TW201241937A - Methods for bonding semiconductor structures involving annealing processes, and bonded semiconductor structures and intermediate structures formed using such methods - Google Patents
Methods for bonding semiconductor structures involving annealing processes, and bonded semiconductor structures and intermediate structures formed using such methods Download PDFInfo
- Publication number
- TW201241937A TW201241937A TW101108739A TW101108739A TW201241937A TW 201241937 A TW201241937 A TW 201241937A TW 101108739 A TW101108739 A TW 101108739A TW 101108739 A TW101108739 A TW 101108739A TW 201241937 A TW201241937 A TW 201241937A
- Authority
- TW
- Taiwan
- Prior art keywords
- metal
- semiconductor structure
- bonding
- annealing
- bonded
- Prior art date
Links
Classifications
-
- H10W99/00—
-
- H10W72/019—
-
- H10W72/01931—
-
- H10W72/01951—
-
- H10W72/01971—
-
- H10W72/07536—
-
- H10W72/90—
-
- H10W72/923—
-
- H10W72/926—
-
- H10W72/931—
-
- H10W72/934—
-
- H10W72/941—
-
- H10W72/9415—
-
- H10W72/942—
-
- H10W72/952—
-
- H10W80/035—
-
- H10W80/041—
-
- H10W80/102—
-
- H10W80/312—
-
- H10W80/314—
-
- H10W80/327—
-
- H10W80/333—
-
- H10W80/701—
-
- H10W80/721—
-
- H10W80/732—
-
- H10W80/754—
-
- H10W90/792—
Landscapes
- Internal Circuitry In Semiconductor Integrated Circuit Devices (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Abstract
Description
201241937 六、發明說明: 【發明所屬之技術領域】 本揭示内容之實施例係關於將半導體結構接合至一起之 方法及使用該等方法形成之經接合的半導體結構及中間結 構。 【先前技術】 兩個或更多個半導體結構之三維(3D)整合可對微電子應 用產生若干個益處。舉例而言,微電子組件之31)整合可產 生改良之電效能及電力消耗同時減小裝置佔用面積。例如 參見P. Ganrou等人,「The Handbook of 3D Integration」, Wiley-VCH (2008)。 半導體結構之3D整合可藉由半導體晶粒至一或多個其他 半導體晶粒(亦即,晶粒至晶粒(D2D))、半導體晶粒至一 或多個半導體晶圓(亦即,晶粒至晶圓(D2W))以及半導體 晶圓至一或多個其他半導體晶圓(亦即,晶圓至晶圓 (W2W))之附接或其組合而發生。 在將一個半導體結構接合至另一半導體結構中使用之接 合技術可以不同方式進行分類,一種係在兩個半導體結構 之間是否提供有中間材料層以將其接合至一起且第二種 係接合界面是否允許電子(亦即,電流)通過該界面。所謂 的「直接接合方法」係如下方法:其中在兩個半導體結構 之間建立直接固體至固體化學接合以將其接合至一起而不 在該等兩個半導體結構之間使用中間接合材料來將其接合 至起。直接金屬至金屬接合方法已經研發而用於將第一 162378.doc 201241937 半導體結構之表面處之金屬材料接合至第二半導體結構之 表面處之金屬材料。 直接金屬至金屬接合方法亦可按實施每—方法所處之溫 度範圍來分類。舉例而言些直接金屬至金屬接合方法 係在相對高溫下實施,從而導致接合界面處之金屬材料之 至少部分炫化。該等直接接合程序可能不期望供在接合包 含一或多個裝置結構之經處理半導體結構中使用,此乃因 相對高溫可不利地影響較早形成之裝置結構。 「熱壓縮接合」方法係如下接合方法〔其中在介於2〇〇 攝氏度(200t )與約500攝氏度(500。〇)之間(且通常介於約 300攝氏度(300°C )與約400攝氏度(40(rc )之間)之高溫下在 接合表面之間施加壓力。 已研發可在200攝氏度(200。(:)或小於200攝氏度之溫度 下實施之其他直接接合方法。在200攝氏度(2〇(rc)或小於 200攝氏度之溫度下實施之該等直接接合程序在本文中稱 為「超低溫」直接接合方法。可藉由仔細去除表面雜質及 表面化合物(例如,自然氧化物)及藉由以原子標度增加兩 個表面之間之緊密接觸區而實施超低溫直接接合方法。通 常藉由以下方式實現兩個表面之間之緊密接觸區:對接合 表面進行拋光以將表面粗糙度減小至接近原子標度之值; 在接合表面之間施加壓力從而引起塑膠變形;或對接合表 面進行拋光並施加壓力以獲得該塑膠變形。 一些超低溫直接接合方法可在不在接合界面處之接合表 面之間施加壓力之情形下實施,但在其他超低溫直接接合 162378.doc 201241937 方法中可在接合界面處之接合表面之間施加壓力以達成接 σ界面處之適宜接合強度。在接合表面之間施加壓力之超 低'皿直接接合方法在業内通常稱為「表面辅助接合」或 SAB」方法。因此,本文所用之術語「表面輔助接合」 及「SAB」意指且包含如下任一直接接合程序:藉由在 200攝氏度(200。〇或小於200攝氏度之溫度下抵靠第二材料 鄰接第一材料且在接合界面處之接合表面之間施加壓力而 將該第一材料直接接合至該第二材料。 在一些情形下,半導體結構中主動導電特徵之間之直接 金屬至金屬接合可易於在一定時間之後發生機械故障或電 故障,即使最初可在半導體結構之導電特徵之間建立可接 文之直接金屬至金屬接合。儘管並未完全理解,但據信, 該故障可至少部分地由三種相關機制中之一或多者引起。 該等一種相關機制係應變局部化(可由較大晶粒促進)、變 形相關性晶粒生長及接合界面處之質量傳遞。接合界面處 之該質量傳遞可至少部分地歸因於電遷移、相分離等。 電遷移係導電材料中由電流引起之金屬原子遷移。業内 已論述改良互連件之電遷移壽命之各種方法。舉例而言, 改良銅互連件之電磁壽命之方法論述於j_ Gambino等人, 「Copper Interconnect Technology for· the 32 nm Node and201241937 VI. Description of the Invention: TECHNICAL FIELD [0001] Embodiments of the present disclosure are directed to methods of joining semiconductor structures together and bonded semiconductor structures and intermediate structures formed using such methods. [Prior Art] Three-dimensional (3D) integration of two or more semiconductor structures can yield several benefits for microelectronic applications. For example, 31) integration of microelectronic components can result in improved electrical performance and power consumption while reducing device footprint. See, for example, P. Ganrou et al., "The Handbook of 3D Integration", Wiley-VCH (2008). 3D integration of semiconductor structures can be through semiconductor dies to one or more other semiconductor dies (ie, die-to-die (D2D)), semiconductor dies to one or more semiconductor wafers (ie, crystal Particle-to-wafer (D2W) and attachment of semiconductor wafers to one or more other semiconductor wafers (ie, wafer-to-wafer (W2W)) or combinations thereof occur. The bonding technique used in bonding a semiconductor structure to another semiconductor structure can be classified in different ways, one whether an intermediate material layer is provided between the two semiconductor structures to bond them together and the second bonding interface Whether electrons (ie, current) are allowed to pass through the interface. The so-called "direct bonding method" is a method in which a direct solid-to-solid chemical bonding is established between two semiconductor structures to bond them together without using an intermediate bonding material between the two semiconductor structures to bond them. Up to the beginning. Direct metal to metal bonding methods have been developed for bonding metal materials at the surface of the first 162378.doc 201241937 semiconductor structure to metal materials at the surface of the second semiconductor structure. Direct metal to metal joining methods can also be classified according to the temperature range in which each method is implemented. For example, direct metal to metal bonding processes are performed at relatively high temperatures, resulting in at least partial smearing of the metallic material at the joint interface. Such direct bonding procedures may not be desirable for use in bonding processed semiconductor structures that include one or more device structures, as relatively high temperatures can adversely affect earlier formed device structures. The "thermocompression bonding" method is a bonding method in which between 2 〇〇 Celsius (200 t) and about 500 ° C (500 〇) (and usually between about 300 ° C (300 ° C) and about 400 ° C) Pressure is applied between the joint surfaces at high temperatures (between 40 (rc)) Other direct joining methods that can be carried out at temperatures of 200 degrees Celsius (200 (.) or less than 200 degrees Celsius have been developed. At 200 degrees Celsius (2 Such direct bonding procedures performed at temperatures of 〇 (rc) or less than 200 degrees Celsius are referred to herein as "ultra-low temperature" direct bonding methods by careful removal of surface impurities and surface compounds (eg, natural oxides) and by An ultra-low temperature direct bonding method is performed by increasing the close contact area between two surfaces on an atomic scale. The intimate contact area between the two surfaces is usually achieved by polishing the bonding surface to reduce the surface roughness to a value close to the atomic scale; applying pressure between the bonding surfaces to cause deformation of the plastic; or polishing the bonding surface and applying pressure to obtain the plastic deformation Some ultra-low temperature direct bonding methods can be practiced without applying pressure between the bonding surfaces at the bonding interface, but in other ultra-low temperature direct bonding 162378.doc 201241937 methods, pressure can be applied between the bonding surfaces at the bonding interface to achieve Suitable joint strength at the σ interface. The ultra-low 'tank direct bonding method for applying pressure between the joint surfaces is commonly referred to in the industry as the "surface assisted joint" or SAB method. Therefore, the term "surface assisted joint" is used herein. And "SAB" means and includes any of the following direct bonding procedures: by abutting the first material against the second material at a temperature of 200 degrees Celsius (200. or less than 200 degrees Celsius and between the bonding surfaces at the joint interface) Pressure is applied to bond the first material directly to the second material. In some cases, direct metal-to-metal bonding between active conductive features in the semiconductor structure can easily cause mechanical or electrical failure after a certain time, even if initially Direct metal-to-metal bonding can be established between conductive features of semiconductor structures Although not fully understood, it is believed that the fault can be caused, at least in part, by one or more of the three related mechanisms. The one related mechanism is strain localization (promoted by larger grains), deformation-dependent crystals Grain growth and mass transfer at the joint interface. This mass transfer at the joint interface can be at least partially attributed to electromigration, phase separation, etc. Electromigration is the migration of metal atoms by currents in conductive materials. Various methods of electromigration life of interconnects. For example, a method for improving the electromagnetic lifetime of copper interconnects is discussed in j_Gambino et al., "Copper Interconnect Technology for · the 32 nm Node and
Beyond j > IEEE 2009 Custom Integrated Circuits Conference (CICC),第 141-148頁中。 【發明内容】 提供本發明内容以按簡化形式介紹概念之選擇,在下文 162378.doc 201241937 本揭不内容之—些實例性實施例之詳細說明中進一步闡述 該等概念。本發明内容既不意欲鑑別所主張標的物之關鍵 特徵或基本特徵,亦不意欲用以限制所主張標的物之範 圍。 在一些實施*例中’本揭示内容包含將第一半導體結構直 接接合至第二半導體結構之方法。根據該等方法,可將金 屬沈積於第一半導體結構上。可去除沈積於第一半導體結 構上之金屬之一部分,且可使沈積於第一半導體結構上之 金屬之剩餘部分經受第一熱預算以將該沈積於第一半導體 結構上之金屬之剩餘部分退火。可將第一半導體結構之至 少一個金屬特徵(包括沈積於第一半導體結構上之金屬之 剩餘部分)直接接合至第二半導體結構之至少一個金屬特 徵以形成經接合的金屬結構’該經接合的金屬結構包含第 一半導體結構之至少一個金屬特徵及第二半導體結構之至 少一個金屬特徵。可使經接合的金屬結構經受第二熱預算 以將該經接合的金屬結構退火。經接合的金屬結構所經受 之第二熱預算可小於第一熱預算。 在將第一半導體結構直接接合至第二半導體結構之方法 之其他實施例中,可將金屬沈積於第一半導體結構上,然 後可去除沈積於第一半導體結構上之金屬之一部分。可使 沈積於第一半導體結構上之金屬之剩餘部分經受第一熱預 算以將該沈積於第一半導體結構上之金屬之剩餘部分退 火。在將沈積於第一半導體結構上之金屬之剩餘部分退火 之後’可去除沈積於第一半導體結構上之金屬之其他部 162378.doc 201241937 分。可將第—半.導體結構之至少一個金屬肖徵(包括沈積 於第一半導體結構上之金屬之剩餘部分)直接接合至第二 半導體結構之至少一個金屬特徵以形成經接合的金屬結 構,該經接合的金屬結構包含第一半導體結構之至少一個 金屬特徵及第二半導體結構之至少一個金屬特徵。可使經 接合的金屬結構經受第二熱預算以將該經接合的金屬結構 退火。第二熱預算可小於第一熱預算。 在將第一半導體結構直接接合至第二半導體結構之方法 之其他貫施例中’直接接合程序可在大於或等於約〇〇之 溫度(例如室溫)下實施。可使第一半導體結構之至少—個 金屬特徵(包括沈積於第一半導體結構上之金屬之剩餘部 分)經受介於約2〇它與400。(:之間之接合溫度。 在將第一半導體結構直接接合至第二半導體結構之方法 之其他實施例中,可將金屬沈積於第一半導體結構上且可 在金屬中形成至少一個空隙。可將第一半導體結構之至少 一個金屬特徵(包括金屬之一部分)直接接合至第二半導體 結構之至少一個金屬特徵以形成經接合的金屬結構該經 接合的金屬結構包含第一半導體結構之至少一個金屬特徵 及第二半導體結構之至少一個金屬特徵。可藉由使經接合 的金屬結構經受後接合熱預算來將該經接合的金屬結構退 火’且可使第一半導體結構之至少一個金屬特徵之金屬擴 展至先前由金屬中之空隙佔據的空間中。 本揭示内容之其他實施例包含根據本文所述方法製得之 經接合的半導體結構及根據本文所述方法形成之中間結 162378.doc 201241937 構。 舉例而言’在其他實施例中’本揭示内容包含經接合的 半導體結構’纟包括第-半導體結構(具有至少一個金屬 特徵)及第二半導體結構(包括至少一個直接接合至第一半 導體結構之至少一個金屬特徵之金屬特徵)。第一半導體 結構之至少一個金屬特徵具有至少一個界定該第一半導體 結構之至少一個金屬特徵内之空隙的内表面。 在其他實施例中,本揭示内容包含在製造經接合的半導 體結構期間形成之中間結構。中間結構包括第—半導體結 構(具有至少一個金屬特徵及接合表面)及第二半導體結構 (包括至少一個具有接合表面之金屬特徵,該接合表面直 接鄰接第一半導體結構之至少一個金屬特徵之接合表 面)》舉例而言且並不加以限制,金屬可包括金屬或金屬 合金,例如銅、鋁、鎳、鎢、鈦或其合金或混合物。在一 些實施例中,金屬可經選擇以包括銅或銅合金。 【實施方式】 可藉由參照本揭示内容之實例性實施例之下列詳細說明 來更全面地理解本揭示内容之實施例,該等實施例係以附 圖形式繪示。 本文令所呈現之闡釋並非意欲作為任一特定材料、裝 置、系統或方法之實際視圖,而僅係用以闡述本揭示内容 之實施例之理想化表示。 本文中所使用之任何標題皆不應視為限制由以下申請專 利範圍及其合法等效物界定之本發明實施例之範圍。在整Beyond j > IEEE 2009 Custom Integrated Circuits Conference (CICC), pp. 141-148. The Summary of the Invention The present invention is provided to introduce a selection of concepts in a simplified form, which are further described in the following detailed description of the exemplary embodiments. The present invention is not intended to identify key features or essential features of the claimed subject matter, and is not intended to limit the scope of the claimed subject matter. In some implementations, the disclosure includes a method of directly bonding a first semiconductor structure to a second semiconductor structure. According to these methods, metal can be deposited on the first semiconductor structure. A portion of the metal deposited on the first semiconductor structure can be removed, and the remaining portion of the metal deposited on the first semiconductor structure can be subjected to a first thermal budget to anneal the remaining portion of the metal deposited on the first semiconductor structure . At least one metal feature of the first semiconductor structure (including the remaining portion of the metal deposited on the first semiconductor structure) may be directly bonded to at least one metal feature of the second semiconductor structure to form a bonded metal structure 'the bonded The metal structure includes at least one metal feature of the first semiconductor structure and at least one metal feature of the second semiconductor structure. The joined metal structure can be subjected to a second thermal budget to anneal the bonded metal structure. The second thermal budget experienced by the bonded metal structure can be less than the first thermal budget. In other embodiments of the method of directly bonding the first semiconductor structure to the second semiconductor structure, a metal can be deposited over the first semiconductor structure and then a portion of the metal deposited on the first semiconductor structure can be removed. The remainder of the metal deposited on the first semiconductor structure can be subjected to a first thermal budget to anneal the remainder of the metal deposited on the first semiconductor structure. After annealing the remaining portion of the metal deposited on the first semiconductor structure, the other portion of the metal deposited on the first semiconductor structure can be removed 162378.doc 201241937 points. At least one metal trace of the first-half. conductor structure (including the remainder of the metal deposited on the first semiconductor structure) may be directly bonded to at least one metal feature of the second semiconductor structure to form a bonded metal structure, The bonded metal structure includes at least one metal feature of the first semiconductor structure and at least one metal feature of the second semiconductor structure. The joined metal structure can be subjected to a second thermal budget to anneal the joined metal structure. The second thermal budget can be less than the first thermal budget. In other embodiments of the method of directly bonding the first semiconductor structure to the second semiconductor structure, the direct bonding process can be performed at a temperature greater than or equal to about 〇〇 (e.g., room temperature). At least one metal feature of the first semiconductor structure (including the remaining portion of the metal deposited on the first semiconductor structure) can be subjected to between about 2 Å and 400. (: bonding temperature between. In other embodiments of the method of directly bonding the first semiconductor structure to the second semiconductor structure, metal may be deposited on the first semiconductor structure and at least one void may be formed in the metal. Bonding at least one metal feature of the first semiconductor structure (including a portion of the metal) directly to at least one metal feature of the second semiconductor structure to form a bonded metal structure comprising at least one metal of the first semiconductor structure a feature and at least one metal feature of the second semiconductor structure. The bonded metal structure can be annealed by subjecting the bonded metal structure to a post-bond thermal budget and the metal of at least one metal feature of the first semiconductor structure can be Extensions to spaces previously occupied by voids in the metal. Other embodiments of the present disclosure include bonded semiconductor structures made according to the methods described herein and intermediate junctions formed according to the methods described herein 162378.doc 201241937. For example, 'in other embodiments' the disclosure includes The bonded semiconductor structure '纟 includes a first-semiconductor structure (having at least one metal feature) and a second semiconductor structure (including at least one metal feature directly bonded to at least one metal feature of the first semiconductor structure). At least one of the first semiconductor structures A metal feature has at least one inner surface defining a void within at least one of the metal features of the first semiconductor structure. In other embodiments, the present disclosure includes an intermediate structure formed during fabrication of the bonded semiconductor structure. a first semiconductor structure (having at least one metal feature and bonding surface) and a second semiconductor structure (including at least one metal feature having a bonding surface directly adjoining a bonding surface of at least one metal feature of the first semiconductor structure) By way of example and not limitation, the metal may comprise a metal or metal alloy such as copper, aluminum, nickel, tungsten, titanium or alloys or mixtures thereof. In some embodiments, the metal may be selected to include copper or a copper alloy. Implementation method] can be referred to by reference The following detailed description of the exemplary embodiments of the present invention is intended to provide a more complete understanding of the embodiments of the present invention, which are illustrated in the accompanying drawings. The actual view of the device, the system, or the method is merely intended to illustrate an idealized representation of the embodiments of the present disclosure. Any of the headings used herein should not be construed as limiting the scope of the following claims and their legal equivalents. Defining the scope of embodiments of the invention.
C 162378.doc -9· 201241937 個說明書通篇中,在任一特定標題中闡述之概念通常適用 於其他部分中。 本文所用之術語「半導體結構」意指且包含在形成半導 體裝置中使用之任一結構。半導體結構包含(例如)晶粒及 晶圓(例如,載體基板及裝置基板)以及包含彼此三維地整 合至一起之兩個或更多個晶粒及/或晶圓之總成或複合結 構。半導體結構亦包含經完全製造之半導體裴置以及在製 造半導體裝置期間形成之中間結構。 本文所用之術語「經處理半導體結構」意指且包含含有 一或多個至少部分地形成之裴置結構之任一半導體結構。 經處理半導體結構係半導體結構之子組,且所有經處理半 導體結構皆係半導體結構。 本文所用之術語「經接合的半導體結構」意指且包含含 有附接至一起之兩個或更多個半導體結構之任一結構。經 接合的半導體結構係半導體結構之子組,且所有經接合的 半導體結構皆係半導體結構。另外,包含一或多個經處理 半導體結構之經接合的半導體結構亦係經處理半導體会士 構。 本文所用之術S吾「裝置結構」意指且包含經處理半導體 結構之任一部分,亦即’包含或界定將在半導體結構上或 在其中形成之半導體裝置之主動或被動組件之至少一部 分。舉例而言,裝置結構包含積體電路之主動及被動組 件’例如電晶體、轉換器、電容器、電阻器、傳導線、傳 導通孔及傳導接觸墊。 162378.doc •10- 201241937 人本文所用之術語「穿晶圓互連件」s「TWI」意指且包 3延伸穿過第一半導體結構之至少-部分之任一傳導通 孔’該傳導通孔用以跨越該第—半導體結構與第二半導體 結構之間之界面提供該第一半導體結構與該第二半導體結 構之間的結構及/或電互連件。穿晶圓互連件亦在業内提 ,為其他術語,例如「穿料孔」、「穿基板通孔」、 「穿晶圓通扎」或該等術語之縮寫(例如「TSV」或 TWV」)。TWI通常沿大體垂直於半導體結構之大體平 坦主表面之方向(亦即,沿平行於「Z」軸之方向)延伸穿 過該半導體结構。 本文所用之術語「作用表面」在結合經處理半導體結構 使用時意指且包含該經處理半導體結構之經暴露主表面, 該經暴露主表面已經處理或將經處理以在該經處理半導體 結構之該經暴露主表面中及/或在其上形成一或多個裝置 結構。 本文所用之術語「背表面」在結合經處理半導體結構使 用時意指且包含該經處理半導體結構之經暴露主表面,該 經暴露主表面位於該經處理半導體結構之與該半導體結構 之作用表面相對之一側上。 本文所用之術語「熱預算」在結合退火程序使用時係指 為繪退火程序溫度隨貫施退火程序之時間而變化之直線或 曲線下面積。在於單一溫度下實施之退火程序(亦即,等 溫退火程序)中,退火程序之熱預算僅僅為實施退火程序 之溫度與實施退火程序之時間長度的乘積。C 162378.doc -9· 201241937 Throughout the specification, the concepts stated in any particular heading generally apply to other parts. The term "semiconductor structure" as used herein means and includes any structure used in forming a semiconductor device. The semiconductor structure includes, for example, dies and wafers (e.g., carrier substrate and device substrate) and an assembly or composite structure comprising two or more dies and/or wafers that are three-dimensionally integrated together. The semiconductor structure also includes a fully fabricated semiconductor device and an intermediate structure formed during fabrication of the semiconductor device. The term "processed semiconductor structure" as used herein means and includes any semiconductor structure comprising one or more at least partially formed structures. The semiconductor structure is a subset of semiconductor structures, and all of the processed semiconductor structures are semiconductor structures. The term "bonded semiconductor structure" as used herein means and includes any structure comprising two or more semiconductor structures attached together. The bonded semiconductor structures are a subset of the semiconductor structures, and all of the bonded semiconductor structures are semiconductor structures. In addition, bonded semiconductor structures comprising one or more processed semiconductor structures are also processed semiconductors. As used herein, "device structure" means and encompasses any portion of a processed semiconductor structure, i.e., 'includes or defines at least a portion of an active or passive component of a semiconductor device to be formed on or in a semiconductor structure. For example, the device structure includes active and passive components of integrated circuits such as transistors, converters, capacitors, resistors, conductive lines, vias, and conductive contact pads. 162378.doc •10-201241937 The term "through-wafer interconnect" s "TWI" as used herein means that the package 3 extends through at least a portion of the conductive via of the first semiconductor structure. A hole is provided to provide a structure and/or electrical interconnection between the first semiconductor structure and the second semiconductor structure across an interface between the first semiconductor structure and the second semiconductor structure. Through-wafer interconnects are also mentioned in the industry for other terms such as "through holes", "through substrate vias", "through wafer vias" or abbreviations of such terms (eg "TSV" or TWV" ). The TWI typically extends through the semiconductor structure in a direction generally perpendicular to the generally planar major surface of the semiconductor structure (i.e., in a direction parallel to the "Z" axis). The term "active surface" as used herein, when used in connection with a treated semiconductor structure, means and includes the exposed major surface of the processed semiconductor structure that has been processed or will be processed to be processed in the processed semiconductor structure. One or more device structures are formed in and/or on the exposed major surface. The term "back surface" as used herein, when used in connection with a treated semiconductor structure, means and includes the exposed major surface of the processed semiconductor structure, the exposed major surface being located on the active surface of the processed semiconductor structure and the semiconductor structure. On one side of the opposite side. As used herein, the term "thermal budget" as used in connection with an annealing procedure refers to the area under the line or curve that varies as the temperature of the annealing process varies with the time of the annealing process. In an annealing procedure (i.e., an isothermal annealing procedure) performed at a single temperature, the thermal budget of the annealing process is simply the product of the temperature at which the annealing process is performed and the length of time during which the annealing process is performed.
S 162378.doc 201241937 在一些貫施例中,本揭示内容包括將第一半導體結構直 接接合至第二半導體結構以形成經接合的半導體結構之改 良方法。特定而言,本揭示内容之實施例可包括在第—半 導體結構之金屬特徵與第二半導體結構之金屬特徵之間形 成直接金屬至金屬接合的方法,從而直接金屬至金屬捿合 之強度、穩定性及/或操作壽命相對於先前已知方法有所 改良。 在一些實施例中,本揭示内容之直接金屬至金屬接合方 法可包括在約2〇t與400。〇間之溫度下實施之非熱壓縮接 合方法以補償經接合的金屬特徵的碟形凹陷。 本揭示内容之方法實施例之程序流程繪示於圖1中且 可根據此一程序流程形成之有關結構繪示於圖2A_2G中。 忒等方法涉及將第一半導體結構直接接合至第二半導體杜 構。 、’ 參照圖1,在動作10中,可將金屬沈積於第一半導體結 構上。如圖2Α中所展示,可形成第一半導體結構1〇〇。第 半導體結構100可包括經處理半導體結構,且可包含— 或夕個主動裝置特徵,例如以下中之一或多者:複數個電 曰曰體102 (其在圖中示意性示出)、複數個垂直延伸之導電 通孔104及複數個水平延伸之導電跡線1〇6。主動裝置特徵 可L括由非導電塊體材料112 (例如,未摻雜塊體半導體材 料(例如矽/鍺等)或介電材料(例如氧化物))環繞之導電材料 及/或半導體材料。舉例而言且並不加以限制,導電通孔 1〇4及導電跡線106中之一或多者可包括一或多種導電金屬 162378.doc 201241937 或金屬合金,例如,銅、鋁或其合金或混合物。 第一半導體結構100亦可包括複數個凹陷13〇,在該等凹 陷中期望形成複數個接合墊丨08 (圖2C)。為形成接合墊 108,可將金屬132沈積於第一半導體結構1〇〇之作用表面 11〇上方(例如,上面),從而金屬132至少完全填充凹陷 13〇,如圖2A中所展示。可將過量金屬132沈積於第一半導 體結構1〇〇上,從而凹陷130完全經金屬132填充,且從而 將其他金屬132佈置(例如,覆蓋)於第一半導體結構1〇〇之作 用表面no上。舉例而言且並不加以限制,金屬132可包括 金屬或金屬合金,例如銅、鋁、鎳、鎢、鈦或其合金或混 合物。在一些實施例中,可選擇金屬132包括銅或銅合 金0 可使用(例如)以下程序中之一或多者將金屬132沈積於 第一半導體結構100上:無電電鍍程序、電解電鍍程序' 濺鍍程序、化學氣相沈積(CVD)程序、物理氣相沈積 (PVD)程序及原子層沈積(ALD)程序。根據一非限制性實 例,可使用化學氣相沈積(CVD)程序沈積銅晶種層,然後 可使用電化學沈積(ECD)電鍍程序以相對較快速率將額外 銅沈積於該鋼晶種層上。 再次參照圖卜在動作14中,可自第一半導體結構去 除沈積金屬132之一部分(圖2A)以形成接合墊1〇8,該等接 合墊包括佈置於凹陷130中之沈積金屬132之剩餘部分如 圖2C中所展示。可根據動作14 (圖1}使帛(例如)飿刻程序 (例如,濕式化學蝕刻程序、乾式反應性離子蝕刻程序 s 162378.doc 201241937 等)、拋光或研磨程序或其組合(例如化學-機械拋光(CMp) 程序)去除沈積金屬132之一部分。舉例而言,可使第一半 導體結構100之作用表面110經受CMP程序以去除沈積金屬 132 (圖2A)上覆於凹陷130外側之塊體材料112區之部分, 從而僅保留沈積金屬132在凹陷13〇内之區域(該等區域界 定且包括接合墊108),且從而塊體材料112在橫向毗鄰凹 陷130内之沈積金屬132區域之區中之作用表面ιι〇處暴 露。因此,接合墊108中之一或多者可在第一半導體結構 100之作用表面110處暴露。 如圖2C中所展示,用於自第一半導體結構1〇〇去除過量 金屬132之程序(例如,CMP程序)可得到接合墊1〇8相對於 作用表面110處之暴露塊體材料112凹陷之暴露表面。暴露 表面可具有弓形凹入形狀,如圖2C中所展示。此現象在業 内通常稱為「碟形凹陷」。相對於具有較小暴露主表面之 接合塾108,在具有較大暴露主表面之接合塾中碟形凹 陷現象可能相對更為明顯》 再次參照圖1 ’在動作16中,可藉由使第一半導體結構 100及由此包括沈積金屬132之剩餘部分之接合墊108經受 第一熱預算來將接合墊108 (其包括沈積金屬132之剩餘部 分)退火。換言之’可使沈積金屬132中界定接合墊1〇8之 剩餘部分經受第一熱預算以將金屬132之剩餘部分退火。 舉例而言且並不加以限制’可藉由使沈積金屬13 2之剩餘 部分經受約兩小時或更短(例如,介於約三十分鐘(30分鐘) 與約一小時(1小時)之間)退火時間段之退火溫度或低於約 162378.doc • 14· 201241937 4〇〇°C之溫度來將沈積金屬132之剩餘部分退火。 在一些實施例中,如上所述,可在第一半導體結構1〇〇 之作用表面110中選擇性實施動作16之退火程序以補償由 動作14之去除程序所引起接合墊丨〇8的任一碟形凹陷。在 該等實施例中,動作16之退火程序可包括單一晶圓處理方 法’例如雷射退火程序。在雷射退火程序中,可使用雷射 來選擇性僅退火具有「碟形」凹入接合表面1〇9之接合墊 108。動作16之選擇性退火程序之另一實例係使用具有可 個別地及單獨地控制之加熱元件之熱板或加熱晶圓夾盤。 已觀察到’藉由電鐘程序(例如彼等在上文提及者)沈積 之銅膜可在沈積之後發生微結構變化.該微結構變化可包 含重結晶及’或晶粒生長。重結晶程序可使晶粒發生空間 定向變化β該微結構變化可使經沈積銅膜之電性質(例 如’電阻)及/或物理性質(硬度)發生變化。發生該等微結 構變化之速率可具有溫度依賴性,且可隨著銅膜溫度之增 加而增加β 因金屬132所經受之隨後程序之參數、以及電性能及自 金屬132最終形成之裝置結構之結構完整性可至少部分地 取決於金屬132之電性質及/或物理性質,可將在動作1〇中 沈積於第一半導體結構100上之金屬132在動作16中退火 (圖1)以誘導及/或促進在沈積金屬132中發生微結構變化, 該專微結構變化原本可在足夠時間及室溫下、或在隨後處 理中將沈積金屬132暴露於高溫後發生於沈積金屬132中。 如下所述,在使第一半導體結構100經受隨後處理之前,S 162378.doc 201241937 In some embodiments, the present disclosure includes an improved method of directly bonding a first semiconductor structure to a second semiconductor structure to form a bonded semiconductor structure. In particular, embodiments of the present disclosure can include a method of forming a direct metal-to-metal bond between a metal feature of a first semiconductor structure and a metal feature of a second semiconductor structure such that direct metal to metal bond strength and stability The sexual and/or operational lifetime is improved over previously known methods. In some embodiments, the direct metal to metal joining methods of the present disclosure can be included at about 2 Torr and 400. A non-thermal compression bonding method implemented at the temperature of the day to compensate for the dishing of the joined metal features. The program flow of the method embodiment of the present disclosure is shown in FIG. 1 and the related structure formed according to this program flow is shown in FIG. 2A-2G. The method involves bonding the first semiconductor structure directly to the second semiconductor structure. Referring to Figure 1, in act 10, metal can be deposited on the first semiconductor structure. As shown in FIG. 2A, a first semiconductor structure 1A can be formed. The first semiconductor structure 100 can include a processed semiconductor structure, and can include - or an active device feature, such as one or more of the following: a plurality of electrical bodies 102 (shown schematically in the figures), plural A vertically extending conductive via 104 and a plurality of horizontally extending conductive traces 1〇6. The active device features may include a conductive material and/or a semiconductor material surrounded by a non-conductive bulk material 112 (e.g., an undoped bulk semiconductor material (e.g., ruthenium/iridium) or a dielectric material (e.g., oxide). By way of example and not limitation, one or more of the conductive vias 〇4 and the conductive traces 106 may include one or more conductive metals 162378.doc 201241937 or a metal alloy such as copper, aluminum or alloys thereof or mixture. The first semiconductor structure 100 can also include a plurality of recesses 13 in which it is desired to form a plurality of bond pads 08 (Fig. 2C). To form bond pads 108, metal 132 may be deposited over (e.g., above) the active surface 11'' of the first semiconductor structure 1'', such that metal 132 at least completely fills the recesses 13, as shown in Figure 2A. Excess metal 132 may be deposited on the first semiconductor structure 1 , such that the recess 130 is completely filled with the metal 132 and thereby the other metal 132 is disposed (eg, covered) on the active surface no of the first semiconductor structure 1 . By way of example and not limitation, metal 132 may comprise a metal or metal alloy such as copper, aluminum, nickel, tungsten, titanium, or alloys or mixtures thereof. In some embodiments, the selectable metal 132 comprises copper or a copper alloy. 0 The metal 132 can be deposited on the first semiconductor structure 100 using, for example, one or more of the following procedures: electroless plating process, electrolytic plating process Plating procedures, chemical vapor deposition (CVD) procedures, physical vapor deposition (PVD) procedures, and atomic layer deposition (ALD) procedures. According to one non-limiting example, a copper seed layer can be deposited using a chemical vapor deposition (CVD) process, and then additional copper can be deposited on the steel seed layer at a relatively faster rate using an electrochemical deposition (ECD) plating process. . Referring again to FIG. 4, a portion of the deposition metal 132 (FIG. 2A) may be removed from the first semiconductor structure to form bond pads 1〇8 that include the remainder of the deposition metal 132 disposed in the recess 130. As shown in Figure 2C. According to act 14 (Fig. 1}, for example, a etch process (for example, a wet chemical etch process, a dry reactive ion etch process s 162378.doc 201241937, etc.), a polishing or grinding process, or a combination thereof (eg, chemistry - Mechanical polishing (CMp) process) removes a portion of the deposited metal 132. For example, the active surface 110 of the first semiconductor structure 100 can be subjected to a CMP process to remove the bulk of the deposited metal 132 (FIG. 2A) overlying the recess 130. Portions of the region of material 112 such that only regions of the deposited metal 132 within the recess 13〇 are retained (the regions define and include the bond pads 108), and thus the bulk material 112 is laterally adjacent to the region of the deposited metal 132 within the recess 130. The surface of the active surface is exposed. Thus, one or more of the bond pads 108 can be exposed at the active surface 110 of the first semiconductor structure 100. As shown in Figure 2C, for use from the first semiconductor structure 1 The process of removing excess metal 132 (eg, a CMP process) results in an exposed surface of bond pad 1 8 that is recessed relative to exposed bulk material 112 at active surface 110. The exposed surface can have The arcuate concave shape, as shown in Figure 2C. This phenomenon is commonly referred to in the art as a "dish-shaped depression." In contrast to a joint 108 having a smaller exposed major surface, in a joint having a larger exposed major surface The dishing phenomenon may be relatively more pronounced. Referring again to Figure 1 'in act 16, the first semiconductor structure 100 and thus the bond pads 108 including the remainder of the deposited metal 132 may be subjected to a first thermal budget. The bond pad 108 (which includes the remainder of the deposition metal 132) is annealed. In other words, the remainder of the bond metal 132 defining the bond pads 1 8 can be subjected to a first thermal budget to anneal the remainder of the metal 132. Without limitation, the annealing period can be achieved by subjecting the remainder of the deposited metal 13 2 to about two hours or less (eg, between about thirty minutes (30 minutes) and about one hour (1 hour)) The annealing temperature is less than about 162378.doc • 14·201241937 4°°C to anneal the remainder of the deposited metal 132. In some embodiments, as described above, the first semiconductor junction can be The annealing process of action 16 is selectively performed on the surface 110 to compensate for any dishing of the bond pads 8 caused by the removal process of action 14. In these embodiments, the annealing process of action 16 A single wafer processing method, such as a laser annealing process, may be included. In a laser annealing process, a laser may be used to selectively anneal only bond pads 108 having "disc shaped" concave bonding surfaces 1 〇 9. Action 16 Another example of a selective annealing procedure is to use a hot plate or heated wafer chuck with individually and individually controllable heating elements. It has been observed that 'by electric clock procedures (eg, those mentioned above) The deposited copper film may undergo a microstructure change after deposition. The microstructure change may include recrystallization and 'or grain growth. The recrystallization procedure can cause spatial orientation changes in the grains. This microstructure change can change the electrical properties (e.g., 'resistance) and/or physical properties (hardness) of the deposited copper film. The rate at which such microstructure changes occur can be temperature dependent and can increase as the temperature of the copper film increases. β The parameters of the subsequent process experienced by the metal 132, as well as the electrical properties and the device structure ultimately formed from the metal 132. The structural integrity may depend, at least in part, on the electrical and/or physical properties of the metal 132, and the metal 132 deposited on the first semiconductor structure 100 in act 1 can be annealed in act 16 (FIG. 1) to induce / or promoting a microstructural change in the deposited metal 132 that would otherwise occur in the deposited metal 132 after exposing the deposited metal 132 to a high temperature for sufficient time and at room temperature or during subsequent processing. As described below, before subjecting the first semiconductor structure 100 to subsequent processing,
C 162378.doc -15· 201241937 經由動作16之退火程序’可誘導沈積金屬132中之微結構 變化以穩定沈積金屬132之微結構(及由此沈積金屬132之 電性質及/或物理性質)。 因此,在一些實施例中,動作16之退火程序可包括使金 屬132内之至少一些晶粒發生重結晶。金屬132内晶粒之重 結晶可使得金屬132内之晶粒定向發生變化。因此,根據 一些實施例,如下所述,可選擇(例如,優化)動作16之退 火程序中熱循環之各種參數(例如,退火溫度之斜升、退 火溫度之斜降、退火時間段等)以使得在接合程序之前在 金屬132中形成穩定微結構。 另外,金屬132内晶粒之重結晶可進一步使得金屬132之 電性質及金屬132之物理性質中之至少一者有所改變。舉 例而言,動作16之退火程序可使得金屬132電阻在第一半 導體結構100之作用表面11〇之至少一個橫向方向(例如圖 2D之透視圖之垂直方向)上有所降低。根據另一實例,動 作16之退火程序可使得金屬132之硬度有所降低。 如圖2D巾所展示,在使沈積金屬132之剩餘部分經受第 -熱預算以將金屬132退火並誘導其中之微結構變化時, 可,得沈積金屬132發生體積膨脹(在局部藉由(例如)晶粒 ί定向及/或晶粒生長’或在整體上藉由(例如)相變化)並 改變接合塾Η)8中界定接合塾刚之接合表面⑽之暴露表 面之形貌。 參照圖1,在動作18中,可使接合塾1〇8之接合表面1〇9 準備用於接u。動作18可包括(例如)修補⑽?程序(t_h_ 162378.doc 201241937 up CMP process)、化學處理程序及清洗程序中之一或多 者。舉例而言且並不加以限制,可藉由首先將第一半導體 結構100浸泡於去離子水中來清洗接合墊1 〇8之接合表面 109。此外,可利用氫氧化銨(NH4〇H)作為CMp後清洗方 法。為防止過度銅粗糙化,可將氫氧化氨(ΝΗ4〇Η)清洗劑 與銅腐蝕抑制劑(例如,苯并三唑(ΒΤΑ))組合使用或使用 其不含溶解氨(ΝΑ)氣體之形式(例如,四甲基氫氧化銨 (ΤΜΑΗ))。 繼續參照圖1,在動作20中,接合墊1〇8可直接接合至第 一半導體結構之金屬特徵。下文參照圖2Ε至2G來閣述可 用於將接合塾1〇8直接接合至第二半導體結構之金屬特徵 之直接接合程序之實例。 參照圖2E,可將第一半導體結構1〇〇與第二半導體結構 200對準從而將第一半導體結構丨〇〇之接合墊1〇8與第二半 導體結構200之導電金屬接合墊2〇8對準。如圖2e中所展 不,第一半導體結構2〇〇亦可包括經處理半導體結構,且 可包含其他主動裝置結構’例如,垂直延伸之導電通孔 204及橫向延伸之導電跡線2〇6。儘管並未展示於圖中,但 第二半導體結構200亦可包括電晶體。 接合墊108之暴露表面可界定接合墊1〇8之一或多個接合 表面 且接&墊208之外部暴露表面可界定第二半導體 結構200之接合墊208之接合表面22〇。 參照圖2F,在將第一半導體結構1〇〇與第二半導體結構 200對準從而第一半導體結構1〇〇之接合墊1〇8與第二半導 162378.doc •17- 201241937 體結構200之導電金屬接合墊208對準之後,第一半導體結 構100可鄰接第二半導體結構2〇〇 ,從而第一半導體結構 1〇〇之接合墊108之接合表面12〇直接鄰接第二半導體結構 200之接合墊208之接合表面220且其間沒有任何中間接合 材料(例如,黏著劑)。 參照圖2G ’然後可將第一半導體結構1 〇〇之接合墊1 〇8之 接合表面120直接接合至第二半導體結構2〇〇之接合墊2〇8 之接合表面220 (圖2F)以形成經接合的半導體結構3〇〇。接 合程序使得形成包含已接合至一起之接合塾1〇8及接合塾 208之經接合的金屬結構。在直接金屬至金屬(例如,銅至 銅)非熱壓縮接合程序中,可將第二半導體結構2〇〇之接合 墊208之接合表面220直接接合至第一半導體結構1〇〇之接 合墊108之接合表面120。在一些實施例中,非熱壓縮接合 程序可包括在以下環境中實施之超低溫直接接合程序:在 約400攝氏度(4〇〇。〇或更低之一或多個溫度下之環境中, 或甚至在約200攝氏度(200。〇或更低之一或多個溫度下之 環境中。在一些實施例中,非熱壓縮接合程序可在以下溫 度下實施:在介於約20攝氏度(2(rc )與約4〇〇攝氏度 (4〇〇°C)之間之-或多個溫度下’或甚至在介於約攝氏 度(200°C )與約350攝氏度(35(TC )之間之一或多個溫度下。 在其他實施例中,可在約室溫下之環境中(亦即,並未施 加任何除由周圍環境所提供熱量外之熱量)實施非熱壓縮 接合程序。 在將第一半導體結構1〇〇接合至第二半導體結構2〇〇之 162378.doc -18 - 201241937 前’可處理第一半導體結構100及第二半導體結構200以去 除表面雜質及不期望表面化合物,且可實施平坦化以增加 接合墊108之接合表面120與接合墊208之接合表面220之間 原子標度的緊密接觸區。可藉由以下方式來達成接合表面 120與接合表面220之間之緊密接觸區:藉由將接合表面 120及接合表面220拋光以將其表面粗糙度減小至接近原子 標度之值,藉由在接合表面120與接合表面220之間施加壓 力以得到塑膠變形’或藉由將接合表面12〇、220拋光及在 第一半導體結構100與第二半導體結構200之間施加壓力以 獲得該塑膠變形二者。 在一些實施例中,可將第一半導體結構1〇〇直接接合至 第二半導體結構200且並不在其間之接合界面處之接合表 面120、220之間施加壓力,但可在一些超低溫直接接合方 法中在接合界面處之接合表面12〇、220之間施加壓力,以 在接合界面處達成適宜接合強度。換言之,在本揭示内容 之一些實施例中,用於將第一半導體結構1〇〇之接合墊1〇8 接合至第二半導體結構2〇〇之接合墊208之直接接合方法可 包括表面輔助接合(SAB)方法。 在一些實施例中’接合墊108及接合墊2〇8之尺寸及形狀 中之至少一者可不同。更特定而言’接合墊1〇8在平行於 接合墊108與接合墊208之間之經接合界面之平面中可具有 第一橫載面面積,且接合墊2〇8在平行於接合墊1〇8與接合 墊208之間之經接合界面之平面中可具有第二橫截面面 積’該第二橫截面面積與接合墊1〇8之第一橫截面面積不 c 162378.doc -19- 201241937 同。在該等實施例卜接合墊108之接合表面i2〇可具有第 一尺寸,且接合墊208之接合表面22〇可具有與第一尺寸不 同之第二尺寸。接合塾刚在平行於接合塾⑽與接合勢 208之間之經接合界面之平面中可具有第—橫截面形狀, 且接合塾2GS在平行於接合墊⑽與接合墊扇之間之經接 合界面之平面中可具有第二橫截面形狀,該第二橫截面形 狀與接合墊108之第一橫截面形狀不同。在該等實施例 中’接合墊108之接合表面12〇可具有第一形狀且接合墊 208之接合表面22〇可具有與第一形狀不同之第二形狀。在 接合墊108之接合表面12〇與接合墊2〇8之接合表面具有 不同形狀之實施财,#可具有相同或不同尺寸(亦即, 相同或不同面積)。 在其他實施例中,接合墊1〇8之接合表面12〇與接合墊 2〇8之接合表面22G可具有至少實質上相同之尺寸及形狀。 在該等實施例中’在一些情況下’接合墊1〇8與接合墊細 可有意或無意地彼此橫向未對準。 在接合墊具有不同尺寸及/或未對準之實施例中,應注 意銅/氧化物表面。可在後接合退火之前接合銅/氧化物表 面。此外,氧化物可經一材料(例如電介質)覆蓋/包覆以確 保可抑制銅之熱機械行為之適當鈍化,此對於低介電常數 (低K)氧化物尤其可為一項顧慮。減小銅熱機械行為之方 法之非限制性實例係確保在與其他銅墊不重疊(亦即,墊 未對準)之區中將銅接合至介電表面(例如,具有矽氮化物 SixNy)。在該等實施例中,可在退火之前接合鋼/矽氮化物 162378.doc •20- 201241937 表面以獲得矽氮化物鈍化,從而抑制熱機械行為。對於其 他資訊而言,例如參見「Effect of passivation on stress relaxation in electroplated copper films」 Dongwen Gan及 Paul S. Ho、Yaoyu Pang及 Rui Huanga、Jihperng Leu、 Jose Maiz及Tracey Scherban,J. Mater. Res.,第 21卷,第 6期,2006 年 6 月 © 2006 Materials Research Society。 再次參照圖1,在動作22中,可藉由將經接合的半導體 結構300 (及由此經接合的金屬結構)暴露於第二熱預算來 將包括接合墊108及接合墊208之經接合的金屬結構退火。 在一些實施例中,動作22之第二熱預算可小於動作16之第 一熱預算。換言之,可使經接合的金屬結構經受小於第一 熱預算之第二熱預算以將經接合的金屬結構退火。舉例而 言且並不加以限制,可藉由以下方式將經接合的金屬結構 退火:使接合墊108及接合墊208在約2小時或更短(例如, 介於約三十分鐘(30分鐘)與約一小時(1小時)之間)之退火 時間段内經受低於約400°C之一或多個退火溫度。 在一些實施例中,動作22之退火程序可在室或亦實施動 作20之接合程序之其他殼體中原位實施。在該等實施例 中,動作22之退火程序可包括在室或其他殼體中使第一半 導體結構100經受連續熱循環之後續區段或部分。 如前文所述,動作16之退火程序之第一熱預算可大於動 作22之退火程序之第二熱預算。因熱預算隨退火時間段及 退火溫度而變化,故動作16中退火程序之第一熱預算大於 動作22中退火程序之第二熱預算之方式可包含如下:在動 162378.doc -21 - 201241937 作16之退火程序與動作22之退火程序之間改變退火溫度、 改變退火時間段或改變退火溫度及退火時間段二者。 在一些貫施例中’動作22之退火程序之一或多個退火溫 度可至少與動作16之退火程序之一或多個退火溫度實質上 相同。在該等實施例中’動作22之退火程序之退火時間段 可短於該動作16之退火程序之退火時間段。 在其他實施例中,動作22之退火程序之退火時間段可至 少與動作16之退火程序之退火時間段實質上相同。在該等 實施例中,動作22之退火程序之平均退火溫度可低於動作 16之退火程序之平均退火溫度。 在其他實施例中,動作22之退火程序之退火時間段可短 於動作16之退火程序之退火時間段,且動作22之退火程序 之平均退火溫度可低於動作16之退火程序之平均退火溫 度。 參照圖1,在一些實施例中,在根據動作2〇將第一半導 體結構100之金屬特徵直接接合至第二半導體結構2〇〇之金 屬特徵之前,可使第一半導體結構1〇〇經受兩個或更多個 單獨退火程序。換言之’在動作20之接合程序之前,可使 第一半導體結構100經受一或多個除動作16外之退火程 序。舉例而言,如圖1中所展示,在根據動作1〇將金屬132 沈積於第一半導體結構100上之後且在根據動作14去除沈 積金屬132之一部分之前,可使第一半導體結構1〇〇在動作 12中經受其他退火程序。根據第二實例,如圖1中所展 示’在第一半導體結構100與第二半導體結構2〇〇之間之接 162378.doc •22· 201241937 合接觸之前,可使第一半導體結構100在動作20中經受其 他退火程序。 圖2B繪示在根據動作1〇將金屬132沈積於第一半導體社 構100上(圖1)之後且在根據動作12使圖2A中所展示第一半 導體結構1〇〇經受退火程序(圖1)之後之第一半導體結構 100 ° 如圖2B中所展示,根據動作12使沈積金屬U2經受熱預 算以將金屬132退火可誘導其中之微結構變化’如前文結 合圖2D所論述,且可使得沈積金屬132發生體積膨脹(在局 部藉由(例如)晶粒重定向及/或晶粒生長,或在整體上藉由 (例如)相變化)並改變沈積金屬132之暴露表面134之形貌。 在一些實施例中,動作12之退火程序可在室或亦實施動 作1 〇之沈積程序之其他殼體中原位實施。在該等實施例 中’可在動作10之沈積程序之後但在自室或其他殼體取出 第一半導體結構1〇〇之前,在室或其他殼體中實施動作12 之退火程序。 根據使第一半導體結構100在動作2〇之接合程序之前經 受兩個或更多個單獨退火程序之一些實施例,如上所述, 動作16之第一熱預算可大於動作22之第二熱預算。然而, 根據其他該等實施例,動作16之第一熱預算可小於動作22 之第二熱預算,但動作12及16之退火程序之組合熱預算可 大於動作22之第二熱預算。 在其他實施例中,根據本文參照圖1及2A至2(3結合接合 墊108之形成及退火所述之方法,可形成第二半導體結構 162378.doc -23- 201241937 200之一或多個主動特徵(例如接合墊2〇8)並退火。 藉由如上所述使前接合退火熱預算等於或大於後接合退 火熱預算,擬在直接接合程序中接合之金屬特徵之膨脹 (由其微結構之成熟引起)可至少在直接接合程序之前實質 上完成’此可改良半導體結構之間之接合。 根據本揭示内容之其他實施例,在根據圖i之動作2〇將 第一半導體結構100之至少一個金屬特徵直接接合至第二 半導體結構之至少一個金屬特徵之前,包括與接合擬金屬 特徵不同之材料之帽蓋層可形成或以其他方式提供於第一 半導體結構1〇〇之至少一個金屬特徵的表面上如下文參 照圖3 A至3 F進一步詳細所述。 根據一非限制性實例,在根據圖1之動作10、動作14及 動作16 (及視需要動作12)形成接合墊1〇8,後,可將氧化物 材料114佈置於第一半導體結構1〇〇•之接合墊1〇8,之暴露主 表面處(例如’其上或其中),如圖3Α中所展示。舉例而言 且並不加以限制,接合墊1〇8,之金屬132可包括銅或銅合 金,且氧化物材料114可包括銅氧化物(例如,。氧 化物材料114可源自接合墊1〇8,之暴露表面之有意或無音氧 化,且可源自一或多種先前實施之程序,例如在圖丨之動 作14期間實施之化學-機械拋光(CMp)方法。氧化物材料 114亦可簡單地源自接合塾丨〇 8,暴露於包括氧之氣體(例 如,空氣)。 參照圖3B ’可自接合墊108,去除氧化物材料114。舉例 而言且並不加以限制,可使用濕式化學蝕刻程序或乾式電 162378.doc • 24· 201241937 漿餘刻程序自接合塾1G8,去除氧化物材料η#。在去除可存 在於接σ墊108之表面處之任—氧化物材料ιι4之後,包括 與金屬132不同之材料之帽蓋層U6可形成於接合墊ι〇8,之 ,露主表面處(例如,其上或其中),如圖3C中所展示。帽 蓋層116可包括具有如下組成之材料:其經選擇以阻止或 防止可發生於在動作20之接合程序期間(圖υ形成之接合界 面處之不期望原子擴散及/或熱機械現象。在一些實施例 中’帽蓋層m可包括矽。舉例而言,帽蓋層116可包括金 屬矽化物。根據一非限制性實例,在接合墊1〇8,包括鋼或 鋼合金之實施例中,帽蓋層116可包括銅矽化物(例如, CuSix)。可藉由(例如)以下方式在包括銅或銅合金之接合 墊108’之表面處形成銅矽化物:將接合墊1〇8,之暴露表面 115 (圖3B)暴露於包括SiH4之氣體中。在其他實施例中, 帽蓋層116可包括可藉由將銅矽化物暴露於含有氮之氣體 或電漿(例如,包括ΝΑ之氣體或電漿)中形成之銅矽氮化 物(CuSiN) ’然而,此可有助於增加接觸電阻。在其他實 施例中’帽蓋層116可包括金屬或金屬合金,例如包含 始、鎢及磷原子之金屬合金(CoWP)。位於〜頂部之選擇 性及無電沈積之金屬帽(CoWP)可進一步減小界面擴散。 改良界面擴散之另一方法可為使用通常引入CU晶種層中之 雜質(例如Al、Ag或Μη)來摻雜Cu。在退火之後,雜質在 晶粒邊界及界面(包含臨界接合界面)處分離。雜質在界面 處之存在減小了 Cu擴散但可增加Cu電阻率。 在一些實施例中’所形成之帽蓋層116可具有約1〇奈米C 162378.doc -15· 201241937 The microstructure change in the deposited metal 132 can be induced via the annealing procedure of action 16 to stabilize the microstructure of the deposited metal 132 (and thus the electrical and/or physical properties of the deposited metal 132). Thus, in some embodiments, the annealing process of act 16 can include recrystallizing at least some of the grains within the metal 132. Recrystallization of the grains within the metal 132 can cause changes in grain orientation within the metal 132. Thus, in accordance with some embodiments, various parameters of the thermal cycling in the annealing process of action 16 (eg, ramping of the annealing temperature, ramping of the annealing temperature, annealing time period, etc.) may be selected (eg, optimized) as described below. A stable microstructure is formed in the metal 132 prior to the bonding process. Additionally, recrystallization of the grains within the metal 132 may further alter at least one of the electrical properties of the metal 132 and the physical properties of the metal 132. For example, the annealing process of act 16 can cause the metal 132 resistance to decrease in at least one of the lateral directions of the active surface 11 of the first semiconductor structure 100 (e.g., the vertical direction of the perspective of Figure 2D). According to another example, the annealing process of action 16 can result in a decrease in the hardness of metal 132. As shown in FIG. 2D, when the remaining portion of the deposited metal 132 is subjected to a first thermal budget to anneal the metal 132 and induce a change in microstructure therein, the deposited metal 132 may be volume expanded (eg, by local (eg, The grain ί orientation and/or grain growth 'or by, for example, a phase change as a whole, and alters the morphology of the exposed surface of the joint surface (10) that defines the joint. Referring to Fig. 1, in act 18, the joint surface 1〇9 of the joint 塾1〇8 can be prepared for engagement u. Act 18 can include, for example, patching (10)? One or more of the program (t_h_ 162378.doc 201241937 up CMP process), chemical processing procedures, and cleaning procedures. By way of example and not limitation, the bonding surface 109 of the bonding pads 1 〇 8 can be cleaned by first immersing the first semiconductor structure 100 in deionized water. Further, ammonium hydroxide (NH 4 〇 H) can be used as a post-CMp cleaning method. In order to prevent excessive copper roughening, an ammonia hydroxide (ΝΗ4〇Η) cleaning agent may be used in combination with a copper corrosion inhibitor (for example, benzotriazole (ΒΤΑ)) or in the form of a gas containing no dissolved ammonia (ΝΑ) gas. (for example, tetramethylammonium hydroxide (ΤΜΑΗ)). With continued reference to Figure 1, in act 20, bond pads 1 〇 8 can be bonded directly to the metal features of the first semiconductor structure. An example of a direct bonding procedure that can be used to bond bond 塾1〇8 directly to a metal feature of a second semiconductor structure is described below with reference to Figures 2A through 2G. Referring to FIG. 2E, the first semiconductor structure 1A can be aligned with the second semiconductor structure 200 to bond the bonding pads 1〇8 of the first semiconductor structure and the conductive metal bonding pads 2〇8 of the second semiconductor structure 200. alignment. As shown in FIG. 2e, the first semiconductor structure 2A may also include a processed semiconductor structure, and may include other active device structures 'eg, vertically extending conductive vias 204 and laterally extending conductive traces 2〇6 . Although not shown in the figures, the second semiconductor structure 200 can also include a transistor. The exposed surface of the bond pad 108 can define one or more bond surfaces of the bond pads 1 〇 8 and the outer exposed surface of the pads 208 can define the bond surface 22 接合 of the bond pads 208 of the second semiconductor structure 200. Referring to FIG. 2F, the first semiconductor structure 1 is aligned with the second semiconductor structure 200 such that the first semiconductor structure 1 is bonded to the pad 1 〇 8 and the second half 162 378. doc • 17- 201241937 body structure 200 After the conductive metal bond pads 208 are aligned, the first semiconductor structure 100 can abut the second semiconductor structure 2 〇〇 such that the bonding surface 12 接合 of the bond pads 108 of the first semiconductor structure 1 〇 directly adjoins the second semiconductor structure 200 The bonding surface 220 of the bond pad 208 is free of any intermediate bonding material (eg, an adhesive) therebetween. Referring to FIG. 2G', the bonding surface 120 of the bonding pad 1 〇 8 of the first semiconductor structure 1 can then be directly bonded to the bonding surface 220 (FIG. 2F) of the bonding pad 2 〇 8 of the second semiconductor structure 2 to form The bonded semiconductor structure 3〇〇. The joining procedure results in the formation of a joined metal structure comprising joining jaws 8 8 and joining jaws 208 that have been joined together. In a direct metal to metal (eg, copper to copper) non-thermal compression bonding process, the bonding surface 220 of the bonding pad 208 of the second semiconductor structure 2 can be directly bonded to the bonding pad 108 of the first semiconductor structure 1 The joint surface 120. In some embodiments, the non-thermal compression bonding procedure can include an ultra-low temperature direct bonding procedure implemented in an environment of about 400 degrees Celsius (4 Torr, one or more temperatures, or even In an environment at about one or more temperatures of about 200 degrees Celsius (200 Torr or lower. In some embodiments, the non-thermal compression bonding procedure can be performed at a temperature of between about 20 degrees Celsius (2 (rc) ) or between about 4 ° C (4 ° C) - or at multiple temperatures ' or even between about Celsius (200 ° C) and about 350 ° C (35 (TC) or In a plurality of temperatures, in other embodiments, the non-thermal compression bonding process can be performed in an environment at about room temperature (i.e., without applying any heat other than the heat provided by the surrounding environment). The semiconductor structure is bonded to the second semiconductor structure 2 162378.doc -18 - 201241937 before the first semiconductor structure 100 and the second semiconductor structure 200 can be processed to remove surface impurities and undesired surface compounds, and can be implemented Flattening to increase bond pads 108 An intimate contact area between the bonding surface 120 and the bonding surface 220 of the bonding pad 208. The intimate contact area between the bonding surface 120 and the bonding surface 220 can be achieved by: bonding the surface 120 and bonding The surface 220 is polished to reduce its surface roughness to a value close to the atomic scale, by applying pressure between the bonding surface 120 and the bonding surface 220 to obtain plastic deformation' or by polishing the bonding surfaces 12, 220 and Pressure is applied between the first semiconductor structure 100 and the second semiconductor structure 200 to obtain both of the plastic deformations. In some embodiments, the first semiconductor structure 1 可 can be directly bonded to the second semiconductor structure 200 and not Pressure is applied between the joint surfaces 120, 220 at the joint interface therebetween, but pressure may be applied between the joint surfaces 12, 220 at the joint interface in some ultra-low temperature direct bonding methods to achieve a suitable joint strength at the joint interface In other words, in some embodiments of the present disclosure, the bonding pads 1 〇 8 of the first semiconductor structure 1 接合 are bonded to the second semiconductor The direct bonding method of the bonding pads 208 of the structure may include a surface assisted bonding (SAB) method. In some embodiments, at least one of the size and shape of the bonding pads 108 and the bonding pads 2〇8 may be different. In particular, the bonding pad 1 8 may have a first cross-sectional area in a plane parallel to the bonded interface between the bonding pad 108 and the bonding pad 208, and the bonding pads 2〇8 are parallel to the bonding pads 1〇 8 may have a second cross-sectional area in the plane of the joint interface with the bond pad 208', the second cross-sectional area and the first cross-sectional area of the bond pad 1〇8 are not c 162378.doc -19- 201241937 . The engagement surfaces i2 of the bond pads 108 may have a first dimension and the engagement surfaces 22 of the bond pads 208 may have a second dimension that is different from the first dimension. The joint jaws may have a first cross-sectional shape in a plane parallel to the joint interface between the joint jaws (10) and the joint potential 208, and the joint jaws 2GS are parallel to the joint interface between the bond pads (10) and the bond pad fans. There may be a second cross-sectional shape in the plane that is different from the first cross-sectional shape of the bond pad 108. In such embodiments, the engagement surface 12 of the bond pad 108 can have a first shape and the engagement surface 22 of the bond pad 208 can have a second shape that is different than the first shape. In the case where the joint surface 12 of the bonding pad 108 and the bonding surface of the bonding pad 2〇8 have different shapes, # may have the same or different sizes (i.e., the same or different areas). In other embodiments, the engagement surface 12A of the bond pads 1A8 and the engagement surface 22G of the bond pads 2A8 can have at least substantially the same size and shape. In these embodiments, 'in some cases' the bond pads 1 与 8 and the bond pads may be laterally misaligned with each other, either intentionally or unintentionally. In embodiments where the bond pads are of different sizes and/or misalignments, the copper/oxide surface should be noted. The copper/oxide surface can be bonded prior to post-bond annealing. In addition, the oxide may be coated/coated with a material such as a dielectric to ensure proper passivation that inhibits the thermo-mechanical behavior of copper, which may be a particular concern for low dielectric constant (low K) oxides. A non-limiting example of a method of reducing the thermomechanical behavior of copper is to bond copper to a dielectric surface (eg, having niobium nitride SixNy) in regions that do not overlap (ie, the pads are misaligned) with other copper pads. . In such embodiments, the steel/germanium nitride 162378.doc • 20-201241937 surface may be bonded prior to annealing to obtain niobium nitride passivation to inhibit thermomechanical behavior. For other information, see, for example, "Effect of passivation on stress relaxation in electroplated copper films" Dongwen Gan and Paul S. Ho, Yaoyu Pang and Rui Huanga, Jihperng Leu, Jose Maiz and Tracey Scherban, J. Mater. Res., Volume 21, Issue 6, June 2006 © 2006 Materials Research Society. Referring again to FIG. 1, in act 22, the bonded pads 108 and bond pads 208 can be joined by exposing the bonded semiconductor structure 300 (and thus the bonded metal structure) to a second thermal budget. Metal structure annealing. In some embodiments, the second thermal budget of action 22 can be less than the first thermal budget of action 16. In other words, the joined metal structure can be subjected to a second thermal budget that is less than the first thermal budget to anneal the bonded metal structure. By way of example and not limitation, the joined metal structures can be annealed by bonding pads 108 and bond pads 208 for about 2 hours or less (eg, between about thirty minutes (30 minutes) One or more annealing temperatures of less than about 400 ° C are experienced during the annealing period of about one hour (between one hour). In some embodiments, the annealing process of act 22 can be performed in situ in the chamber or other housing that also performs the bonding procedure of action 20. In such embodiments, the annealing process of act 22 can include subjecting the first semiconductor structure 100 to a subsequent section or portion of a continuous thermal cycle in a chamber or other housing. As previously described, the first thermal budget of the annealing process of action 16 may be greater than the second thermal budget of the annealing process of action 22. Since the thermal budget varies with the annealing time period and the annealing temperature, the first thermal budget of the annealing process in action 16 is greater than the second thermal budget of the annealing process in action 22, which may include the following: 162378.doc -21 - 201241937 The annealing temperature is changed between the annealing process of 16 and the annealing process of action 22 to change the annealing temperature, change the annealing time period, or change the annealing temperature and the annealing time period. In some embodiments, one or more of the annealing procedures of the 'action 22' may be at least substantially the same as one or more of the annealing temperatures of the action 16 of the action 16. The annealing time period of the annealing process of 'action 22 in these embodiments may be shorter than the annealing time period of the annealing process of act 16. In other embodiments, the annealing period of the annealing process of act 22 can be at least substantially the same as the annealing period of the annealing process of act 16. In such embodiments, the annealing temperature of the annealing process of action 22 may be lower than the average annealing temperature of the annealing process of act 16. In other embodiments, the annealing period of the annealing process of act 22 may be shorter than the annealing time of the annealing process of act 16, and the average annealing temperature of the annealing process of act 22 may be lower than the average annealing temperature of the annealing process of act 16. . Referring to FIG. 1, in some embodiments, the first semiconductor structure 1 can be subjected to two prior to bonding the metal features of the first semiconductor structure 100 directly to the metal features of the second semiconductor structure 2 according to act 2 One or more separate annealing procedures. In other words, the first semiconductor structure 100 can be subjected to one or more annealing processes other than the action 16 prior to the bonding process of the action 20. For example, as shown in FIG. 1, after depositing metal 132 on first semiconductor structure 100 in accordance with act 1 and before removing a portion of deposited metal 132 in accordance with act 14, first semiconductor structure 1 may be Other annealing procedures are experienced in act 12. According to the second example, the first semiconductor structure 100 can be made to operate before the contact between the first semiconductor structure 100 and the second semiconductor structure 2 162 162 378.doc • 22· 201241937 as shown in FIG. 20 is subjected to other annealing procedures. 2B illustrates the first semiconductor structure 1 图 shown in FIG. 2A being subjected to an annealing process after depositing metal 132 on the first semiconductor fabric 100 according to act 1 (FIG. 1) (FIG. 1). The first semiconductor structure 100° thereafter, as shown in FIG. 2B, subjecting the deposited metal U2 to a thermal budget according to act 12 to anneal the metal 132 may induce a change in microstructure therein as discussed above in connection with FIG. 2D and may The deposited metal 132 undergoes volume expansion (either locally by, for example, grain reorientation and/or grain growth, or by, for example, phase change) and alters the morphology of the exposed surface 134 of the deposited metal 132. In some embodiments, the annealing process of action 12 can be performed in situ in the chamber or other housing that also performs the deposition procedure of the actuator. In these embodiments, the annealing process of action 12 may be performed in a chamber or other housing after the deposition process of act 10, but before the first semiconductor structure 1 is removed from the chamber or other housing. According to some embodiments in which the first semiconductor structure 100 is subjected to two or more separate annealing procedures prior to the bonding process of the action 2, as described above, the first thermal budget of the action 16 may be greater than the second thermal budget of the action 22. . However, according to other such embodiments, the first thermal budget for action 16 may be less than the second thermal budget for action 22, but the combined thermal budget for the annealing procedures of actions 12 and 16 may be greater than the second thermal budget for action 22. In other embodiments, one or more of the second semiconductor structures 162378.doc -23-201241937 200 may be formed in accordance with the methods described herein with reference to FIGS. 1 and 2A through 2 (3 in combination with the formation and annealing of bond pads 108). Features (eg, bond pads 2〇8) and annealed. By making the front bond annealing thermal budget equal to or greater than the post bond annealing thermal budget as described above, the expansion of the metal features to be bonded in the direct bonding process (by its microstructure) The maturity can be substantially completed at least prior to the direct bonding process. This can improve the bonding between the semiconductor structures. According to other embodiments of the present disclosure, at least one of the first semiconductor structures 100 is operated according to the action of FIG. A cap layer comprising a material different from the bonding pseudo metal feature may be formed or otherwise provided to at least one metal feature of the first semiconductor structure 1 before the metal feature is directly bonded to the at least one metal feature of the second semiconductor structure The surface is described in further detail below with reference to Figures 3A to 3F. According to a non-limiting example, in action 10, action 14 and in accordance with Figure 1 Forming bonding pads 1〇8 (and optionally action 12), after which the oxide material 114 can be disposed on the bonding pads 1〇8 of the first semiconductor structure 1 to expose the main surface (eg, Above or in it, as shown in FIG. 3A. By way of example and not limitation, bonding pads 1〇8, metal 132 may comprise copper or a copper alloy, and oxide material 114 may comprise copper oxide (eg, The oxide material 114 may be derived from the bonding pad 1 〇 8 with intentional or silent oxidation of the exposed surface, and may be derived from one or more previously implemented procedures, such as chemical-mechanical polishing performed during action 14 of the figure ( CMp) Method. Oxide material 114 may also be simply derived from bonded germanium 8 and exposed to a gas comprising oxygen (eg, air). Referring to Figure 3B, 'self-bonding pad 108 may be used to remove oxide material 114. For example In other words, it is not limited, and the oxide material η# can be removed by using a wet chemical etching process or a dry electric 162378.doc • 24· 201241937 slurry remnant program. The removal can be present in the sigma pad 108. The surface of the material - oxide material After ι 4, a cap layer U6 comprising a material different from the metal 132 may be formed on the bond pad 8 (eg, thereon or therein), as shown in Figure 3C. The cap layer 116 Materials may be included that are selected to prevent or prevent undesired atomic diffusion and/or thermomechanical phenomena that may occur during the bonding process of action 20 (the joint interface formed by the figure). In some embodiments The cap layer m may comprise a crucible. For example, the cap layer 116 may comprise a metal telluride. According to one non-limiting example, in embodiments of the bond pad 1 8 , including steel or steel alloy, the cap layer 116 can include a copper telluride (eg, CuSix). The copper telluride can be formed at the surface of the bonding pad 108' including copper or copper alloy by, for example, exposing the bonding pad 1〇8 to the exposed surface 115 (Fig. 3B) in a gas including SiH4. In other embodiments, the cap layer 116 can include copper beryllium nitride (CuSiN) that can be formed by exposing the copper telluride to a gas or plasma containing nitrogen (eg, a gas or plasma including helium). However, this can help increase the contact resistance. In other embodiments, the cap layer 116 may comprise a metal or metal alloy, such as a metal alloy (CoWP) comprising an initial, tungsten and phosphorus atom. Selective and electrolessly deposited metal caps (CoWP) at the top of the top further reduce interface diffusion. Another method of improving interfacial diffusion can be to dope Cu using impurities (e.g., Al, Ag, or Mn) that are typically introduced into the CU seed layer. After annealing, the impurities separate at grain boundaries and interfaces (including critical bonding interfaces). The presence of impurities at the interface reduces Cu diffusion but increases Cu resistivity. In some embodiments, the cap layer 116 formed may have about 1 nanometer.
162378.doc -25- C 201241937 (10 nm)或更小之初始平均厚度(亦即,在接合及/或其他隨 後處理之前)。 在形成帽蓋層116之後’可根據圖1之動作2〇將接合墊 108’直接接合至第二半導體結構2〇〇之金屬特徵β可如前文 參照圖2Ε至2G所述來實施接合程序。 參照圖3D ’可將第一半導體結構100’與第二半導體結構 200對準從而將第一半導體結構1〇〇’之接合塾1〇8,與第二半 導體結構200之導電金屬接合墊208對準。如圖3D中所展 示’第二半導體結構200可包含其他主動裝置結構,例 如,垂直延伸之導電通孔2〇4及橫向延伸之導電跡線2〇6。 儘管並未展示於圖中,但第二半導體結構2〇〇亦可包括電 晶體。 接合墊108’之帽蓋層116之表面可界定接合墊1〇8,之一或 多個接合表面120 ’且接合墊208之外部暴露表面可界定第 二半導體結構200之接合墊2〇8之接合表面220。 參照圖3Ε ’在將第一半導體結構1〇〇,與第二半導體結構 200對準從而第一半導體結構1〇〇,之接合墊1〇8,與第二半導 體結構200之導電金屬接合墊2〇8對準之後,第一半導體結 構100'可鄰接第二半導體結構2〇〇,從而第一半導體結構 1〇〇’之接合墊108’之接合表面120直接鄰接第二半導體結構 200之接合墊208之接合表面220。 參照圖3F,然後可將第一半導體結構100,之接合墊1〇8' 之接合表面120 (圖3Ε)直接接合至第二半導體結構200之接 合塾208之接合表面220 (圖3Ε)以形成經接合的半導體結構 162378.doc •26- 201241937 300 °舉例而έ ’在直接金屬至金屬(例如,銅至銅)非熱 塵縮接合程序中’可將第二半導體結構200之接合墊208之 接合表面220直接接合至第一半導體結構1〇〇,之接合墊1〇8, 之接合表面120«在一些實施例中,非熱壓縮接合程序可 包括在以下環境中實施之超低溫直接接合程序:在約4〇〇 攝氏度(400°C)或更低之一或多個溫度下之環境中,或甚至 在約200攝氏度(2〇〇。(〕)或更低之一或多個溫度下之環境 中。在一些實施例中,非熱壓縮接合程序可在以下溫度下 實施:在介於約20攝氏度(20。〇與約4〇〇攝氏度(4〇〇t)之 間之一或多個溫度下’或甚至在介於約2〇〇攝氏度(2〇(rc) 與』350攝氏度(350 C )之間之一或多個溫度下。在其他實 施例中,可在約室溫下之環境中(亦即’並未施加任何除 由周圍環境所提供熱量外之熱量)實施非熱壓縮接合程 序。 如圖3F中所展示,在—些實施例中,在將第—半導體結 構⑽,之接合墊清直接接合至第二半導體結構·之接合 墊208後,接合墊108,與接合塾間之界面處帽蓋層μ之 一或多種元素可擴散至接合墊1〇8,及/或接合墊2〇8中從 而帽蓋層不再以單獨相形式存在於接合墊與接合塾 208間之經接合界面處。帽蓋層116之至少一部分可保留於 接合墊1〇8’之至少一部分中,如圖3F中所展示。在接合程 序後帽蓋層116之至少一部分存在於接合墊1〇8,上可較為有 益’其原因進一步詳細論述於下文中。 在接合墊1〇8,及接合塾208在尺寸及形狀中之至少一者 162378.doc -27-162378.doc -25- C 201241937 (10 nm) or less initial average thickness (i.e., prior to bonding and/or other subsequent processing). After forming the cap layer 116, the bonding feature can be directly bonded to the metal features β of the second semiconductor structure 2 according to the action 2 of Fig. 1 as described above with reference to Figs. 2A to 2G. Referring to FIG. 3D', the first semiconductor structure 100' may be aligned with the second semiconductor structure 200 to bond the first semiconductor structure 1'' to the conductive metal bond pad 208 of the second semiconductor structure 200. quasi. As shown in Figure 3D, the second semiconductor structure 200 can include other active device structures, such as vertically extending conductive vias 2〇4 and laterally extending conductive traces 2〇6. Although not shown in the figures, the second semiconductor structure 2A may also include a transistor. The surface of the cap layer 116 of the bond pad 108' may define a bond pad 1 〇 8 , one or more bond surfaces 120 ′ and the outer exposed surface of the bond pad 208 may define a bond pad 2 〇 8 of the second semiconductor structure 200 Engagement surface 220. Referring to FIG. 3A, the first semiconductor structure 1 is aligned with the second semiconductor structure 200 such that the first semiconductor structure 1 is bonded to the bonding pad 1 〇 8 and the conductive metal bonding pad 2 of the second semiconductor structure 200 After the 〇8 is aligned, the first semiconductor structure 100' may abut the second semiconductor structure 2'', such that the bonding surface 120 of the bonding pad 108' of the first semiconductor structure 1'' directly abuts the bonding pad of the second semiconductor structure 200 Bonding surface 220 of 208. Referring to FIG. 3F, the bonding surface 120 (FIG. 3A) of the bonding pad 1 8' of the first semiconductor structure 100 may be directly bonded to the bonding surface 220 (FIG. 3A) of the bonding pad 208 of the second semiconductor structure 200 to form Bonded semiconductor structure 162378.doc • 26- 201241937 300 ° exemplified by 'in a direct metal to metal (eg, copper to copper) non-thermal dust-shrink bonding process 'the bonding pad 208 of the second semiconductor structure 200 can be The bonding surface 220 is directly bonded to the first semiconductor structure 1 〇〇, the bonding pad 1 〇 8 , the bonding surface 120 « In some embodiments, the non-thermal compression bonding process can include an ultra-low temperature direct bonding process implemented in the following environments: In an environment at one or more temperatures of about 4 degrees Celsius (400 ° C) or lower, or even at one or more temperatures of about 200 degrees Celsius (2 〇〇 ( )) or lower In some embodiments, the non-thermal compression bonding procedure can be performed at a temperature between one or more of about 20 degrees Celsius (20. Torr and about 4 〇〇 Celsius (4 〇〇t) At temperature 'or even at about 2 〇〇 Degree (1 〇 (rc) and 』 350 ° C (350 C ) at one or more temperatures. In other embodiments, it may be in an environment at about room temperature (ie, 'no application of any Non-thermal compression bonding process is performed by the heat provided by the surrounding environment. As shown in FIG. 3F, in some embodiments, the bonding pad of the first semiconductor structure (10) is directly bonded to the second semiconductor structure. After the bonding pad 208, one or more elements of the cap layer μ at the interface between the bonding pad 108 and the bonding pad can be diffused into the bonding pad 1〇8, and/or the bonding pad 2〇8 so that the cap layer is no longer Present in a separate phase at the bonded interface between the bond pad and the bond pad 208. At least a portion of the cap layer 116 can remain in at least a portion of the bond pad 1 8', as shown in Figure 3F. At least a portion of the back cap layer 116 may be present on the bond pads 1 〇 8 , which may be beneficial. The reason for this is discussed in further detail below. The bond pads 1 〇 8 and the bond pads 208 are at least one of size and shape. 162378.doc -27-
S 201241937 中有所不同及/或彼此未對準之實施例中,位於接合墊ι〇8, 中之一或多者上之帽蓋層116之至少一部分可能並不鄰接 接合墊208之任一部分,且可能並不直接接合至接合墊2〇8 之任一部分。舉例而言,帽蓋層116之該等部分可鄰接環 繞接合墊208之塊體材料212。帽蓋層116之該等部分可或 可不接合至鄰接塊體材料212,且在將接合墊1〇8,接合至接 合墊208後可能並不完全溶解至接合墊1〇8,中1在該等實施 例中,在接合程序之後在接合墊1〇8,與塊體材料212間之界 面處存在帽蓋層116之至少一部分可改良藉由鄰近接合墊 1〇8’及接合墊208所形成導電結構之可用壽命及/或改良其 性能。舉例而言,在接合墊1〇8,與塊體材料212間之界面處 存在帽蓋層116可阻止或防止在接合墊1〇8,與塊體材料212 間之界面處之質量傳遞,該質量傳遞可因(例如)電遷移而 發生。帽蓋層116之存在亦可抑制不期望熱機械現象之發 生’例如’可源自在隨後處理及/或操作期間結構可經受 之溫度波動之微結構中之不期望變化。 在其他實施例中,可如上文結合第一半導體結構丨〇〇,之 接合墊108’所述來處理第二半導體結構2〇〇之一或多個主動 特徵之暴露表面(例如接合墊2〇8之暴露表面),從而接合墊 208之接合表面220包括帽蓋層(例如帽蓋層丨16)。 在將第一半導體結構1〇〇·接合至第二半導體結構200以 形成圖3F之經接合的半導體結構3〇〇ι之後,可根據圖1之 動作22藉由將經接合的金屬結構暴露於第二熱預算來將包 括接合墊108’及接合墊2〇8之經接合的金屬結構退火,如前 162378.doc -28* 201241937 文參照圖2A至2G之實施例所述。 圖4繪示本揭示内容之方法之其他實施例之程序流程, 且圖5結合圖2A至2G使用以繪示根據圖4之程序流程來製 造經接合的半導體結構》如圖4中所展示,其中繪示之程 序流程包含根據動作14將金屬132沈積於第一半導體結構 1〇〇上,根據動作16自第一半導體結構1〇〇去除沈積金屬 13 2之一部分’及根據動作16藉由使金屬13 2之剩餘部分經 受第一熱預算來將金屬132之剩餘部分退火。圖4之程序流 程亦可包含根據動作12沈積金屬132之其他可選退火。該 等動作10、12、14及16可如前文參照圖2Α至2D所述進行 以形成圖2D巾所展示之第一半導體結構丨〇〇。 如圖2D中所展示,動作16之退火程序可使得沈積金屬 132發生體積膨脹(在局部藉由(例如)晶粒重定向及/或晶粒 生長’或在整體上藉由(例如)相變化)並改變接合墊1〇8之 暴露表面(界定接合墊1〇8之接合表面1〇9)之形貌。因此, 接合墊108之接合表面109可垂直延伸(自圖2£)之透視圖)至 超過作用表面110上環繞塊體材料112之暴露表面,及/或 可增加接合表面109之表面粗糙度。 再-人參照圖4,根據本揭示内容之一些實施例,在動作 16之退火程序之後,可根據動作17在其他去除程序中去除 接合墊108之經沈積及退火金屬132之其他部分。動作口之 去除程序可包括(例如)平坦化程序,該平坦化程序會改良 半導體結構100之作用表面110之平坦性(並降低其總體平 句表面粗糙度)’及/或降低接合墊108之接合表面109之表In embodiments where S 201241937 is different and/or misaligned with each other, at least a portion of the cap layer 116 on one or more of the bond pads 8 may not abut any portion of the bond pads 208. And may not be directly bonded to any portion of the bond pads 2〇8. For example, the portions of the cap layer 116 can abut the block material 212 that surrounds the bond pads 208. The portions of the cap layer 116 may or may not be joined to the adjacent block material 212, and may not completely dissolve to the bond pads 1〇8 after bonding the bond pads 1〇8 to the bond pads 208, where In other embodiments, at least a portion of the cap layer 116 at the interface between the bond pads 1 , 8 and the bulk material 212 after the bonding process can be modified to be formed by the adjacent bond pads 1 〇 8 ′ and bond pads 208 . The useful life of the conductive structure and / or improve its performance. For example, the presence of the cap layer 116 at the interface between the bond pads 1〇8 and the bulk material 212 can prevent or prevent mass transfer at the interface between the bond pads 1〇8 and the bulk material 212, which Mass transfer can occur due to, for example, electromigration. The presence of the cap layer 116 also inhibits the occurrence of undesirable thermomechanical phenomena, e.g., may result from undesirable changes in the microstructure that the structure can withstand during subsequent processing and/or operation. In other embodiments, the exposed surface of one or more of the active features of the second semiconductor structure 2 can be processed as described above in connection with the first semiconductor structure, bond pad 108' (eg, bond pad 2〇) The exposed surface of 8 is such that the bonding surface 220 of the bond pad 208 includes a cap layer (eg, cap layer 16). After bonding the first semiconductor structure 1 to the second semiconductor structure 200 to form the bonded semiconductor structure 3 图 of FIG. 3F, the bonded metal structure can be exposed according to the action 22 of FIG. The second thermal budget is to anneal the bonded metal structure including bond pads 108' and bond pads 2〇8 as described in the previous embodiment of Figures 162378.doc -28* 201241937. 4 is a flow chart of another embodiment of the method of the present disclosure, and FIG. 5 is used in conjunction with FIGS. 2A through 2G to illustrate the fabrication of a bonded semiconductor structure according to the program flow of FIG. 4, as shown in FIG. The program flow illustrated therein includes depositing a metal 132 on the first semiconductor structure 1 according to act 14 and removing a portion of the deposited metal 13 2 from the first semiconductor structure 1 according to act 16 and by act 16 The remainder of the metal 13 2 is subjected to a first thermal budget to anneal the remainder of the metal 132. The process flow of Figure 4 may also include other optional anneals of depositing metal 132 in accordance with act 12. The actions 10, 12, 14 and 16 can be performed as previously described with reference to Figures 2A through 2D to form the first semiconductor structure shown in Figure 2D. As shown in FIG. 2D, the annealing process of act 16 can cause volume expansion of the deposited metal 132 (either locally by, for example, grain reorientation and/or grain growth) or by, for example, phase changes as a whole. And changing the topography of the exposed surface of the bonding pad 1〇8 (defining the bonding surface 1〇9 of the bonding pad 1〇8). Accordingly, the engagement surface 109 of the bond pad 108 can extend vertically (from a perspective view of FIG. 2) to an exposed surface that surrounds the bulk material 112 on the active surface 110, and/or can increase the surface roughness of the engagement surface 109. Referring again to Figure 4, in accordance with some embodiments of the present disclosure, after the annealing process of action 16, other portions of the deposited and annealed metal 132 of bonding pad 108 may be removed in accordance with act 17 in other removal procedures. The process of removing the motion port can include, for example, a planarization process that improves the flatness of the active surface 110 of the semiconductor structure 100 (and reduces its overall flat surface roughness) and/or reduces the bonding pad 108. Table of joint surfaces 109
C 162378.doc •29- 201241937 面粗糙度。因此’圖5繪示表面粗糙度相對於圖2D有所降 低之接合墊108之接合表面109 ’且繪示與作用表面11〇處 環繞塊體材料112之暴露表面共面之接合表面。 在動作17中’可使用(例如)蝕刻程序(例如,濕式化學餘 刻程序、乾式反應性離子#刻程序等)、拋光或研磨程序 或其組合(例如化學-機械抛光(CMP)程序)去除經沈積及退 火金屬132之其他部分》舉例而言,可使第一半導體结構 100之作用表面110經受CMP程序以去除接合墊1〇8之其他 經沈積及退火金屬132。 再次參照圖4,在根據動作17去除接合墊108之經沈積及 退火金屬132之其他部分以形成如圖5中所展示之第一半導 體結構100之後’可根據動作20將第一半導體結構1 〇〇之接 合墊108直接接合至第二半導體結構2〇〇之接合墊2〇8,如 前文參照圖1及圖2Ε至2G所述。在動作20之直接接合程序 之後,包括第一半導體結構100之接合塾1〇8及第二半導體 結構200之接合墊2〇8之經接合的金屬特徵可藉由以下方式 進行退火:使該等經接合的金屬特徵經受低於第一熱預算 之第一熱預算,如前文參照圖1及圖2G所述。儘管並未展 示於圖4中,但可根據動作18 (圖1)藉由使第一半導體結構 100之作用表面110經受清洗程序來製備接合墊1〇8之接合 表面109以用於接合’如前文參照圖1所述。 在其他實施例中’可在第一半導體結構1〇〇之至少一個 金屬特徵之表面處形成或以其他方式提供帽蓋層116,然 後根據圖4之動作20將該金屬特徵直接接合至第二半導體 162378.doc • 30· 201241937 結構之至少一個金屬特徵,如前文參照圖3 A至3F所述。 圖6繪示本揭示内容之方法之其他實施例之程序流程, 且圖7A至7E繪示根據圖6之程序流程來製造經接合的半導 體結構。 參照圖6 ’在動作50中,可將金屬432沈積於第一半導體 結構上。如圖7A中所展示,可形成第一半導體結構4〇〇。 第一半導體結構400可實質上類似於前文結合圖2A所述之 第一半導體結構100,且可包括經處理半導體結構,該經 處理半導體結構包含一或多個主動裝置特徵,例如以下中 之一或多者:複數個電晶體4〇2 (其在圖中示意性示出)、 複數個垂直延伸之導電通孔4〇4及複數個水平延伸之導電 跡線406 »主動裝置特徵可包括由非導電塊體材料4丨2環繞 之導電材料及/或半導體材料。舉例而言且並不加以限 制’導電通孔404及導電跡線406中之一或多者可包括一或 多種導電金屬或金屬合金,例如,銅、鋁或其合金或混合 物。 第一半導體結構400亦可包括複數個凹陷43〇,在該等凹 陷中期望形成複數個接合墊408 (圖7C)。為形成接合墊 4〇8,可將金屬432沈積於第一半導體結構4〇〇之作用表面 410上方(例如,其上),從而金屬432至少完全填充凹陷 430,如圖7A中所展示。可將過量金屬432沈積於第一半導 體結構400上,從而凹陷430完全經金屬432填充,且從而 將其他金屬432佈置(例如,覆蓋)於第一半導體結構4〇〇之作 用表面410上。舉例而言且並不加以限制,金屬432可包括 162378.doc •31- 201241937 金屬或金屬合金,例如銅、鋁或其合金或混合物。在一此 實施例中’可選擇金屬432包括銅或銅合金。 如圖7Α中所展示’可將金屬432沈積於第—半導體結構 400上從而在凹陷43〇内之沈積金屬432部分中形成空隙 436。換言之’所形成之金屬432可包含至少一個界定凹陷 430内之沈積金屬432部分中之空隙436的内表面。可(例如) 在電沈積程序期間藉由增加線及通孔之垂直側上之金屬生 長速度來產生空隙。在該等條件下,空隙在通孔或線中自 發產生。產生該等空隙之其他方法可藉由非保形沈積擴散 障壁(或金屬晶種層)來達成。藉由增加通孔/線中障壁/晶 種層之側面厚度,可在障壁沈積程序之同時或在金屬沈積 階段之早期階段直接產生空隙。可使用(例如)以下程序中 之一或多者將金屬432沈積於第一半導體結構400上:無電 電鑛程序、電解電鍍程序、化學氣相沈積(CVD)程序及物 理氣相沈積(PVD)程序。根據一非限制性實例,可使用無 電電鍍程序沈積銅晶種層’然後可使用電解電鍍程序以相 對較快速率將額外銅沈積於該銅晶種層上。可使用(例如) 以下程序中之一或多者將金屬432沈積於第一半導體結構 400上:無電電鑛程序、電解電鐘程序、化學氣相沈積 (CVD)程序及物理氣相沈積(pvD)程序。根據一非限制性 實例’可使用無電電鍍程序沈積銅晶種層,然後可使用電 解電鍍程序以相對較快速率將額外銅沈積於該銅晶種層 上。 再次參照圖6,在動作54中,可自第一半導體結構400去 162378.doc -32· 201241937 除沈積金屬432之一部分(圖7A)以形成接合墊408,該等接 合墊包括佈置於凹陷430中之沈積金屬432之剩餘部分,如 圖7C中所展示。可根據動作14 (圖6)使用(例如)蝕刻程序 (例如’濕式化學蝕刻程序、乾式反應性離子蝕刻程序 等)、拋光或研磨程序或其组合(例如化學_機械拋光(CMp) 程序)去除沈積金屬432之一部分。舉例而言,可使第一半 導體結構400之作用表面410經受CMP程序以去除沈積金屬 432 (圖7A)上覆於凹陷430外側之塊體材料412區之部分, 從而僅保留沈積金屬432在凹陷430内之區域(該等區域界 定且包括接合墊408),且從而塊體材料412在橫向毗鄰凹 陷430内之沈積金屬432區域之區中之作用表面41〇處暴 露。因此,接合墊408中之一或多者可在第一半導體結構 400之作用表面41〇處暴露。 如圖7C中所展示,在一些實施例中,用於自第一半導體 、’-«構400去除過量金屬432之程序(例如,CMP程序)可使得 接合墊408之暴露表面發生碟形凹陷。另外,在一些實施 例中,在根據動作54去除沈積金屬432之一部分之後,接 合墊408之暴露表面可相對於作用表面41〇處環繞塊體材料 412之暴露主表面輕微凹陷。 再次參照圖6,在動作60中,接合墊408可直接接合至第 一半V體^構之金屬特徵。下文參照圖7〇及7E來闡述可 用於將接合塾4G8直接接合至第:半導體結構之金屬特徵 之直接接合程序之實例。 夕”、、圖7D,可將第一半導體結構4〇〇與第二半導體結構 c I62378.doc •33· 201241937 500對準從而將第一半導體結構400之接合墊408與第二半 導體結構500之導電金屬接合墊508對準。如圖7D中所展 示,第二半導體結構500可實質上類似於前文參照圖2E至 2G所述之第二半導體結構200,且亦可包括含有其他主動 裝置結構之經處理半導體結構,例如,垂直延伸之導電通 孔504及橫向延伸之導電跡線506。儘管並未展示於圖中, 但第二半導體結構500亦可包括電晶體。如圖7D中所展 示,在一些實施例中,第二半導體結構500之接合墊508可 至少與第一半導體結構400之接合墊408實質上相同,且可 包含位於接合墊508之導電金屬中之空隙536,例如第一半 導體結構400之接合墊408之金屬432中之空隙436。在其他 實施例中,接合墊508中可能並不包含該等空隙536。 接合墊408之暴露表面可界定接合墊408之一或多個接合 表面420,且接合墊508之外部暴露表面可界定第二半導體 結構500之接合墊508之接合表面520。 繼續參照圖7D,在將第一半導體結構400與第二半導體 結構500對準從而第一半導體結構400之接合墊408與第二 半導體結構500之導電金屬接合墊508對準之後,第一半導 體結構400可鄰接第二半導體結構500,從而第一半導體結 構400之接合墊408之接合表面420直接鄰接第二半導體結 構500之接合墊508之接合表面520且其間沒有任何中間接 合材科(例如,黏著劍)。 然後可將第一半導體結構400之接合墊408之接合表面 420直接接合至第二半導體結構500之接合墊508之接合表 162378.doc • 34- 201241937 面5 20以形成經接合的半導體結構600。接合程序導致形成 包含已接合至一起之接合墊408及接合墊5 08之經接合的金 屬結構。在直接金屬至金屬(例如,銅至銅)非熱壓縮接合 程序中,可將第二半導體結構500之接合墊508之接合表面 520直接接合至第一半導體結構400之接合墊4〇8之接合表 面420。在一些實施例中,非熱壓縮接合程序可包括在以 下環境中實施之超低溫直接接合程序:在約4〇〇攝氏度 (400°C )或更低之一或多個溫度下之環境中,或甚至在約 200攝氏度(200°C)或更低之一或多個溫度下之環境中。在 一些實施例中’非熱壓縮接合程序可在以下湓度下實施: 在介於約20攝氏度(20°C )與約400攝氏度(400。(:)之間之一 或多個溫度下’或甚至在介於約200攝氏度(2〇〇艺)與約350 攝氏度(350°C )之間之一或多個溫度下。在其他實施例中, 可在約室溫下之環境中(亦即,並未施加任何除由周圍環 境所提供熱量外之熱量)實施非熱壓縮接合程序。 在將第一半導體結構4〇〇接合至第二半導體結構5〇〇之 前,可處理第一半導體結構400及第二半導體結構5〇〇以去 除表面雜質及不期望表面化合物,且可實施平坦化以增加 接合墊408之接合表面420與接合墊5〇8之接合表面520之間 原子標度的緊密接觸區。可藉由以下方式來達成接合表面 420與接合表面520之間之緊密接觸區:藉由將接合表面 420及接合表面520拋光以將其表面粗糙度減小至接近原子 標度之值,藉由在接合表面420與接合表面52〇之間施加壓 力以得到塑膠變形,或藉由將接合表面42〇、52〇拋光及在 162378.doc -35- 201241937 第一半導體結構400與第二半導體結構500之間施加壓力以 獲得該塑膠變形二者。 在一些實施例中’可將第一半導體結構400直接接合至 第二半導體結構500且並不在其間之接合界面處之接合表 面420、520之間施加壓力,但可在一些超低溫直接接合方 法中在接合界面處之接合表面420、520之間施加壓力以在 接合界面處達成適宜接合強度。換言之,在本揭示内容之 一些實施例中,用於將第一半導體結構4〇〇之接合墊4〇8接 合至第二半導體結構5〇〇之接合墊5〇8之直接接合方法可包 括表面辅助接合(SAB)方法。 如圖7D中所展示,在將第一半導體結構4〇〇之接合墊4〇8 接合至第二半導體結構5〇〇之接合墊5〇8後,接合界面可保 持在放大下觀察時相對地可鑑別其微結構。另外,空隙 436可保留於接合塾408内,且空隙536亦可保留於接合墊 508 内。 再次參照圖6,在動作62中,可藉由將經接合的半導體 結構600 (及由此經接合的金屬結構)暴露於熱預算來將包 括接合墊408及接合墊508之經接合的金屬特徵退火。舉例 而言且並不加以限制,可藉由以下方式將經接合的金屬結 構退火··使接合墊408及接合墊508在約2小時或更短(例 如,介於約三十分鐘(30分鐘)與約一小時(1小時)之間)之 退火時間段内經受低於約40(TC之一或多個退火溫度。 在一些實施例中,動作62之退火程序可在室或亦實施動 作60之接合程序之其他殼體中原位實施。在該等實施例 162378.doc -36 - 201241937 中,動作62之退火程序可包括在室或其他殼體中使半導體 結構400經受連續熱循環之後續區段或部分。 動作62之退火程序可誘導接合墊408及接合墊508中之微 結構變化,且可使得接合墊408及508之金屬發生體積膨脹 (在局部藉由(例如)晶粒重定向及/或晶粒生長,或在整體 上藉由(例如)相變化)。接合墊408中空隙43 6及接合墊508 中空隙53 6之存在可提供金屬432可因該體積膨脹而擴展之 空間。因此,在動作62之退火程序之後,分別在接合墊 408及508内之空隙436及536可佔據較小體積(亦即,具有 較小平均橫截面尺寸)。在一些實施例中,在動作62之退 火程序之後,空隙436、536可能不再存在於接合墊408、 508内。另外,在一些實施例中,在動作62之退火程序之 後,在放大下觀察時在接合墊408與接合墊508之間之微結 構中可能沒有任何離散可鑑別接合界面。 如圖6中所屐示,在一些實施例中,在動作60之接合程 序之前,可使金屬432之至少一部分(圖7A)經受一或多個 退火程序。 舉例而言,在一些實施例中,在根據動作5 0如前文參照 圖7A所述將金屬432沈積於第一半導體結構400上之後,且 在根據動作54如前文參照圖7C所述去除金屬432之一部分 之前,可使沈積金屬432經受熱預算以將金屬432退火。圖 7B繪示在根據動作50將金屬432沈積於第一半導體結構400 上(圖6)之後且在根據動作52使如圖7A中所展示之半導體 結構400經受退火程序(圖6)之後的第一半導體結構400。C 162378.doc •29- 201241937 Surface roughness. Thus, Fig. 5 illustrates the joint surface 109' of the bond pad 108 having a reduced surface roughness relative to Fig. 2D and showing the joint surface coplanar with the exposed surface of the bulk material 112 at the active surface 11〇. In act 17, 'for example, an etching process (eg, a wet chemical remnant program, a dry reactive ion process, etc.), a polishing or grinding process, or a combination thereof (eg, a chemical-mechanical polishing (CMP) program) may be used. Removal of Other Portions of Deposited and Annealed Metal 132 By way of example, the active surface 110 of the first semiconductor structure 100 can be subjected to a CMP process to remove other deposited and annealed metals 132 of the bond pads 1〇8. Referring again to FIG. 4, after removing the other portions of the bonding pad 108 that are deposited and annealed to the metal 132 in accordance with act 17 to form the first semiconductor structure 100 as shown in FIG. 5, the first semiconductor structure 1 may be removed according to act 20. The bonding pads 108 of the germanium are directly bonded to the bonding pads 2〇8 of the second semiconductor structure 2, as described above with reference to FIGS. 1 and 2A to 2G. After the direct bonding process of act 20, the bonded metal features including bonding pads 1 8 of the first semiconductor structure 100 and bonding pads 2 〇 8 of the second semiconductor structure 200 can be annealed by: The bonded metal features are subjected to a first thermal budget that is lower than the first thermal budget, as previously described with reference to Figures 1 and 2G. Although not shown in FIG. 4, the bonding surface 109 of the bonding pad 1 8 can be prepared for bonding as shown by act 18 (FIG. 1) by subjecting the active surface 110 of the first semiconductor structure 100 to a cleaning process. The foregoing is described with reference to FIG. In other embodiments, the cap layer 116 may be formed or otherwise provided at the surface of at least one of the metal features of the first semiconductor structure 1 , and then the metal feature is directly bonded to the second according to act 20 of FIG. Semiconductor 162378.doc • 30· 201241937 At least one metal feature of the structure, as previously described with reference to Figures 3A through 3F. 6 is a flow diagram of another embodiment of a method of the present disclosure, and FIGS. 7A through 7E illustrate a fabrication of a bonded semiconductor structure in accordance with the program flow of FIG. Referring to Figure 6', in action 50, metal 432 can be deposited on the first semiconductor structure. As shown in FIG. 7A, a first semiconductor structure 4A can be formed. The first semiconductor structure 400 can be substantially similar to the first semiconductor structure 100 previously described in connection with FIG. 2A, and can include a processed semiconductor structure that includes one or more active device features, such as one of the following Or more: a plurality of transistors 4〇2 (shown schematically in the figures), a plurality of vertically extending conductive vias 4〇4, and a plurality of horizontally extending conductive traces 406 » active device features may include A conductive material and/or a semiconductor material surrounded by a non-conductive bulk material 4丨2. By way of example and not limitation, one or more of the conductive vias 404 and conductive traces 406 can include one or more conductive metals or metal alloys, such as copper, aluminum, or alloys or mixtures thereof. The first semiconductor structure 400 can also include a plurality of recesses 43 in which it is desired to form a plurality of bond pads 408 (Fig. 7C). To form the bond pads 4A8, a metal 432 can be deposited over (e.g., over) the active surface 410 of the first semiconductor structure 4'', such that the metal 432 at least completely fills the recess 430, as shown in Figure 7A. Excess metal 432 can be deposited on first semiconductor structure 400 such that recess 430 is completely filled with metal 432 and thereby other metal 432 is disposed (e.g., over) on surface 410 of first semiconductor structure 4 . By way of example and not limitation, metal 432 may comprise 162378.doc • 31- 201241937 metal or metal alloys such as copper, aluminum or alloys or mixtures thereof. In one embodiment, the selectable metal 432 comprises copper or a copper alloy. A metal 432 can be deposited on the first semiconductor structure 400 as shown in FIG. 7A to form a void 436 in the portion of the deposited metal 432 within the recess 43. In other words, the formed metal 432 can comprise at least one inner surface that defines a void 436 in the portion of the deposited metal 432 within the recess 430. The voids can be created, for example, during the electrodeposition process by increasing the metal growth rate on the vertical sides of the lines and vias. Under these conditions, voids spontaneously occur in the vias or lines. Other methods of creating such voids can be achieved by non-conformal deposition of a diffusion barrier (or metal seed layer). By increasing the side thickness of the barrier/seed layer in the via/line, voids can be created directly at the same time as the barrier deposition process or at an early stage of the metal deposition phase. Metal 432 can be deposited on first semiconductor structure 400 using, for example, one or more of the following procedures: electroless ore procedure, electrolytic plating procedure, chemical vapor deposition (CVD) procedure, and physical vapor deposition (PVD). program. According to one non-limiting example, a copper seed layer can be deposited using an electroless plating process. Then additional copper can be deposited on the copper seed layer at a relatively faster rate using an electrolytic plating process. Metal 432 may be deposited on first semiconductor structure 400 using, for example, one or more of the following procedures: electroless ore procedure, electrolysis clock procedure, chemical vapor deposition (CVD) procedure, and physical vapor deposition (pvD) )program. A copper seed layer can be deposited using an electroless plating process according to a non-limiting example, and then additional copper can be deposited on the copper seed layer at a relatively faster rate using an electroplating procedure. Referring again to FIG. 6, in act 54 a portion (FIG. 7A) of deposited metal 432 may be removed from the first semiconductor structure 400 by 162378.doc -32.201241937 to form bond pads 408 that are disposed in recess 430. The remainder of the deposited metal 432 is shown in Figure 7C. Depending on action 14 (FIG. 6), for example, an etch process (eg, a 'wet chemical etch process, a dry reactive ion etch process, etc.), a polishing or grinding process, or a combination thereof (eg, a chemical-mechanical polishing (CMp) program) may be used. A portion of the deposited metal 432 is removed. For example, the active surface 410 of the first semiconductor structure 400 can be subjected to a CMP process to remove portions of the bulk metal material 412 (FIG. 7A) overlying the bulk material 412 outside of the recess 430, thereby leaving only the deposited metal 432 in the recess. The regions within 430 (the regions define and include bond pads 408), and thus the bulk material 412 is exposed at the active surface 41〇 in the region of the region of deposited metal 432 that is laterally adjacent to the recess 430. Accordingly, one or more of the bond pads 408 can be exposed at the active surface 41 of the first semiconductor structure 400. As shown in Figure 7C, in some embodiments, the process for removing excess metal 432 from the first semiconductor, '-400, (e.g., a CMP process) can cause dishing of the exposed surface of bond pad 408. Additionally, in some embodiments, after removing a portion of the deposited metal 432 in accordance with act 54, the exposed surface of the bond pad 408 can be slightly recessed about the exposed major surface of the bulk material 412 relative to the active surface 41. Referring again to Figure 6, in act 60, bond pads 408 can be bonded directly to the metal features of the first half of the V body. An example of a direct bonding procedure that can be used to bond bonding germanium 4G8 directly to the metal features of the semiconductor structure is set forth below with reference to Figures 7A and 7E. </ RTI>, FIG. 7D, the first semiconductor structure 4 〇〇 can be aligned with the second semiconductor structure c I62378.doc • 33· 201241937 500 to bond the bonding pads 408 of the first semiconductor structure 400 and the second semiconductor structure 500 The conductive metal bond pads 508 are aligned. As shown in Figure 7D, the second semiconductor structure 500 can be substantially similar to the second semiconductor structure 200 previously described with reference to Figures 2E through 2G, and can also include other active device structures. The processed semiconductor structure, for example, vertically extending conductive vias 504 and laterally extending conductive traces 506. Although not shown, the second semiconductor structure 500 can also include a transistor. As shown in Figure 7D, In some embodiments, the bond pads 508 of the second semiconductor structure 500 can be at least substantially identical to the bond pads 408 of the first semiconductor structure 400, and can include voids 536 in the conductive metal of the bond pads 508, such as the first semiconductor. The voids 436 in the metal 432 of the bond pads 408 of the structure 400. In other embodiments, the voids 536 may not be included in the bond pads 508. The exposed surfaces of the bond pads 408 are boundaryable One or more bonding surfaces 420 of bond pads 408, and the outer exposed surface of bond pads 508 can define bonding surface 520 of bond pads 508 of second semiconductor structure 500. With continued reference to FIG. 7D, first semiconductor structures 400 and After the second semiconductor structure 500 is aligned such that the bond pads 408 of the first semiconductor structure 400 are aligned with the conductive metal bond pads 508 of the second semiconductor structure 500, the first semiconductor structure 400 can abut the second semiconductor structure 500 such that the first semiconductor structure The bonding surface 420 of the bonding pad 408 of 400 directly abuts the bonding surface 520 of the bonding pad 508 of the second semiconductor structure 500 without any intermediate bonding material (eg, a bonding sword). The bonding pad of the first semiconductor structure 400 can then be used. Bonding surface 420 of 408 is bonded directly to bond table 162378.doc • 34-201241937 face 5 20 of bond pad 508 of second semiconductor structure 500 to form bonded semiconductor structure 600. The bonding process results in the formation of bonds that have been bonded together Bonded metal structure of pad 408 and bond pad 508. Non-thermal compression of direct metal to metal (eg, copper to copper) In the bonding process, the bonding surface 520 of the bonding pads 508 of the second semiconductor structure 500 can be bonded directly to the bonding surface 420 of the bonding pads 4〇8 of the first semiconductor structure 400. In some embodiments, the non-thermal compression bonding process can be Includes an ultra-low temperature direct bonding procedure implemented in an environment at one or more temperatures of about 4 degrees Celsius (400 ° C) or lower, or even at about 200 degrees Celsius (200 ° C) or more Low in one or more temperatures in an environment. In some embodiments, the 'non-thermal compression bonding procedure can be performed at a temperature of between about 20 degrees Celsius (20 ° C) and about 400 degrees Celsius (400: (:) at one or more temperatures' Or even at one or more temperatures between about 200 degrees Celsius (about 2 degrees Celsius) and about 350 degrees Celsius (350 degrees Celsius). In other embodiments, it may be in an environment at about room temperature (also That is, the non-thermal compression bonding process is performed without applying any heat other than the heat supplied by the surrounding environment. The first semiconductor structure can be processed before the first semiconductor structure 4 is bonded to the second semiconductor structure 5? 400 and the second semiconductor structure 5 to remove surface impurities and undesired surface compounds, and planarization may be performed to increase the tightness of the atomic scale between the bonding surface 420 of the bonding pad 408 and the bonding surface 520 of the bonding pad 5〇8. Contact area. The intimate contact area between the bonding surface 420 and the bonding surface 520 can be achieved by polishing the bonding surface 420 and the bonding surface 520 to reduce the surface roughness to a value close to the atomic scale. ,borrow Applying pressure between the bonding surface 420 and the bonding surface 52A to obtain plastic deformation, or by polishing the bonding surfaces 42〇, 52〇 and at 162378.doc -35 - 201241937, the first semiconductor structure 400 and the second semiconductor structure 500 Pressure is applied between them to obtain both of the plastic deformations. In some embodiments, the first semiconductor structure 400 can be directly bonded to the second semiconductor structure 500 and not applied between the bonding surfaces 420, 520 at the bonding interface therebetween. Pressure, but pressure may be applied between the joint surfaces 420, 520 at the joint interface in some ultra-low temperature direct bonding methods to achieve a suitable joint strength at the joint interface. In other words, in some embodiments of the present disclosure, The direct bonding method of bonding pads 4〇8 of the first semiconductor structure 4 to the bonding pads 5〇8 of the second semiconductor structure 5可 may include a surface assisted bonding (SAB) method. As shown in FIG. 7D, After the bonding pads 4〇8 of the first semiconductor structure 4 are bonded to the bonding pads 5〇8 of the second semiconductor structure 5〇〇, the bonding interface can be kept under magnification. The microstructure can be identified relatively. Additionally, voids 436 can remain in bond pads 408, and voids 536 can remain in bond pads 508. Referring again to Figure 6, in act 62, the bonded semiconductor can be The structure 600 (and thus the bonded metal structure) is exposed to a thermal budget to anneal the bonded metal features including bond pads 408 and bond pads 508. By way of example and not limitation, the Bonded Metal Structure Annealing - Annealing Period of Bond Pad 408 and Bond Pad 508 over about 2 hours or less (eg, between about thirty minutes (30 minutes) and about one hour (1 hour)) The interior is subjected to less than about 40 (TC one or more annealing temperatures. In some embodiments, the annealing process of act 62 can be performed in situ in the chamber or other housing that also performs the bonding procedure of act 60. In these embodiments 162378.doc -36 - 201241937, the annealing process of act 62 can include subjecting semiconductor structure 400 to subsequent sections or portions of continuous thermal cycling in a chamber or other housing. The annealing process of act 62 can induce microstructural changes in bond pads 408 and bond pads 508, and can cause volume expansion of the pads 408 and 508 (in particular by, for example, grain redirection and/or die Growing, or by way of example, for example, phase change). The presence of voids 436 in bond pads 408 and voids 563 in bond pads 508 can provide space for metal 432 to expand due to this volume expansion. Thus, after the annealing process of act 62, voids 436 and 536 in bond pads 408 and 508, respectively, can occupy a smaller volume (i.e., have a smaller average cross-sectional dimension). In some embodiments, after the anneal procedure of act 62, voids 436, 536 may no longer be present in bond pads 408, 508. Additionally, in some embodiments, after the annealing process of act 62, there may be no discrete identifiable bonding interface in the microstructure between bond pad 408 and bond pad 508 when viewed under magnification. As illustrated in Figure 6, in some embodiments, at least a portion of the metal 432 (Figure 7A) can be subjected to one or more annealing procedures prior to the bonding process of act 60. For example, in some embodiments, the metal 432 is deposited on the first semiconductor structure 400 as described above with respect to FIG. 7A in accordance with act 50, and the metal 432 is removed as described above with respect to FIG. 7C in accordance with act 54. Prior to a portion, the deposited metal 432 can be subjected to a thermal budget to anneal the metal 432. 7B illustrates the second embodiment after deposition of metal 432 on first semiconductor structure 400 in accordance with act 50 (FIG. 6) and after subjecting semiconductor structure 400 as shown in FIG. 7A to an annealing process (FIG. 6) in accordance with act 52. A semiconductor structure 400.
S 162378.doc -37- 201241937 如圖7B中所展示,根據動作52使沈積金屬432經受熱預 算以將金屬432退火可誘導其中之微結構變化,如前文結 合圖2D所論述,且可使得沈積金屬432發生體積膨脹(在局 部藉由(例如)晶粒重定向及/或晶粒生長,或在整體上藉由 (例如)相變化)並改變沈積金屬432之暴露表面434之形貌。 在一些實施例中,動作52之退火程序可在室或亦實施動 作50之沈積程序之其他殼體中原位實施。在該等實施例 中’可在沈積程序之後但在自室或其他殼體取出第一半導 體結構400之前,在室或其他殼體中實施動作52之退火程 序。 在根據動作52將沈積金屬432退火之實施例中,動作52 之退火程序之熱預算可大於動作6:2之退火程序之熱預算。 在一些實施例中’動作62之退火程序之一或多個退火溫度 可至少與動作52之退火程序之一或多個退火溫度實質上相 同。在該等貫施例中’動作62之退火程序之退火時間段可 短於動作52之退火程序之退火時間段。在其他實施例中, 動作62之退火程序之退火時間段可至少與動作52之退火程 序之退火時間段實質上相同。在該等實施例中,動作62之 退火程序之平均退火溫度可低於動作52之退火程序之平均 退火溫度。在其他實施例中’動作62之退火程序之退火時 間段可短於動作52之退火程序之退火時間段,且動作62之 退火程序之平均退火溫度可低於動作52之退火程序之平均 退火溫度。 再次參照圖6 ’在一些實施例中’在根據動作54如前文 162378.doc -38· 201241937 參照圖7C所述去除沈積金屬432之一部分之後,且在動作 60之接合程序之前,可使沈積金屬432之剩餘部分經受熱 預算以將金屬432之剩餘部分退火。此一退火程序可至少 與如前文參照圖2D所述圖1之動作16之退火程序實質上相 同。在該等實施例中,動作54之退火程序之熱預算可大於 動作62之退火程序之熱預算《在一些實施例中,動作62之 退火程序之一或多個退火溫度可至少與動作54之退火程序 之一或多個退火溫度實質上相同。在該等實施例中,動作 62之退火程序之退火時間段可短於動作54之退火程序之退 火時間段。在其他實施例中,動作62之退火程序之退火時 間段可至少與動作54之退火程序之退火時間段實質上相 同。在該等實施例中’動作62之退火程序之平均退火溫度 可低於動作5 4之退火程序之平均退火溫度。在其他實施例 中’動作62之退火程序之退火時間段可短於動作54之退火 程序之退火時間段,且動作62之退火程序之平均退火溫度 可低於動作54之退火程序之平均退火溫度。 在一些實施例中’圖6之程岸流程可包含動作52之退火 程序及動作56之退火程序二者。根據一些該等實施例,動 作52之熱預算可大於動作62之熱預算,且動作56之熱預算 可小於、等於或大於動作52之退火程序之熱預算。根據其 他該等實施例’動作56之熱預算可大於動作62之熱預算, 且動作52之熱預算可小於、等於或大於動作56之退火程序 之熱預算。在其他該等實施例中,動作5 2之熱預算可小於 動作62之熱預算’且動作56之熱預算可小於動作62之熱預 £ 162378.doc -39· 201241937 算,但動作52及動作56之退火程序之組合熱預算可大於動 作62之熱預算。 在其他實施例中,根據本文參照圖6及7八至7£結合接合 墊408之形成及退火所述之方法,可形成第二半導體結構 5〇〇之一或多個主動特徵(例如接合墊5〇8)並退火。 另外,在其他實施例中,可在第一半導體結構4〇〇之至 少一個金屬特徵之表面處形成或以其他方式提供帽蓋層 U6,然後根據圖ό之動作60將該金屬特徵直接接合至第二 半導體、構之至少一個金屬特徵,如前文參照圖3 Α至3 F所 述。 儘管上文參照將第一半導體結構之接合墊直接接合至第 二半導體結構之接合墊來闡述本揭示内容之實施例,但涵 蓋可處理除第一及第二半導體結構之接合墊外之金屬特徵 並如本文所述直接接合。舉例而言,該等其他金屬特徵可 包括導電通孔、穿晶圓互連件、導電跡線或暴露於表面半 導體結構處之任一其他金屬特徵。另外,本文涵蓋,可形 成第二半導體結構之導電特徵(例如接合墊、導電通孔及 導電跡線中之一或多者),且如本文中結合第一半導體結 構之接合墊(與第一半導體結構之導電特徵之處理一起或 作為替代方式)所述進行處理(例如,退火),然後將第一半 導體結構之一或多個導電特徵與第二半導體結構之一或多 個導電特徵直接接合至一起。 本揭不内容之其他非限制性實例性實施例闡述如下: 實施例1: 一種將第一半導體結構直接接合至第二半導 162378.doc -40- 201241937 體結構之方法’其包括:將金屬沈積於第 上;去除沈積於第—半導體 體、·、。構 穑於筮一盅道遍 再炙I屬之—部分;使沈 算、且蔣:上之金屬之剩餘部分經受第-執預 算,且將沈積於第一半導體結構上之金:熱預 火;將第-半導體結構之至少一個二部为退 第一半導體結構上之金屬 ’,-(匕括沈積於 導體結構之至少—個金屬餘一分)直接接合至第二半 該經接合的金屬結:Γ=經接合的金屬結構, 特徵及第二半導體導體結構之至少-個金屬 … 構之至少-個金屬特徵;及使經接人 的金屬結構經受第二献預算 ° 々 算並將經接合的金屬結構退火, 第一熱預异小於或等於第—熱預算。 實施例2:如實施例1之方法,其中使沈積於第-半導體 結構上之金屬之剩餘部分經受第-熱預算並將沈積於第— ^導體結構上之金屬之剩餘部分退火包括:使金屬之剩餘 部分在第-退火時間段内經受第—平均退火溫度,且 使經接合的金屬結構經受第二熱預算並將經接合的金屬莊 構退火包括:使經接合的金屬結構在第二退火時間段内緩 受第二平均退火溫度。 其中第一平均退火溫度高 其中第一退火時間段長於 實施例3 :如實施例2之方法 於或等於第二平均退火溫度。 實施例4 :如實施例2之方法 或等於第二退火時間段。 實施例5:如實施例2之方法,其中第一平均退火溫度高 於或等於第二平均退火溫度’且其中第一退火時間段長於 162378.doc -41- c 201241937 或等於第二退火時間段。 實施例6 :如實施例1至5中任一項之方法,其進一步包 括在去除沈積於第一半導體結構上之金屬部分之前,將沈 積於第一半導體結構上之金屬退火。 實施例7 :如實施例1至6中任一項之方法,其中去除沈 積於第一半導體結構上之金屬部分包括使第一半導體結構 經受化學-機械拋光程序。 實施例8 :如實施例1至7中任一項之方法,其進一步包 括選擇沈積於第一半導體結構上之金屬包括銅或銅合金。 實施例9 :如實施例1至8中任一項之方法,其進一步包 括在將第一半導體結構之至少一個金屬特徵直接接合至第 二半導體結構之至少一個金屬特徵之前,在第一半導體結 構之至少一個金屬特徵之表面處形成帽蓋層。 實施例10 :如實施例9之方法,其中形成帽蓋層包括形 成包括金屬矽化物之帽蓋層。 實施例11 :如實施例9之方法’其中形成帽蓋層包括形 成包括金屬、矽及氮之帽蓋層。 實施例12 :如實施例9之方法,其中形成帽蓋層包括形 成包括金屬合金之帽蓋層。 實施例13 :如實施例12之方法,其進一步包括形成包括 CoWP之帽蓋層。 實施例14 :如實施例9至13中任一項之方法,其進—步 包括形成平均厚度為約1〇奈米(10 nm)或更小之帽蓋層。 實施例15 :如實施例1至14中任一項之方法,其中將第 162378.doc •42· 201241937 一半導體結構之至少一個金屬特徵直接接合至第二半導體 結構之至少一個金屬特徵包括在介於2〇〇c與4〇(rc間之溫 度下且並不施加壓力下進行接合。 實施例16 :如實施例丨至15中任一項之方法,其中將第 一半導體結構之至少一個金屬特徵直接接合至第二半導體 結構之至少一個金屬特徵包括表面辅助接合程序。 實施例17 :如實施例丨至16中任一項之方法,其中將第 一半導體結構之至少一個金屬特徵直接接合至第二半導體 結構之至少一個金屬特徵包括:在溫度小於約4〇〇攝氏度 (4〇〇°C)之環境中,使第一半導體結構之至少一個金屬特^ 之第一接合表面直接鄰接第二半導體結構之至少一個金屬 特徵之第二接合表面。 實施例1 8 :如實施例17之方法,其進一步包括在溫度小 於約400攝氏度(4〇(TC)之環境中,在第一接合表面與=二 接合表面之間施加壓力。 實施例19 :如實施例18之方法,其中在溫度小於約 攝氏度(400°C )之環境中在第一接合表面與第二接合表面之 間施加壓力包括:在溫度小於約200攝氏度(20(rc )之環境 中在第一接合表面與第二接合表面之間施加壓力。 實施例20 :如實施例19之方法,其中在溫度小於約2〇〇 攝氏度(200C)之環境中在第一接合表面與第二接合表面之 間施加壓力包括在約室溫環境中在第一接合表面與第二接 合表面之間施加壓力。 實施例21: —種將第一半導體結構接合至第二半導體結 162378.doc •43·S 162378.doc -37- 201241937, as shown in FIG. 7B, subjecting the deposited metal 432 to a thermal budget to anneal the metal 432 according to act 52 induces a change in microstructure therein, as discussed above in connection with FIG. 2D, and may result in deposition Metal 432 undergoes volume expansion (either locally by, for example, grain reorientation and/or grain growth, or by, for example, phase change) and alters the morphology of exposed surface 434 of deposited metal 432. In some embodiments, the annealing process of act 52 can be performed in situ in the chamber or other housing that also performs the deposition process of action 50. In these embodiments, the annealing process of action 52 may be performed in a chamber or other housing after the deposition process but before the first semiconductor structure 400 is removed from the chamber or other housing. In an embodiment in which the deposited metal 432 is annealed according to act 52, the thermal budget of the annealing process of action 52 may be greater than the thermal budget of the annealing process of act 6:2. In some embodiments, one or more of the annealing temperatures of the 'action 62 may be at least substantially the same as one or more of the annealing temperatures of the action 52. The annealing time period of the annealing process of 'action 62 may be shorter than the annealing time period of the annealing process of action 52 in the various embodiments. In other embodiments, the annealing period of the annealing process of act 62 can be at least substantially the same as the annealing period of the annealing process of act 52. In such embodiments, the average annealing temperature of the annealing process of action 62 may be lower than the average annealing temperature of the annealing process of action 52. In other embodiments, the annealing period of the annealing process of the action 62 may be shorter than the annealing period of the annealing process of the operation 52, and the annealing temperature of the annealing process of the operation 62 may be lower than the average annealing temperature of the annealing process of the operation 52. . Referring again to FIG. 6 'in some embodiments', after removing a portion of the deposited metal 432 as described with reference to FIG. 7C in accordance with act 54 162 378 . doc - 38 · 201241937, and prior to the bonding process of act 60, the deposited metal may be The remainder of 432 is subjected to a thermal budget to anneal the remainder of metal 432. This annealing procedure can be at least substantially the same as the annealing procedure of act 16 of Figure 1 as previously described with reference to Figure 2D. In such embodiments, the thermal budget of the annealing process of action 54 may be greater than the thermal budget of the annealing process of act 62. In some embodiments, one or more of the annealing temperatures of act 62 may be at least with action 54. One or more of the annealing temperatures are substantially the same. In such embodiments, the annealing period of the annealing process of act 62 may be shorter than the annealing period of the annealing process of act 54. In other embodiments, the annealing time of the annealing process of act 62 can be at least substantially the same as the annealing time of the annealing process of act 54. The average annealing temperature of the annealing process of 'Action 62 in these embodiments may be lower than the average annealing temperature of the annealing process of Action 54. In other embodiments, the annealing period of the annealing process of the action 62 may be shorter than the annealing period of the annealing process of the action 54, and the annealing temperature of the annealing process of the operation 62 may be lower than the average annealing temperature of the annealing process of the action 54. . In some embodiments, the process of the process of Figure 6 can include both the annealing process of act 52 and the annealing process of act 56. According to some of these embodiments, the thermal budget of action 52 may be greater than the thermal budget of action 62, and the thermal budget of action 56 may be less than, equal to, or greater than the thermal budget of the annealing process of action 52. According to other such embodiments, the thermal budget of action 56 may be greater than the thermal budget of action 62, and the thermal budget of action 52 may be less than, equal to, or greater than the thermal budget of the annealing process of action 56. In other such embodiments, the thermal budget for action 52 may be less than the thermal budget of action 62 and the thermal budget for action 56 may be less than the thermal budget for action 62 162378.doc -39·201241937, but action 52 and action The combined thermal budget for the 56 annealing process can be greater than the thermal budget for action 62. In other embodiments, one or more active features of the second semiconductor structure 5 (eg, bond pads) may be formed in accordance with the methods described herein with reference to FIGS. 6 and 7-8 through bonding bond pad 408 formation and annealing. 5〇8) and annealed. Additionally, in other embodiments, the cap layer U6 can be formed or otherwise provided at the surface of at least one of the metal features of the first semiconductor structure 4, and then bonded directly to the metal feature according to act 60 of the figure The second semiconductor, the at least one metal feature, as previously described with reference to Figures 3A through 3F. Although the embodiments of the present disclosure are described above with reference to bonding pads of a first semiconductor structure directly to bond pads of a second semiconductor structure, covering metal features that can handle bond pads other than the first and second semiconductor structures And directly joined as described herein. For example, the other metal features can include conductive vias, through-wafer interconnects, conductive traces, or any other metal feature exposed at the surface semiconductor structure. Additionally, it is contemplated herein that conductive features of the second semiconductor structure (eg, one or more of bond pads, conductive vias, and conductive traces) can be formed, and as described herein in conjunction with the bond pads of the first semiconductor structure (with the first The processing of the conductive features of the semiconductor structure, together or alternatively, is performed (eg, annealed), and then one or more of the conductive features of the first semiconductor structure are directly bonded to one or more of the conductive features of the second semiconductor structure Together. Other non-limiting, exemplary embodiments of the present disclosure are set forth below: Embodiment 1: A method of directly bonding a first semiconductor structure to a second semiconductor 162378.doc-40-201241937 body structure, which includes: metal Deposited on the first; removed deposited on the first semiconductor body, ·,.穑 穑 穑 遍 遍 遍 炙 炙 炙 炙 部分 部分 部分 部分 部分 ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; And bonding at least one of the two portions of the first semiconductor structure to the metal on the first semiconductor structure, and (directly including at least one metal deposited on the conductor structure) directly bonded to the second half of the bonded metal Junction: Γ = bonded metal structure, features and at least one metal of the second semiconductor conductor structure ... at least one metal feature; and subjecting the joined metal structure to a second budget The joined metal structure is annealed and the first thermal pre-equivalent is less than or equal to the first thermal budget. Embodiment 2: The method of Embodiment 1, wherein subjecting a remaining portion of the metal deposited on the first semiconductor structure to a first thermal budget and annealing the remaining portion of the metal deposited on the first conductive structure comprises: The remainder is subjected to a first-average annealing temperature during the first-annealing period, and subjecting the bonded metal structure to a second thermal budget and annealing the bonded metal includes: subjecting the bonded metal structure to a second annealing The second average annealing temperature is relieved during the time period. Wherein the first average annealing temperature is high wherein the first annealing period is longer than Example 3: the method as in Example 2 is at or equal to the second average annealing temperature. Example 4: The method as in Example 2 is equal to or equal to the second annealing period. Embodiment 5: The method of Embodiment 2, wherein the first average annealing temperature is higher than or equal to the second average annealing temperature 'and wherein the first annealing period is longer than 162378.doc -41 - c 201241937 or equal to the second annealing period . The method of any one of embodiments 1 to 5, further comprising annealing the metal deposited on the first semiconductor structure prior to removing the metal portion deposited on the first semiconductor structure. The method of any one of embodiments 1 to 6, wherein removing the metal portion deposited on the first semiconductor structure comprises subjecting the first semiconductor structure to a chemical-mechanical polishing process. The method of any one of embodiments 1 to 7, further comprising selectively selecting a metal deposited on the first semiconductor structure comprising copper or a copper alloy. The method of any one of embodiments 1 to 8, further comprising, prior to bonding the at least one metal feature of the first semiconductor structure directly to the at least one metal feature of the second semiconductor structure, in the first semiconductor structure A cap layer is formed at the surface of at least one of the metal features. Embodiment 10: The method of Embodiment 9, wherein forming the cap layer comprises forming a cap layer comprising a metal telluride. Embodiment 11: The method of Embodiment 9 wherein forming the cap layer comprises forming a cap layer comprising metal, niobium and nitrogen. Embodiment 12: The method of Embodiment 9, wherein forming the cap layer comprises forming a cap layer comprising a metal alloy. Embodiment 13: The method of Embodiment 12, further comprising forming a cap layer comprising CoWP. Embodiment 14: The method of any one of embodiments 9 to 13, further comprising forming a cap layer having an average thickness of about 1 nanometer (10 nm) or less. The method of any one of embodiments 1 to 14, wherein the at least one metal feature of the semiconductor structure of the first semiconductor structure is directly bonded to the at least one metal feature of the second semiconductor structure including 162378.doc • 42· 201241937 The method of any one of Embodiments 1 to 15, wherein at least one metal of the first semiconductor structure is bonded at a temperature between 2 〇〇c and 4 〇 (rc). The at least one metal feature of the first semiconductor structure is directly bonded to the at least one metal feature of the first semiconductor structure directly to the method of any one of the embodiments At least one metal feature of the second semiconductor structure includes: adjoining the first bonding surface of the at least one metal of the first semiconductor structure directly adjacent to the second in an environment having a temperature of less than about 4 〇〇 Celsius (4 ° C) a second bonding surface of at least one metal feature of the semiconductor structure. Embodiment 1 8: The method of embodiment 17, further comprising at a temperature of less than about 400 In an environment of 4 〇 (TC), a pressure is applied between the first joint surface and the second joint surface. Embodiment 19: The method of Embodiment 18, wherein the temperature is less than about Celsius (400 ° C) Applying pressure between the first engagement surface and the second engagement surface includes applying pressure between the first engagement surface and the second engagement surface in an environment having a temperature of less than about 200 degrees Celsius (20 (rc). Example 20: The method of embodiment 19, wherein applying pressure between the first joining surface and the second joining surface in an environment having a temperature of less than about 2 degrees Celsius (200 C) comprises at the first joining surface and at about the room temperature environment Pressure is applied between the two bonding surfaces. Embodiment 21: Bonding the first semiconductor structure to the second semiconductor junction 162378.doc • 43·
C 201241937 構之方法,其包枯.從 *金屬沈積於第一半導體結構上,·去 除沈積於第一丰莫鍊注祖 導體,-。構上之金屬之一部分 一半導體結構上之厶麗今孟, 使况檟於第 沈積於第丰道屬之剩餘部分經受第-熱預算’且將 X積於弟一+導體結構 籍扒笛褥上之金屬之剩餘部分退火,•在將沈 積於第一+導體結 之金屬之剩餘部分退火之後,去险 沈積於第一半導體結構 “ ^ <金屬之其他部分;將第一半導 體結構之至少一個全眉姓外,—1 金屬特徵(包括沈積於第一半導體結構 屬之剩餘。(5分)直接接合至第二半導體結構之至少 一個金屬特徵以形成經接合的金屬結構,該經接合的金屬 構巴括帛半導體結構之至少一個金屬特徵及第二半導 體結構之至少一個金屬特徵;及使經接合的金屬結構經受 第二熱預算並將經接合的金屬結構退火,第二熱預算小於 或等於第一熱預算。 實施例22 :如實施例21之方法,其中使沈積於第一半導 體結構上之金屬之㈣部分經受第—熱預算並將沈積於第 一半導體結構上之金屬之剩餘部分退火包括:使金屬之剩 餘部分在第-退火時間段内經受第—平均退火溫度,且其 中使經接合的金屬結構經受第二熱預算並將經接合的金屬 結構退火包括:使經接合的金屬結構在第二退火時間段内 經受第二平均退火溫度。 實施例23 :如實施例22之方法,其中第一平均退火溫度 咼於或等於第二平均退火溫度。 實施例24 :如實施例22之方法,其中第一退火時間段長 於或等於第二退火時間段。 162378.doc -44 - 201241937 實施例25 :如實施例22之方法,盆φ货 古认# 八第一平均退火溫度 二笛弟-平均退火溫度,且其中第—退火時間段長於或等 於第二退火時間段。 實施例26 :如實施例21至25中任一頂♦ + ^ 方法,其進一步 匕括在去除沈積於第-半導體結構上之金屬部分之前 沈積於第一半導體結構上之金屬退火。 實施例27:如實施例21至26中任一項之方法… 沈積於第-半導體結構上之金屬部分包括使第^導體社 構經受化學-機械拋光程序。 μ 實施例28 ••如實施例21至27中任一項之方法,呈 沈積於第-半導體結構上之金屬之其他部分包括使第一半 導體結構經受化學-機械拋光程序。 實施例29:如實施例21至28中任一項之方法,宜中 一半導體結構之至少-個金屬特徵直接接合至第二半導體 結構之至少—個金屬特徵包括超低溫接合程序。 實施例3〇 :如實施例21至29中任一項之方法,其中將第 :半導體結構之至少一個金屬特徵直接接合至第二半導體 、’·。構之至少一個金屬特徵包括表面輔助接合程序。 實施例3!:如實施例21至3〇中任一項之方法其十 一+導體結構之至少—個金屬特徵直接接合至第二半導體 結構之至少一個金屬特徵包括:在溫度小於約400攝氏戶 (400°C)之環境中,使第一 " 半導體結構之至少一個金屬特徵 口表面直接鄰接第二半導體結構之至 特徵之第二接合表面。 固金屬C 201241937 The method of construction, which is carried out. From the metal deposited on the first semiconductor structure, · removed from the first Fengmo chain ancestor conductor. One part of the metal of the structure, a semiconductor structure, is beautiful, and the situation is that the remaining part of the genus Dijon is subjected to the first-thermal budget' and the X is accumulated in the second-conductor structure. The remaining portion of the metal is annealed, and after annealing the remaining portion of the metal deposited on the first + conductor junction, is deposited on the first semiconductor structure "^ < the other portion of the metal; at least the first semiconductor structure a full eyebrow surname, -1 metal features (including remaining in the first semiconductor structure genus. (5 points) directly bonded to at least one metal feature of the second semiconductor structure to form a bonded metal structure, the bonded At least one metal feature of the metal structure and the at least one metal feature of the second semiconductor structure; and subjecting the bonded metal structure to a second thermal budget and annealing the bonded metal structure, the second thermal budget being less than or Equal to the first thermal budget. Embodiment 22: The method of Embodiment 21, wherein the (four) portion of the metal deposited on the first semiconductor structure is subjected to a first thermal budget Annealing the remaining portion of the metal deposited on the first semiconductor structure includes subjecting the remaining portion of the metal to a first average annealing temperature during the first annealing period, and wherein subjecting the bonded metal structure to a second thermal budget and Annealing the bonded metal structure includes subjecting the bonded metal structure to a second average annealing temperature during the second annealing period. Embodiment 23: The method of Embodiment 22, wherein the first average annealing temperature is equal to or equal to The second average annealing temperature. Embodiment 24: The method of Embodiment 22, wherein the first annealing period is longer than or equal to the second annealing period. 162378.doc -44 - 201241937 Embodiment 25: The method of Embodiment 22, The first average annealing temperature is two flute-average annealing temperatures, and wherein the first annealing period is longer than or equal to the second annealing period. Embodiment 26: as in any of the embodiments 21 to 25 ♦ + ^ method further comprising metal annealing deposited on the first semiconductor structure prior to removing the metal portion deposited on the first semiconductor structure. Example 27: The method of any one of embodiments 21 to 26: depositing the metal portion on the first semiconductor structure comprises subjecting the second conductor structure to a chemical-mechanical polishing procedure. μ Example 28 • As in Examples 21 to 27 In one method, the other portion of the metal deposited on the first semiconductor structure comprises subjecting the first semiconductor structure to a chemical-mechanical polishing process. Embodiment 29: The method of any one of embodiments 21 to 28, preferably At least one metal feature of a semiconductor structure directly bonded to the second semiconductor structure comprises a cryogenic bonding process. Embodiment 3: The method of any one of embodiments 21 to 29, wherein: At least one metal feature of the structure is bonded directly to the second semiconductor, '. The at least one metal feature comprises a surface assisted bonding procedure. Embodiment 3: The method of any one of embodiments 21 to 3, wherein at least one metal feature of the eleven+conductor structure directly bonded to the at least one metal feature of the second semiconductor structure comprises: at a temperature of less than about 400 Celsius In the environment of the household (400 ° C), at least one of the metal feature port surfaces of the first " semiconductor structure directly adjoins the second bonding surface of the second semiconductor structure to the feature. Solid metal
C 162378.doc •45· 201241937 實施例32:如實施例31之方法,其進一步包括在溫度小 於約400攝氏度(400ΐ)之環境中,在第一接合表面與第二 接合表面之間施加壓力。 實施例33 : —種將第一半導體結構接合至第二半導體結 構之方法,其包括:將金屬沈積於第一半導體結構上並在 金屬中形成至少一個空隙;將第一半導體結構之至少一個 金屬特徵(包括金屬之一部分)直接接合第二半導體結構之 至少一個金屬特徵以形成經接合的金屬結構,該經接合的 金屬結構包括第一半導體結構之至少一個金屬特徵及第二 半導體結構之至少一個金屬特徵;及藉由以下方式將經接 合的金屬結構退火:使經接合的金屬結構經受後接合熱預 算並使第一半導體結構之至少一個金屬特徵之金屬擴展至 先前由金屬中之空隙所佔據的空間中。 實施例34:如實施例33之方法,其進一步包括去除沈積 於第一半導體結構上之金屬之一部分,第一半導體結構之 至少一個金屬特徵包括第一半導體結構上之金屬之剩餘部 分。 實施例35 :如實施例33或實施例34之方法,其進一步包 括藉由以下方式將至少一個金屬特徵之金屬退火:使至少 一個金屬特徵之金屬經受前接合熱預算,然後將第一半導 體結構之至少一個金屬特徵直接接合至第二半導體結構之 至少一個金屬特徵。 實施例36 :如實施例35之方法,其進一步包括使前接合 熱預算等於或高於後接合熱預算。 J62378.doc -46· 201241937 實施例3 7 :如實施例3 5或實施例3 6之方法,其中藉由使 至少一個金屬特徵之金屬經受前接合熱預算來將至少一個 金屬特徵之金屬退火包括:將沈積於第一半導體結構上之 金屬退火’然後去除沈積於第一半導體結構上之金屬部 分。 實施例38 :如實施例37之方法,其中藉由使至少—個金 屬特徵之金屬經受前接合熱預算來將至少一個金屬特徵之 金屬退火進一步包括:在去除沈積於第一半導體結構上之 金屬部分之後,將第一半導體結構上之金屬之剩餘部分退 火。 實施例39:如實施例35或實施例36之方法,其中藉由使 至少一個金屬特徵之金屬經受前接合熱預算來將至少一個 金屬特徵之金屬退火包括:在去除沈積於第一半導體纟士構 上之金屬部分之後,將第一半導體結構上之金屬之剩^部 分退火。 實施例40 :如實施例33至39中任一項之方法,其中使第 一半導體結構之至少一個金屬特徵之金屬擴展至先前由金 屬中之空隙所佔據的空間中包括減小空隙體積。 * • 實施例41 :如實施例40之方法,其中減小空隙體積包括 消除空隙。 實施例42: —種經接合的半導體結構’其係根據實施例 1至41中任一項所述之方法形成。 實施例43 : —種經接合的半導體結構,其包括:第一半 導體結構’其包括至少一個金屬特徵,該第一半導體妗構The method of embodiment 31, further comprising applying a pressure between the first joining surface and the second joining surface in an environment having a temperature of less than about 400 degrees Celsius (400 inches). Embodiment 33: A method of bonding a first semiconductor structure to a second semiconductor structure, comprising: depositing a metal on the first semiconductor structure and forming at least one void in the metal; and at least one metal of the first semiconductor structure A feature (including a portion of the metal) directly bonding at least one metal feature of the second semiconductor structure to form a bonded metal structure, the bonded metal structure comprising at least one of the at least one metal feature of the first semiconductor structure and the second semiconductor structure Metal features; and annealing the bonded metal structure by subjecting the bonded metal structure to a post-bonding thermal budget and expanding the metal of at least one metal feature of the first semiconductor structure to previously occupied by voids in the metal In the space. Embodiment 34: The method of Embodiment 33, further comprising removing a portion of the metal deposited on the first semiconductor structure, the at least one metal feature of the first semiconductor structure comprising a remaining portion of the metal on the first semiconductor structure. Embodiment 35: The method of Embodiment 33 or Embodiment 34, further comprising annealing the metal of the at least one metal feature by subjecting the metal of the at least one metal feature to a pre-bonding thermal budget, and then the first semiconductor structure At least one metal feature is directly bonded to at least one metal feature of the second semiconductor structure. Embodiment 36: The method of Embodiment 35, further comprising the pre-bonding thermal budget being equal to or higher than the post-joining thermal budget. The method of Embodiment 3 or Embodiment 36, wherein the metal of the at least one metal feature is annealed by subjecting the metal of the at least one metal feature to a pre-bonding thermal budget. : annealing the metal deposited on the first semiconductor structure 'and then removing the metal portion deposited on the first semiconductor structure. The method of embodiment 37, wherein annealing the metal of the at least one metal feature by subjecting the at least one metal feature metal to a front bonding thermal budget further comprises: removing the metal deposited on the first semiconductor structure After the portion, the remaining portion of the metal on the first semiconductor structure is annealed. Embodiment 39: The method of Embodiment 35 or Embodiment 36, wherein annealing the metal of the at least one metal feature by subjecting the metal of the at least one metal feature to a pre-bonding thermal budget comprises: removing the deposited first semiconductor gentleman After the metal portion is structured, the remaining portion of the metal on the first semiconductor structure is annealed. The method of any one of embodiments 33 to 39, wherein expanding the metal of the at least one metal feature of the first semiconductor structure to the space previously occupied by the voids in the metal comprises reducing the void volume. The method of embodiment 40, wherein reducing the void volume comprises eliminating voids. Embodiment 42: A bonded semiconductor structure is formed according to the method of any of Embodiments 1 to 41. Embodiment 43: A bonded semiconductor structure comprising: a first semiconductor structure 'which includes at least one metal feature, the first semiconductor structure
C 162378.doc -47- 201241937 之至少一個金屬特徵具有至少一個界定該第一半導體結構 之至少一個金屬特徵内之空隙的内表面;及第二半導體結 構,其包括至少一個直接接合至第一半導體結構之至少一 個金屬特徵之金屬特徵。 實施例44 :如實施例43之經接合的半導體結構,其中第 二半導體結構之至少一個金屬特徵具有至少一個界定第二 半導體結構之至少一個金屬特徵内之空隙的内表面。 本揭示内容之上述實例性實施例並不限制本發明範圍, 此乃因該等實施例僅係本發明實施例之實例,本發明範圍 係由申請專利範圍之範圍及其合法等效物界定。任何等效 實施例皆意欲涵蓋於本發明範圍内。實際上,除彼等展示 及闡述於本文中者(例如所述要素之替代性有用組合)外, 彼等熟習此項技術者自本說明將明瞭本揭示内容之各種修 改。換言之,本文所述一實例性實施例之一或多個特徵可 與本文所述另-實例性實施例之—或多個特徵進行組合以 提供本揭示内容之其他實施例。該等修改及實施例亦意欲 涵蓋於隨附申請專利範圍之範圍内。 【圖式簡單說明】 的半導體結構之方 圖1係繪不形成.本揭不内容中經接人 法之實例性實施例之程序流程的流程圖 不方法之一實施例來形成 圖2A至2G繪示根據圖1中所綠 經接合的半導體結構; 一實施例來形 圖3A至3F繪示根據圖1中所繪示方法之另 成經接合的半導體結構; 162378.doc -48 · 201241937 圖4係繪示形成本揭示内纟中經接合的半導體結構之方 法之其他實例性實施例之程序流程的流程圖; 繪示可在根據圖4中所緣示方法之實施例形成本揭示 内容之經接合的半導體結構中製得之半導體結構; 、圖6係繪不形成本揭示内容中經接合的半導體結構之方 法之其他實例性實施例之程序流程的流程圖;且 圖7A至7E繪示根據圖6中所繪示方法之一實施例來 經接合的半導體結構。 夕成 【主要元件符號說明】 100 第一半導體結構 100, 第一半導體結構 102 電晶體 104 導電通孔 106 導電跡線 108 接合墊 108, 接合墊 109 接合表面 110 作用表面 112 塊體材料 115 暴露表面 116 帽蓋層 130 凹陷 132 金屬 134 暴露表面 162378.doc -49- £ 201241937 200 第二半導體結構 204 導電通孔 206 導電跡線 208 導電金屬接合墊 212 塊體材料 220 接合表面 300 經接合的半導體結構 300' 經接合的半導體結構 400 第一半導體結構 402 電晶體 404 導電通孔 406 導電跡線 408 接合墊 410 作用表面 412 非導電塊體材料 420 接合表面 430 凹陷 432 金屬 434 暴露表面 436 空隙 500 第二半導體結構 504 導電通孔 506 導電跡線 508 導電金屬接合墊 162378.doc -50- 201241937 520 536 600 接合表面 空隙 經接合的半導體結構 162378.doc -51 -At least one metal feature of C 162378.doc -47-201241937 having at least one inner surface defining a void in at least one metal feature of the first semiconductor structure; and a second semiconductor structure including at least one directly bonded to the first semiconductor A metallic feature of at least one metal feature of the structure. Embodiment 44: The bonded semiconductor structure of Embodiment 43, wherein the at least one metal feature of the second semiconductor structure has at least one inner surface defining a void in at least one of the metal features of the second semiconductor structure. The above-described exemplary embodiments of the present disclosure are not intended to limit the scope of the invention, and the embodiments are intended to be illustrative only, and the scope of the invention is defined by the scope of the claims and their legal equivalents. Any equivalent embodiments are intended to be included within the scope of the invention. In fact, various modifications of the present disclosure will be apparent to those skilled in the art in the <RTIgt; </ RTI> <RTIgt; </ RTI> <RTIgt; </ RTI> <RTIgt; In other words, one or more of the features of an exemplary embodiment described herein can be combined with the other exemplary embodiments described herein, or a plurality of features to provide further embodiments of the present disclosure. The modifications and examples are intended to be included within the scope of the appended claims. BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a schematic diagram of a semiconductor structure of an exemplary embodiment of an embodiment of the present invention. FIG. 2A to FIG. 2G are formed. FIG. 3A to FIG. 3F illustrate another bonded semiconductor structure according to the method illustrated in FIG. 1; 162378.doc -48 · 201241937 4 is a flow chart showing the flow of a procedure of another exemplary embodiment of a method of forming a bonded semiconductor structure in the present invention; the present disclosure can be formed in accordance with an embodiment of the method illustrated in FIG. A semiconductor structure fabricated in a bonded semiconductor structure; FIG. 6 is a flow chart showing a flow of a procedure of other example embodiments of a method of forming a bonded semiconductor structure in the present disclosure; and FIGS. 7A through 7E A bonded semiconductor structure in accordance with one embodiment of the method illustrated in FIG.于成 [Main component symbol description] 100 first semiconductor structure 100, first semiconductor structure 102 transistor 104 conductive via 106 conductive trace 108 bonding pad 108, bonding pad 109 bonding surface 110 active surface 112 bulk material 115 exposed surface 116 Cap layer 130 recess 132 metal 134 exposed surface 162378.doc -49- £ 201241937 200 second semiconductor structure 204 conductive via 206 conductive trace 208 conductive metal bond pad 212 bulk material 220 bonding surface 300 bonded semiconductor structure 300' bonded semiconductor structure 400 first semiconductor structure 402 transistor 404 conductive via 406 conductive trace 408 bond pad 410 active surface 412 non-conductive bulk material 420 bonding surface 430 recess 432 metal 434 exposed surface 436 void 500 second Semiconductor structure 504 conductive via 506 conductive trace 508 conductive metal bond pad 162378.doc -50- 201241937 520 536 600 joint surface void bonded semiconductor structure 162378.doc -51 -
Claims (1)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/076,745 US8716105B2 (en) | 2011-03-31 | 2011-03-31 | Methods for bonding semiconductor structures involving annealing processes, and bonded semiconductor structures and intermediate structures formed using such methods |
| FR1153081A FR2973937B1 (en) | 2011-04-08 | 2011-04-08 | METHODS OF BONDING SEMICONDUCTOR STRUCTURES COMPRISING ANNEALING PROCESSES, AND BOUND SEMICONDUCTOR STRUCTURES AND INTERMEDIATE STRUCTURES FORMED BY MEANS OF SUCH PROCESSES |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| TW201241937A true TW201241937A (en) | 2012-10-16 |
| TWI471951B TWI471951B (en) | 2015-02-01 |
Family
ID=45876783
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| TW101108739A TWI471951B (en) | 2011-03-31 | 2012-03-14 | Semiconductor structure bonding method including annealing process, bonded semiconductor structure, and intermediate structure formed using the same |
Country Status (2)
| Country | Link |
|---|---|
| TW (1) | TWI471951B (en) |
| WO (1) | WO2012130730A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI826009B (en) * | 2018-05-14 | 2023-12-11 | 美商艾德亞半導體接合科技有限公司 | Structures for bonding elements |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3011679B1 (en) * | 2013-10-03 | 2017-01-27 | Commissariat Energie Atomique | IMPROVED METHOD FOR DIRECT COLLAR ASSEMBLY BETWEEN TWO ELEMENTS, EACH ELEMENT COMPRISING METAL PORTIONS AND DIELECTRIC MATERIALS |
| US10002844B1 (en) | 2016-12-21 | 2018-06-19 | Invensas Bonding Technologies, Inc. | Bonded structures |
| US10508030B2 (en) | 2017-03-21 | 2019-12-17 | Invensas Bonding Technologies, Inc. | Seal for microelectronic assembly |
| US11380597B2 (en) | 2017-12-22 | 2022-07-05 | Invensas Bonding Technologies, Inc. | Bonded structures |
| US12374641B2 (en) | 2019-06-12 | 2025-07-29 | Adeia Semiconductor Bonding Technologies Inc. | Sealed bonded structures and methods for forming the same |
| CN119381371A (en) * | 2024-10-29 | 2025-01-28 | 武汉新芯集成电路股份有限公司 | Semiconductor device and method for manufacturing the same |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050003652A1 (en) * | 2003-07-02 | 2005-01-06 | Shriram Ramanathan | Method and apparatus for low temperature copper to copper bonding |
| US7193323B2 (en) * | 2003-11-18 | 2007-03-20 | International Business Machines Corporation | Electroplated CoWP composite structures as copper barrier layers |
| US20060003548A1 (en) * | 2004-06-30 | 2006-01-05 | Kobrinsky Mauro J | Highly compliant plate for wafer bonding |
| FR2872625B1 (en) * | 2004-06-30 | 2006-09-22 | Commissariat Energie Atomique | MOLECULAR ADHESION ASSEMBLY OF TWO SUBSTRATES, ONE AT LEAST SUPPORTING ELECTRICALLY CONDUCTIVE FILM |
| US7354862B2 (en) * | 2005-04-18 | 2008-04-08 | Intel Corporation | Thin passivation layer on 3D devices |
| US8716132B2 (en) * | 2009-02-13 | 2014-05-06 | Tokyo Electron Limited | Radiation-assisted selective deposition of metal-containing cap layers |
-
2012
- 2012-03-14 TW TW101108739A patent/TWI471951B/en not_active IP Right Cessation
- 2012-03-22 WO PCT/EP2012/055119 patent/WO2012130730A1/en not_active Ceased
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI826009B (en) * | 2018-05-14 | 2023-12-11 | 美商艾德亞半導體接合科技有限公司 | Structures for bonding elements |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2012130730A1 (en) | 2012-10-04 |
| TWI471951B (en) | 2015-02-01 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8716105B2 (en) | Methods for bonding semiconductor structures involving annealing processes, and bonded semiconductor structures and intermediate structures formed using such methods | |
| US8501537B2 (en) | Methods for bonding semiconductor structures involving annealing processes, and bonded semiconductor structures formed using such methods | |
| US12154880B2 (en) | Method and structures for low temperature device bonding | |
| JP2025509316A (en) | Expansion control for bonding | |
| TWI458072B (en) | Method for directly bonding semiconductor structures together and adhesive semiconductor structures formed by applying the same | |
| TW202341359A (en) | Controlled grain growth for bonding and bonded structure with controlled grain growth | |
| JP2024501559A (en) | Structures with conductive features and methods of forming the same | |
| JP2024513304A (en) | Contact structure for direct bonding | |
| TW201241937A (en) | Methods for bonding semiconductor structures involving annealing processes, and bonded semiconductor structures and intermediate structures formed using such methods | |
| TWI234814B (en) | Method of manufacturing a semiconductor device | |
| US8778773B2 (en) | Methods for directly bonding together semiconductor structures, and bonded semiconductor structures formed using such methods | |
| US20120161320A1 (en) | Cobalt metal barrier layers | |
| TWI619171B (en) | Barrier layer | |
| TW201030855A (en) | Method for improving electromigration lifetime of copper interconnection by extended post anneal | |
| TW546772B (en) | Method of manufacturing a semiconductor device | |
| TWI506699B (en) | Method for bonding semiconductor structures involving annealing treatment and bonded semiconductor structures formed using such methods | |
| TW201225230A (en) | Method for segregating the alloying elements and reducing the residue resistivity of copper alloy layers | |
| FR2973934A1 (en) | Method for bonding semiconductor structures e.g. dies and wafer used in manufacturing of semiconductor device, involves subjecting bonded metal structure to thermal budget and annealing the bonded metal structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | Annulment or lapse of patent due to non-payment of fees |