performed at a temperature lower than the temperature of the thermal process of FIG. Thus, an oxygen precipitate core 404 is produced. Since the thermal process is performed at a low temperature, the oxygen precipitate core 404 is formed in the first ablation zone DZ1 and the second ablation zone DZ2 and the body region BK. The thermal process can be an RTP or an annealing process. Preferably, the first thermal process comprises RTP. When the thermal process is RTP, the thermal process is performed for a period of approximately 10 seconds to approximately 30 seconds at a temperature ranging from approximately 950 ° C to approximately 1000 ° C. When the thermal process is an annealing process, the thermal process is performed at a temperature ranging from approximately 950 ° C to approximately 1000 ° C for approximately 100 minutes to approximately 200 minutes.

隨後,對矽晶圓400順序地執行第一退火製程及第二退火製程,使得產生氧析出物核404及氧析出物405A。在與圖3之第一退火製程及第二退火製程之彼等條件相同的條件下執行第一退火製程及第二退火製程。Subsequently, the first annealing process and the second annealing process are sequentially performed on the germanium wafer 400 such that the oxygen precipitate core 404 and the oxygen precipitate 405A are generated. The first annealing process and the second annealing process are performed under the same conditions as those of the first annealing process and the second annealing process of FIG.

圖5為說明根據本發明之第四實施例的用於製造矽晶圓之方法的橫截面圖。Figure 5 is a cross-sectional view illustrating a method for fabricating a germanium wafer in accordance with a fourth embodiment of the present invention.

參看圖5,與圖2至圖4中展示之退火製程不同,根據本發明之第四實施例的退火製程無需第一退火製程及第二退火製程之前的額外熱製程。亦即,提供為裸晶圓之矽晶圓500,且對矽晶圓500順序地執行第一退火製程及第二退火製程,使得形成第一剝蝕區DZ1及第二剝蝕區DZ2以及本體區域BK。在與圖2至圖4展示之第一退火製程及第二退火製程之彼等條件相同的條件下執行第一退火製程及第二退火製程。Referring to FIG. 5, unlike the annealing process shown in FIGS. 2 through 4, the annealing process according to the fourth embodiment of the present invention does not require an additional annealing process and an additional thermal process prior to the second annealing process. That is, the germanium wafer 500 is provided as a bare wafer, and the first annealing process and the second annealing process are sequentially performed on the germanium wafer 500, so that the first ablation zone DZ1 and the second ablation zone DZ2 and the body region BK are formed. . The first annealing process and the second annealing process are performed under the same conditions as those of the first annealing process and the second annealing process shown in FIGS. 2 to 4.

在圖5中,參考數字「501」表示頂面,「502」表示背面,「503」表示氧化物元素,「504」表示氧析出物核,「505A」表示氧析出物且「505B」表示經增大之氧析出物。In Fig. 5, reference numeral "501" indicates the top surface, "502" indicates the back surface, "503" indicates the oxide element, "504" indicates the oxygen precipitate core, "505A" indicates the oxygen precipitate, and "505B" indicates the Increased oxygen precipitates.

如上文所描述,參看圖2至圖5描述根據本發明之用於製造矽晶圓之方法。如先前所述,在圖2至圖4所展示之第一至第三實施例中,RTP偏好在第一退火製程及第二退火製程之前使用熱製程。As described above, a method for fabricating a germanium wafer in accordance with the present invention is described with reference to FIGS. 2 through 5. As described previously, in the first to third embodiments shown in FIGS. 2 to 4, the RTP prefers to use a thermal process before the first annealing process and the second annealing process.

矽晶圓中之氧析出物或空隙缺陷之內部缺陷可在成長單晶矽期間受到控制,或在成長單晶矽後藉由熱製程控制。如上文所描述,熱製程可包括使用鹵素燈之RTP及使用爐裝置之退火製程。The internal defects of the oxygen precipitates or void defects in the germanium wafer can be controlled during the growth of the single crystal germanium or by the thermal process after the growth of the single crystal germanium. As described above, the thermal process can include an RTP using a halogen lamp and an annealing process using a furnace device.

在氬(Ar)氣或氫(H2 )氣氛圍下於高於大致1000℃之高溫下執行使用爐裝置之退火製程歷時多於大致100分鐘之長時間。經由此退火製程引起之矽晶圓中氧化物元素之擴散及矽重排,在矽晶圓之頂面的一部分中形成器件理想區(亦即,無缺陷區(DFZ))。然而,隨著矽晶圓之大小增加,此退火製程難以控制歸因於高溫熱處理之矽晶圓之污染或滑動位錯。The annealing process using the furnace apparatus is performed for more than about 100 minutes at an elevated temperature of approximately 1000 ° C under an argon (Ar) gas or hydrogen (H 2 ) atmosphere. The diffusion of the oxide elements in the germanium wafer and the rearrangement of the germanium caused by the annealing process form an ideal region of the device (i.e., a defect free region (DFZ)) in a portion of the top surface of the germanium wafer. However, as the size of the germanium wafer increases, it is difficult to control the contamination or sliding dislocations of the germanium wafer due to the high temperature heat treatment.

因此,RTP獲得優於退火製程的矽晶圓特性。然而,當使用各種缺陷偵測方法評估由RTP製造之矽晶圓時,僅控制氧析出物在自頂面大致3微米至大致10微米之深度內。此外,當藉由僅執行RTP一次或兩次來製造矽晶圓時,存在對實現本體區域內高BMD密度之限制。更具體言之,當藉由執行RTP一次來製造矽晶圓時,BMD密度經確定在自1×106 ea/cm2 至3×106 ea/cm2 之範圍內,且難以使BMD密度超出該範圍。Therefore, RTP achieves the characteristics of germanium wafers superior to the annealing process. However, when various defect detection methods are used to evaluate tantalum wafers fabricated by RTP, only oxygen precipitates are controlled to be within a depth of from about 3 microns to about 10 microns from the top surface. Furthermore, when a germanium wafer is fabricated by performing RTP only once or twice, there is a limit to achieving high BMD density in the body region. More specifically, when a germanium wafer is manufactured by performing RTP once, the BMD density is determined to be in the range of from 1 × 10 6 ea/cm 2 to 3 × 10 6 ea/cm 2 , and it is difficult to make the BMD density. Beyond this range.

在本發明之實施例中,如圖2至圖4所展示,在熱製程後執行兩步驟退火製程,藉此移除靠近矽晶圓之頂面的空隙缺陷及氧析出物。結果,本發明可確保無缺陷區(DFZ)且增加BMD密度(包括本體區域中之本體堆疊缺陷及氧析出物),藉此藉由增加本體區域中之吸取位點來改良吸取效應。In an embodiment of the present invention, as shown in FIGS. 2 through 4, a two-step annealing process is performed after the thermal process, thereby removing void defects and oxygen precipitates near the top surface of the germanium wafer. As a result, the present invention can ensure a defect-free zone (DFZ) and increase the BMD density (including bulk stack defects and oxygen precipitates in the body region), thereby improving the suction effect by increasing the suction sites in the body region.

在下文中,參看表1及表2詳細描述由本發明之實施例製造之矽晶圓之特性。Hereinafter, the characteristics of the germanium wafer manufactured by the embodiment of the present invention will be described in detail with reference to Tables 1 and 2.

在表1中,使用氬(Ar)氣、氮(N2 )氣、氨(NH3 )氣或其組合在快速熱處理下執行「高溫RTP」及「低溫RTP」歷時大致10秒至大致30秒。使用氧(O2 )氣執行「低溫退火製程」及「高溫退火製程」歷時大致100分鐘至大致180分鐘。In Table 1, "high temperature RTP" and "low temperature RTP" are performed under rapid thermal processing using argon (Ar) gas, nitrogen (N 2 ) gas, ammonia (NH 3 ) gas or a combination thereof for approximately 10 seconds to approximately 30 seconds. . The "low temperature annealing process" and the "high temperature annealing process" are performed using oxygen (O 2 ) gas for approximately 100 minutes to approximately 180 minutes.

在表1及表2中,「條件1」表示圖2中展示之第一實施例,「條件2」表示圖3中展示之第二實施例,「條件3」表示圖4中展示之第三實施例且「條件4」表示圖5中展示之第四實施例。表2展示根據每一條件中之氧濃度(Oi)之BMD密度及剝蝕區(DZ)深度。In Tables 1 and 2, "Condition 1" indicates the first embodiment shown in Figure 2, "Condition 2" indicates the second embodiment shown in Figure 3, and "Condition 3" indicates the third shown in Figure 4. The embodiment and "Condition 4" represent the fourth embodiment shown in FIG. Table 2 shows the BMD density and the ablation zone (DZ) depth according to the oxygen concentration (Oi) in each condition.

圖7至圖12為展示表1及表2之參數的曲線圖。詳言之,圖7為說明關於每一條件之BMD密度之曲線圖。圖8為說明關於每一條件之DZ深度之曲線圖。圖9至圖12為說明關於每一條件之本體區域中氧濃度之曲線圖。7 to 12 are graphs showing the parameters of Tables 1 and 2. In detail, Figure 7 is a graph illustrating the BMD density for each condition. Figure 8 is a graph illustrating the DZ depth for each condition. 9 to 12 are graphs illustrating the oxygen concentration in the body region for each condition.

參看表2及圖7,在所有條件下獲得大於1×105 ea/cm2 之BMD密度。特定言之,在條件1下獲得大於1×106 ea/cm2 之BMD密度(與氧濃度無關)。儘管未呈現關於藉由僅執行RTP一次或兩次而製造之矽晶圓之BMD密度的資料,但可預測該BMD密度與以上條件下之BMD密度相比將顯著較低。Referring to Table 2 and Figure 7, a BMD density greater than 1 x 10 5 ea/cm 2 was obtained under all conditions. Specifically, a BMD density (regardless of oxygen concentration) of more than 1 × 10 6 ea/cm 2 was obtained under Condition 1. Although no data is presented regarding the BMD density of tantalum wafers fabricated by performing RTP only once or twice, it is predicted that the BMD density will be significantly lower than the BMD density under the above conditions.

如先前所述,藉由吸取BMD來控制金屬污染物。然而,因為在高溫製程期間BMD密度傾向於降低,所以在製造矽晶圓期間需要確保高BMD密度。一般而言,半導體器件需要在高壓環境下操作之高壓器件。為製造此高壓器件,必需執行重度離子植入製程及高溫退火製程,此係因為需要具有深分布之接合區域(亦即,摻雜區域)。當BMD密度在高溫退火製程期間降低時,不僅歸因於缺陷評估而且歸因於低吸取能力,在後繼淺渠溝隔離(STI)後出現環狀位錯。Metal contaminants are controlled by pipetting BMD as previously described. However, since the BMD density tends to decrease during the high temperature process, it is necessary to ensure a high BMD density during the fabrication of the germanium wafer. In general, semiconductor devices require high voltage devices that operate in a high voltage environment. In order to manufacture such a high voltage device, it is necessary to perform a heavy ion implantation process and a high temperature annealing process because a junction region having a deep distribution (i.e., a doped region) is required. When the BMD density decreases during the high temperature annealing process, not only due to defect evaluation but also due to low suction capability, annular dislocations occur after subsequent shallow trench isolation (STI).

作為量測BMD密度之結果,當BMD密度為大致2.5×105 ea/cm2 時部分出現環狀位錯,但當BMD密度為大致4.4×105 ea/cm2 時不出現環狀位錯。因此,需要控制BMD密度大於至少1×105 ea/cm2 。在本實施例中,與製造矽晶圓期間之習知熱製程無關,另外執行兩步驟退火製程以用於製造半導體器件之初始製程。初始製程包括在用於形成一井之離子植入之前執行的氧化製程。氧化製程對應於在用於形成一井之離子植入(在下文中,稱為井離子植入)期間用於形成遮蔽氧化物層之製程。As a result of measuring the BMD density, a circular dislocation occurs partially when the BMD density is approximately 2.5 × 10 5 ea/cm 2 , but no annular dislocation occurs when the BMD density is approximately 4.4 × 10 5 ea/cm 2 . . Therefore, it is necessary to control the BMD density to be greater than at least 1 x 10 5 ea/cm 2 . In this embodiment, a two-step annealing process is additionally performed for the initial process of fabricating a semiconductor device, regardless of the conventional thermal process during the fabrication of the germanium wafer. The initial process includes an oxidation process performed prior to ion implantation for forming a well. The oxidation process corresponds to a process for forming a masking oxide layer during ion implantation for forming a well (hereinafter, referred to as well ion implantation).

參看表2及圖8,展示根據每一條件之DZ深度。DZ深度與BMD密度及氧濃度緊密相關。隨著BMD密度及氧濃度增加,DZ深度變得減小。當氧濃度在每一條件下相同(例如,表2中之11.6)時,條件1及條件2下之BMD密度高於條件3及條件4下之BMD密度,但條件1及條件2下之DZ深度低於條件3及條件4下之DZ深度。因此,DZ深度可為BMD密度之量測。Referring to Table 2 and Figure 8, the DZ depth is shown for each condition. DZ depth is closely related to BMD density and oxygen concentration. As the BMD density and oxygen concentration increase, the DZ depth becomes smaller. When the oxygen concentration is the same under each condition (for example, 11.6 in Table 2), the BMD density under conditions 1 and 2 is higher than the BMD density under conditions 3 and 4, but the DZ under conditions 1 and 2. The depth is lower than the DZ depth under Condition 3 and Condition 4. Therefore, the DZ depth can be measured by the BMD density.

參看表2及圖9至圖12,展示每一條件下根據氧濃度之BMD密度及DZ深度。隨著氧濃度(Oi)增加,BMD密度變得增加但DZ深度變得減小。因此,氧濃度(Oi)亦為BMD密度之量測。亦即,可藉由量測DZ深度及氧濃度(Oi)來計算本體區域中之BMD密度。Referring to Table 2 and Figures 9 through 12, the BMD density and DZ depth according to oxygen concentration under each condition are shown. As the oxygen concentration (Oi) increases, the BMD density increases but the DZ depth becomes smaller. Therefore, the oxygen concentration (Oi) is also a measure of the BMD density. That is, the BMD density in the body region can be calculated by measuring the DZ depth and the oxygen concentration (Oi).

圖13及圖14為矽晶圓之橫截面圖。13 and 14 are cross-sectional views of a germanium wafer.

詳言之,圖13展示藉由僅執行RTP但無兩步驟退火製程而製造之矽晶圓之橫截面圖,且圖14展示藉由執行根據本發明之一實施例的兩步驟退火製程製造之矽晶圓之橫截面圖。In detail, FIG. 13 shows a cross-sectional view of a germanium wafer fabricated by performing only RTP but without a two-step annealing process, and FIG. 14 shows fabrication by performing a two-step annealing process in accordance with an embodiment of the present invention. A cross-sectional view of the wafer.

如所展示,在圖13之矽晶圓中出現複數個矽位錯,但在圖14之矽晶圓中不存在矽位錯。此外,當藉由使用磊晶成長形成磊晶層時,矽晶圓之本體區域(其中形成磊晶層)中之晶體缺陷顯著得以減少。As shown, a plurality of erroneous dislocations occur in the wafer of FIG. 13, but there are no erroneous dislocations in the wafer of FIG. Further, when an epitaxial layer is formed by using epitaxial growth, crystal defects in the body region of the germanium wafer in which the epitaxial layer is formed are remarkably reduced.

圖15及圖16說明矽晶圓中本體區域(其中形成磊晶層)之晶體缺陷圖。使用由KLA公司製造之檢驗裝置執行此檢驗。15 and 16 illustrate crystal defect diagrams of a body region (in which an epitaxial layer is formed) in a germanium wafer. This test was performed using an inspection device manufactured by KLA Corporation.

如圖15所展示,在執行不具有兩步驟退火製程之氧化製程時,大量晶體缺陷分布於圖中。在本文中,氧化製程在井離子植入期間形成遮蔽氧化物層。相反,如圖16所展示,在執行具有本發明之兩步驟退火製程之氧化製程時,晶體缺陷顯著減少。As shown in Figure 15, a large number of crystal defects are distributed in the figure when performing an oxidation process without a two-step annealing process. Herein, the oxidation process forms a masking oxide layer during well ion implantation. In contrast, as shown in FIG. 16, crystal defects are significantly reduced when performing an oxidation process having the two-step annealing process of the present invention.

在下文中,將參看圖17A至圖17D詳細描述用於製造具有用於高壓器件之井之半導體器件的方法,該方法包括根據本發明之一實施例的兩步驟退火製程。Hereinafter, a method for fabricating a semiconductor device having a well for a high voltage device will be described in detail with reference to FIGS. 17A through 17D, which includes a two-step annealing process according to an embodiment of the present invention.

圖17A至圖17D為說明根據本發明之實施例的用於製造半導體器件之方法。17A through 17D are diagrams illustrating a method for fabricating a semiconductor device in accordance with an embodiment of the present invention.

參看圖17A,使用圖6中展示之兩步驟退火製程在矽晶圓600上形成遮蔽氧化物層601。矽晶圓600可為如圖2至圖4中所描述之對其應用RTP一次或兩次的晶圓,或為如圖5中所描述之不對其應用RTP之裸晶圓。遮蔽氧化物層601可為氧化矽層,且形成至範圍為大致100至大致140之厚度。Referring to Figure 17A, a mask oxide layer 601 is formed over the germanium wafer 600 using the two-step annealing process illustrated in FIG. The germanium wafer 600 may be a wafer to which RTP is applied once or twice as described in FIGS. 2 to 4, or a bare wafer to which RTP is not applied as described in FIG. 5. The masking oxide layer 601 may be a hafnium oxide layer and formed to a range of approximately 100 To roughly 140 The thickness.

參看圖17B,在矽晶圓600中形成井602至一預定深度。視高壓器件之導電類型而定,井602可具有p型或n型導電類型。Referring to Figure 17B, well 602 is formed in tantalum wafer 600 to a predetermined depth. Well 602 may have a p-type or n-type conductivity type depending on the conductivity type of the high voltage device.

經由離子植入製程及擴散過程形成井602。僅使用離子植入製程難以形成用於高壓器件之井。因此,應在完成離子植入製程後另外執行擴散過程以及離子植入製程,以便形成具有圖17B之摻雜分布之井602。使用諸如爐之高溫加熱裝置經由退火製程執行擴散過程歷時長時間。較佳地,僅使用氮(N2 )氣在範圍為大致1100℃至大致1250℃之溫度下執行擴散過程歷時大致6小時至大致10小時。Well 602 is formed via an ion implantation process and a diffusion process. It is difficult to form a well for a high voltage device using only an ion implantation process. Therefore, the diffusion process and the ion implantation process should be additionally performed after the ion implantation process is completed to form the well 602 having the doping profile of FIG. 17B. The diffusion process is performed for a long time via an annealing process using a high temperature heating device such as a furnace. Preferably, the diffusion process is performed using a nitrogen (N 2 ) gas at a temperature ranging from approximately 1100 ° C to approximately 1250 ° C for a period of from about 6 hours to about 10 hours.

參看圖17C,充當硬式光罩之襯墊氮化物層(未圖示)形成於遮蔽氧化物層601上,或襯墊氮化物層形成於緩衝層(未圖示)上,該緩衝層係藉由在移除遮蔽氧化物層601後執行額外氧化製程而形成。移除遮蔽氧化物層601之原因為遮蔽氧化物層601不適合於緩衝層,因為遮蔽氧化物層601在離子植入製程期間受到損壞。接著在襯墊氮化物層上形成用於形成STI渠溝之光阻圖案604。Referring to FIG. 17C, a pad nitride layer (not shown) serving as a hard mask is formed on the mask oxide layer 601, or a pad nitride layer is formed on a buffer layer (not shown). It is formed by performing an additional oxidation process after removing the mask oxide layer 601. The reason for removing the masking oxide layer 601 is that the masking oxide layer 601 is not suitable for the buffer layer because the masking oxide layer 601 is damaged during the ion implantation process. A photoresist pattern 604 for forming an STI trench is then formed over the pad nitride layer.

可經由低壓化學氣相沈積(LPCVD)製程形成襯墊氮化物層,以便在沈積製程期間藉由最小化施加至矽晶圓600之應力而防止矽晶圓600受到損壞。襯墊氮化物層可由氮化矽形成。可形成襯墊氮化物層至範圍為大致1400至大致2000之厚度。The pad nitride layer can be formed via a low pressure chemical vapor deposition (LPCVD) process to prevent damage to the germanium wafer 600 during the deposition process by minimizing stress applied to the germanium wafer 600. The pad nitride layer may be formed of tantalum nitride. A pad nitride layer can be formed to a range of approximately 1400 To roughly 2000 The thickness.

使用光阻圖案604作為蝕刻遮罩來按順序部分地蝕刻襯墊氮化物層、遮蔽氧化物層601及矽晶圓600,藉此形成襯墊氮化物圖案603、遮蔽氧化物圖案601A、矽晶圓600A及井602A。結果,在矽晶圓600A中形成具有預定深度及傾角之渠溝605。The pad nitride layer, the mask oxide layer 601, and the germanium wafer 600 are partially etched in order using the photoresist pattern 604 as an etch mask, thereby forming the pad nitride pattern 603, the mask oxide pattern 601A, and the twin crystal Round 600A and well 602A. As a result, a trench 605 having a predetermined depth and inclination is formed in the germanium wafer 600A.

參看圖17D,形成填充渠溝605之器件隔離結構606,且隨後移除襯墊氮化物圖案603及遮蔽氧化物圖案601A。器件隔離結構606可由具有優良間隙填充性質之高密度電漿(HDP)層形成。Referring to FIG. 17D, a device isolation structure 606 filling the trench 605 is formed, and then the pad nitride pattern 603 and the mask oxide pattern 601A are removed. Device isolation structure 606 may be formed from a high density plasma (HDP) layer having excellent gap fill properties.

在比較本發明之方法與比較性實例的同時,下文將描述本發明之以上實施例之有利效應。本發明之方法包括經由使用兩步驟退火製程之氧化製程形成遮蔽氧化物層,而比較性實例包括經由使用一步退火製程之氧化製程形成遮蔽氧化物層。在此比較性實例之氧化製程中,使用濕式氧化製程在範圍為800℃至850℃之單一溫度下氧化矽晶圓。While comparing the method of the present invention with the comparative examples, the advantageous effects of the above embodiments of the present invention will be described below. The method of the present invention includes forming a masking oxide layer via an oxidation process using a two-step annealing process, and a comparative example includes forming a masking oxide layer via an oxidation process using a one-step annealing process. In the oxidation process of this comparative example, a tantalum wafer was oxidized using a wet oxidation process at a single temperature ranging from 800 °C to 850 °C.

圖18至圖21說明由比較性實例之氧化製程製備之矽晶圓中的缺陷。18 to 21 illustrate defects in a germanium wafer prepared by the oxidation process of the comparative example.

詳言之,圖18說明在由比較性實例之氧化製程製備之矽晶圓中經由STI製程形成一渠溝後由KLA公司所製造之檢驗裝置所檢驗之晶體缺陷之圖資料。如圖18所展示,可觀察到大多數缺陷晶圓中存在諸如環狀矽位錯之晶體缺陷。In particular, FIG. 18 illustrates a graph of crystal defects examined by an inspection apparatus manufactured by KLA Corporation after forming a trench through a STI process in a germanium wafer prepared by a comparative example oxidation process. As shown in Figure 18, the presence of crystal defects such as annular germanium dislocations in most defective wafers can be observed.

圖19及圖20為由KLA公司所製造之檢驗裝置所獲取的矽晶圓之掃描電子顯微鏡微觀(SEM)圖片。19 and 20 are scanning electron microscope microscopic (SEM) images of a germanium wafer obtained by an inspection apparatus manufactured by KLA Corporation.

具體而言,圖19為展示矽晶圓之截面之SEM影像,且圖20為平面傾斜STM影像。如圖19及圖20所展示,可觀察到存在晶體缺陷及位錯。Specifically, FIG. 19 is an SEM image showing a cross section of a germanium wafer, and FIG. 20 is a planar tilted STM image. As shown in Figures 19 and 20, the presence of crystal defects and dislocations was observed.

圖21為展示對具有環狀缺陷之矽晶圓進行之本體微觀缺陷(BMD)密度分析的顯微照片。Figure 21 is a photomicrograph showing the bulk microscopic defect (BMD) density analysis of a germanium wafer with a ring defect.

如圖21所展示,可觀察到大多數BMD緊靠矽晶圓之頂面形成,但少數BMD形成於矽晶圓之中央部分中,亦即,形成於本體區域中。亦即,本體區域之BMD密度顯著低於矽晶圓之頂面之BMD密度。As shown in Figure 21, it can be observed that most of the BMD is formed immediately adjacent to the top surface of the wafer, but a small number of BMDs are formed in the central portion of the germanium wafer, i.e., formed in the body region. That is, the BMD density of the body region is significantly lower than the BMD density of the top surface of the germanium wafer.

圖22至圖24為藉由使用根據本發明之實施例的兩步驟退火製程之氧化製程製備的矽晶圓中晶體缺陷之檢驗結果。使用由KLA公司製造之檢驗裝置執行此檢驗。22 to 24 are test results of crystal defects in a germanium wafer prepared by an oxidation process using a two-step annealing process according to an embodiment of the present invention. This test was performed using an inspection device manufactured by KLA Corporation.

詳言之,圖22說明在於藉由使用本發明之兩步驟退火製程之氧化製程製備的矽晶圓中經由STI製程形成渠溝後矽晶圓之晶體缺陷的檢驗結果。如圖22所展示,可觀察到晶體缺陷經移除且僅偵測到一些微粒或粉塵。In detail, FIG. 22 illustrates the inspection results of the crystal defects of the germanium wafer after the trench is formed by the STI process in the germanium wafer prepared by the oxidation process using the two-step annealing process of the present invention. As shown in Figure 22, it was observed that the crystal defects were removed and only some particles or dust were detected.

圖23為由KLA公司所製造之檢驗裝置所獲取的矽晶圓之平面傾斜STM影像。與圖22之結果類似,可觀察到僅偵測到一些微粒。Figure 23 is a plan view of a tilted STM of a germanium wafer obtained by an inspection apparatus manufactured by KLA Corporation. Similar to the results of Figure 22, it was observed that only some of the particles were detected.

圖24為展示對藉由使用本發明之兩步驟退火製程之氧化製程製備的矽晶圓進行BMD密度分析之顯微照片。如圖24所展示,可觀察到遍及矽晶圓均勻形成BMD。Figure 24 is a photomicrograph showing the BMD density analysis of a tantalum wafer prepared by an oxidation process using the two-step annealing process of the present invention. As shown in Figure 24, it is observed that the BMD is uniformly formed throughout the germanium wafer.

圖25為說明靜態隨機存取記憶體(SRAM)之待用模式期間漏電流之比較結果的曲線圖。在圖25中,左視圖展示藉由使用本發明之兩步驟退火製程之氧化製程製備的高壓器件之樣本,且右視圖展示比較性實例之高壓器件之樣本。如圖25所展示,可觀察到與藉由比較性實例之氧化製程製備之樣本相比,藉由本發明之氧化製程製備之樣本呈現均勻漏電流特徵。Figure 25 is a graph illustrating the comparison of leakage currents during a standby mode of a static random access memory (SRAM). In Fig. 25, a left side view shows a sample of a high voltage device prepared by an oxidation process using the two-step annealing process of the present invention, and a right side view shows a sample of a high voltage device of a comparative example. As shown in Figure 25, it was observed that the samples prepared by the oxidation process of the present invention exhibited uniform leakage current characteristics as compared to the samples prepared by the oxidation process of the comparative example.

圖26為說明生產良率之比較結果的曲線圖。在圖26中,左視圖展示藉由使用本發明之兩步驟退火製程之氧化製程製備的高壓器件之樣本,且右視圖展示比較性實例之高壓器件之樣本。如圖26所展示,與比較性實例之樣本相比,藉由本發明之氧化製程製備之樣本的生產良率高大致5%-9%。Fig. 26 is a graph showing the comparison result of the production yield. In Fig. 26, a left side view shows a sample of a high voltage device prepared by an oxidation process using the two-step annealing process of the present invention, and a right side view shows a sample of a high voltage device of a comparative example. As shown in Fig. 26, the production yield of the sample prepared by the oxidation process of the present invention was as high as about 5% to 9% as compared with the sample of the comparative example.

根據本發明,首先,可藉由在不同溫度下執行兩步驟退火製程而在矽晶圓中充分地產生吸取位點。此使得可能防止晶體缺陷歸因於由後繼高溫熱處理製程引起之熱預算而產生。According to the present invention, first, a suction site can be sufficiently produced in a germanium wafer by performing a two-step annealing process at different temperatures. This makes it possible to prevent crystal defects from being attributed to the thermal budget caused by the subsequent high temperature heat treatment process.

其次,本發明可藉由在不同溫度下執行兩步驟退火製程來提供在本體區域中具有高且均勻之BMD密度之矽晶圓。Second, the present invention can provide a germanium wafer having a high and uniform BMD density in the body region by performing a two-step annealing process at different temperatures.

第三,根據本發明,在於不同溫度下對矽晶圓執行兩步驟退火製程後,使用磊晶成長在矽晶圓上形成磊晶層。結果,本發明可提供形成有具優良特性之磊晶層的半導體器件。Third, according to the present invention, after performing a two-step annealing process on the germanium wafer at different temperatures, an epitaxial layer is formed on the germanium wafer using epitaxial growth. As a result, the present invention can provide a semiconductor device in which an epitaxial layer having excellent characteristics is formed.

第四,根據本發明,在藉由在不同溫度下對矽晶圓執行兩步驟退火製程來在矽晶圓上形成遮蔽氧化物層後,藉由使用遮蔽氧化物層作為離子遮罩執行離子植入製程來在矽晶圓中形成一井。結果,本發明可在矽晶圓中充分地產生吸取位點以藉此防止晶體缺陷歸因於由後繼高溫熱處理製程引起之熱預算而產生。Fourth, according to the present invention, after the shadow oxide layer is formed on the germanium wafer by performing a two-step annealing process on the germanium wafer at different temperatures, ion implantation is performed by using the mask oxide layer as an ion mask. The process is entered to form a well in the germanium wafer. As a result, the present invention can sufficiently generate the gettering sites in the germanium wafer to thereby prevent crystal defects from being generated due to the thermal budget caused by the subsequent high temperature heat treatment process.

儘管已關於特定實施例描述了本發明,但熟習此項技術者將顯而易見可在不偏離由以下申請專利範圍定義之本發明的精神及範疇的情況下做出各種改變及修改。While the invention has been described with respect to the specific embodiments thereof, it will be apparent to those skilled in the art that various changes and modifications can be made without departing from the spirit and scope of the invention as defined by the following claims.

100...矽晶圓100. . . Silicon wafer

101...頂面101. . . Top surface

102...背面102. . . back

103...本體微觀缺陷(BMD)103. . . Ontology micro defect (BMD)

200...矽晶圓200. . . Silicon wafer

201...頂面201. . . Top surface

202...背面202. . . back

203...氧化物元素203. . . Oxide element

204...氧析出物核204. . . Oxygen precipitate core

205A...氧析出物205A. . . Oxygen precipitate

205B...經增大之氧析出物205B. . . Increased oxygen precipitate

300...矽晶圓300. . . Silicon wafer

301...頂面301. . . Top surface

302...背面302. . . back

303...氧化物元素303. . . Oxide element

304...氧析出物核304. . . Oxygen precipitate core

305...氧析出物305. . . Oxygen precipitate

400...矽晶圓400. . . Silicon wafer

401...頂面401. . . Top surface

402...背面402. . . back

403...氧化物元素403. . . Oxide element

404...氧析出物核404. . . Oxygen precipitate core

405A...氧析出物405A. . . Oxygen precipitate

405B...經增大之氧析出物405B. . . Increased oxygen precipitate

500...矽晶圓500. . . Silicon wafer

501...頂面501. . . Top surface

502...背面502. . . back

503...氧化物元素503. . . Oxide element

504...氧析出物核504. . . Oxygen precipitate core

505A...氧析出物505A. . . Oxygen precipitate

505B...經增大之氧析出物505B. . . Increased oxygen precipitate

600...矽晶圓600. . . Silicon wafer

600A...矽晶圓600A. . . Silicon wafer

601...遮蔽氧化物層601. . . Masking oxide layer

601A...遮蔽氧化物圖案601A. . . Masking oxide pattern

602...井602. . . well

602A...井602A. . . well

603...襯墊氮化物圖案603. . . Pad nitride pattern

604...光阻圖案604. . . Resistive pattern

605...渠溝605. . . trench

606...器件隔離結構606. . . Device isolation structure

BK...本體區域BK. . . Body area

DZ1...第一剝蝕區DZ1. . . First ablation zone

DZ2...第二剝蝕區DZ2. . . Second ablation zone

圖1為根據本發明之一實施例的矽晶圓之橫截面圖;1 is a cross-sectional view of a germanium wafer in accordance with an embodiment of the present invention;

圖2為說明根據本發明之第一實施例的用於製造一矽晶圓之方法的橫截面圖;2 is a cross-sectional view illustrating a method for fabricating a germanium wafer in accordance with a first embodiment of the present invention;

圖3為說明根據本發明之第二實施例的用於製造一矽晶圓之方法的橫截面圖;3 is a cross-sectional view illustrating a method for fabricating a germanium wafer in accordance with a second embodiment of the present invention;

圖4為說明根據本發明之第三實施例的用於製造一矽晶圓之方法的橫截面圖;4 is a cross-sectional view illustrating a method for fabricating a germanium wafer in accordance with a third embodiment of the present invention;

圖5為說明根據本發明之第四實施例的用於製造一矽晶圓之方法的橫截面圖;5 is a cross-sectional view illustrating a method for fabricating a tantalum wafer in accordance with a fourth embodiment of the present invention;

圖6為說明根據本發明之一實施例的兩步驟退火製程方法之曲線圖;6 is a graph illustrating a two-step annealing process in accordance with an embodiment of the present invention;

圖7為說明在各種條件下BMD密度之曲線圖;Figure 7 is a graph illustrating BMD density under various conditions;

圖8為說明在各種條件下剝蝕區之深度之曲線圖;Figure 8 is a graph illustrating the depth of the ablation zone under various conditions;

圖9至圖12為說明在各種條件下根據氧濃度之BMD密度及剝蝕區之深度之曲線圖;9 to 12 are graphs illustrating the BMD density and the depth of the ablation zone according to the oxygen concentration under various conditions;

圖13為根據比較性實例製造之矽晶圓之橫截面圖;Figure 13 is a cross-sectional view of a germanium wafer fabricated in accordance with a comparative example;

圖14為根據本發明之實施例製造之矽晶圓之橫截面圖;Figure 14 is a cross-sectional view of a germanium wafer fabricated in accordance with an embodiment of the present invention;

圖15說明根據比較性實例製造之矽晶圓中本體區域之晶體缺陷圖;Figure 15 illustrates a crystal defect map of a body region in a germanium wafer fabricated according to a comparative example;

圖16說明使用根據本發明之一實施例的兩步驟退火製程製造之矽晶圓中本體區域之晶體缺陷圖;16 illustrates a crystal defect diagram of a body region in a germanium wafer fabricated using a two-step annealing process in accordance with an embodiment of the present invention;

圖17A至圖17D為說明根據本發明之一實施例的用於製造半導體器件之方法;17A-17D are diagrams illustrating a method for fabricating a semiconductor device in accordance with an embodiment of the present invention;

圖18說明根據比較性實例製備之矽晶圓中之晶體缺陷的檢驗結果;Figure 18 illustrates test results of crystal defects in a germanium wafer prepared according to a comparative example;

圖19為藉由比較性實例之氧化製程製備的矽晶圓之掃描電子顯微鏡(SEM)圖像;Figure 19 is a scanning electron microscope (SEM) image of a germanium wafer prepared by an oxidation process of a comparative example;

圖20為藉由比較性實例之氧化製程製備的矽晶圓之平面影像;20 is a plan view of a germanium wafer prepared by an oxidation process of a comparative example;

圖21為展示對藉由比較性實例之氧化製程製備的矽晶圓進行之BMD密度分析的微觀圖像;21 is a microscopic image showing BMD density analysis of a germanium wafer prepared by an oxidation process of a comparative example;

圖22說明根據本發明之一實施例之矽晶圓的晶體缺陷之檢驗結果;22 illustrates test results of crystal defects of a germanium wafer in accordance with an embodiment of the present invention;

圖23為根據本發明之一實施例之矽晶圓的平面影像;23 is a plan view of a germanium wafer in accordance with an embodiment of the present invention;

圖24為展示對根據本發明之一實施例的矽晶圓進行之BMD密度分析的顯微照片;24 is a photomicrograph showing BMD density analysis of a germanium wafer in accordance with an embodiment of the present invention;

圖25為說明在靜態隨機存取記憶體(SRAM)之待用模式期間漏電流之比較結果的曲線圖;及25 is a graph illustrating a comparison result of leakage currents during a standby mode of a static random access memory (SRAM); and

圖26為說明生產良率之比較結果之曲線圖。Fig. 26 is a graph showing the comparison result of the production yield.

100...矽晶圓100. . . Silicon wafer

101...頂面101. . . Top surface

102...背面102. . . back

103...本體微觀缺陷(BMD)103. . . Ontology micro defect (BMD)

BK...本體區域BK. . . Body area

DZ1...第一剝蝕區DZ1. . . First ablation zone

DZ2...第二剝蝕區DZ2. . . Second ablation zone

Claims (36)

一種矽晶圓,其包含:一第一剝蝕區,其經形成具有始於該矽晶圓之一頂面的一預定深度;及一本體區域,其形成於該第一剝蝕區與該矽晶圓之一背面之間,其中該第一剝蝕區經形成具有範圍為始於該頂面的大致20微米至大致80微米之一深度,且其中該本體區域中氧之一濃度遍及該本體區域以在10%內之一變化均勻分布。 A germanium wafer comprising: a first ablation region formed to have a predetermined depth starting from a top surface of the germanium wafer; and a body region formed in the first ablation region and the twin Between one of the back sides of the circle, wherein the first ablation zone is formed to have a depth ranging from approximately 20 microns to approximately 80 microns from the top surface, and wherein a concentration of oxygen in the body region is throughout the body region One of the changes within 10% is evenly distributed. 如請求項1之矽晶圓,其中該本體區域中一本體微觀缺陷(BMD)之一密度的範圍為大致1×105 ea/cm2 至大致1×107 ea/cm2The wafer of claim 1 wherein the density of one of the bulk microscopic defects (BMD) in the body region ranges from approximately 1 x 10 5 ea/cm 2 to approximately 1 x 10 7 ea/cm 2 . 如請求項1之矽晶圓,其中該本體區域中氧之一濃度的範圍為大致10.5 PPMA至大致13 PPMA(原子百萬分率)。 As claimed in claim 1, the concentration of one of the oxygen in the body region ranges from approximately 10.5 PPMA to approximately 13 PPMA (atomic parts per million). 如請求項1之矽晶圓,其進一步包含一磊晶層,該磊晶層經由一磊晶成長而形成在該矽晶圓之該頂面上。 The wafer of claim 1, further comprising an epitaxial layer formed on the top surface of the germanium wafer by epitaxial growth. 如請求項1之矽晶圓,其進一步包含一第二剝蝕區,該第二剝蝕區經形成於該本體區域下方且具有自該背面朝向該頂面之方向的一預定深度。 The wafer of claim 1, further comprising a second ablation zone formed under the body region and having a predetermined depth from the back surface toward the top surface. 如請求項5之矽晶圓,其中該第二剝蝕區經形成具有範圍為始於該背面的大致20微米至大致80微米之一深度。 The wafer of claim 5, wherein the second ablation zone is formed to have a depth ranging from about 20 microns to about 80 microns starting from the back side. 一種半導體處理方法,其包含:熱處理一矽晶圓以形成在該矽晶圓中一剝蝕區及一本 體區域;於一裝載溫度下將經熱處理之該矽晶圓裝載於一加熱裝置;在一第一溫度下對該矽晶圓執行一第一退火製程以在該本體區域中補充產生氧析出物核及氧析出物;及在高於該第一溫度之一第二溫度下對該矽晶圓執行一第二退火製程以增大該本體區域中之該等氧析出物,其中該矽晶圓的該熱處理發生於經熱處理之該矽晶圓的該裝載之前。 A semiconductor processing method comprising: heat treating a wafer to form an ablation region and a book in the germanium wafer a body region; the heat-treated tantalum wafer is loaded on a heating device at a loading temperature; and a first annealing process is performed on the silicon wafer at a first temperature to replenish oxygen precipitates in the body region a core and an oxygen precipitate; and performing a second annealing process on the silicon wafer at a second temperature higher than the first temperature to increase the oxygen precipitates in the body region, wherein the germanium wafer This heat treatment occurs prior to the loading of the heat treated tantalum wafer. 如請求項7之方法,其中該第一退火製程係在範圍為大致750℃至大致800℃之一溫度下執行。 The method of claim 7, wherein the first annealing process is performed at a temperature ranging from approximately 750 ° C to approximately 800 ° C. 如請求項7之方法,其中該第二退火製程係在範圍為大致1000℃至大致1150℃之一溫度下執行。 The method of claim 7, wherein the second annealing process is performed at a temperature ranging from approximately 1000 ° C to approximately 1150 ° C. 如請求項7之方法,其中經熱處理之該矽晶圓包括:在等於或低於該第二溫度之一第三溫度下對該矽晶圓執行一第一熱製程以形成該剝蝕區及該本體區域;及在高於該第一溫度且低於該第三溫度之一第四溫度下對該矽晶圓執行一第二熱製程以在該本體區域中形成該等氧析出物核。 The method of claim 7, wherein the heat-treated tantalum wafer comprises: performing a first thermal process on the tantalum wafer at a third temperature equal to or lower than the second temperature to form the ablated region and a body region; and performing a second thermal process on the silicon wafer at a temperature above the first temperature and below the third temperature to form the oxygen precipitate cores in the body region. 如請求項10之方法,其中該第一熱製程及該第二熱製程係藉由一快速熱製程(RTP)或一退火製程執行。 The method of claim 10, wherein the first thermal process and the second thermal process are performed by a rapid thermal process (RTP) or an annealing process. 如請求項10之方法,其中該第一熱製程係在範圍為大致1050℃至大致1150℃之一溫度下執行,且該第二熱製程係在範圍為大致950℃至大致1000℃之一溫度下執行。 The method of claim 10, wherein the first thermal process is performed at a temperature ranging from approximately 1050 ° C to approximately 1150 ° C, and the second thermal process is at a temperature ranging from approximately 950 ° C to approximately 1000 ° C. Execute. 如請求項10之方法,其中該第一熱製程及該第二熱製程使用氬(Ar)氣、氮(N2 )氣、氨(NH3 )氣或其之一組合。The method of claim 10, wherein the first thermal process and the second thermal process use argon (Ar) gas, nitrogen (N 2 ) gas, ammonia (NH 3 ) gas, or a combination thereof. 如請求項7之方法,其中經熱處理之該矽晶圓包括:在等於或低於該第二溫度之一第三溫度下對該矽晶圓執行一熱製程以形成該剝蝕區及該本體區域。 The method of claim 7, wherein the heat-treated tantalum wafer comprises: performing a thermal process on the tantalum wafer at a third temperature equal to or lower than the second temperature to form the ablated region and the body region . 如請求項14之方法,其中該熱製程係在範圍為大致1050℃至大致1150℃之一溫度下執行。 The method of claim 14, wherein the thermal process is performed at a temperature ranging from approximately 1050 ° C to approximately 1150 ° C. 如請求項7之方法,其中經熱處理之該矽晶圓包括:在高於該第一溫度且低於該第二溫度的一第三溫度下對該矽晶圓執行一熱製程以形成該剝蝕區及該本體區域。 The method of claim 7, wherein the heat-treated tantalum wafer comprises: performing a thermal process on the tantalum wafer at a third temperature higher than the first temperature and lower than the second temperature to form the ablation Zone and the body area. 如請求項16之方法,其中該熱製程係在範圍為大致950℃至大致1000℃之一溫度下執行。 The method of claim 16, wherein the thermal process is performed at a temperature ranging from approximately 950 ° C to approximately 1000 ° C. 如請求項7之方法,其中該第一退火製程及該第二退火製程係在氧(O2 )氣氛圍下執行。The method of claim 7, wherein the first annealing process and the second annealing process are performed under an oxygen (O 2 ) gas atmosphere. 如請求項7之方法,其中該第一退火製程及該第二退火製程中之每一者執行歷時大致100分鐘至大致180分鐘。 The method of claim 7, wherein each of the first annealing process and the second annealing process is performed for a period of from about 100 minutes to about 180 minutes. 如請求項7之方法,其中該剝蝕區經形成具有範圍為始於該矽晶圓之一頂面的大致20微米至大致80微米之一深度。 The method of claim 7, wherein the ablated region is formed to have a depth ranging from substantially 20 microns to substantially 80 microns from a top surface of the one of the germanium wafers. 如請求項7之方法,其中在執行該第二退火製程後,該本體區域中包括該等氧析出物之一本體微觀缺陷(BMD)之一密度經控制到大致1×105 ea/cm2 至大致1×107 ea/cm2 的範圍。The method of claim 7, wherein after performing the second annealing process, a density of one of the bulk microscopic defects (BMD) including the one of the oxygen precipitates in the body region is controlled to approximately 1×10 5 ea/cm 2 It is approximately 1×10 7 ea/cm 2 . 如請求項7之方法,其中在執行該第二退火製程後,該本體區域中氧之一濃度經控制為遍及該本體區域以10%內之一變化均勻分布。 The method of claim 7, wherein after performing the second annealing process, a concentration of oxygen in the body region is controlled to be uniformly distributed throughout the body region by one of 10%. 如請求項7之方法,其中在執行該第二退火製程後,該本體區域中氧之一濃度經控制到大致10.5至大致13 PPMA的範圍。 The method of claim 7, wherein after performing the second annealing process, a concentration of oxygen in the body region is controlled to a range of approximately 10.5 to approximately 13 PPMA. 如請求項7之方法,其進一步包含:移除在該第二退火製程期間在該矽晶圓之一頂面上形成之一層氧化物層;及經由一磊晶成長形成一磊晶層,該磊晶層係形成在該矽晶圓之該頂面上。 The method of claim 7, further comprising: removing one of the oxide layers formed on one of the top surfaces of the germanium wafer during the second annealing process; and forming an epitaxial layer via epitaxial growth, An epitaxial layer is formed on the top surface of the germanium wafer. 如請求項7之方法,其進一步包含:藉由使用一層氧化物層作為一緩衝層在該矽晶圓中形成一井,其中該氧化物層係在該第二退火製程期間形成在該矽晶圓之一頂面上。 The method of claim 7, further comprising: forming a well in the germanium wafer by using an oxide layer as a buffer layer, wherein the oxide layer is formed in the twin crystal during the second annealing process On one of the tops of the circle. 如請求項7之方法,其中經熱處理之該矽晶圓包括:成長一單晶矽;將該經成長之單晶矽切割為一晶圓形狀;及執行一刻蝕製程以蝕刻該經切割之矽晶圓之表面或使該經切割之矽晶圓之側面變圓。 The method of claim 7, wherein the heat-treated tantalum wafer comprises: growing a single crystal germanium; cutting the grown single crystal germanium into a wafer shape; and performing an etching process to etch the cut wafer The surface of the wafer or the sides of the diced wafer are rounded. 一種半導體處理方法,其包含:熱處理一矽晶圓以在該矽晶圓中形成一剝蝕區及一本體區域;於一裝載溫度下將經熱處理之該矽晶圓裝載於一加熱 裝置中;對已裝載之該矽晶圓進行第一次加熱,以從該裝載溫度加熱至一第一溫度;對已進行第一次加熱之該矽晶圓於該第一溫度下進行第一次退火,以在已進行第一次加熱之該矽晶圓中產生氧析出物;直接對已進行第一次退火之該矽晶圓進行第二次加熱,以從該第一溫度加熱至一第二溫度,其中該第二溫度大於該第一溫度;對已進行第二次加熱之該矽晶圓於該第二溫度下進行第二次退火,以擴大及增加已進行第二次加熱之該矽晶圓中的該等氧析出物之一密度;對已進行第二次退火之該矽晶圓進行冷卻,以從該第二溫度冷卻至一卸載溫度;以及將已進行冷卻之該矽晶圓於該卸載溫度下從該加熱裝置中卸載,其中該矽晶圓的該熱處理發生於經熱處理之該矽晶圓的該裝載之前。 A semiconductor processing method includes: heat treating a wafer to form an ablation region and a body region in the germanium wafer; and loading the heat treated tantalum wafer on a heating temperature at a loading temperature In the apparatus, performing the first heating on the loaded wafer to heat from the loading temperature to a first temperature; and performing the first heating on the first wafer at the first temperature Sub-annealing to generate oxygen precipitates in the germanium wafer that has been heated for the first time; directly heating the germanium wafer that has been subjected to the first annealing for a second heating to heat from the first temperature to one a second temperature, wherein the second temperature is greater than the first temperature; and the second wafer having been subjected to the second heating is subjected to a second annealing at the second temperature to expand and increase the second heating a density of one of the oxygen precipitates in the germanium wafer; cooling the germanium wafer that has been a second annealed to cool from the second temperature to an unloading temperature; and cooling the crucible that has been cooled The wafer is unloaded from the heating device at the unloading temperature, wherein the heat treatment of the germanium wafer occurs prior to the loading of the heat treated tantalum wafer. 如請求項27之方法,其中該裝載溫度之範圍為大致600℃至大致700℃。 The method of claim 27, wherein the loading temperature ranges from approximately 600 ° C to approximately 700 ° C. 如請求項27之方法,其中已裝載之該矽晶圓的該第一次加熱之一升溫速率的範圍為大致5℃/分鐘至大致8℃/分鐘。 The method of claim 27, wherein the rate of temperature rise of the first heating of the germanium wafer that has been loaded ranges from approximately 5 ° C/minute to approximately 8 ° C/minute. 如請求項27之方法,其中該第一溫度之範圍為大致 750℃至大致800℃。 The method of claim 27, wherein the first temperature range is approximately 750 ° C to approximately 800 ° C. 如請求項27之方法,其中已進行第一次退火之該矽晶圓的該第二次加熱之一升溫速率的範圍為大致5℃/分鐘至大致8℃/分鐘。 The method of claim 27, wherein the second heating rate of the second heating of the tantalum wafer that has been subjected to the first annealing ranges from approximately 5 ° C/min to approximately 8 ° C/min. 如請求項27之方法,其中該第二溫度之範圍為大致1000℃至大致1150℃。 The method of claim 27, wherein the second temperature ranges from approximately 1000 ° C to approximately 1150 ° C. 如請求項27之方法,其中已進行第二次退火之該矽晶圓的該冷卻之一降溫速率的範圍為大致2℃/分鐘至大致4℃/分鐘。 The method of claim 27, wherein the cooling rate of the cooling of the tantalum wafer that has been subjected to the second annealing ranges from approximately 2 ° C/min to approximately 4 ° C/min. 如請求項27之方法,其中該卸載溫度之範圍為大致750℃至大致800℃。 The method of claim 27, wherein the unloading temperature ranges from approximately 750 ° C to approximately 800 ° C. 如請求項27之方法,其中該卸載該矽晶圓係使用氮(N2 )氣執行。The method of claim 27, wherein the unloading the germanium wafer is performed using nitrogen (N 2 ) gas. 如請求項27之方法,其中該第一次退火及該第二次退火係使用氧(O2 )氣執行。The method of claim 27, wherein the first annealing and the second annealing are performed using oxygen (O 2 ) gas.
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