TW200922852A - Load lock fast pump vent - Google Patents
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- TW200922852A TW200922852A TW97118332A TW97118332A TW200922852A TW 200922852 A TW200922852 A TW 200922852A TW 97118332 A TW97118332 A TW 97118332A TW 97118332 A TW97118332 A TW 97118332A TW 200922852 A TW200922852 A TW 200922852A
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Abstract
Description
200922852 九、發明說明: 【發明所屬之技術領域】 本發明係關於一種控制式常壓環境,更詳細而言係關於在 該環境下之生產率增進。 【先前技術】 電子組件之生產業界,尤其是構成更為精進之電子組件之 半導體裝置之生產業界均冀望取得效率提昇。 通過採用群集工具同時使組件數目及組裝體之複雜度減為 最低之方式使應用靜定加載互鎖室冷卻套之熱晶圓之生產率最 適化,尤其可減免加載互鎖室内之任何活動/裝置。傳統方式係 採用複數加載互鎖室模組以取得群集工具之較高生產率。此舉 將增加裝備複雜度與最終用戶之成本。 一般上在半導體加工系統中係採用常壓門以密封加載互鎖 室與諸如裝備前端模組(EFEM)或加載埠模組上之常壓介面之間 之晶圓縫隙開口。常壓門通常係藉液壓驅動作垂直移動以覆蓋 縫隙開口。然後該常壓門係被驅動與縫隙開口周邊之加載互鎖 室密封接觸面進行接觸以密封開口與外界氛圍。 在密封加載互鎖室接觸面時,破損之門封,失效之門活動 及外來雜質等均可能損毁加載互鎖室接觸面而在加載互鎖室被 抽下時造成漏入加載互鎖室内。加載互鎖室密封接觸面之維修 非常耗時及耗費人力,表面必須重新切削車光或磨砂以產生初 始之表面狀況。密封接觸面之重新加工可能需要耗費數小時而 造成加工工具之停機時間劇增。當密封接觸面無法維修時將需 要替換加載互鎖室。 5 200922852 宜在加载互鎖室上設置一常壓門接觸面以供快速更換以使 加工工具停機時間減為最短。 當基板從諸如一加工模組轉移至加載互鎖模組或反向逆行 時防護基板以免受到微粒污染係半導體基板製造過程中之—項 重要事項。為了使基板受污染程度減為最低,基板運送模組之 所有活動組件一般係設在基板路徑下方。 通常習用於基板加工裝備之常壓門與有槽閥係包括(但不 限於)設置在基板轉移平面下方之加載互鎖室以使基板之空氣 挾帶微粒污染減為最低。諸如採用疊置或雙加載互鎖常壓門及 有槽閥安裝於加載互鎖室反面之基板轉移平面上方之場合,門 啟動器係設置於基板轉移區内。當門啟動器設在基板轉移平面 上方時’由於門啟動器將導致局機率之基板微粒污染。 最好常壓門之門啟動器係不設在基板轉移平面上方或在基 板轉移區内’藉此可使基板微粒污染減為最低。 【發明内容】 本發明之第一實施例係提供一種基板加工工具。基板加工 工具包括構成至少一個隔離艙用以保持控制氛圍之—構架,設 置在各該至少一個隔離擒内之至少二個基板支承,各該至少: 個基板支承係互相疊置及用以抓持相對基板及聯通性聯結於該 至少二個基板支承上之冷卻單元,於是該至少二個基板支承與 冷卻單元將啟動設置於該至少二個基板支承上之各該相對基板 之同時傳導性冷卻作用。 【實施方式】 以下將參照附圖§尤明本案實施例之上述及其他特徵。 200922852 第1A-1B圖係具有實施例特徵之一基板加工模組10之示意 透視圖。雖以下將參照附圖所示實施例予以說明,須知該實施 例亦可以多種變更態樣予以實施。此外,任何適當尺寸,形狀 或類型之元素或材料均可採用。 由第1A-1B圖可知,模組10具有可供模组配對預期數目之 加工工具部份之通用構造以對基板進行一或多項預期加工(諸 如材料鍍積,蝕刻,石版印刷,離子植入,洗淨,抛光等)。該 基板係任何適當類型者,諸如200mm,300mm,450mm直徑半 導體晶圓,光柵,平面屏幕顯示器之液面膜或屏幕。第1A-1B 圖所示之實施例之模組係一加載互鎖室模組,而在變更態樣中 之模組係任何適當類型者。實施例中所示之模組之構造僅作為 實例說明,變更態樣之加載互鎖室模組可具有任何其他預期構 造。 其中一實施例之加載互鎖室模組10係如第2及第3圖所示 聯通於加工工具之不同部份之間。各該不同部份可具有不同氛 圍(例如一側為惰性氣體而另一側為真空,或一側為大氣清淨 空氣而另一側為真空/惰性氣體)。如第2圖係顯示諸如一實施例 之半導體工具站690之加工裝置。雖然圖中係顯示一種半導體 工具,本實施例可應用於任何工具站或採用機人操縱器之應 用。本實施例之工具690係示為一種群組工具,然而此實施例 可應用於任何適當工具站,諸如第3圖所示線性工具站及見述 於2006年5月26曰提出申請之美國專利申請案第11/442,511 號,“線性分佈半導體工作件加工工具”一文,以下將援引作為 本案參考。工具站690 —般係包括一常壓前端部600, 一加載互 7 200922852 鎖真空室610及一真空後端部620。變更態樣之工具站可具有任 何適當構造。各該前端部600,加載互鎖室610及後端部620 可連接至控制器691作為諸如群組設計控制之任何適當控制設 s十之一部伤。控制系統係具有主控制器,群組控制器及自動遙 控器之封閉迴路控制器,諸如2005年7月11日提出申請之美 國專利申請案第11/178,615號,以下將援引作為本案參考,變 更態樣中可採用任何適當控制器及/或控制系統。 / 實施例之前端部600 一般係包括有加載埠模組605及諸如 裝備前端部模組(EFEM)等之微型環境660。加載埠模組605係 工具標準(BOLTS)介面之開盒器/加載器,符合3〇〇mm加載埠, 前端開口或底部開口盒/容器及匣盒之SEMI標準E15.1,E47.1, E62,E19.5或E1.9。變更態樣之加載埠模組係設計為2〇〇mrn晶 圓介面或任何其他適當基板介面,諸如平面屏幕顯示器之較大 或較小晶圓或平面屏幕等。雖然在第2圖中係顯示有二個加載 埠模組,然而變更態樣可將任何適當數目之加載埠模組加入前 端部600。加載埠模組605可設計以承納來自高架運送系統,自 I. 動導引機動車,人工導引機動車,軌道導引機動車或任何其他 , 適當運送方式之基板載具或匣盒650。加載埠模組605可通過加 載埠640與微型環境660連接。加載埠640可允許基板通過基 板匣盒650及微型環境660之間之通道。微型環境660 —般係 包括一轉移機器人(未予圖示)以將基板從匣盒65〇運送至諸 如加載互鎖室610。其中一實施例中之轉移機器人係一種軌跡安 裝機器人,如美國專利案第6,002,840號所揭述者,以下將援引 作為本案參考。該微型環境660可提供基板在複數個加載埠模 200922852 組之間轉移之控制性清淨區。 加載互鎖真空至610係大致類似第ia_if圖所示之模組 10,並可設在微型環境660與後端部620之間及連接於其上。 加載互鎖室610之基板保持艙一般係包括有類似以下將述之閥 12,13 (見第4A圖)方式之常壓與真空有槽閥。圖中所示之有 槽閥係彼此對齊或呈大約180度隔距,而變更態樣之有槽閱可 能呈大約90度隔距以形成具有大致約為9〇度角之基板運送路 仏另變更態樣之有槽閥係具有任何適當之空間關係。艙室 之各有槽閥係由有槽閥之適當門提供獨立關閉性。有槽閥可提 供環境隔離作為加載互鎖室610從常壓前端部6〇〇加載一基板 後之抽氣及在排出互鎖室之諸如氮氣等惰氣時維持運送艙 内之真空。參照第2圖,其中一實施例之加載互鎖室61〇亦包 括有對準器用以將基板之基點對準至預期位置以供進行加工^ 變更態樣之加载互鎖真空室可被設置於加工裝置之任何適當位 置,並可具有任何適當構造,包括任何適當基板加工設備。200922852 IX. DESCRIPTION OF THE INVENTION: TECHNICAL FIELD OF THE INVENTION The present invention relates to a controlled atmospheric environment, and more particularly to productivity enhancement in such an environment. [Prior Art] The manufacturing industry of electronic components, especially the semiconductor devices constituting more advanced electronic components, is expected to achieve efficiency improvements. Optimize the productivity of hot wafers that use statically loaded lock chamber cooling jackets by using cluster tools while minimizing component count and assembly complexity, especially for any activity/device in the load lock chamber . The traditional approach is to use multiple load lock chamber modules to achieve higher productivity of cluster tools. This will increase the complexity of the equipment and the cost of the end user. A normal pressure gate is typically employed in a semiconductor processing system to seal a wafer gap opening between a load lock chamber and an atmospheric interface such as an equipment front end module (EFEM) or a load port module. The normal pressure door is usually vertically moved by a hydraulic drive to cover the slit opening. The atmospheric door is then driven into contact with the load lock chamber sealing contact surface around the slit opening to seal the opening from the outside atmosphere. When sealing the contact surface of the interlocking chamber, the broken door seal, the failed door activity and foreign matter may damage the contact area of the load lock chamber and cause leakage into the load lock chamber when the load lock chamber is removed. Repair of the load lock chamber sealing contact surface is very time consuming and labor intensive, and the surface must be re-cut or burned to create an initial surface condition. Reprocessing of the sealing contact surface can take several hours and cause a significant increase in downtime for the processing tool. The load lock chamber will need to be replaced when the seal contact surface is not serviceable. 5 200922852 A normal pressure door contact surface should be placed on the load lock chamber for quick replacement to minimize tool downtime. The substrate is protected from the importance of particulate contamination in the fabrication of semiconductor substrates when the substrate is transferred from, for example, a processing module to a load-lock module or reverse retrograde. In order to minimize contamination of the substrate, all of the active components of the substrate transport module are typically disposed below the substrate path. Commonly used and grooved valve systems commonly used in substrate processing equipment include, but are not limited to, load lock chambers disposed below the substrate transfer plane to minimize airborne particulate contamination of the substrate. The door actuator is disposed in the substrate transfer zone, such as with a stacked or double load interlocking normal pressure gate and a slotted valve mounted over the substrate transfer plane opposite the reverse side of the load lock chamber. When the door actuator is placed above the substrate transfer plane, the substrate actuator will cause localized particle contamination. Preferably, the door actuator of the normal pressure door is not disposed above the substrate transfer plane or within the substrate transfer area, thereby minimizing substrate particulate contamination. SUMMARY OF THE INVENTION A first embodiment of the present invention provides a substrate processing tool. The substrate processing tool includes at least one isolation frame for maintaining a control atmosphere, and at least two substrate supports disposed in each of the at least one spacer, each of the at least one substrate support being stacked on each other and used for grasping The opposite substrate and the cooling unit coupled to the at least two substrate supports, wherein the at least two substrate supporting and cooling units simultaneously activate the opposite cooling substrates disposed on the at least two substrate supports . [Embodiment] The above and other features of the embodiment of the present invention will be hereinafter described with reference to the accompanying drawings. 200922852 1A-1B is a schematic perspective view of a substrate processing module 10 having one of the features of the embodiment. Although the following description will be made with reference to the embodiments shown in the drawings, it should be understood that the embodiments may be embodied in various modifications. In addition, any suitable size, shape or type of element or material may be employed. As can be seen from Figures 1A-1B, the module 10 has a common configuration for the module to pair the desired number of processing tool portions to perform one or more desired processing on the substrate (such as material plating, etching, lithography, ion implantation). , wash, polish, etc.). The substrate is of any suitable type, such as 200 mm, 300 mm, 450 mm diameter semiconductor wafers, gratings, liquid film or screens for flat screen displays. The modules of the embodiment shown in Figures 1A-1B are one loaded with an interlocking chamber module, and the modules in the modified form are of any suitable type. The construction of the modules shown in the embodiments is described by way of example only, and the modified load lock chamber module can have any other desired configuration. The load lock chamber module 10 of one embodiment is connected between different portions of the processing tool as shown in Figures 2 and 3. Each of the different portions may have a different atmosphere (e.g., one side is an inert gas and the other side is a vacuum, or one side is atmospheric clean air and the other side is vacuum/inert gas). Figure 2 shows a processing apparatus such as a semiconductor tool station 690 of an embodiment. Although a semiconductor tool is shown in the drawings, the present embodiment is applicable to any tool station or application using a manipulator. The tool 690 of the present embodiment is shown as a group tool, however this embodiment can be applied to any suitable tool station, such as the linear tool station shown in FIG. 3 and the US patent filed on May 26, 2006. Application No. 11/442,511, “Linear Distributed Semiconductor Workpiece Processing Tools”, which is hereby incorporated by reference. The tool station 690 generally includes a constant pressure front end portion 600, a load mutual 7 200922852 lock vacuum chamber 610 and a vacuum rear end portion 620. The tool station of the modified aspect can have any suitable configuration. Each of the front end portion 600, the load lock chamber 610 and the rear end portion 620 can be coupled to the controller 691 as one of the appropriate control devices, such as group design control. The control system is a closed loop controller having a main controller, a group controller, and an automatic remote controller, such as U.S. Patent Application Serial No. 11/178,615, filed on Jul. 11, 2005, which is incorporated herein by reference. Any suitable controller and/or control system can be employed in the aspect. The front portion 600 of the prior embodiment typically includes a loading cassette module 605 and a micro environment 660 such as an equipment front end module (EFEM). Loaded 埠 module 605 is the opener/loader of the tool standard (BOLTS) interface, which conforms to 3mm load 埠, SEMI standard E15.1, E47.1 for front opening or bottom open box/container and cassette. E62, E19.5 or E1.9. The modified loading module is designed as a 2 〇〇mrn crystal interface or any other suitable substrate interface, such as a larger or smaller wafer or flat screen of a flat screen display. Although two loading cassettes are shown in Figure 2, the modified aspect can add any suitable number of loading cassette modules to the front end 600. The loading cassette module 605 can be designed to receive a substrate carrier or cassette 650 from an overhead transport system, from an I. moving guided motor vehicle, a manually guided motor vehicle, a track guided motor vehicle, or any other suitable transport method. . The loading cassette module 605 can be coupled to the micro environment 660 via an loading port 640. Loading the crucible 640 allows the substrate to pass through the channel between the substrate cassette 650 and the microenvironment 660. Microenvironment 660 typically includes a transfer robot (not shown) for transporting substrates from cassette 65 to, for example, load lock chamber 610. The transfer robot in one of the embodiments is a trajectory mounting robot, as disclosed in U.S. Patent No. 6,002,840, which is incorporated herein by reference. The microenvironment 660 provides a controlled cleansing zone for the substrate to be transferred between a plurality of loaded die 200922852 groups. The interlocking vacuum is loaded to the 610 system substantially similar to the module 10 shown in the ia_if diagram and may be disposed between and connected to the microenvironment 660 and the rear end portion 620. The substrate holding chamber of the load lock chamber 610 typically includes a normal pressure and vacuum slotted valve in a manner similar to the valves 12, 13 (see Figure 4A) described below. The slotted valves shown are aligned with each other or at approximately 180 degrees apart, and the modified aspects may have a groove of approximately 90 degrees to form a substrate transport path having an angle of approximately 9 degrees. The modified slotted valve system has any suitable spatial relationship. Each slotted valve of the compartment is independently closed by a suitable door with a slotted valve. The slotted valve provides environmental isolation as the load lock chamber 610 draws air from a normal pressure front end portion 6 〇〇 and maintains a vacuum in the transport chamber when exhausting an inert gas such as nitrogen from the interlock chamber. Referring to FIG. 2, the load lock chamber 61 of one embodiment also includes an aligner for aligning the base point of the substrate to a desired position for processing. The load lock chamber can be set to Any suitable location of the processing device, and can have any suitable configuration, including any suitable substrate processing equipment.
真空後端部620 一般係包括有運送艙625, 一或多個加工站 63〇及一轉移機器人(未予圖示)。轉移機器人係設在運送艙625 内以將基板運送於加載互鎖室610與各個加工站630之間。加 工站630可通過各種鑛積,姓刻,或其他類型之加工作業 行基板作業而構成電子電路或其他職結構於基板h典 :作”括(但不限於)採用諸如電漿蝕刻或其他蝕刻作 植ΐ學蒸鐘(CVD),電漿蒸鑛(PVD)’諸如離子 鐘積(ALD),氧化/^作業,快速熱處理(RTP),乾條帶原子層 乳化/擴政,形成氮化物,真空電版印刷,晶體衍 9 200922852 生(EPI) ’絲銲及蒸發或採用真空壓之其他薄膜加工作業,加工 站630係連接於運送艙625以供基板通過運送艙625至加工站 630或逆向方式。 第3圖係顯示具有不同部份之基板加工工具71〇之另一實 例。本實施例中之加工工具係一種線性加工工具,其中工具介 面部712係安裝於運送艙模組718上使介面部712係面向(例 如朝内)但偏離運送艙718之縱轴X。運送搶模組71g係將另The vacuum rear end portion 620 generally includes a transport compartment 625, one or more processing stations 63A, and a transfer robot (not shown). The transfer robot is disposed within the shipping bay 625 to transport the substrate between the load lock chamber 610 and the various processing stations 630. The processing station 630 can form an electronic circuit or other structure on the substrate through various mineral deposits, surnames, or other types of processing operations, such as (but not limited to) using such as plasma etching or other etching. Phytosanitary steam (CVD), plasma distillation (PVD) such as ion clock (ALD), oxidation / ^ operation, rapid thermal processing (RTP), dry strip atomic layer emulsification / expansion, formation of nitride , vacuum electro-printing, crystal derivative 9 200922852 (EPI) 'Wire welding and evaporation or other film processing operations using vacuum pressure, processing station 630 is connected to the transport compartment 625 for the substrate to pass through the transport compartment 625 to the processing station 630 or In the reverse mode, Fig. 3 shows another example of a substrate processing tool 71 having different portions. The processing tool in this embodiment is a linear processing tool in which the tool interface portion 712 is mounted on the shipping compartment module 718. The mediator face 712 is oriented (eg, facing inward) but offset from the longitudinal axis X of the transport compartment 718. The transport grab module 71g will be another
一運送驗模組718A ’ 7181,718J附接於介面750,760,770以 作任何適當方向之伸展,如前所援引作為參考之美國專利申請 案第11/442,511號所揭述。該介面75〇,76〇,77〇係大致類似 文中所述之加載互鎖室1〇。各運送艙模組718,719A , 7181, 718J包括有適當基板運送裝置78〇以運送基板通過加工系統 710及進出諸如加工模組pM。由此可知,各艙室模組可用以維 持隔離或控制性氛圍(例如N2,清淨空氣,真空等)。變更態 樣之運送艙模組718,719A,718I,而可包括文中所述之二 載互鎖室1〇之特徵。 _再參照第1A及1B圖,加載互鎖室模組1〇可聯通各具有不 :氛例如-側為惰性氣體而另-側為真空,或-側為常壓 清淨空氣而另_側為真空/惰性氣體)之加工工具之不同部份(未 予圖不加載互鎖线組1G將形成數個基板維持搶Μ, 、先稱為艙室⑷,以下將予詳述,各可予以隔離及可且有 結模組之"'具部份中之氛圍之驗室氛圍循環。雖然i圖 中僅顯不二個基板維躲14A,14B,須知加載互鎖室触κ 可具有多或少過二個基板維持艙。實施例中之加載互鎖室模組 10 200922852 艙14係φ λ以提供艙室氛圍之快速循環,以下將予詳述。再參 ’、’、第1C 1Ε圖’基板維持艙14可具有設在模組侧面之基板運送 開口 16’ 18。圖中所不之運送開口 16, 18之位置僅作為實例說 明’而變更態樣之臉室可與在模組任何其他預期側面(例如她 鄰侧面)聯通。驗至之各運送開口係由適當門有槽閥η,13予 以獨立開關。 第2Α-2Β圖分別顯示模組1〇之斷面圖,實施例中之内部模 組可形成二個或更多獨立_及可循環之基板維持擒“a, 14b實施例中之艙室係呈蕈形配置。該二搶室係屬密實擒室, 以下將予4明。變更態樣之整合式模組具有更多或更少繪室。 實把例中之餘至各具有由諸如設在模組共同側面之適當闊12, 13 (例如㊅壓與真空有槽閥)予以控制之獨立開關式開口。於 是基板通過各艙室之運送方向係沿著大致平行之轴,更態樣 之艙至具有設在模組不同側面之對應運送開口。實施例之閥(例 如設計為可卸離式連接(例如螺固式)模組)可設在由模組構 成之艙室部之外侧。 第4A-4B圖分別顯示模組1〇之斷面,實施例之模組1〇内 部可形成二或多個獨立隔離及/或循環式基板維持艙 14A,14B » 實施例中之艙室14A,14B係呈蕈形配置。變更態樣之艙室係並 排配置或任何其他適當之相互間之空間配置。如前所述,該二 艙至14A,14B係密實艙室。變更態樣之整合式模組可具有更多 或更少艙室。實施例之艙室各具有設在模組相對侧面之由諸如 適當閥12,13 (例如常壓及真空有槽閥)控制之獨立開關式運 送開口 14AO,14BO (見第1B圖)。於是基板通過各艙室之運 200922852 送方向係沿著大致平行軸。在一實施例中,艙室14A,14B係經 設計使通過各艙室14A,14B之運送方向係雙向者。另一實施例 之艙室係經設計使基板通過其中一個艙室14A,14B之運送方向 係與基板通過另一個艙室14A,14B之運送方向不同《作為非限 制性實例,艙室14A可允許基板從一前端單元轉移至加工工具 之後端部之加工艙室,而艙室14B可允許基板從加工艙室轉移 至前端部單元。參照第2及第3圖之前述說明,變更態樣之艙 室在模組不同侧面可設有對應之運送開口。各艙室14A,14B 及其相對有槽閥12,13係獨立操作,例如在其中一艙室14A, 14B之基板係被冷卻而另一艙室HA,14B可放置或移走基板。 實施例之閥12,13係經設計為卸離式連接性(例如螺固或 其他適當脫接性連接)模組,可設置於由模組10形成之艙室部 份14A,14B之外側。變更態樣之閥模組係可脫接式整合於模組 10之壁體内’以下將予詳細說明。另一變更態樣之閥或閥之一 部份係無法與模組10脫離者。 第1F圖顯示模組1〇之分解圖(頂部與底部封蓋2〇,22係 未予圖示以利圖解)。實施例之模組備有一般之中心或骨架構架 30,及頂部與底部蓋體32, 34。實施例之構架3〇係由諸如鋁合 金等任何適當材料製成之一件式構件(例如單體構造)。變更態 樣之構架係一組裝體,並可由任何適當材料或任何數目之部份 作成。如第1F圖所示,實施例中之構架3〇 一般將形成模組外 周面及艙室周邊。如第1F圖及第4A圖所示之腹板構件w可將 模組10分段以形成疊置艙室。變更態樣之艙室可具有超過一個 腹板構件W。另一變更態樣之疊置艙室可藉任何適當方式構 12 200922852 成。舉例而言,模組ίο具有通用開口可供艙室次模組鑲嵌,該 . 艙室次模組包括具有任何數目之艙室之疊置艙室。由此可知, 艙室14A,14B可藉封蓋32,34關閉其頂部及底部,該封蓋係 藉諸如(但不限於)機械,電子及/或化學固定器等任何預期連 接方式配對於構架30上。有槽閥12,13之介面係以諸如圖示 • 及以下將予詳述之方式等之任何適當方式配對於構架30。加載 互鎖室模組10係一種提供基板在其所連結之工具部件之間轉移 之聯通模組。因此模組10之高度必須與毗連部件或模組之高度 相關連,並取決於基板運送裝置在毗連模組之行進軸z等因素 (通過加載互鎖室模組之通過率,並由諸如模組之尺寸或z-驅 動及/或結構考量等因素予以定界)。貫通模組10與旋轉模組15 之間之關係係示於第6圖,其中係顯示加載互鎖室模組10配對 於群組工具之基板運送艙7。由此可知,當模組10之高度比運 送裝置之有效z-行進更高時,將導致不穩定之加載互鎖室容積 而增加抽取/排氣時間。同理,當模組高度比有效z-行進更低時, 將無法運用運送裝置之整體有效行進頻寬,因而將限制加載互 i 鎖室模組之生產率。實施例之加載互鎖艙室14A,14B之特徵將 ' 構成可提供疊置之加載互鎖艙室在模組10内形成之高度之構 造。如前及第4A-4B圖所示,實施例之二加載互鎖艙室14A, 14B係呈疊置配置於模組10内,而變更態樣之單體模組内之加 載互鎖艘疊置可包括更多(或更少)加載互鎖搶室,例如三個 或更多個艙室。由此可知,在共同模組10之密實空間封套内提 供複數個獨立加載互鎖艙室14A,14B將產生複數個獨立及不受 偈限之運送路徑,模組10之生產率有同等增加。第1A-1E圖所 13 200922852 不實把例中,各加載互鎖艙室14A,14B係大致彼此類似》在其 中一實施例中,加載互鎖艙室14A,14B沿著分隔加載互鎖室之 中間平面有對立構造。變更態樣之加載互鎖室可能互不相同, 用以操持不同尺寸及或類型之基板。第1F圖所示之模組10具 有模ja化配置’可供加載互鎖室由類似或不同之構造安裝組 成。實施例之加載互鎖艙室14A,14B具有足以容納數個疊置基 板(第4&4b圖中顯示在各艙室中有二個基板)之高度。變更 態樣之加栽互鎖艙室14A,14B可容納預期之更多或更少疊置基 板。 再參照第4A-4B圖,實施例中各加載互鎖搶室i4A,14B 可具有個加熱裝置或一個冷卻裝置,或兩者兼具,以在加載 互鎖室氛圍在循環時對其内所容納之基板進行加熱或冷卻。加 載互鎖室之—適當實例具有以下將述之冷卻/加熱特徵。如第4A 圖所示,實施例之各加載互鎖室具有支承架22A,22B通過傳導 性等方式對基板進行熱處理作業。實施例之支承架22A,22B 係經設計以在諸如加載互鎖室排氣期間進行基板之冷卻。舉例 而言’支承架可藉任何預期方式連接諸如冷卻區塊27等之適當 熱處理槽以在各支承架22A,22B之上側面形成基板冷卻表面 24A’ 24L其中一實施例之冷卻區塊27包括有輻射翼片(未予 圖示)以提供基板冷卻表面24A,24B之溫度轉移,而另一實施 例之冷卻區塊具有冷卻液在其内流動以吸取基板冷卻表面 24A ’ 24B之熱量。再一實施例中之冷卻區塊27具有輻射翼片 與冷卻液流之組合。變更態樣之支承架具有一基板加熱表面。 另一變更態樣中之加載互鎖室係經設計以加熱加載互鎖室内之 14 200922852 氣體。 實施例中各加載互鎖室設有具備冷卻表面24a,24b之二個 支承架22A,22B (然而如前所述可提供更多或更少晶圓冷卻表 面)。由此可知,通過在基板與支承架以,22B之冷卻表面之 間之傳導之熱交換可藉基板坐設於支承架ΜΑ.之冷卻表面 24A ’ 24B而達成。實施例中之支承架係―固態裝置(例如不設 有傳動性/活動性機械組件)。此舉何提供支承架Μa,22B最少 樣式及高度(於是有助於提供加載互鎖室之密實高度)。作為實 例說明,支承架22Α,22Β係相對於構架部30呈固定或靜定, 並具有大約10mm之高度足以允許利用運送裝置之末端作用器 EE從坐s又狀態直接抓取及放置基板於冷卻表面24A,上以 1/ 將基板轉移自/至加載互鎖室14A,14B (見第5A-5B圖及第ό 圖)。變更態樣之支架可具有任何適當高度。另一實施例之支承 架22Α,22Β係可相對於構架部30移動以使支架之高度可根據 支架22Α,22Β之間之預定距離予以調整。如第4Β圖所示,支 承架22A ’ 22Β係配置形成末端作用器ΕΕ之通道空隙26。實施 例之支承架22A ’ 22B可分段形成空隙26以供容納末端作用器 葉片。該空隙26可提供末端作用器之z運動以抓取及放置基板 於冷卻表面。作為實例說明,末端作用器EE可大致同時放置基 板於支承架22A,22B (在其中一個疊置加載互鎖室上)之冷卻 表面24A,24B上。例如當加載互鎖室在排氣之同時可冷卻基 板。經過冷卻之基板可大致同時從加載互鎖室22A上被抓取及 運送。當基板在其中一個加載互鎖室14A,14B中進行冷卻時, 另一個(加載互鎖室模組10之)加載互鎖室14A,14B之操作 15 200922852 係以大致未侷限方式進行。變更態樣中,各加載互鎖室所進行 之操作係以任何適當方式按照順序互相聯結。 再參照第1Α-1Β囷,實施例中各加載互鎖室14Α,14Β (亦 見第4Α,4Β圖)具有對應之真空控制閥4〇Α,4〇Β及排氣閥 42Α,42Β (諸如設有或不設有擴散器者)以提供相對加載互鎖 室氛圍之獨立循環。實施例之真空控制閥4〇Α,40Β及排氣閥 42Α,42Β可設置於模組中作為彼此互換性,以下將予詳述。再 參照第1F圖,實施例之構架部3〇具有璋口 36Α,36Β,37Α, 37Β。該珲口將在各加載互鎖室14Α,14Β中形成相對之真空埠 口 36Α,36Β及排氣琿口 37Α,3*7Β。圖中所示之排氣與真空埠 口之配置僅作為實例說明,而變更態樣之排氣與真空埠口可具 有任何其他適當配置。實施例之真空埠口 36Α,36Β係設置於模 組10之一側,而排氣埠口 37Α,37Β係設置於模組1〇之不同側。 變更態樣之排氣與真空埠口可設置於模組之同一側。如第1F圖 所示,相對加載互鎖室14Α’ 14Β之真空與排氣埠口 36Α,37Α , 36Β,37Β係彼此呈垂直偏離。變更態樣之真空與排氣埠口係彼 此垂直對齊或具有任何其他空間關係。各埠口具有適當配對介 面(例如淳口周圍)以利將預期之真空或排氣閥連接於碑·口(及 模組)。實施例中相對埠口之二個或更多配對介面38Α,38Β, 39Α,39Β可設計成具有大致類似配對之配置(例如配對凸緣, 密封面,螺合樣式等)以供具有互補配對介面之任何閥可與任 何埠口之配對介面配對。舉例而言’如第1Β及if圖所示,排 氣閥可併合於排氣閥模組42Α,42Β,各具有類似配對介面421 以供任一模組可互換性安裝於任一艙室之排氣埠口介面。實施 16 200922852 例中具有單體構造之壓力罩箱或保護罩之排氣_m2a,42b 可包括排㈣本體42VB以提供;j;同流動速率或控制構造(例如 節流閥及/或不同容量之箱閥)。實施例係針對個別排氣與真空埠 口予以說明,而其他實施例之閥可經設計以通過單一蟑口從搶 室排氣及抽氣。例如該閥可設計具有適當閥特性以轉換於真空 源與排氣源之間。另一變更態樣中之各模組具有一排氣及真空 埠口,利用單一排氣/真空模組可進行艙室之排氣及/或抽氣。 圖示實施例中之排氣閥模組罩箱42A,42B可允許安裝具有 共同來源及共同排出口之三個閥本體42 VB。該閥模組42 A,42B 係經設計以提供任何預期數目之閥本體42 VB以達至任何預期 之預定閥形體。變更態樣之模組本體42A,42B可容納更多或更 少之閥。排氣模組42A ’ 42B,42A’之不同實施例係顯示於第 1A-1F圖及第8A-8D圖。圖中所示之排氣模組之實施例僅作為 實例說明’而排氣模組可具有任何適當模組本體42AB構造以將 排氣模組連接於諸如氣體入口,閥本體42VB,及擴散器44A 等。然而具有不同模組本體42AB及閥42VB之不同模組可能共 用共同配對介面配置421,於是可允許加載互鎖室1〇之排氣模 級42A,42B ’ 42A’之互換性。實施例之排氣閥模組42A,42B 亦可包括適當擴散器44A,當安裝閥模組42A,42B於加載互鎖 室之排氣埠口 37A,37B時,擴散器44A可大致設置於進入加 栽互鎖室之排氣埠口之排出面上或近處。其中一實施例之排氣 閥模組42A,42B係經設計以接收及/或固定擴散器44A於凹部 (或模組本體42AB上之其他適當凹槽或槽口)。變更態樣之擴 散器可加入或固定於諸如加載互鎖室10之壁體之排氣埠口 17 200922852 36A,37A,36B,37B 上。 第7A-7B圖分顯示另一實施例之模組1〇,之透視圖及斷面 圖。模組10’大致類似前述之模組10。圖示實施例之真空控制 閥與排氣閥可與單一模組40A’,40B’合併為一。如第7B圖所 示,模组結構具有埠口 36A’,36B’,37A,,37B,。圖示實施例 之皡口係以大致對稱配置排列,(例如如圖示般將蜂口設在兩側 壁上以供真空與排氣管道附設在模組之兩側)。於是各加載互鎖 室具有四個有效埠口以連接真空與排氣管道,諸如在各側面設 置二埠口。變更態樣中之各加載互鎖室可具有任何適當數目之 槔口,彼此之間具有適當空間關係。實施例中璋口 36A,,Mb,, 37A’,37B’之配對介面38A’,38B’,39A,,39B’係類似以提供 模组40A’,40B’之互換性。變更態樣之一或多個配對介面係非 類似性以提供介面與具有對應介面之相對模組之間之選擇互換 性。如第7B圖所示,配對介面38A,,38B,,39A,,39B,可配置 於埠口對上,其中一個設置於另一個之上。舉例而言,埠口 36八, 及36B’係設置於同__模組壁上’其中__個設在另—個之上及共 用一配對介面39A’。本實施例之各閥模組4〇A,,4〇B,係互換性 配對於任何對埠口配對介面38A,,38B,,39A,,39B,。閥模組 40A’ ’ 40B’係設計以在配對艙室模組1〇,(如帛7a_7b圖所示) 時與各該料口之各和(例如36A,,36B,)。實施射闊模組 40A 4GB具有模組本體⑽,以構成—配對介面設計以與模組 ίο配對’其中該模組本體41B,之配對介面包括相對之排氣(排 出口)與真空(入π )埠口。將—真^控制閥稱安裝於模組 本體41B’與真料口保持流Mit。_,在模組本體41B,上 18 200922852 設有一排氣閥42VB’,與排氣埠口保持流體聯通。其中— 例之閥模組配置導致一模組40A,,40B,操作以提供特定知 鎖室14A,,14B,之排氣而另一模組4〇A,,4〇B,操作以提供 互鎖室14A’,HB’之抽氣。閥模組4〇A,,働,包括有一排氣擴 散器,例如以前述方式設置。如第7八及7B圖所示,模組仞八, 及40B’係經設計使各模組與該二艙室14A’,14B,聯通。舉例而 言,模組40B’可聯結於模組1〇,使模組4〇B,進行艙室14八,之排 氣及艙室14B’之抽氣(例如通過真空進行抽氣)。模組4〇a,係 聯結於模組10’使模組40A’進行艙室14β,之排氣及艙室14A,之 抽氣》其中該加載互鎖室模組包括有一單一加載互鎖室,該單 一加載互鎖室備有抽/排氣介面,具有大致類似前述之一對排氣 與真空埠口。該對埠口可設計以與類似模組4〇A,,4〇B,之抽/ 排氣模組進行連接,使單一艙室可利用單一模組進行排氣及抽 氣以使單一加載互鎖室模組之複雜度,尺寸及成本減低或減為 最少。 第9圖顯示另一實施例之加載互鎖室模組之基板支承架 22A,22B之斷面圖。雖然在第9圖中顯示有四個支承加(如前 述在各艙室設有二支承架),以下僅將對二個支架22A,22B進 行說明。須知其餘基板支承架係大致類似於支架22A,22B。第 9圖所示之實施例中之支承架22A,22B係大致類似於前述參照 第5A及5B圖所述之支承架。該支承架22A,22B係靜定及設 置於預期距離p(例如1 〇mm或比10mm更多或更少之任何其他 適當距離)以支承基板S疊置。其中一實施例之支承架22A, 22B係可調整性及用以提供距離P之調整。另一實施例之支架 19 200922852 22A,22B係可作彼此相對移動性,以下將予詳細說明。變更態 樣之支承架22A,22B係模組化,可隨著預期距離p添加(或 移除)附加支架。實施例之各支承架22A,22B具有冷卻表面 24A,24B以對坐設在相對其中一個支架冷卻表面24A,24B上 之基板SI ’ S2進行傳導性冷卻作用。第9圖所示之實施例中, 各基板支承架22A ’ 22B可設有氣埠54 (圖示支承架數目僅作 為實例說明,而變更態樣中可設有更多或更少支承架)。該氣埠 54在第9圖中僅作示意圖示’並具有沿著支承架上分佈之任何 數目及任何預期尺寸之埠口。該氣埠54係經設計使通過埠口之 氣體係屬層流以使微粒形成減為最低。其中一實施例之氣埠54 可包括任何適當擴散器,而另一實施例之擴散器可設置於氣埠 54上游部份。變更態樣之擴散器係與相對埠口具有任何適當之 空間關係。如第9圖所示,氣埠54係設置於坐設在支承架22A, 22B之冷卻表面24A ’ 24B上之相對之上側與下側基板SI,S2 之相對下側與上側表面之間。氣埠54係通過合形成於支承架 22A,22B上之適當通道以連接適合加載立鎖室排氣(例如排出 氣體)之適當氣體供應。變更態樣之通道可能未與支承架合併 而成。如第9圖所示,氣埠54係設計以將氣體排入曝露基板表 面之間之間隙6(例如赴鄰之冷卻基板s 1,S2(見第7及9圖))。 舉例而言’一或多個支承架22A,22B具有間隙或孔口 6 (例如 類似第5B圖所示可供末端作用器進入之間隙26)使在支承架 22A上接受冷卻作用之上侧基板(升溫狀態)曝露於在支承架 22B上亦具有升溫及接受冷卻之另一下側基板。在間隙6中由 氣埠54排出之氣體將形成加熱下側基板S1與上側基板S2之未 20 200922852 覆蓋表面之間之熱隔或屏障TB (圖示尺寸與位置僅作為實例說 明)’藉此使上側基板S2受到下側基板si之對流加熱作用減為 最低或完全免除。循環氣體除了傳導性冷卻作用之外亦提供相 對於基板之對流冷卻作用。由此可知,從氣埠54Α,54排出之 氣體可能流經間隙6’中斷間隙6之停滯氣體及中斷下側熱基板 S1與上侧熱基板S2之曝露表面之間通過對流之非預期溫度轉 移。同時,由氣埠54Α,54所引入之氣體可通過諸如適當設在 艙室内(例如在空隙6或其他適當位置上)之適當真空或除氣 埠予以去除或被促使流動(產生氣體循環其中—實施例之真 空埠係以類似前述參照氣埠54之方式附設在支承架22A,22Β 上。另一實施例之真空埠可設置於支承架之間之艙室壁中,如 參照第9圖之真空埠55所述者。由於疊置基板上之冷卻分佈係 保持於基板疊置上’因此基板疊置之冷卻時間將減少。從氣埠 54’ 54A排出之氣體具有低速層流之設定雷諾係數(Re),防止前 述微粒澱積於下側基板之上側表面。 第10A及10B圖係顯示另一實施例之加載互鎖室模組1〇〇 之分解圖。模組丨〇〇係大致類似前述之加載互鎖室模組1〇。實 施例之模組1〇〇亦具有二個互相疊置之加載互鎖室U4A, 114B ’但在變更態樣中之加載互鎖室模組可具有任何適當數目 之疊置艙室。模組100亦包括冷卻夹頭12〇A,120B。各加載互 鎖室114A,ii4B具有設在其中之冷卻夾頭。冷卻夾頭120A, 120B可進行z轴運動,由適當z驅動器120Z所驅動。變更態 樣之夾頭亦可進行水平(例如X及Y)移動。夾頭120A,120B 係大致排列於如圖示之對置構造,於是夾頭在箭頭700方向之 21 200922852A transport inspection module 718A ' 7181, 718J is attached to the interface 750, 760, 770 for extension in any suitable orientation, as disclosed in U.S. Patent Application Serial No. 11/442,511, the disclosure of which is incorporated herein by reference. The interface 75 〇, 76 〇, 77 大致 is substantially similar to the load lock chamber 1 文 described herein. Each of the transport module modules 718, 719A, 7181, 718J includes a suitable substrate transport device 78 to transport the substrate through the processing system 710 and into and out of the processing module pM. It can be seen that each compartment module can be used to maintain an isolated or controlled atmosphere (e.g., N2, clean air, vacuum, etc.). The modified transport module modules 718, 719A, 718I may be characterized as including the two-load interlocking chamber 1A described herein. _ Referring again to FIGS. 1A and 1B, the load lock chamber module 1 can be connected to each other with no atmosphere: for example, the side is inert gas and the other side is vacuum, or the side is normal pressure clean air and the other side is Vacuum/inert gas) different parts of the processing tool (not shown in Figure 1G will not be loaded with interlocking wire group 1G will form several substrates to maintain the robbery, first known as the cabin (4), as will be detailed below, each can be isolated There can be a combination of the module's atmosphere with a part of the atmosphere of the laboratory. Although there are only two substrates in the i-picture to hide 14A, 14B, it is necessary to know how much more or less the load-lock chamber can touch κ. The two compartments maintain the cabin. In the embodiment, the load lock chamber module 10 200922852 cabin 14 is φ λ to provide a rapid cycle of the cabin atmosphere, which will be described in more detail below. Refer to the ', ', 1C 1Ε' substrate The maintenance compartment 14 can have a substrate transport opening 16' 18 disposed on the side of the module. The location of the transport openings 16, 18 in the figure is merely illustrative; and the altered aspect of the face can be any other expectation in the module The side (for example, her adjacent side) is connected. The inspection opening is slotted by the appropriate door. The valves η, 13 are independently switched. The second Α-2 Β diagram shows a sectional view of the module 1 ,, the internal module in the embodiment can form two or more independent _ and the recyclable substrate maintains 擒 "a, The compartments in the embodiment of 14b are in the shape of a dome. The second compartment is a compact chamber, which will be described below. The integrated module of the modified aspect has more or less painting chambers. Each has a separate switch opening that is controlled by a suitable width 12, 13 (eg, a six-pressure and vacuum slotted valve) disposed on the common side of the module. Thus, the direction of transport of the substrate through the various chambers is substantially parallel. The shaft, the more aspect of the cabin, has corresponding transport openings provided on different sides of the module. The valve of the embodiment (for example, a detachable connection (for example, a screw-on type) module) may be provided by a module. The outer side of the compartment. Sections 4A-4B show the section of the module 1〇. The module 1〇 of the embodiment can form two or more independent isolation and/or circulating substrate maintenance compartments 14A, 14B. The cabins 14A and 14B in the middle are in a dome shape. Side-by-side configuration or any other suitable spatial configuration of each other. As mentioned above, the two-chamber to 14A, 14B-based compact compartments. The integrated modular module of the modified form may have more or fewer compartments. Each has independent switch-type transport openings 14AO, 14BO (see Figure 1B) that are located on opposite sides of the module, such as appropriate valves 12, 13 (e.g., atmospheric and vacuum slotted valves). The substrate is then transported through the various compartments. 200922852 The direction of travel is along a substantially parallel axis. In one embodiment, the compartments 14A, 14B are designed such that the direction of travel through each of the compartments 14A, 14B is bidirectional. The compartment of another embodiment is designed to pass the substrate therethrough. The transport direction of one of the compartments 14A, 14B is different from the transport direction of the substrate through the other compartments 14A, 14B. As a non-limiting example, the compartment 14A may allow the substrate to be transferred from a front end unit to a processing chamber at the rear end of the processing tool, and The chamber 14B may allow the substrate to be transferred from the processing chamber to the front end unit. Referring to the foregoing description of Figures 2 and 3, the compartments of the modified aspect may be provided with corresponding transport openings on different sides of the module. Each of the compartments 14A, 14B and their associated slotted valves 12, 13 operate independently, for example, the substrates of one of the compartments 14A, 14B are cooled and the other compartments HA, 14B can be placed or removed. The valves 12, 13 of the embodiment are designed to be detachable (e.g., screw or other suitable detachment) modules that may be disposed on the outside of the chamber portions 14A, 14B formed by the module 10. The valve module of the modified state is detachably integrated into the wall of the module 10, which will be described in detail below. One of the other variants of the valve or valve is incapable of being disconnected from the module 10. Figure 1F shows an exploded view of the module 1 (the top and bottom covers 2〇, 22 are not shown for illustration). The module of the embodiment is provided with a general center or skeleton frame 30, and top and bottom covers 32, 34. The frame 3 of the embodiment is made of a piece of a member (e.g., a unitary construction) made of any suitable material, such as an aluminum alloy. The framework of the altered state is an assembly and may be made of any suitable material or any number of parts. As shown in Fig. 1F, the frame 3 of the embodiment will generally form the outer periphery of the module and the periphery of the chamber. The web member w as shown in Figures 1F and 4A can segment the module 10 to form a stacked compartment. The modified compartment may have more than one web member W. Another alternative aspect of the stacked compartment can be constructed in any suitable manner. For example, the module ίο has a universal opening for the cabin sub-module to be inlaid, and the cabin sub-module includes a stacked compartment having any number of compartments. It can be seen that the compartments 14A, 14B can be closed by their closures 32, 34 at the top and bottom thereof, the closure being attached to the frame 30 by any intended connection means such as, but not limited to, mechanical, electronic and/or chemical fasteners. on. The interface with the slotted valves 12, 13 is associated with the frame 30 in any suitable manner, such as shown in the drawings and in the manner which will be described in detail below. The load lock chamber module 10 is a communication module that provides for the transfer of substrates between the tool components to which they are attached. Therefore, the height of the module 10 must be related to the height of the adjacent component or module, and depends on factors such as the traveling axis z of the substrate transport device adjacent to the module (by passing the rate of the interlocking module, and by, for example, the mode Group size or z-drive and/or structural considerations are delimited). The relationship between the through module 10 and the rotary module 15 is shown in Fig. 6, which shows the substrate transfer compartment 7 in which the load lock chamber module 10 is paired with the group tool. It can be seen that when the height of the module 10 is higher than the effective z-travel of the transport device, it will result in an unstable load lock chamber volume and increase the extraction/exhaustion time. Similarly, when the module height is lower than the effective z-travel, the overall effective travel bandwidth of the transport device will not be utilized, thus limiting the productivity of loading the inter-lock chamber module. The load lock compartments 14A, 14B of the embodiment are characterized by a configuration that provides a height at which the stacked load lock compartments are formed within the module 10. As shown in the foregoing and 4A-4B, the second embodiment of the load lock compartments 14A, 14B are stacked in the module 10, and the load interlocking cages in the modified single module are stacked. More (or fewer) load lock chambers may be included, such as three or more compartments. It can be seen that the provision of a plurality of independent load lock compartments 14A, 14B within the compact space envelope of the common module 10 will result in a plurality of independent and unrestricted transport paths, and the productivity of the module 10 is equally increased. 1A-1E Figure 13 200922852 In the example, each of the load lock compartments 14A, 14B are substantially similar to each other. In one embodiment, the load lock compartments 14A, 14B are placed along the middle of the partition load lock chamber. The plane has a contradictory structure. The loading interlock chambers of the modified aspects may be different from each other for operating substrates of different sizes and types. The module 10 shown in Fig. 1F has a modular configuration. The loadable interlocking chamber is composed of similar or different configurations. The load lock compartments 14A, 14B of the embodiment have a height sufficient to accommodate a plurality of stacked substrates (two substrates are shown in each of the compartments in Figures 4 & 4b). The modified interlocking compartments 14A, 14B can accommodate more or less stacked substrates as desired. Referring again to Figures 4A-4B, in the embodiment, each of the load lock chambers i4A, 14B may have a heating device or a cooling device, or both, to accommodate the interior of the load lock chamber when the atmosphere is in circulation. The contained substrate is heated or cooled. The loading of the interlocking chamber - a suitable example has the cooling/heating features described below. As shown in Fig. 4A, each of the load lock chambers of the embodiment has support frames 22A, 22B for heat treatment of the substrate by conductivity or the like. The support brackets 22A, 22B of the embodiment are designed to cool the substrate during exhaust such as load lock chambers. For example, the support frame may be coupled to a suitable heat treatment tank such as cooling block 27 in any desired manner to form a substrate cooling surface 24A' 24L on the side of each of the support frames 22A, 22B. The cooling block 27 of one embodiment includes Radiation fins (not shown) are provided to provide temperature transfer of the substrate cooling surfaces 24A, 24B, while another embodiment of the cooling block has heat within which the coolant flows to absorb the substrate cooling surface 24A '24B. The cooling block 27 in still another embodiment has a combination of a radiating fin and a coolant flow. The modified support frame has a substrate heating surface. In another variation, the load lock chamber is designed to heat the 14 200922852 gas in the load lock chamber. Each of the load lock chambers in the embodiment is provided with two support frames 22A, 22B having cooling surfaces 24a, 24b (although more or less wafer cooling surfaces are provided as previously described). From this, it is understood that heat exchange by conduction between the substrate and the support frame, the cooling surface of 22B, can be achieved by the substrate being seated on the cooling surface 24A' 24B of the support frame. The support frame in the embodiment is a solid state device (e.g., without a transmission/active mechanical component). This provides a minimum of style and height of the support frames Μa, 22B (thus helping to provide a dense height for loading the interlocking chamber). By way of example, the support brackets 22, 22 are fixed or static relative to the frame portion 30 and have a height of about 10 mm sufficient to allow the end effector EE of the transport device to directly grasp and place the substrate from the seat s state for cooling. On the surface 24A, the substrate is transferred from/to the load lock chambers 14A, 14B at 1/(see Figures 5A-5B and Figure )). The stent of the modified aspect can have any suitable height. The support frame 22, 22 of another embodiment is movable relative to the frame portion 30 such that the height of the bracket can be adjusted according to a predetermined distance between the brackets 22, 22". As shown in Fig. 4, the support frame 22A' 22 is configured to form a passage gap 26 of the end effector. The support frame 22A' 22B of the embodiment can be segmented to form a void 26 for receiving the end effector vanes. The void 26 provides z movement of the end effector to grasp and place the substrate on the cooling surface. By way of example, the end effector EE can place the substrate substantially simultaneously on the cooling surfaces 24A, 24B of the support frames 22A, 22B (on one of the stacked load lock chambers). For example, the load lock chamber can cool the substrate while exhausting. The cooled substrate can be grasped and transported from the load lock chamber 22A substantially simultaneously. When the substrate is cooled in one of the load lock chambers 14A, 14B, the other operation (loading the lock chamber module 10) loading the lock chambers 14A, 14B is performed in a substantially unrestricted manner. In a variant, the operations performed by each load lock chamber are interconnected in sequence in any suitable manner. Referring again to the first Α-1Β囷, in the embodiment, each of the load lock chambers 14Α, 14Β (see also Fig. 4, Fig. 4) has corresponding vacuum control valves 4〇Α, 4〇Β and exhaust valves 42Α, 42Β (such as With or without a diffuser) to provide an independent cycle of loading the interlocking chamber atmosphere. The vacuum control valves 4〇Α, 40Β and the exhaust valves 42Α, 42Β of the embodiment can be disposed in the module as interchangeability, as will be described in detail below. Referring again to Fig. 1F, the frame portion 3 of the embodiment has openings 36, 36, 37, 37. The cornice will form a relative vacuum port 36Α, 36Β and an exhaust port 37Α, 3*7Β in each load lock chamber 14Α, 14Β. The configuration of the exhaust and vacuum ports shown in the figures is for illustrative purposes only, and the modified exhaust and vacuum ports may have any other suitable configuration. The vacuum vents of the embodiment 36 Α, 36 设置 are disposed on one side of the mold set 10, and the exhaust vents 37 Α, 37 Β are disposed on different sides of the module 1 。. The modified exhaust and vacuum ports can be placed on the same side of the module. As shown in Fig. 1F, the vacuum and exhaust ports 36 Α, 37 Α , 36 Β, 37 相对 relative to the load lock chamber 14 Α ' 14 垂直 are vertically offset from each other. The vacuum and exhaust ports of the modified aspect are vertically aligned or have any other spatial relationship. Each mouth has a suitable mating interface (such as around the cornice) to connect the intended vacuum or vent valve to the monument (and module). In the embodiment, two or more mating interfaces 38 Α, 38 Β, 39 Α, 39 埠 relative to the mouth can be designed to have a substantially similar pairing configuration (eg, mating flange, sealing surface, screwing style, etc.) for having a complementary mating interface. Any of the valves can be paired with any of the mouthpiece's mating interfaces. For example, as shown in the first and if figures, the exhaust valve can be combined with the exhaust valve modules 42A, 42Β, each having a similar mating interface 421 for each module to be interchangeably mounted in either compartment. Air mouth interface. Embodiment 16 200922852 Example venting _m2a, 42b of a pressure enclosure or shroud having a unitary construction may include a row (four) body 42VB to provide; j; same flow rate or control configuration (eg, throttle and/or different capacity) Box valve). Embodiments are described with respect to individual exhaust and vacuum ports, while valves of other embodiments may be designed to vent and evacuate from a chamber through a single port. For example, the valve can be designed with appropriate valve characteristics to be translated between the vacuum source and the exhaust source. In another variation, each module has an exhaust and vacuum port, and a single exhaust/vacuum module can be used to vent and/or pump the cabin. The vent valve module housings 42A, 42B of the illustrated embodiment may permit the installation of three valve bodies 42 VB having a common source and a common discharge port. The valve modules 42 A, 42B are designed to provide any desired number of valve bodies 42 VB to achieve any desired predetermined valve body. The modular body 42A, 42B of the modified aspect can accommodate more or fewer valves. Different embodiments of the exhaust modules 42A' 42B, 42A' are shown in Figures 1A-1F and 8A-8D. The embodiment of the exhaust module shown in the figures is by way of example only and the exhaust module may have any suitable module body 42AB configuration to connect the exhaust module to, for example, a gas inlet, a valve body 42VB, and a diffuser. 44A and so on. However, different modules having different module bodies 42AB and 42VB may share a common mating interface configuration 421, thus permitting the interchangeability of the exhaust mold stages 42A, 42B' 42A' of the load lock chamber 1〇. The exhaust valve modules 42A, 42B of the embodiment may also include a suitable diffuser 44A that may be disposed substantially when entering the valve modules 42A, 42B in the exhaust ports 37A, 37B of the load lock chamber. Add the discharge surface of the interlocking chamber to the discharge surface or near. The exhaust valve modules 42A, 42B of one of the embodiments are designed to receive and/or secure the diffuser 44A to the recess (or other suitable recess or slot on the module body 42AB). The modified diffuser can be added or fixed to an exhaust port 17 200922852 36A, 37A, 36B, 37B such as a wall of the load lock chamber 10. Sections 7A-7B show a perspective view and a cross-sectional view of a module 1 of another embodiment. The module 10' is substantially similar to the module 10 described above. The vacuum control valve and exhaust valve of the illustrated embodiment can be combined with a single module 40A', 40B'. As shown in Fig. 7B, the module structure has ports 36A', 36B', 37A, 37B. The jaws of the illustrated embodiment are arranged in a generally symmetrical configuration (e.g., as shown, the bee is placed on the side walls for vacuum and exhaust ducts to be attached to both sides of the module). The load lock chambers then have four active ports to connect the vacuum and exhaust lines, such as two ports on each side. Each of the load lock chambers in the modified aspect can have any suitable number of ports with a suitable spatial relationship to each other. In the embodiment, the mating interfaces 38A', 38B', 39A, 39B' of the mouthpieces 36A, Mb, 37A', 37B' are similar to provide interchangeability of the modules 40A', 40B'. One or more of the matching aspects are non-similar to provide selective interchangeability between the interface and the opposing modules having corresponding interfaces. As shown in Fig. 7B, the mating interfaces 38A, 38B, 39A, 39B can be disposed on the pair of jaws, one of which is disposed on the other. For example, the ports 36, and 36B' are disposed on the same wall as the __ module wall, wherein __ is disposed on the other and a shared interface 39A' is shared. The valve modules 4A, 4B of the present embodiment are interchangeably matched to any pair of port matching interfaces 38A, 38B, 39A, 39B. The valve module 40A'' 40B' is designed to be in the mating compartment module 1 (as shown in Figure 7a-7b) with each of the bays (e.g., 36A, 36B). The implementation of the wide module 40A 4GB has a module body (10) to form a mating interface design to be paired with the module ί 'where the module body 41B, the mating interface includes a relative exhaust (discharge port) and a vacuum (into π ) 埠 mouth. The "true" control valve is mounted on the module body 41B' to maintain the flow Mit with the true port. _, in the module body 41B, upper 18 200922852 is provided with an exhaust valve 42VB' to maintain fluid communication with the exhaust port. Wherein - the valve module configuration results in a module 40A, 40B that operates to provide specific lock chambers 14A, 14B, and the other modules 4A, 4B, operate to provide mutual Pumping chambers 14A', HB' are pumped. The valve module 4A, 働 includes an exhaust diffuser, for example, as previously described. As shown in Figures 7 and 7B, the modules ,8, and 40B' are designed such that the modules are in communication with the two compartments 14A', 14B. For example, the module 40B' can be coupled to the module 1 〇 to cause the module 4 〇 B to perform the venting of the chamber 14 and the chamber 14B' (e.g., by vacuum). The module 4A is coupled to the module 10' to cause the module 40A' to perform the chamber 14β, the exhaust and the chamber 14A, and the pumping chamber includes a single load lock chamber. The single load lock chamber is provided with an extraction/exhaust interface having a plurality of exhaust and vacuum ports substantially similar to the foregoing. The pair of ports can be designed to be connected to similar modules 4〇A, 4〇B, and the exhaust/exhaust module, so that a single compartment can be vented and pumped with a single module to make a single load interlock. The complexity, size and cost of the chamber modules are reduced or minimized. Figure 9 is a cross-sectional view showing the substrate holders 22A, 22B of the load lock chamber module of another embodiment. Although four support additions are shown in Fig. 9 (two support frames are provided in each compartment as described above), only two brackets 22A, 22B will be described below. It is to be understood that the remaining substrate support frames are generally similar to the brackets 22A, 22B. The support frames 22A, 22B of the embodiment shown in Fig. 9 are substantially similar to the support frames described above with reference to Figs. 5A and 5B. The support frames 22A, 22B are statically set and placed at an expected distance p (e.g., 1 〇 mm or any other suitable distance greater than 10 mm) to support the substrate S stack. The support frames 22A, 22B of one of the embodiments are adjustable and provide an adjustment of the distance P. The bracket 19 200922852 22A, 22B of another embodiment can be moved relative to each other, as will be described in detail below. The modified support frames 22A, 22B are modularized and additional brackets can be added (or removed) with the expected distance p. Each of the support frames 22A, 22B of the embodiment has cooling surfaces 24A, 24B for conductive cooling of the substrate SI'S2 seated on one of the support cooling surfaces 24A, 24B. In the embodiment shown in Fig. 9, each of the substrate support frames 22A'22B may be provided with a gas damper 54 (the number of support frames is illustrated as an example only, and more or fewer support frames may be provided in the modified aspect) . The gas cartridge 54 is shown schematically in Figure 9 and has any number and any desired size of the cornice distributed along the support frame. The gas raft 54 is designed such that the gas system through the cornice is laminar to minimize particle formation. The gas cartridge 54 of one of the embodiments may include any suitable diffuser, and the diffuser of another embodiment may be disposed at the upstream portion of the gas cartridge 54. The diffuser of the modified aspect has any suitable spatial relationship with the relative mouth. As shown in Fig. 9, the air dam 54 is disposed between the opposite upper side on the cooling surfaces 24A' to 24B of the support frames 22A, 22B and the lower side and the upper side surface of the lower substrates S1, S2. The pneumatic raft 54 is coupled through a suitable passage formed in the support frames 22A, 22B to connect a suitable gas supply suitable for loading the lock chamber venting (e.g., venting gas). The channel of the altered aspect may not be merged with the support frame. As shown in Fig. 9, the gas cylinder 54 is designed to discharge gas into the gap 6 between the surfaces of the exposed substrates (e.g., to the neighboring cooling substrates s 1, S2 (see Figures 7 and 9)). For example, one or more of the support frames 22A, 22B have a gap or aperture 6 (e.g., a gap 26 similar to that shown in Figure 5B for the end effector to enter) to receive cooling on the support frame 22A. The (heating state) is exposed to another lower substrate which is also heated and cooled by the support frame 22B. The gas exhausted by the gas enthalpy 54 in the gap 6 will form a thermal barrier or barrier TB between the covered surface of the lower substrate S1 and the upper substrate S2, which is not covered by the cover surface (illustrated size and position are merely illustrative) The convection heating effect of the upper substrate S2 by the lower substrate si is minimized or completely eliminated. The circulating gas also provides convective cooling relative to the substrate in addition to conductive cooling. It can be seen that the gas discharged from the gas cylinders 54Α, 54 may flow through the gap 6' to interrupt the stagnant gas of the gap 6 and interrupt the unintended temperature transfer between the lower thermal substrate S1 and the exposed surface of the upper thermal substrate S2 through convection. . At the same time, the gas introduced by the gas cylinders 54, 54 can be removed or promoted by appropriate vacuum or degassing, such as suitably placed in the chamber (e.g., in the void 6 or other suitable location) (generating gas circulation therein - The vacuum crucible of the embodiment is attached to the support frames 22A, 22A in a manner similar to the aforementioned reference gas manifold 54. The vacuum crucible of another embodiment may be disposed in the chamber wall between the support frames, as described in reference to FIG. According to the above, since the cooling distribution on the stacked substrates is kept on the substrate stack, the cooling time of the substrate stacking will be reduced. The gas discharged from the gas cylinder 54' 54A has a set Reynolds coefficient of the low velocity laminar flow ( Re), preventing the particles from being deposited on the upper surface of the lower substrate. Figures 10A and 10B are exploded views showing the load lock chamber module 1 of another embodiment. The module is substantially similar to the foregoing. The load lock chamber module 1〇. The module 1〇〇 of the embodiment also has two load lock chambers U4A, 114B' stacked on each other. However, in the modified aspect, the load lock chamber module can have any Appropriate number of stacks The module 100 also includes cooling collets 12A, 120B. Each of the load lock chambers 114A, ii4B has a cooling collet disposed therein. The cooling collets 120A, 120B are capable of z-axis movement by a suitable z-driver 120Z The chuck can also be moved horizontally (for example, X and Y). The chucks 120A and 120B are arranged substantially in the opposite configuration as shown in the figure, so that the chuck is in the direction of the arrow 700 21 200922852
傳動時將會彼此相向或偏離對方》參照第10B圖所顯示之模組 100之斷面圖’其中加載互鎖室係處於預備狀態,各加載互鎖室 114A,114B具有支承架122A,122B以支承二基板S1,S2於 各加載互鎖室114A,114B (變更態樣中提供更多或更少基板) (亦見第11C圖)。實施例之支承架122A係靜定,(例如固定於 擒至結構或艙室内之任何其他適當之固定結構)而支承架^22B 係活動(例如依附於活動夾頭12〇A,120B或任何其他適當活動 支承架)。變更態樣之二個支承架係靜定,而另一變更態樣之二 個支承架係活動。其中一實施例之支承架122B係由夾頭12〇A, 120B所支承及利用延伸部或支承架121A,121B連接。延伸部 121A’121B係相對於其中一個夾頭12〇A,12〇B&/或支架122B 呈單體結構。變更態樣之支承架121A,121B可具有任何適當構 造。如第10B圖所示,延伸部121A,121B係從夹頭12〇A,12〇B 之表面124A向外延伸,於是固定支架ι22Α係設置於表面ι24Α 與支架122B之間(依附自延伸部121Α,121Β)β當夾頭12〇A, 120B在收縮狀態時,支架122A,mB之間有充裕空間以供基 板運送裝置之末端作用器將基板放置於支架mB上。 支承架係排列於實施例中使基板可利用轉移臂末端作用器 之z運動予以抓取或裝戴於相對之支承架i22A ’ 。變更態 樣之支承架及/或艙室可移動以將基板從末端作用器上舉起。夾 頭120A ’ 120B係如第1〇B圖所示設置於層架式開放之收縮狀 態(亦見第11D圖)用以將基板裝卸於加載互鎖室U4A,114B。 實施例中炎頭120A’ 120B之位置係可改變(沿著z軸方向(即 箭頭700之方向),例如第UE圖所示之關閉狀態)以使加載互 22 200922852 鎖室114A,114B之支承架122A,122B上之基板同時進行冷卻 作用。變更態樣之夾頭可實施基板之加熱作用,或冷卻與加熱 作用。第10B圖所示實施例中,夾頭120A,120B具有溫度轉 移接觸面124A(例如傳導性冷卻表面)。夾頭120A,120B上之 溫度轉移表面124A可熱聯通式連接於適當之熱槽152A。第10B 圖所示實施例中,此種熱聯通係圖示為夾頭及搶室上之連接韓 射翼片150A’ 152A,經設計可允許夾頭作z-方向之自由移動。 變更態樣之熱槽可具有任何適當構造。如第7B圖所示,各艙室 114A,114B具有靜溫度轉移接觸面124B (例如冷卻表面),一 般係設置於夾頭120A,120B之對面》亦參照第11A圖,圖示 之模組100具有開啟狀態之冷卻夾頭120A,120B,而基板S1, S2係被裝載於加載互鎖室114A,114B之相對支承架上。如前 所述,冷卻基板時,夾頭120A係被移動(沿著z方向)至關閉 狀態。如第11B圖所示(亦可參照第11D-11E圖分別顯示在開 啟與關閉狀態之夹頭之斷面圖)。須知夹頭120B之操作係大致 類似夾頭120A者。各該夾頭120A,120B係獨立操作,而第UB 圖所示之夾頭120A,120B僅作為實例說明。變更態樣中,其中 一加載互鎖室114A,114B之夾頭120A,120B係開啟而另一加 載互鎖室114A,114B之另一夾頭120A,120B係關閉或介於開 啟與關閉之間之任何其他預期狀態。如第11B圖所示,朝向關 閉狀態之運動將使夾頭抓持基板SI,S2 (例如支架122B上之 基板)朝向及大致與疊置冷卻表面124B接觸,並使夾頭冷卻表 面124A移向接觸在靜定支架122A上之相對基板S1’S2。因此, 夾頭120A,120B與加載互鎖室114A,114B之間之差異活動將 23 200922852 對複數個基板進行同時冷卻。夾頭120A,120B係回返至開啟狀 態以卸下基板SI,S2。變更態樣中之夾頭係設計以提供不需回 返開啟狀態即可除下(及鑲嵌)基板SI,S2。 第12A-12B圖係顯示另一實施例之冷卻夾頭熱交換器配置 1000之模組斷面,其中係利用適當導管1001將熱交換流體導引 至夾頭120A,120B之頭部使溫度轉移板維持預期溫度。流體導 管1001係呈撓性以允許前述之夾頭之3-轴活動》變更態樣之流 體導管1001之間之介面係剛固或半剛固性,夾頭120A,120B 係滑動性或伸縮性介面/聯結,具有適當密封構件以密封介面同 時允許導管1001與夹頭120A,120B之間之相對移動。 如第12A及12B圖所示,熱交換器配置亦包括將熱交換流 體導引進入靜溫度轉移表面124B之導管1002。冷卻流體係任 何適當流體,包括(但不限於)水,油,空氣或可將夾頭120A, 120B及靜溫度轉移表面124B之熱能予以轉移之任何其他適當 流體。冷卻夾頭熱交換器配置可包括任何適當流體溫度調節裝 置(未予圖示),諸如具有適當饋流與回流線之散熱器以在流體 循環進入及離開夾頭120A,120B及/或靜溫度轉移表面124B 時對流體進行冷卻作用。圖中僅顯示冷卻流饋流線(例如將冷 卻流體運送進入夾頭及靜溫度轉移表面之線路)作為實例說 明。變更態樣之夾頭120A,120B及靜溫度轉移表面124B係由 個別冷卻線路及/或個別熱交換器系統所饋流。 第13圖顯示另一實施例之模組1〇〇’之加載互鎖室H4A’之 局部斷面圖。模組100,係與模組1〇〇類似,並包括有一活動夾 頭120A’。夾頭120A’具有類似前述之衍生基板支承架。加載互 24 200922852 鎖室114A’具有衍生之基板支承架mA%夾頭ι2〇Α,具有溫度 轉移表面124A’。加載互鎖室U4A,具有設置其上之溫度轉移表 面124B’。該溫度轉移表面124B’係通過適當熱交換裝置而聯通 式連接於熱源+q。實施例中,進行加載互鎖室之抽氣時,可傳 動夾頭以縮減加載互鎖室支承架122A,上之基板與夾頭表面 124A’之間之空隙,或在夾頭支承架122B,上之基板與加載互鎖 室表面124B’之間之空隙。基板與毗鄰表面之間之縮減空隙可用 以增加氣體溫度,藉此減緩抽氣時之微粒產生。 此外,溫度表面124A’,124B’可被加熱以聯同夾頭活動或 自己本身直接加熱氣體,進一步減緩加載互鎖室抽氣時之微粒 產生。 第14A-14E圖顯示一實施例之加載互鎖室10100之實例。 雖然實施例係參照常壓門或有槽閥予以說明,實施例亦同樣適 用於基板加工裝備中之真空門或有槽閥。 本實施例中之加載互鎖室10100係設計成具有第一加載互 鎖室10140及第二加載互鎖室10150之疊置加載互鎖室。變更 態樣之加載互鎖室具有任何適當構造。各個加載互鎖室10140, 10150具有任何適當構造,包括(但不限於)前述者。舉例而言, 加載互鎖室10140,10150係設計成雙加載互鎖室(即各個加載 互鎖室係設計以抓持二個基板)或單一加載互鎖室(即各個加 載互鎖室係設計以抓持一個基板)。變更態樣之各個加載互鎖室 10140,10150係設計以抓持超過二個基板。各個加載互鎖室 10140, 10150可具有常壓加載互鎖室門10130 ’ 1012〇及一真空 加載互鎖室門或有槽閥10160,1〇161。本實施例中之常壓加載 25 200922852 互鎖室門10130及真空有槽閥10160係分別為加載互鎖室1〇14〇 之常壓門及真空門,而加載互鎖室1〇12〇及有槽閥1〇161係分 別為加載互鎖室10150之常壓門及真空門。常壓門1〇13〇,1〇12〇 可供加載互鎖室聯結於常壓加工單元,包括(但不限於)設備 刖端模組(EFEM),而有槽閥10160,10161可供加載互鎖室聯結 於真空模組,包括(但不限於)前述參照第2及3圖所述之加 工模組等。 第14A及14D圖顯示加載互鎖室ι0100之常壓門1〇13〇, 10120係呈關閉狀態,而第14b及圖顯示之常壓門1〇13〇, iono係呈開啟狀態,藉以提供基板進出相對加載互鎖室 ^140,10150之通道。同時參照第15圖,加載互鎖室門係利用 諸如驅動模組10200,10210等一或多個驅動模組予以操作。本 實鈿例所示之驅動模組T0200,1〇21〇係設在門1〇13〇,1〇12〇 之任一侧作為實例說明》另—實施例僅有一驅動模組設在門 10130,10120之任一側,而適當之基板支承模組係設在門之另 、側以適當支承該Η,以下將予說明n更態樣中有任何 適田數目之驅動模組設置於相對^門之任何適當位置。如第ι4Β 及i4c @所不’驅動模組1Q2⑽,1G21G係設置於基板轉移區 lorn之外側。將驅動模組10200,10210設置於基板轉移區外 側可供免除用以防護基板⑼設在基板上方之活動部件所產生 之微粒污染之防護風箱或微粒場。 驅動模組1G2GG 1G21G係至少局部設置於加載互鎖室之密 封接觸表面1G23G之前側。變更Μ之驅純組係適當地設計 以任何適當方式設置於密封接觸表面·Q之前側或後側。密 26 200922852 封接觸表面10230係加載互鎖室10100與常壓門10130, 10120 相互協作以構成密封體以防止泄漏加載互鎖室10140,10150中 之大氣之表面。其中一實施例之驅動模組10200,10210係模組 化單元,利用諸如機械固定物,化學固定物,膠黏劑或焊接等 方式聯結於加載互鎖室10100之表面。由此可知驅動模組 10200, 10210可永久性或可卸性聯結於加載互鎖室10100之表 面。另一實施例之驅動單元係合併於加載互鎖室10100,使驅動 模組構成加載互鎖室罩箱之一部份《圖示實施例之驅動模組 10200,10210係包括適當存取板或蓋體以供存取設在驅動模組 内之驅動器10210A,10210B,10200A,10200B,以下將予說 明。變更態樣之驅動器10210A,10210B,10200A,10200B之 存取可藉任何適當方式提供。 驅動模組10200,10210各分別包括有上側驅動傳動器 10200A,10210A及下側驅動傳動器10200B,10210B。驅動傳 動器10210A,10210B,10200A,10200B係任何適當驅動器, 包括(但不限於)液壓驅動器,油壓驅動器,差異壓力驅動器, 電子旋轉或線性驅動器及磁性驅動器。驅動傳動器係設計成單 軸或雙轴驅動器10210A,10210B,10200A,10200B。變更態 樣之驅動器可具有超過二個轴。驅動器可設計在門開啟時將門 ^130,10120移離接觸表面10230以使微粒生產及基板污染減 為最低。驅動器亦經設計將門10130,10120移動以接觸密封接 觸表面10230而使微粒生產減為最低。 上侧驅動傳動器10200A,10210A可彼此合作以開啟及關 閉門10130,而下側驅動傳動器10200B,10210B可彼此合作以 27 200922852 開啟及關閉門10120。本實施例中之門10130,10120係個別操 作,例如其中一門可開啟及關閉而另一門保持關閉,或其中一 門可開啟而另一門係關閉。變更態樣中各驅動模組10200,丨02 1 0 之一驅動器係聯結於相對之門,於是二門係同時開啟及同時關 閉。另一變更態樣中各驅動模組10200,1 〇21 〇之單一驅動器係 差異性聯結於相對之門’於是其中一門開啟時另一門係關閉。 再一變更態樣中僅只一個驅動模組10200, 10210係包括一或多 個驅動器而另一驅動模組10200,10210係由第一驅動模組作被 動式驅動。舉例而言,驅動模組10210係適當支承及驅動門 10130,10120而驅動模組10200包括適當線性軸承以支承及允 許門10130,10120之移動。 再參照第15圖,各驅動模組10200,10210可包括設在接 觸表面10230之前侧之開口,用以提供各常壓門1〇13〇,1〇12〇 聯結於其相對驅動器。舉例而言,驅動模組1〇2〇〇可包括開口 10203以供門10130聯結於上側驅動器1〇2〇〇A及開口 1〇2〇4以 供門10120聯結於下側驅動器1〇2〇〇B。本實施例之開口係大致 正交於門接觸表面10230’然而變更態樣之開口係大致平行於接 觸表面1G23G1-變更態樣之開口可具有相對於接觸表面 10230之任何適當空間關係。驅動模組1〇21〇可包括開口 ι〇2〇ι 以供門10130聯結於上側驅動器1〇21〇八,而開口 1〇2〇2可供門 10120聯結於下侧驅動$ !咖B。其中—實施例之開口 10201-102G4可包括任何適當密封部,包括(但不限於)波紋管 式密封部’藉此使職器所產生之任何微粒係被容納及不致污 染進出加載互鎖至10100之任何基板。門丨〇13〇,ι〇ι2〇係以任 28 200922852 何適當方式聯結於相對之驅動器。舉例而言,門1〇13〇可藉連 桿10204A聯結於上側驅動器1〇2〇〇A,及藉連桿1〇2〇4B聯結於 上側驅動器10200A。如圖所示,連桿1〇2〇4A,10204B係大致 平行於接觸表面10230’但可適當與接觸表面1〇23〇保持間距藉 以防止產生微粒。其中一實施例之連桿係從相對之門1〇13〇, 10120延伸,並與門一體成型。另一實施例之門及其相對連桿係 一組裝,其中該連桿係以任何適當方式聯結於門。該門1〇12〇 可利用連桿10203A聯結於下側驅動器1〇21〇B,及利用連桿 10203B聯結於下側驅動器i〇2〇〇B。連桿i〇204A,10204B,The drive will face or deviate from each other. Referring to the cross-sectional view of the module 100 shown in FIG. 10B, wherein the load lock chamber is in a standby state, each load lock chamber 114A, 114B has a support frame 122A, 122B. The two substrates S1, S2 are supported in each of the load lock chambers 114A, 114B (more or less substrates are provided in the modified aspect) (see also Figure 11C). The support frame 122A of the embodiment is statically fixed (e.g., fixed to the structure or any other suitable fixed structure within the compartment) and the support frame 22B is active (e.g., attached to the movable collet 12A, 120B or any other Properly active support frame). The two support frames of the modified aspect are statically set, while the two support frames of the other modified form are active. The support frame 122B of one of the embodiments is supported by the collets 12A, 120B and connected by extensions or support frames 121A, 121B. The extension 121A'121B has a unitary structure with respect to one of the chucks 12A, 12B, and/or the bracket 122B. The modified support frames 121A, 121B can have any suitable configuration. As shown in Fig. 10B, the extending portions 121A, 121B extend outward from the surface 124A of the chuck 12A, 12B, so that the fixing bracket ι22 is disposed between the surface ι24Α and the bracket 122B (attached to the extension portion 121Α) , 121Β) β When the collet 12〇A, 120B is in the contracted state, there is ample space between the brackets 122A, mB for the end effector of the substrate transport device to place the substrate on the bracket mB. The support frame is arranged in the embodiment such that the substrate can be grasped or attached to the opposite support frame i22A' by the z-movement of the transfer arm end effector. The modified support frame and/or compartment can be moved to lift the substrate from the end effector. The chuck 120A' 120B is disposed in a collapsed state of the shelf type as shown in Fig. 1B (see also Fig. 11D) for attaching and detaching the substrate to the load lock chambers U4A, 114B. In the embodiment, the position of the head 120A' 120B can be changed (along the z-axis direction (i.e., the direction of the arrow 700), such as the closed state shown in the UE map) to support the loading of the 22-2222852 lock chambers 114A, 114B. The substrates on the shelves 122A, 122B are simultaneously cooled. The chuck of the modified aspect can perform the heating action of the substrate, or the cooling and heating. In the embodiment illustrated in Figure 10B, the collets 120A, 120B have temperature transfer contact surfaces 124A (e.g., conductive cooling surfaces). The temperature transfer surface 124A on the chucks 120A, 120B can be thermally coupled to a suitable heat sink 152A. In the embodiment illustrated in Fig. 10B, such a thermal communication system is illustrated as a connecting tab and a connecting fin 150A' 152A on the grab chamber, designed to allow the chuck to move freely in the z-direction. The heat sink of the modified aspect can have any suitable configuration. As shown in FIG. 7B, each of the compartments 114A, 114B has a static temperature transfer contact surface 124B (eg, a cooling surface), generally disposed opposite the chucks 120A, 120B. Referring also to FIG. 11A, the illustrated module 100 has The cooling chucks 120A, 120B are in an open state, and the substrates S1, S2 are mounted on opposite support frames of the load lock chambers 114A, 114B. As described above, when the substrate is cooled, the chuck 120A is moved (along the z direction) to the closed state. As shown in Fig. 11B (see also the sectional view of the chuck in the open and closed states as shown in Fig. 11D-11E). It is to be understood that the operation of the collet 120B is substantially similar to that of the collet 120A. Each of the collets 120A, 120B operates independently, and the collets 120A, 120B shown in the UB diagram are illustrated by way of example only. In a variant, the chucks 120A, 120B of one of the load lock chambers 114A, 114B are open and the other chucks 120A, 120B of the other load lock chambers 114A, 114B are closed or between open and closed. Any other expected state. As shown in Fig. 11B, the movement toward the closed state will cause the collet to grip the substrate SI, S2 (e.g., the substrate on the bracket 122B) toward and substantially in contact with the stacked cooling surface 124B, and move the collet cooling surface 124A toward The opposing substrate S1'S2 on the stationary stent 122A is contacted. Thus, the difference between the chucks 120A, 120B and the load lock chambers 114A, 114B will simultaneously cool 23 substrates 222009. The chucks 120A, 120B are returned to the open state to remove the substrates SI, S2. The chuck system in the modified aspect is designed to remove (and inlay) the substrate SI, S2 without the need to return to the open state. 12A-12B is a cross-sectional view of a module of a cooling collet heat exchanger arrangement 1000 of another embodiment in which a heat transfer fluid is directed to the heads of the collets 120A, 120B using a suitable conduit 1001 for temperature transfer. The board maintains the expected temperature. The fluid conduit 1001 is flexible to allow the interface between the fluid conduits 1001 of the aforementioned 3-axis movement of the collet to be rigid or semi-rigid, and the collets 120A, 120B are slidable or stretchable. The interface/coupling has a suitable sealing member to seal the interface while allowing relative movement between the catheter 1001 and the collets 120A, 120B. As shown in Figures 12A and 12B, the heat exchanger arrangement also includes a conduit 1002 that directs the heat exchange fluid into the static temperature transfer surface 124B. The cooling stream system is any suitable fluid including, but not limited to, water, oil, air or any other suitable fluid that can transfer the thermal energy of the chucks 120A, 120B and the static temperature transfer surface 124B. The cooling collet heat exchanger configuration can include any suitable fluid temperature adjustment device (not shown), such as a heat sink with appropriate feed and return lines to circulate into and out of the collet 120A, 120B and/or static temperature during fluid circulation. The fluid is cooled as it is transferred to surface 124B. Only the cooling flow feed line (e.g., the line that transports the cooling fluid into the chuck and the static temperature transfer surface) is shown as an example. The modified chucks 120A, 120B and the static temperature transfer surface 124B are fed by individual cooling lines and/or individual heat exchanger systems. Fig. 13 is a partial cross-sectional view showing the load lock chamber H4A' of the module 1' of another embodiment. The module 100 is similar to the module 1 and includes a movable collet 120A'. The collet 120A' has a derivative substrate support similar to that described above. Loading Mutual 24 200922852 The lock chamber 114A' has a derivatized substrate holder mA% collet ι2 〇Α having a temperature transfer surface 124A'. The load lock chamber U4A has a temperature transfer surface 124B' disposed thereon. The temperature transfer surface 124B' is connected in series to the heat source +q by a suitable heat exchange means. In an embodiment, when pumping the load lock chamber, the chuck can be driven to reduce the gap between the load lock chamber support frame 122A, the substrate and the chuck surface 124A', or the chuck support frame 122B. The gap between the upper substrate and the load lock chamber surface 124B'. The reduced void between the substrate and the adjacent surface can be used to increase the temperature of the gas, thereby slowing the generation of particles during pumping. In addition, the temperature surfaces 124A', 124B' can be heated to act in conjunction with the collet or directly heat the gas by itself, further slowing the generation of particulates during pumping of the interlocking chamber. 14A-14E illustrate an example of a load lock chamber 10100 of an embodiment. Although the embodiment is described with reference to a normal pressure gate or a grooved valve, the embodiment is equally applicable to a vacuum door or a grooved valve in a substrate processing apparatus. The load lock chamber 10100 in this embodiment is designed to have a stack load lock chamber of the first load lock chamber 10140 and the second load lock chamber 10150. The loading interlocking chamber of the modified aspect has any suitable configuration. Each of the load lock chambers 10140, 10150 has any suitable configuration including, but not limited to, the foregoing. For example, the load lock chambers 10140, 10150 are designed as dual load lock chambers (ie, each load lock chamber is designed to grip two substrates) or a single load lock chamber (ie, each load lock chamber design) To grasp a substrate). Each of the load lock chambers 10140, 10150 is designed to grip more than two substrates. Each of the load lock chambers 10140, 10150 can have a normal pressure load lock chamber door 10130' 1012 〇 and a vacuum load lock chamber door or slotted valve 10160, 1 161. In the present embodiment, the atmospheric pressure loading 25 200922852 interlocking chamber door 10130 and the vacuum slotted valve 10160 are respectively an atmospheric pressure door and a vacuum door for loading the interlocking chamber 1〇14〇, and the loading interlocking chamber 1〇12〇 and The slotted valve 1 161 is a normal pressure gate and a vacuum door for loading the interlocking chamber 10150, respectively. Normal pressure door 1〇13〇, 1〇12〇 loadable interlocking chamber is connected to the atmospheric processing unit, including but not limited to the equipment end module (EFEM), and the slotted valve 10160, 10161 is available for loading. The interlocking chamber is coupled to the vacuum module, including but not limited to the processing modules described above with reference to Figures 2 and 3. Figures 14A and 14D show that the atmospheric pressure door 1〇13〇 of the load lock chamber ι0100 is closed, and the normal pressure gate 1〇13〇 shown in Fig. 14b and the figure is turned on, thereby providing the substrate. Access to the channel of the load lock chambers ^140, 10150. Referring also to Fig. 15, the load lock chamber door is operated by one or more drive modules such as drive modules 10200, 10210. The driving module T0200,1〇21〇 shown in this embodiment is set on the door 1〇13〇, 1〇12〇 as an example. “Another embodiment has only one driving module located in the door 10130. Any one of the sides of the 10120, and the appropriate substrate supporting module is disposed on the other side of the door to properly support the cymbal, and the following will explain that any suitable number of driving modules in the n-th aspect is set in the opposite ^ Any suitable position of the door. For example, the first module is 1Q2 (10), and the 1G21G is disposed outside the substrate transfer region lorn. The drive modules 10200, 10210 are disposed on the outer side of the substrate transfer area to protect the protective bellows or particle fields from the particulate contamination caused by the movable parts disposed on the substrate (9). The drive module 1G2GG 1G21G is at least partially disposed on the front side of the seal contact surface 1G23G of the load lock chamber. The modified group is suitably designed to be placed on the front side or the back side of the sealing contact surface Q in any suitable manner. The sealing contact surface 10230 is loaded with the interlocking chamber 10100 and the atmospheric pressure gates 10130, 10120 cooperate to form a sealing body to prevent leakage of the surface of the atmosphere in the loading interlocking chambers 10140, 10150. The drive module 10200, 10210 of one embodiment is a modular unit that is coupled to the surface of the load lock chamber 10100 by means of, for example, mechanical fixtures, chemical fixtures, adhesives, or soldering. It can be seen that the drive modules 10200, 10210 can be permanently or detachably coupled to the surface of the load lock chamber 10100. The drive unit of another embodiment is incorporated in the load lock chamber 10100 such that the drive module forms part of the load lock chamber cover. The drive module 10200, 10210 of the illustrated embodiment includes a suitable access plate or The cover is for accessing the drivers 10210A, 10210B, 10200A, 10200B provided in the drive module, as will be described below. Access to the altered aspects of the drives 10210A, 10210B, 10200A, 10200B can be provided in any suitable manner. The drive modules 10200, 10210 each include an upper drive actuator 10200A, 10210A and a lower drive actuator 10200B, 10210B, respectively. Drive actuators 10210A, 10210B, 10200A, 10200B are any suitable drivers including, but not limited to, hydraulic drives, hydraulic drives, differential pressure drives, electronic rotary or linear drives, and magnetic drives. The drive actuators are designed as single or dual axis drives 10210A, 10210B, 10200A, 10200B. A modified drive can have more than two axes. The actuator can be designed to move the door ^130, 10120 away from the contact surface 10230 when the door is opened to minimize particle production and substrate contamination. The actuator is also designed to move the doors 10130, 10120 to contact the sealing contact surface 10230 to minimize particle production. The upper drive actuators 10200A, 10210A can cooperate with each other to open and close the door 10130, while the lower drive actuators 10200B, 10210B can cooperate with each other to open and close the door 10120 with 27 200922852. The doors 10130, 10120 in this embodiment are individually operated, for example, one of the doors can be opened and closed while the other door remains closed, or one of the doors can be opened and the other door is closed. In the change mode, each of the driving modules 10200 and 丨02 1 0 is connected to the opposite door, so that the two doors are simultaneously opened and closed at the same time. In another variation, the single driver of each of the drive modules 10200, 1 〇 21 差异 is differentially coupled to the opposite door' such that when one of the doors is open, the other is closed. In yet another variation, only one drive module 10200, 10210 includes one or more drivers and the other drive modules 10200, 10210 are driven by the first drive module. For example, the drive module 10210 suitably supports and drives the doors 10130, 10120 and the drive module 10200 includes suitable linear bearings to support and permit movement of the doors 10130, 10120. Referring again to Fig. 15, each of the drive modules 10200, 10210 can include an opening disposed on a front side of the contact surface 10230 for providing each of the atmospheric pressure gates 1 〇 13 〇, 1 〇 12 联 to be coupled to their opposite drivers. For example, the driving module 1〇2〇〇 may include an opening 10203 for the door 10130 to be coupled to the upper driver 1〇2〇〇A and the opening 1〇2〇4 for the door 10120 to be coupled to the lower driver 1〇2〇. 〇B. The opening of this embodiment is generally orthogonal to the door contact surface 10230'. However, the opening of the modified aspect may be substantially parallel to the contact surface 1G23G1-the open aspect of the opening may have any suitable spatial relationship with respect to the contact surface 10230. The drive module 1〇21〇 may include an opening ι〇2〇ι for the door 10130 to be coupled to the upper driver 1〇21〇8, and the opening 1〇2〇2 for the door 10120 to be coupled to the lower side drive $! Wherein the opening 10201-102G4 of the embodiment may include any suitable seal including, but not limited to, a bellows seal 'by thereby causing any particulates generated by the appliance to be contained and not contaminated into and out of the load lock to 10100 Any substrate. The threshold is 13丨〇, ι〇ι2 is connected to the opposite drive in any suitable way. For example, the door 1〇13〇 can be coupled to the upper driver 1〇2〇〇A by the link 10204A, and coupled to the upper driver 10200A by the link 1〇2〇4B. As shown, the links 1〇2〇4A, 10204B are generally parallel to the contact surface 10230' but may be suitably spaced from the contact surface 1〇23〇 to prevent the generation of particles. The linkage of one of the embodiments extends from the opposite door 1〇13〇, 10120 and is integrally formed with the door. Another embodiment of the door and its relative linkage are assembled wherein the linkage is coupled to the door in any suitable manner. The door 1〇12〇 can be coupled to the lower driver 1〇21〇B by the link 10203A and to the lower driver i〇2〇〇B by the link 10203B. Connecting rods i〇204A, 10204B,
10203A,10203B係設置於接觸表面1〇23()之前侧,於是接觸表 面10230與連桿之間有充裕淨距以防止或使微粒產生及基板污 染減為最低。變更態樣之連桿i0204A,丨〇2〇4B,丨〇2〇3 A,丨〇2〇3B 與接觸表面10230有任何適當空間關係,並設計以使微粒產生 減為最低。連桿10204A,10204B,10203A,10203B係聯結於 其相對驅動器10210A,10210B,i〇2〇〇A,10200B使門開啟及 關閉時該門保持平行於加載互鎖室1〇1〇〇之接觸表面1〇23〇。變 更態樣之連桿10204A,10204B,10203A,10203B係聯結於其 相對驅動器以供門開啟及關閉時可相對於接觸表面1〇23〇旋轉。 圖中所示之開口 10201-10204係大致呈直形,於是門 10130,10120係沿著大致平行於加載互鎖室之接觸表面1〇23〇 之直線行進。另一實施例之開口 10201-10204可具有任何適當 形狀,以下將予詳述。在門10130,10120與接觸表面10230之 間可提供任何適當密封以防止加載互鎖室1〇14〇,1〇15〇之内部 氛圍之泄漏。本實施例之密封體係設計以使門在開啟及關閉時 29 200922852 之摩擦及微粒產生減為最少。另一實施例之開口 10201-10204 係呈角形或如第15A,15B圖所示,當門10130, 10120開啟時, 門10130’ 10120將會移離接觸表面10230以防止門及/或密封體 摩擦接觸表面10230。第15A圖中之開口 10201,係呈角度偏離 接觸表面10230 ’於是當門沿著箭頭T之方向移動時,開口 10201’將導引門偏離接觸表面10201”,反之亦然。第15B圖顯 示開口 10201”具有凸輪構造,當門沿著箭頭τ之方向移動時可 導引門偏離接觸表面10230,及當門沿著箭頭Τ之相反方向關 閉時將導引門朝向接觸表面10230,使門與接觸表面10230之間 產生密封作用。驅動部10210Α,10210Β,10200Α,10200Β係 適當地聯結於連桿10204Α,10204Β,10203Α,10203Β以提供 如第15Α,15Β圖所述之門10130,10120之凸輪移動。另一實 施例之門係如圖示由二輪驅動於開口内,於是連桿10204Α, 10204Β,10203Α,1〇2〇3Β與其相對開口之間將大致沒有接觸。 變更態樣之門係以任何適當方式驅動。 第丨6及16A-16C圖顯示一實施例之加載互鎖室loioo,。第 16圖之加載互鎖室係大致類似前述之加載互鎖室10100,並圖 示於基被加工系統之一部份,其中該加載互鎖室1〇1〇〇,係聯結 於加工楔組1〇3〇〇。本實施例之加載互鎖室1〇1〇〇,係設計為單 一艙室力0載互鎖室。變更態樣之加載互鎖室10100,可具有任何 適當數目之艙室。加載互鎖室10100’可包括有艙室10150,,密 封接觸表面10230,,常壓門10320及驅動模組1〇31〇,10330。 如前所述,驅動模組10310, 1033〇係設置於如第16Α圖所示之 基板轉移區10110之外側。驅動模組1031〇及1〇33〇係包括有 30 200922852 驅動部 10310A,10330A 及開口 10302。驅動部 10310A,10330A 係大致類似於前述之驅動部10200A,10200B,10210A,10210B。 另一實施例中,如第14A-E圖及第15圖所述,加載互鎖室1〇1〇〇’ 具有設在門之任一側之一驅動部,可支承及啟動門10320之移 動,同時在門之另一側設置被動支承以支承及允許門10320之 移動。開口 10302係大致類似於前述之開口 10201-10204。本實 施例中與前述連桿10204A,10204B,10203A,10203B類似之 連桿10304係通過槽口 10302以諸如前述方式等任何適當方式 聯結常壓門10320至驅動部10310A,10330A。變更態樣之門 10320係以任何適當方式聯結於驅動部10310A,10330A。須知 加載互鎖室10100,亦包括有一真空閥或類似門10320之門 10321,並以類似前述參照門10320之方式操作。變更態樣之真 空閥或門10321可具有任何適當構造。 第17及18圖顯示一實施例之加載互鎖室20100。本實施例 之加載互鎖室20100係設計成右角加載互鎖室,其中常壓介面 20101係設在與真空介面20102大致呈90度角度。變更態樣之 加載互鎖室具有任何適當構造,其中常壓介面20101具有與真 空介面201021之任何適當角度或空間關係。 本實施例之加載互鎖室20100之常壓介面20101包括有一 加載互鎖室門鑲嵌部20130, 一常壓門20120及一門驅動單元 20125。加載互鎖室20100之真空介面係設計成大致類似前述參 照常壓介面20101之方式^變更態樣之真空介面係具有任何適 當構造。門驅動單元20125係設計成當門沿著箭頭H1之方向偏 離門鑲嵌部面20150然後沿著箭頭VI之方向偏離基板開口 31 200922852 20140時可開啟常壓門2〇1 係設計以大致相反方式關閉常第::,驅動 可沿著箭頭V2方向移動^ 2常^脚°舉例而言,驅動單元 1 20120,於是門將與基板開口 20140 對背,:然後沿著箭頭H2方向使門2賴設置於開口 2_之 上如^ 17圖所不,門20120之驅動單元2〇125係設在門2〇12〇 之下’而變更態樣中驅動部可具有相對於門之任何適當位 置二括(但祕於)設在如第UK圖所示在門之側面。 驅動=2G125係任何適當驅動單元,包括(但不限於)氣動 式川電子,液壓式及磁性驅動部等。當門密封部2 面〇15〇之壓力使門移向開口時,在門· = 20150之間將形成密封部。 入I衣® 再參照第17圖及第isi , ι 式適當連接於驅動單元2(^f壓門2簡可藉任何適當方 許門細之尺寸二2_5,包括利用-或多個驅動轴 -〇,使門之一部份將叠:、;=當設計以配合基· 20140周圍形成密封部。可利、面2()15()而在基板開口 鑲欲表面2觀相連接之何適#㈣體2_G聯結於與 係在門表面2函與鑲表面面?n2_之周邊。密封體2咖 適當材料所構成。表面2G15G之間提供密封作用之任何 門鑲喪。卩2G13G可被歲人加載互鎖室2()1⑼ 20101之表面20310中之對應形狀之開口 2額。參昭第12 圖’門職部則0係由任何適當材料製成,包括(但不限於) 金屬塑料H ’複合物或上述之任何組合。鑲嵌部加% 包括有-外周部2G35G及—内槽部2()。外周部2Q35〇具有提 32 200922852 供加# s & & 啊互鎖室20100之常壓介面20101之耐摩損性及防護性之 調^適當厚度T。外周部20350具有任何適當尺寸之長度L與 ^ D (見第17圖),如第20及21圖所示,當門在關閉狀態 周部將可延伸通過門2〇12〇之邊緣。另一實施例 部2〇1:5 踝狀 讓立叫之外周部20350之長度L及高度D係具有適當尺寸使 嵌部可延伸通過門密封部2〇3〇〇但不致通過門緣。變更態樣 之鑲嵌部之外周部20350可具有任何適當尺寸。外周部2〇35〇 可具有設在其外周邊之開口 2〇21〇。該開口係任何適當開口以供 諸如卸除性固定件之通過,包括(但不限於)用以從加載互鎖 室20100上卸除鑲嵌部之螺栓與螺釘。變更態樣之鑲嵌部2〇13〇 吁藉包括(但不限於)化學,磁性及真空聯結等任何適當方式 聯结於加載互鎖室20100上。 内槽部20360可構成基板開口 20140作為基板進出加載互 鎖室2〇1〇0之通道。如第Π圖所示,由内槽部20360所構成之 開口 2〇140可具有任何適當形狀以供基板及裝載基板之運送機 器人之立少一個末端作用器(或其一部份)通過開口 2〇14(^其 中〆實施例之内槽部20360之尺寸係經過設計使内槽部20360 之璧體與基板及至少該末端作用器之間保持有最小淨距。如第 21圖所示,内槽部20360可延伸通過外周部2〇35〇之背面2〇4〇〇 之任何適當距離D2。本實施例之内槽部2〇36〇係延伸至加載互 鎖室20420之内側面20410。變更態樣之内槽部2〇36〇可延伸超 過或在加載互鎖室20420之内侧表面2〇41〇之前方。另一變更 態樣之内槽部20360可能不致延伸超過外周部2〇35〇之背面 20400。 33 200922852 加載互鎖室常壓介面20101之表面20310中之對應開口可 具有外侧凹部20330及内槽部開口 20340。外侧凹部20330之深 度大致相等於鑲嵌部20130之外周部20350之厚度T,而長度 及高度係比鑲嵌部20130之長度L及高度D更大,藉此提供鑲 嵌部20130之外周部20350及凹部20330周圍之充裕淨距以允 許鑲嵌部20130嵌入及卸離凹部20330。變更態樣之外凹部可具 有任何適當尺寸。另一變更態樣之外凹部係經設計以與鑲嵌部 20130壓合或互配。内槽部開口 20340具有適當尺寸使内槽部開 口 20340與鑲嵌部20130之内槽部20360之間有適當淨距藉以 提供鑲嵌部20130之輕易卸離及嵌入。變更態樣之淨距係最小 化使鑲嵌部20130被嵌入外凹部20330及内槽部開口 20340時 可產生連接或壓合互配。雖然圖示鑲嵌部20130係設在凹部 20330中’而變更態樣之鑲嵌部20440之背面(見第21圖)可 連接加載互鎖室20100之表面20310 (例如鑲嵌部之表面20310 並非内凹)。 如第21圖所詳示,外凹部20330之背面20400係包括有一 圍繞内槽部開口 20340之凹槽20221。本實施例中之凹槽20221 係設在内槽部開口 20340與卸離式固定件之開口 2〇21 〇之間。 變更態樣之凹槽20221係設置於相對於内槽部開口 20340與卸 離式固定件之開口 20210之任何適當相對位置。另一變更態樣 之凹槽係設在内槽部20360與内槽部開口 2〇34〇之間。凹槽 20221係设si以承接及保持諸如〇_形環或任何其他適當材料, 藉此當鑲嵌部20130聯結於加載互鎖室2〇丨〇〇時固定件壓合密 封部20420之際在凹部20330之背面20400與鑲嵌部20130之 34 200922852 間產生密封〇术 , 20420將維持^載互鎖室2晴進行抽氣或排氣時,密封部 態樣中在表面室2G1GG内之真空或其他控制氛圍。變更 面2〇310上以^未設有凹部,密封部20·可設在諸如表 封。另部2咖與加載互鎖室構架之間之密 之真空。&樣可藉任何適當方式維持加載互鎖室20100内10203A, 10203B are placed on the front side of the contact surface 1〇23(), so that there is ample clearance between the contact surface 10230 and the connecting rod to prevent or minimize particle generation and substrate contamination. The modified aspect links i0204A, 丨〇2〇4B, 丨〇2〇3 A, 丨〇2〇3B have any suitable spatial relationship with the contact surface 10230 and are designed to minimize particle generation. The connecting rods 10204A, 10204B, 10203A, 10203B are coupled to their opposite drivers 10210A, 10210B, i〇2〇〇A, 10200B such that the door remains parallel to the contact surface of the load lock chamber 1〇1〇〇 when the door is opened and closed. 1〇23〇. The modified links 10204A, 10204B, 10203A, 10203B are coupled to their opposite drivers for rotation relative to the contact surface 1〇23〇 when the door is opened and closed. The openings 10201-10204 shown are generally straight, such that the doors 10130, 10120 travel along a line generally parallel to the contact surface 1〇23〇 of the load lock chamber. The openings 10201-10204 of another embodiment can have any suitable shape, as will be described in more detail below. Any suitable seal may be provided between the doors 10130, 10120 and the contact surface 10230 to prevent leakage of the internal atmosphere of the load lock chambers 1〇14〇1〇15〇. The sealing system of this embodiment is designed to minimize friction and particle generation when the door is opened and closed 29 200922852. The opening 10201-10204 of another embodiment is angular or as shown in Figures 15A, 15B. When the doors 10130, 10120 are open, the door 10130' 10120 will move away from the contact surface 10230 to prevent the door and/or seal from rubbing. Contact surface 10230. The opening 10201 in Fig. 15A is angularly offset from the contact surface 10230' so that when the door is moved in the direction of the arrow T, the opening 10201' deflects the guide door away from the contact surface 10201" and vice versa. Figure 15B shows the opening 10201" has a cam configuration that guides the door away from the contact surface 10230 as it moves in the direction of the arrow τ, and directs the guide door toward the contact surface 10230 when the door is closed in the opposite direction of the arrow ,, causing the door to contact A sealing effect is created between the surfaces 10230. The drive units 10210Α, 10210Β, 10200Α, 10200Β are suitably coupled to the links 10204Α, 10204Β, 10203Α, 10203Β to provide cam movement of the doors 10130, 10120 as described in Figures 15 and 15D. The door of another embodiment is driven in the opening by two wheels as shown, so that the links 10204Α, 10204Β, 10203Α, 1〇2〇3Β will have substantially no contact with their opposite openings. The door to the change is driven in any suitable way. Figures 6 and 16A-16C show a load lock chamber loioo of an embodiment. The load lock chamber of Figure 16 is substantially similar to the load lock chamber 10100 described above and is illustrated in a portion of the base processing system, wherein the load lock chamber is 1〇1, coupled to the machining wedge 1〇3〇〇. The load lock chamber 1〇1〇〇 of this embodiment is designed as a single chamber force 0 load lock chamber. The modified load lock chamber 10100 can have any suitable number of compartments. The load lock chamber 10100' can include a chamber 10150, a seal contact surface 10230, a normal pressure gate 10320, and drive modules 1〇31〇, 10330. As described above, the drive modules 10310, 1033 are disposed on the outer side of the substrate transfer region 10110 as shown in Fig. 16A. The drive modules 1031〇 and 1〇33〇 include 30 200922852 drive units 10310A, 10330A and openings 10302. The drive units 10310A, 10330A are substantially similar to the aforementioned drive units 10200A, 10200B, 10210A, 10210B. In another embodiment, as described in FIGS. 14A-E and 15 , the load lock chamber 1 〇 1 〇〇 ' has a drive portion provided on either side of the door to support and activate the movement of the door 10320 At the same time, a passive support is provided on the other side of the door to support and permit the movement of the door 10320. Opening 10302 is generally similar to opening 10201-10204 described above. The link 10304, which is similar to the aforementioned links 10204A, 10204B, 10203A, 10203B in this embodiment, is coupled to the drive portions 10310A, 10330A via the notches 10302 in any suitable manner, such as in the manner previously described. The door 10320 is coupled to the drive units 10310A, 10330A in any suitable manner. It is noted that the load lock chamber 10100 also includes a vacuum valve or door 10321 similar to the door 10320 and operates in a manner similar to the aforementioned reference door 10320. The modified air valve or door 10321 can have any suitable configuration. Figures 17 and 18 show a load lock chamber 20100 of an embodiment. The load lock chamber 20100 of the present embodiment is designed as a right angle load lock chamber, wherein the atmospheric pressure interface 20101 is disposed at an angle of substantially 90 degrees to the vacuum interface 20102. The loading interlocking chamber of any variation has any suitable configuration in which the atmospheric interface 20101 has any suitable angular or spatial relationship to the vacuum interface 201021. The atmospheric pressure interface 20101 of the load lock chamber 20100 of the present embodiment includes a load lock chamber door inlay 20130, a normal pressure gate 20120 and a door drive unit 20125. The vacuum interface of the load lock chamber 20100 is designed to be substantially similar to the aforementioned reference normal pressure interface 20101. The vacuum interface of the modified aspect has any suitable configuration. The door drive unit 20125 is designed to be opened when the door is offset from the door inset surface 20150 in the direction of the arrow H1 and then offset from the substrate opening 31 in the direction of the arrow VI. 200922852 20140. The normal pressure door 2〇1 is designed to close in a substantially opposite manner. Often::, the drive can be moved in the direction of the arrow V2. 2, for example, the drive unit 1 20120, then the door will be opposite the substrate opening 20140, and then the door 2 is placed along the direction of the arrow H2 Above the opening 2_, as shown in Fig. 17, the driving unit 2〇125 of the door 20120 is disposed under the door 2〇12〇', and in the modified aspect, the driving portion may have any suitable position relative to the door ( But the secret) is located on the side of the door as shown in the UK map. Drive = 2G125 is any suitable drive unit, including but not limited to pneumatic pneumatic, hydraulic and magnetic drive. When the pressure of the door seal portion 2 is 15 移, the door is moved toward the opening, and a seal portion is formed between the door ·=20150. Into the I clothing ® and then refer to Figure 17 and the isi, ι type is properly connected to the drive unit 2 (^f press door 2 can be used to any size of the door to the size of the second 2_5, including the use of - or multiple drive shafts - 〇, so that one part of the door will be stacked:,; = when the design is to form a seal around the base · 20140. Keli, face 2 () 15 () and the substrate opening and the surface 2 #(四)体2_G is connected to the periphery of the door surface 2 and the surface of the inlay?n2_. The sealing body 2 is made of appropriate materials. Any door in the seal between the surface 2G15G provides a sealing effect. 卩2G13G can be aged The person loads the opening 2 of the corresponding shape in the surface 20310 of the interlocking chamber 2 (1) 20101. The 12th drawing of the door is made of any suitable material, including but not limited to metal plastic H 'Composite or any combination of the above. The inlaid portion plus % includes the outer peripheral portion 2G35G and the inner groove portion 2 (). The outer peripheral portion 2Q35 has the mention 32 200922852 for adding # s && & ah interlocking chamber 20100 The tolerance of the atmospheric pressure interface 20101 is adjusted to the appropriate thickness T. The outer peripheral portion 20350 has a length L of any suitable size and ^ D ( Figure 17), as shown in Figures 20 and 21, the door will extend through the edge of the door 2〇12〇 when the door is closed. Another embodiment 2〇1:5 The length L and the height D of the portion 20350 are appropriately sized such that the insert portion can extend through the door seal portion 2〇3 without passing through the door edge. The modified portion outer peripheral portion 20350 can have any suitable size. 2〇35〇 may have an opening 2〇21〇 disposed at an outer periphery thereof. The opening is any suitable opening for passage of a removable fastener, including but not limited to, from the load lock chamber 20100 The bolts and screws of the inlaid portion are removed. The inlaid portion of the inlaid portion is coupled to the loading and interlocking chamber 20100 by any suitable means including, but not limited to, chemical, magnetic and vacuum coupling. 20360 can constitute a substrate opening 20140 as a substrate for accessing the channel of the load lock chamber 2〇1〇0. As shown in the figure, the opening 2〇140 formed by the inner groove portion 20360 can have any suitable shape for the substrate and loading. One end of the substrate transport robot The device (or a portion thereof) passes through the opening 2〇14 (wherein the inner groove portion 20360 of the embodiment is dimensioned such that the body of the inner groove portion 20360 is held between the substrate and the substrate and at least the end effector The minimum groove distance. As shown in Fig. 21, the inner groove portion 20360 can extend through any suitable distance D2 of the back surface 2〇4〇〇 of the outer peripheral portion 2〇35〇. The inner groove portion 2〇36 of the present embodiment is extended. To the inner side 20410 of the load lock chamber 20420. The inner groove portion 2〇36〇 of the modified aspect may extend beyond or before the inner side surface 2〇41〇 of the load lock chamber 20420. In another variation, the inner groove portion 20360 may not extend beyond the back surface 20400 of the outer peripheral portion 2〇35〇. 33 200922852 The corresponding opening in the surface 20310 of the load lock chamber atmospheric interface 20101 may have an outer recess 20330 and an inner groove opening 20340. The depth of the outer concave portion 20330 is substantially equal to the thickness T of the outer peripheral portion 20350 of the inlaid portion 20130, and the length and height are greater than the length L and the height D of the inlaid portion 20130, thereby providing the outer peripheral portion 20350 and the recess 20330 of the inlaid portion 20130. Ample clearance around the surface allows the inlaid portion 20130 to be inserted and removed from the recess 20330. The recesses other than the modified aspect may have any suitable size. The recesses other than the modified aspect are designed to be pressed or mated with the inlaid portion 20130. The inner groove opening 20340 has an appropriate size such that the inner groove opening 20340 has an appropriate clearance between the inner groove portion 20360 and the inner groove portion 20360 of the inlaid portion 20130 to provide easy detachment and embedding of the inlaid portion 20130. The modified aspect of the clearance is minimized such that the inlaid portion 20130 is embedded in the outer recess 20330 and the inner slot opening 20340 to create a connection or press fit. Although the illustrated inlaid portion 20130 is disposed in the recess 20330', the back surface of the inlaid portion 20440 (see FIG. 21) of the modified aspect may be coupled to the surface 20310 of the load lock chamber 20100 (eg, the surface 20310 of the inlaid portion is not concave) . As detailed in Fig. 21, the back surface 20400 of the outer recess 20330 includes a recess 20221 surrounding the inner groove opening 20340. The groove 20221 in this embodiment is disposed between the opening 20340 of the inner groove portion and the opening 2〇21 of the detachable fixing member. The modified groove 20221 is disposed at any suitable relative position relative to the opening 20340 of the inner groove portion and the opening 20210 of the detachable fastener. Another modified embodiment of the recess is provided between the inner groove portion 20360 and the inner groove portion opening 2〇34〇. The groove 20221 is configured to receive and hold such as a 〇-shaped ring or any other suitable material, whereby the fixing member presses the sealing portion 20420 when the mounting portion 20130 is coupled to the loading interlocking chamber 2 在 in the recessed portion A sealing seal is created between the back surface 20400 of the 20330 and the inserting portion 20130 of 34 200922852, and the 20420 will maintain the vacuum or other control in the surface chamber 2G1GG in the sealing portion when the interlocking chamber 2 is cleaned for evacuation or exhaust. Atmosphere. The surface 2〇310 is not provided with a recess, and the sealing portion 20· can be provided, for example, as a seal. The vacuum between the other 2 coffee and the loading interlocking chamber frame. & can be maintained in the load lock chamber 20100 by any suitable means
ϋ山# 9m互鎖至之操作時,基板及/或轉移機器人可能撞擊 20150。之抢封表面2〇150而導致刮損或損壞該表面 m主冑封# 2G3GG上之廢棄物或摩損門㈣部2_〇亦將 、s、 = 20150。失效之門活動亦將導致門揸擊該表面2〇丨5〇 —&成破1 ^該表面2G15()之刮損及其他破壞將造成加載互鎖 室0 00内氛圍之泄漏。與其將加載互鎖室從基板加工系統上 拆^送至機製工廠進行修復,加載互鎖室之用戶可將損壞之 鑲飲β 2G13G卸下及替換新的鑲嵌部以使加載互鎖室及其相關 連加配備之關機時間縮減為最短。損壞之鑲|部係經設計使 表面20150可進行機製或修復使鑲嵌部可再循環使用。 本文所述之卸除式鑲嵌部20130可提供快速成本效益方式 以維持加載互鎖室2_之"介面2刪而不需因為損壞密 封表=而進行加載互鎖室之機製或替換。鑲㈣2G130與加載 互鎖室20100之間之密封部20220可維持加載互鎖室2〇42〇内 之真空或其他氛圍。在此所述之卸除式鎮嵌部可加人任何適當 之基板加工系統之門。 如第22圖所示,加載互鎖室模組5〇1〇〇係包括有構成艙室 50135之構架或罩箱5〇13〇(艙室頂部係被移開作為說明用途)。 35 200922852 其中一實施例之艙室50135係與外界氛圍隔離,並可保持真空 或任何其他適當控制或清淨氛圍。艙室50135在加載互鎖室模 組50100之側面設有基板運送開口 50116,50118。圖中所示運 送開口 50116,50118之位置僅作為實例說明,而變更態樣之艙 室可與模組之任何其他預期側面(例如®it鄰側面)之開口聯通。 艙室之各運送開口係由適當門/有槽閥50120 (圖中僅示其中一 個)予以個別關閉以使艙室50135與外界氛圍密封及隔離。其 中一實施例中之基板轉移裝置50110係至少一部份設置於艙室 50135内以運送基板S通過模組50100。另一實施例中,如以下 參照第1A及1B圖所述,加載互鎖室模組50100未設有基板轉 移以供設在諸如裝備前端模組及/或真空後端之加工工具或系統 之另一部份之基板運送裝置將基板置入及從加載互鎖室模組上 移除。另一實施例之加載互鎖室模組50100可包括任何適當基 板加工裝置,包括(但不限於)對準器,加熱器,冷卻器及度 量工具等。 本實施例之轉移裝置50110係如圖示具有旋轉式聯結於驅 動部(未予圖示)之一上臂部50111。變更態樣之轉移裝置具有 任何適當數目之上臂部。二前臂部50112,50113係在肘關節旋 轉式聯結於上臂部50111之端部。變更態樣之轉移裝置可具有 聯結於上臂部之多或少於二個前臂部。由此可知,各該前臂部 50112,50113包括有設以抓持一或多個基板之末端作用器或基 板抓持器50410 (見第23A圖)。適當轉移裝置之實例係見述於 2005年7月11日提出申請之美國專利申請案第11/179,762號, “不等長連桿選擇性順應關節式機器人臂部”;2005年4月12 36 200922852 曰提出申請之美國專利申請案第11/104,397號,“加載互鎖室之 快速交換雙基板運送裝置”;及美國專利案第6,918,731號,以 下將援引作為本案參考。變更態樣之轉移裝置50110係具有任 何適當臂連桿構造之任何適當轉移裝置,包括(但不限於)具 有支承驅動器,自承驅動器及磁性漂浮臂段件或連桿之轉移裝 置。 以下將予詳述,模組50100可設計以使通過模組50100及 加工工具之基板S之生產率增為最高,其中模組50100係聯結 同時使加載互鎖室模組50100之抽/排氣循環期間可能污染基板 之微粒之產生減為最低。 如前所述’加載互鎖室模組50100可聯通加工工具之各具 有不同氛圍(例如一側為惰性氣體而另一侧為真空,或一側為 常壓清淨空氣而另一側為真空/惰性氣體)之不同部份(未予圖 示)。本實施例之加載互鎖室模組5 01 〇〇可形成一搶室5 013 5以 供持留基板。變更態樣之加載互鎖室模組50100可具有超過一 個艙室,其中各艙室可進行隔離及具有配合毗連模組之工具部 之氛圍之艙室氛圍循環。實施例之加載互鎖室模組艙室5〇135 係密實以提供艙室氛圍之快速循環。When the ϋ山# 9m interlocks to operate, the substrate and/or transfer robot may hit 20150. The surface of the seal is 2〇150 and the surface is scratched or damaged. The waste on the main seal #2G3GG or the damage door (4) 2_〇 will also be s, = 20150. The failure gate activity will also cause the door to slam the surface 2〇丨5〇&&;; broke 1 ^ the surface 2G15() scratches and other damage will cause the atmosphere in the load lock chamber 0 00 to leak. Instead of removing the load lock chamber from the substrate processing system to the mechanism factory for repair, the user loading the lock chamber can remove and replace the damaged insert β 2G13G with a new insert to make the load lock chamber and its The shutdown time of the associated equipment is reduced to the shortest. The damaged inserts are designed such that the surface 20150 can be mechanismd or repaired to allow the inlay to be recycled. The detachable inlay 20130 described herein can provide a fast and cost effective way to maintain the loading/unlocking interface 2_"" interface 2 without the need to load or lock the interlocking chamber = mechanism or replacement. The seal 20220 between the insert (4) 2G130 and the load lock chamber 20100 maintains a vacuum or other atmosphere within the load lock chamber 2〇42〇. The removable housing inserts described herein can be incorporated into any suitable substrate processing system door. As shown in Fig. 22, the load lock chamber module 5〇1〇〇 includes a frame or cover box 5〇13〇 constituting the compartment 50135 (the top of the compartment is removed for illustrative purposes). 35 200922852 The compartment 50135 of one of the embodiments is isolated from the outside atmosphere and may be maintained in a vacuum or any other suitable control or clean atmosphere. The compartment 50135 is provided with substrate transport openings 50116, 50118 on the side of the load lock chamber mold set 50100. The locations of the transport openings 50116, 50118 shown are for illustrative purposes only, and the modified compartments may be in communication with the openings of any other intended side of the module (e.g., the adjacent side of the ®it). Each of the transport openings of the compartment is individually closed by a suitable door/slotted valve 50120 (only one of which is shown) to seal and isolate the compartment 50135 from the outside atmosphere. The substrate transfer device 50110 of one of the embodiments is at least partially disposed in the chamber 50135 for transporting the substrate S through the module 50100. In another embodiment, as described below with reference to Figures 1A and 1B, the load lock chamber module 50100 is not provided with substrate transfer for processing tools or systems such as equipment front end modules and/or vacuum back ends. Another portion of the substrate transport device places and removes the substrate from the load lock chamber module. The load lock chamber module 50100 of another embodiment can include any suitable substrate processing apparatus including, but not limited to, aligners, heaters, coolers, and metric tools. The transfer device 50110 of the present embodiment has an upper arm portion 50111 that is rotatably coupled to a driving portion (not shown) as shown. The modified embodiment of the transfer device has any suitable number of upper arms. The two forearm portions 50112, 50113 are rotatably coupled to the end portion of the upper arm portion 50111 at the elbow joint. The modified aspect transfer device can have more or less than two forearms coupled to the upper arm. Thus, each of the forearm portions 50112, 50113 includes an end effector or substrate gripper 50410 (see Figure 23A) that is configured to grip one or more substrates. An example of a suitable transfer device is described in U.S. Patent Application Serial No. 11/179,762, filed on Jul. 11, 2005. U.S. Patent Application Serial No. 11/104,397, the entire disclosure of which is incorporated herein by reference in its entirety in the entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire entire all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all all The modified aspect transfer device 50110 is any suitable transfer device having any suitable arm link configuration including, but not limited to, a transfer device having a support drive, a self-supporting drive, and a magnetic floating arm segment or link. As will be described in more detail below, the module 50100 can be designed to maximize the productivity of the substrate S through the module 50100 and the processing tool, wherein the module 50100 is coupled while simultaneously pumping/exhausting the load lock chamber module 50100. The generation of particles that may contaminate the substrate during this period is minimized. As described above, the load lock chamber module 50100 can have different atmospheres for each of the processing tools (for example, one side is an inert gas and the other side is a vacuum, or one side is a normal pressure clean air and the other side is a vacuum/the other side is a vacuum/ Different parts of inert gas (not shown). The load lock chamber module 5 01 本 of the embodiment can form a grab chamber 5 013 5 for holding the substrate. The modified load lock compartment module 50100 can have more than one compartment, wherein each compartment can be isolated and have a cabin atmosphere that matches the atmosphere of the tool section of the adjoining module. The load lock chamber module compartment of the embodiment is 5 135 dense to provide a rapid circulation of the cabin atmosphere.
以下將參第23A及23B圖詳細說明加載互鎖室模組 50130。艙室50135係設計成具有相對於組件在艙室5〇135内之 活動路徑及/或基板S通過艙室50135之路徑之最小内部體積。 其中一實把例中艙室50135之側壁Wl,W2係設計以配合基板 S及/或轉移裝置之臂部連桿50112之路徑,同時僅允許基板及/ 或臂部連桿與壁體Wl,W2之間之最小淨距。由第23A及23B 37 200922852 圖可見,壁體W1係設計以配合連接轉移裝置50110之上臂部 50111及前臂部50112之肘關節50460之拱形活動。本實施例中 之壁體W2係設計以配合基板s被轉移裝置50110承載通過加 載互鎖室模組50130時該基板S之邊緣之路徑。 本實施例中艙室50135之底部及/或頂部亦設計成僅提供加 載互鎖室模組50100與搶室50135之頂部及/或底部之活動組件 之間之最小淨距。舉例而言’擒室50135之底部之部份B1之表 面*相對於艘至50135之底部之部份B2之表面而升高(見第 23C圖)。例如該部份B1僅提供末端作用器與坐設其上之基板 之淨距,而該部份B2附加提供轉移裝置50110之上臂部5〇111 與前臂部50112,50113之淨距,藉此提供末端作用器與坐設其 上之基板之淨距。艙室之頂部亦可設計類似前述餘室5〇135之 底部。具有設計内部表面之加載互鎖室之適當實例係見述於 2005年4月12日提出申請之美國專利申請案第u/1〇4,397號, “加載互鎖室之快速轉換雙基板運送裝置”,及前述援引作為參 考之2〇〇7年5月18日立案之美國專利案第6,91 §,731號,“具 有快速轉換機器人之密實基板運送系統”。變更態樣之搶室可具 有任何適當形狀及設計以使内部體積減為最小。艙室5〇135之 最小化内部體積將使在抽排氣循環期間進出艙室5〇135之氣體 體積減為最少。此項氣體G之體積減少可縮減基板轉移通過加 載立鎖室模組50100之循環時間,因較少氣體G被抽出或引入 艘室50135。 再參照第23A及23B圖,艙室50135之内部表面(即頂部, 底部及侧壁)可設計以包括一或多個加熱元件(或表面)5〇45〇, 38 200922852 50451。其中一實施例之加熱元件50450,50451係埋設於艙室 50135之一或多個壁體内使艙室内之氣體G獲得加熱。本實施 例中在整個艙室内之氣體G可被加熱至大致平均溫度。變更態 樣之艙室之任何適當部份内之氣體G均可被加熱。另一變更態 樣之氣體G則未受到平均加熱。其他實施例之加熱元件亦將維 持艙室50135内之氣體G之溫度。舉例而言,可通過在預定升 溫之任何適當管線50455將氣體G引流入艙室内部空間。其中 一實施例中通過管線50455連接於艙室之氣體供源GS可包括有 一氣體加熱器50456,在氣體G被引入艙室之前將氣體G升溫 至預定溫度。變更態樣之氣體G係在被引入艙室50135之前以 任何適當方式予以加熱。 雖然僅顯示二個加熱元件50450,50451作為實例說明,須 知加載互鎖室模組亦可包括任何適當數目之加熱元件。本實施 例之加熱元件係適當設置或埋設於艙室壁體以加熱艙室壁體及 其内之氣體G。另一實施例之艙室50135壁體本身係作為加熱 元件。例如艙室50135之一或多個壁體之表面WS (或任何其他 適當部份)係設計為加熱元件以將熱轉移至艙室50135内之氣 體。變更態之一或多個加熱元件係模組化加熱元件,可卸離式 嵌裝於艙室壁體内β另一變更態樣之一或多個加熱元件係以任 何適當方式固定於艙室50135之表面。舉例而言,艙室壁體可 由諸如鋁合金(或任何其他適當材料)等傳導性材料製成。加 熱元件可固定於一或多個壁體之表面(内或外表面)使壁體被 傳導性加熱至預定溫度。 其中一實施例之加熱元件50450,50451係設置於艙室周圍 39 200922852 以提供任何適當加熱分佈。其中一實施例之加熱元件50450, 50451係設置以使艙室内之氣體G之溫度係大致均勻分佈於艙 室50135内。變更態樣之加熱元件係設置以產生溫度斜率。例 如艙室底部之溫度係比艙室頂部之溫度更高,於是在運送過程 在運送裝置内所產生之任何微粒將被載至艙室底部。可在艙室 50135底部提供適當過濾系統,可用以將因為溫度斜率作用而流 動至艙室底部之微粒予以持留。 加熱元件50450,50451係具有任何適當構造之任何適當加 熱元件。例如其中一實施例中之加熱元件係任何適當電子加熱 元件。另一實施例之加熱元件可包括設在艙室内壁體内之管道 以供熱流體通過壁體。該加熱元件可提升艙室50135之壁體之 溫度,於是壁體可適當增加艙室内氣體之溫度而使艙室50135 之抽氣期間所產生之微粒減為最少。在抽氣循環期間艙室50135 内之氣溫可表示如下: 丁GAS = 丁0 + (丁 對流一T 絶熱) [1] 其中T0係初始氣溫,T Μ係因氣體膨脹之降溫,而T#流係 因熱從壁體轉移至艙室所導致之升溫。絶熱溫度下降之變化速 率係表示如下: d丁绳熱 _TGASSeff ~ 1、 Γ〇ιThe load lock chamber module 50130 will be described in detail below with reference to Figures 23A and 23B. The compartment 50135 is designed to have a minimum internal volume relative to the active path of the assembly within the compartment 5〇135 and/or the path of the substrate S through the compartment 50135. In one embodiment, the side walls W1, W2 of the compartment 50135 are designed to match the path of the substrate S and/or the arm link 50112 of the transfer device, while only allowing the substrate and/or the arm link and the wall W1, W2. The minimum clear distance between them. As can be seen from Figures 23A and 23B 37 200922852, the wall W1 is designed to cooperate with the arched movement of the elbow joint 50460 of the upper arm portion 50111 and the forearm portion 50112 of the transfer device 50110. The wall W2 in this embodiment is designed to cooperate with the substrate s to be carried by the transfer device 50110 through the path of the edge of the substrate S when the interlocking chamber module 50130 is loaded. The bottom and/or top of the compartment 50135 in this embodiment is also designed to provide only a minimum clear distance between the movable components of the top and/or bottom of the load lock chamber module 50100 and the grab chamber 50135. For example, the surface of the portion B1 at the bottom of the chamber 50135 is raised relative to the surface of the portion B2 to the bottom of the 50135 (see Fig. 23C). For example, the portion B1 only provides the clear distance between the end effector and the substrate on which it is placed, and the portion B2 additionally provides the clear distance between the upper arm portion 5〇111 and the forearm portions 50112, 50113 of the transfer device 50110, thereby providing The distance between the end effector and the substrate on which it is placed. The top of the compartment can also be designed to resemble the bottom of the aforementioned chamber 5〇135. A suitable example of a load-locking chamber having a designed internal surface is described in U.S. Patent Application Serial No. U.S. Patent No. 4,397, the entire disclosure of which is incorporated herein by reference. And U.S. Patent No. 6,91 §, No. 731, filed on May 18, 2008, the disclosure of which is incorporated herein by reference. The changing room can have any suitable shape and design to minimize internal volume. Minimizing the internal volume of the chamber 5〇135 will minimize the volume of gas entering and exiting the chamber 5〇135 during the extraction cycle. This reduction in volume of gas G reduces the cycle time for substrate transfer through the loading of the lock chamber module 50100 as less gas G is drawn or introduced into the chamber 50135. Referring again to Figures 23A and 23B, the interior surfaces (i.e., the top, bottom and side walls) of the compartment 50135 can be designed to include one or more heating elements (or surfaces) 5〇45〇, 38 200922852 50451. The heating element 50450, 50451 of one of the embodiments is embedded in one or more walls of the chamber 50135 to heat the gas G in the chamber. The gas G throughout the chamber in this embodiment can be heated to a substantially average temperature. The gas G in any suitable portion of the compartment of the altered state can be heated. Another modified state of the gas G is not subjected to average heating. The heating elements of other embodiments will also maintain the temperature of the gas G within the compartment 50135. For example, gas G can be directed into the interior of the cabin by any suitable line 50455 at a predetermined temperature rise. The gas supply GS, which in one embodiment is connected to the chamber via line 50455, may include a gas heater 50456 that warms the gas G to a predetermined temperature before it is introduced into the chamber. The modified gas G is heated in any suitable manner prior to being introduced into the chamber 50135. Although only two heating elements 50450, 50451 are shown as an example, it is to be understood that the load lock chamber module can also include any suitable number of heating elements. The heating element of this embodiment is suitably disposed or embedded in the chamber wall to heat the chamber wall and the gas G therein. The wall of the compartment 50135 of another embodiment is itself a heating element. For example, the surface WS (or any other suitable portion) of one or more of the walls 50135 is designed as a heating element to transfer heat to the gas within the compartment 50135. One or more of the heating elements are modularized heating elements that are detachably embedded in the chamber wall β. One or more of the other aspects of the heating element are secured to the compartment 50135 in any suitable manner. surface. For example, the cabin wall may be made of a conductive material such as an aluminum alloy (or any other suitable material). The heating element can be attached to the surface (inner or outer surface) of the one or more walls to thermally heat the wall to a predetermined temperature. Heating elements 50450, 50451 of one of the embodiments are disposed around the chamber 39 200922852 to provide any suitable heating profile. The heating elements 50450, 50451 of one of the embodiments are arranged such that the temperature of the gas G in the chamber is substantially evenly distributed within the chamber 50135. The altered heating element is set to produce a temperature slope. For example, the temperature at the bottom of the chamber is higher than the temperature at the top of the chamber, so any particles generated in the transport during transport will be carried to the bottom of the chamber. A suitable filtration system can be provided at the bottom of the compartment 50135 to hold the particles that flow to the bottom of the compartment due to the temperature slope. Heating elements 50450, 50451 are any suitable heating elements of any suitable configuration. For example, the heating element of one of the embodiments is any suitable electronic heating element. Another embodiment of the heating element can include a conduit disposed within the interior wall of the chamber for the passage of heated fluid through the wall. The heating element raises the temperature of the wall of the compartment 50135 so that the wall appropriately increases the temperature of the gas in the compartment to minimize particulates generated during pumping of the compartment 50135. The temperature in the chamber 50135 during the pumping cycle can be expressed as follows: Ding GAS = D + 0 + (Ding convection - T adiabatic) [1] where T0 is the initial temperature, T Μ is due to gas expansion, and T# flow It is caused by heat transfer from the wall to the cabin. The rate of change of the adiabatic temperature drop is expressed as follows: d Ding rope heat _TGASSeff ~ 1, Γ〇ι
~dT~~~V~( J L J 其中TGAS係現有氣體溫度,seff係有效泵抽速率,v係加載 互鎖室體積而γ係氣體熱容量比例。變更態樣可採用任何適當 方程式以定義絶熱降温。如式[2]所示,欲減低絶熱降溫之變化 40 200922852 速率時,可減低泵抽速率或增加艙室體積,兩者均會導致泵抽 時間之增加。 參照第24圖,艙室壁體溫度之增加將增加因對流所產生之 熱量。對流al溫度之改變速率可示如下式: ~^T=^F(t〇_Tgas) [3] 其中h係對流熱轉移係數,S係加載互鎖室表面積,ρ係氣 , 體密度及Cv係氣體熱容量。變更態樣可採用任何適當方程式以 定義對流溫度之改變速率。作為實例說明,如果在抽氣循環期 間艙室内之氣體溫度保持於20°C,氣體將保留在該區域内而沒 有產生任何微粒。由第24圖可見,另一實施例中在抽氣循環期 間艙室内之氣體初始溫度可藉諸如艙室50135之壁體與氣體G 之間之對流熱轉移等方式予以增加,於是在絶熱膨脹期間氣體 溫度減低時,在增加或最大泵抽速率下抽氣期間之氣體溫度將 不致處於微粒產生之區域。見第24圖,線條L1-L4代表相對於 諸如艙室50135之加載互鎖室之抽氣循環之抽氣時間之氣體溫 度。如第24圖所示,提升氣體初始溫度或維持氣體溫度於微粒 ' 產生溫度以上(通過艙室壁體與氣體之間之對流熱轉移)可允 許最長抽氣時間同時保持於無微粒區域内。 在某些情況下要保持極高艙室壁體溫度並不實際。本實施 例中加載互鎖室50100之表面積與體積之比例係最大化(以類 似前述參照第23A及23B圖所述方式)以產生加熱壁體至氣體 之最佳對流熱轉移。最大化之艙室50100之表面積與體積之比 例及加熱之艙室壁體將促成加載互鎖室有最短抽氣循環時間, 41 200922852 同時可防止在艙室50100内產生微粒。 其中一實施例之加載互鎖室50135亦可設計以提供最短排 氣循環時間。一實施例中,加載互鎖室50135内之微粒產生及 污染可藉保持非亂流或層流氣體進入加載互鎖室50135内之方 式予以減為最低或予以避免。其中一實施例中,氣流之雷諾係 數Re係低於2300左右。變更態樣係採用任何適當雷諾係數或 流體特性。任何特定排氣集流管之雷諾係數可藉下式予以計算:~dT~~~V~( JLJ where TGAS is the current gas temperature, seff is the effective pumping rate, v is the load lock chamber volume and the γ system gas heat capacity ratio. Any suitable equation can be used to define the adiabatic cooling. As shown in equation [2], to reduce the adiabatic cooling temperature change 40 200922852 rate, the pumping rate can be reduced or the cabin volume can be increased, both of which will lead to an increase in pumping time. Refer to Figure 24, cabin wall temperature The increase of the degree will increase the heat generated by the convection. The rate of change of the convection al temperature can be expressed as follows: ~^T=^F(t〇_Tgas) [3] where h is the convective heat transfer coefficient, and the S system is loaded with each other. Lock chamber surface area, ρ system gas, bulk density and Cv system gas heat capacity. Any suitable equation can be used to define the rate of change of convective temperature. As an example, if the gas temperature in the chamber is maintained at 20 during the pumping cycle °C, the gas will remain in this area without any particles. As can be seen from Fig. 24, in another embodiment, the initial gas temperature in the chamber during the pumping cycle can be borrowed from the wall of the chamber 50135 and the gas G. The convection heat transfer between the two is increased, so that when the gas temperature is lowered during the adiabatic expansion, the gas temperature during the pumping at the increased or maximum pumping rate will not be in the region where the particles are generated. See Figure 24, line L1- L4 represents the gas temperature relative to the pumping time of the pumping cycle of the load lock chamber, such as chamber 50135. As shown in Fig. 24, the lift gas initial temperature or the maintenance gas temperature is above the particle's generation temperature (through the chamber wall) The convective heat transfer between the gas and the gas allows the longest pumping time to be maintained in the particle-free region at the same time. In some cases it is not practical to maintain a very high chamber wall temperature. In this embodiment, the interlocking chamber 50100 is loaded. The ratio of surface area to volume is maximized (in a manner similar to that described above with reference to Figures 23A and 23B) to produce optimal convective heat transfer from the heated wall to the gas. Maximizing the surface area to volume ratio of the chamber 50100 and heating The cabin wall will contribute to the load lock chamber with the shortest pumping cycle time, 41 200922852 while preventing the generation of particles in the chamber 50100. The load lock chamber 50135 of the embodiment can also be designed to provide the shortest exhaust cycle time. In one embodiment, particulate generation and contamination within the load lock chamber 50135 can be achieved by maintaining non-turbulent or laminar gas into the load lock chamber. The method within 50135 is minimized or avoided. In one embodiment, the Reynolds coefficient Re of the airflow is less than about 2300. The modified state is any suitable Reynolds coefficient or fluid property. Any particular exhaust manifold The Reynolds coefficient can be calculated by the following formula:
Re =p— [4] 其中p係氣體密度,υ係氣體速度,Μ系流動管道之直徑及 η係氣體黏度。變更態樣可採用任何適當方程式以測定雷諾係 數。其中一實施例之氣流與最高氣流之比例不宜超0.5至0.6而 變更態樣之比例係任何適當值。須知艙室135内之軟排氣與快 速排氣之交迭壓力係取決於幾何形狀,並介於數托(torr)至數百 托之範圍,並可藉諸如實驗方式等任何適當方式予以測定。 再參照第1A及1B圖所示之加載互鎖室100之另一實施 例。本實施例之加載互鎖室10包括有疊置之加載互鎖室14A, 14B (圖示之二加載互鎖室僅作為實例說明,變更態樣中之加載 互鎖室10可具有超過或少於二個艙室)。各該加載互鎖室14A, 14B係大致類似前述艙室50135,於是各艙室包括一或多個加熱 元件及具有最大化之内部面積與體積之比例以有效加熱各艙室 内之氣體。本實施例之加載互鎖室14A,14B不包括基板運送裝 置,然而變更態樣之一或多個艙室14A,14B可包括一基板運送 裝置。如第1A及1B圖所示,加載互鎖室模組10可具有任何適 42 200922852 當數目之排氣閥42A,42B。雖然圖中顯示二個排氣閥42A, 42B,須知可設置超過或少於二個排氣閥。各排氣閥42A,42B 係如前述之模組化排氣閥。變更態樣之排氣閥可具有任何適當 構造。排氣閥42A,42B係經設計使氣體之高容積流動速率可流 經閥門以低均勻氣體速度進入艙室14A,14B。自埠口 50650A, 50650B (類似前述參照第7B圖所述之埠口 36A’-37B’)排出之 氣體具有低速層流之定義雷諾係數,並可防止微粒澱積於加載 互鎖室模組10之基板上。其中一實施例之各個排氣閥42A,42B 可包括一擴散器/過濾器651,安裝於排氣管線相對於其中一個 艙室698,699之入口處。本實施例之擴散器651係如圖示設置 於埠口 650A,650B,而變更態樣中之擴散器係設置於相對於相 對艙室14A,14B之任何適當位置。該擴散器/過濾器50651係 任何適當擴散器/過濾器。其中一實施例之擴散器/過濾器5〇651 係設計以減少入口微粒濃度約九個數量級,有超過大約 0.003xl(T6m直徑之去除速率。艙室14A,14B之最短排氣時間 係取決於相對艙室14A,14B之内部體積。其中一實施例之驗室 14A,14B之内部體積係最適化以類似前述參照第23A及UR 圖之方式使生產率最大化。 以下將參照第25圖說明具有最適化抽排循環時間之加載互 鎖室模組50700之操作。該加載互鎖室模組5〇7〇〇係類似前述 加載互鎖室模組50100,可包括如前述之最小化内部加载互鎖室 體積,加熱加載互鎖室壁體及最適化排氣閥之任何適當組合。 本實施例之加載互鎖室模組50700係將前端模組5〇72〇與&空 後端部相連接,包括真空艙室50710及加工模組其中加^ 43 200922852 互鎖室模組50700不包括基板運送裝置,而變更態樣之加載互 鎖室模組50700可包括基板運送裝置。舉例而言,利用設在裝 備前端模組(EFEM)50720内之運送器50721將基板從加載埠 50725轉移進入加載互鎖室模組50700。利用諸如真空後端部 50710之運送器50711將基板從加載互鎖室模組50700移除及轉 移至一或多個加工模組PM。將基板從加工模組PM轉移返回加 載埠50725係以大致逆向方式進行。本實施例之運送器5〇721 係設計以快速轉換基板並包括諸如複數個運送臂。適當之運送 器包括(但不限於)前所援引作為參考之美國專利申請案第 11/179,762號;第U/i〇4,397號;及美國專利案第6,918,731號 所揭述者。其他適當之轉移裝置包括美國專利案第5,72〇,59〇, 5,899,658號,美國專利公開案第2003/0223853號及2008年5 月8日提出申請之美國專利申請案第12/117,355號,“基板運送 裝置”,以下援引作為本案參考。 操作時運送器50721將基板通過聯結EFEM 50720與加載 互鎖室模組50700之開放常壓閥轉移進入加載互鎖室模組 50700 (區塊50750)。加載互鎖室模組50700係與EFEM 50720 隔離並被抽氣成真空以與真空後端部50710產生介面(區塊 50751 )。聯結加載互鎖室模組50700與後端部50710之有槽閥 係開啟以供運送器50711將基板轉換進/出加載互鎖室模組 50700 (區塊50752)。加載互鎖室模組50700係與後端部5〇71〇 隔離並排氣以與前述EPEM 50720產生介面(區塊50753)。在 加載互鎖室模組50700與EPEM 50720產生介面時,後端部 50710之運送器50711將基板轉換進/出加工模組ρΜβ經過加工 44 200922852 之基板係回返至加載互鎖室模組50700而未加工之基板係在繼 後加載互鎖室模級轉換循環(例如區塊50754)中從加載互鎖室 50700中被取出。如第25圖所示,加載互鎖室模組5〇7〇〇係設 a十使其排亂及抽瑕^盾環時間50760..係與後端部50710之基板加 工之循環時間大致相同(或更短),於是將使通過加工工具5〇79〇 之基板生產率成為最大《根據實施例,從加工模組移除之基板 在通過加載互鎖室50700及運送返回諸如加載埠('或工具5二9〇 之任何其他適當部份)之前可能不需要予以緩衝。例如參照第 26圖,具有傳統加載互鎖室模組之加卫卫具及具有本實施例之 加載互鎖室模組之加工工具係進行比較。除了加載互鎖室模組 以外’用以產生如第26圖所示圖表之加卫工具之任何其他部件 係大致相同。如第26 _減作為實例說明,具有傳統加載互 鎖室模組之傳統加U具之晶圓生產率係如線條5麵所示為 大約每小時150個晶圓(基板)’而具有本實施例之加工工具之 生產率係如線條50810所示之大約每小時2〇〇個晶圓。 根據實施例,在抽氣前加載互鎖室内之氣體之初始溫度將 獲得充份提升’於是當氣體發生絶熱膨脹時該溫度將不致降至 加載互鎖室抽氣期間產生微粒之狀範圍以下。内部體積亦將 被最適化以提供快速排氣時間,同時增加從諸如搶室壁體至加 載互鎖室模組内氣體之對流熱轉移,藉此防止或使抽氣期間所 產生之微粒減為最少或獲得阻遏。加栽互鎖室模組5麵之排 氣閥亦被最適化以防止減期產生—。上述特徵之任何適 當組合可提供抽氣及排氣循環期間之更高I抽速度,於是將產 生通過加載互鎖室模組100之基板生產率。 45 200922852 本案一實施例提供一種丰道 且句括*播“,種半導體加工工具。該半導體加工工 具,括有一構成至少一艙室之構架,該搶室具有 沿著開口周緣之密封表面,提供— 、有 封該開口,及設在構架之門一側 =心 閱口夕其缸+結必、τ 芏夕驅勤器,係大致與通過 土 轉移平面大致平行,該至少一個驅動 部份設在密封表面前端之熟哭 ν個㈣具有至少 ㈣之傳動㈢’而驅Re = p— [4] where p is the gas density, the enthalpy gas velocity, the diameter of the lanthanide flow conduit, and the η-system gas viscosity. The variant can be determined using any suitable equation to determine the Reynolds number. In one embodiment, the ratio of the gas flow to the highest gas flow should not exceed 0.5 to 0.6 and the ratio of the modified aspect is any suitable value. The overlap pressure between the soft exhaust and the fast exhaust in the compartment 135 depends on the geometry and ranges from a few torr to hundreds of Torr and can be determined by any suitable means such as experimental means. Referring again to another embodiment of the load lock chamber 100 shown in Figures 1A and 1B. The load lock chamber 10 of the present embodiment includes stacked load lock chambers 14A, 14B (the two load lock chambers are illustrated as an example only, and the load lock chamber 10 in the modified aspect may have more or less In two cabins). Each of the load lock chambers 14A, 14B is substantially similar to the aforementioned chamber 50135, such that each chamber includes one or more heating elements and has a maximized ratio of internal area to volume to effectively heat the gases within each chamber. The load lock chambers 14A, 14B of the present embodiment do not include a substrate transport device, however, one or more of the compartments 14A, 14B may include a substrate transport device. As shown in Figures 1A and 1B, the load lock chamber module 10 can have any number of exhaust valves 42A, 42B. Although two exhaust valves 42A, 42B are shown, it is noted that more or less than two exhaust valves may be provided. Each of the exhaust valves 42A, 42B is a modular exhaust valve as described above. The venting valve of the modified aspect can have any suitable configuration. Exhaust valves 42A, 42B are designed such that a high volumetric flow rate of gas can flow through the valve into the chambers 14A, 14B at a low uniform gas velocity. The gas discharged from the port 50650A, 50650B (similar to the port 36A'-37B' described above with reference to FIG. 7B) has a definition of the Reynolds coefficient of the low velocity laminar flow and prevents the particles from being deposited on the load lock chamber module 10 On the substrate. Each of the exhaust valves 42A, 42B of one of the embodiments may include a diffuser/filter 651 mounted at the inlet of the exhaust line relative to one of the compartments 698, 699. The diffuser 651 of the present embodiment is disposed as shown in the cornices 650A, 650B, and the diffuser in the modified aspect is disposed at any suitable position relative to the opposing compartments 14A, 14B. The diffuser/filter 50651 is any suitable diffuser/filter. The diffuser/filter 5 651 of one embodiment is designed to reduce inlet particle concentration by about nine orders of magnitude, with more than about 0.003 x 1 (T6 m diameter removal rate. The minimum exhaust time of chambers 14A, 14B is dependent on relative The internal volume of the chambers 14A, 14B. The internal volume of the chambers 14A, 14B of one embodiment is optimized to maximize productivity in a manner similar to that described above with reference to Figures 23A and UR. The following description will be made with reference to Figure 25 for optimization. The operation of the load lock chamber module 50700 of the pumping cycle time. The load lock chamber module 5〇7〇〇 is similar to the aforementioned load lock chamber module 50100, and may include a minimized internal load lock chamber as described above. The volume, the heating load lock chamber wall body and any suitable combination of the optimal exhaust valve. The load lock chamber module 50700 of the embodiment connects the front end module 5〇72〇 with the & empty rear end portion. Including the vacuum chamber 50710 and the processing module, wherein the interlocking chamber module 50700 does not include a substrate transport device, and the modified load lock chamber module 50700 can include a substrate transport device. For example, The substrate is transferred from the loading cassette 50725 into the load lock chamber module 50700 using a carrier 50721 disposed within an equipment front end module (EFEM) 50720. The substrate is loaded from the load lock chamber using a carrier 50711 such as a vacuum rear end portion 50710 The module 50700 is removed and transferred to one or more processing modules PM. Transferring the substrate from the processing module PM back to the loading cassette 50725 is performed in a substantially reverse manner. The carrier 5〇721 of the present embodiment is designed to be quickly converted. The substrate includes, for example, a plurality of transport arms. Suitable transporters include, but are not limited to, U.S. Patent Application Serial No. 11/179,762, the disclosure of which is incorporated herein by reference. Other suitable transfer devices include U.S. Patent Nos. 5,72,59,5,899,658, U.S. Patent Publication No. 2003/0223853, and U.S. Patent Application Serial No. No. 12/117,355, "Substrate Transport Device", hereinafter referred to as a reference in this case. In operation, the carrier 50721 transfers the substrate through the open normal pressure valve of the EFEM 50720 and the load lock chamber module 50700. Load the interlock chamber module 50700 (block 50750). The load lock chamber module 50700 is isolated from the EFEM 50720 and evacuated to create a interface with the vacuum rear end 50710 (block 50751). The slotted valve system of the chamber module 50700 and the rear end portion 50710 is opened for the carrier 50711 to convert the substrate into/out of the load lock chamber module 50700 (block 50752). The load lock chamber module 50700 is isolated from the rear end portion 5〇71〇 and vented to create an interface with the aforementioned EPEM 50720 (block 50753). When loading the interlocking chamber module 50700 and the EPEM 50720 to create an interface, the carrier 50711 of the rear end portion 50710 converts the substrate into/out processing module ρΜβ through the substrate of the processing 44 200922852 and returns to the loading and interlocking chamber module 50700. The unprocessed substrate is removed from the load lock chamber 50700 in a subsequent load lock chamber mode transition cycle (e.g., block 50754). As shown in Fig. 25, the load lock chamber module 5〇7〇〇 is set to ten to cause it to be undone and the 盾^ shield ring time is 50760. The cycle time of the substrate processing with the rear end portion 50710 is substantially the same. (or shorter), the substrate productivity through the processing tool will be maximized. According to an embodiment, the substrate removed from the processing module is loaded through the load lock chamber 50700 and shipped back such as loading 埠 ('or Tools 5, 2, and any other appropriate part may not need to be buffered before. For example, referring to Fig. 26, a fastener having a conventional load lock chamber module and a processing tool having the load lock chamber module of the present embodiment are compared. Except for loading the interlocking chamber module, any other components used to create the security tool as shown in Figure 26 are substantially identical. As shown in the example of FIG. 26, the conventional wafer load productivity of the conventional load lock chamber module is as shown by the line 5, which is about 150 wafers per substrate (substrate). The productivity of the processing tool is approximately 2 wafers per hour as indicated by line 50810. According to an embodiment, the initial temperature of the gas loaded into the interlocking chamber prior to pumping will be sufficiently enhanced' so that the temperature will not fall below the range of particulates generated during pumping of the load lock chamber when the gas undergoes adiabatic expansion. The internal volume will also be optimized to provide fast venting time while increasing convective heat transfer from gases such as the chamber wall to the load lock chamber module, thereby preventing or reducing particulates generated during pumping down to At least or get a repression. The exhaust valves of the 5 sides of the interlocking chamber module are also optimized to prevent downtime. Any suitable combination of the above features provides a higher I pumping speed during the pumping and exhaust cycle, which will result in substrate throughput through the loading of the interlocking chamber module 100. 45 200922852 An embodiment of the present invention provides a semiconductor processing tool for a semiconductor processing tool, comprising: a frame constituting at least one chamber having a sealing surface along a circumference of the opening, provided - The opening is provided, and the side of the door of the frame is placed on the side of the door of the frame = the heart of the mouth, the cylinder + the knot, the τ 芏 驱 驱 , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , The front end of the sealing surface is cautious (four) has at least (four) transmission (three)'
使門移動於密封狀態之間,1中 HUM ,L/ 再肀至少一個驅動器係設在基板轉 移區之外側以將基板通過開口轉移進錄I 板轉 本發一實施例係提供一種半導體加工工 ==具有—構成至少—艙室之構架,該構架具有一= 料设在凹部内之至少—個孔口以供存取相對之至少一個搶 至,有一却離式門鑲嵌部聯結於構架,該門鑲嵌部具有設計以 配合凹部之外周緣部’並具有與外周緣部呈單體構造之内槽 二3 = 少—孔口 ’利用連接於構架之至少 智k 孔口 ’該至少一門具有門密封部以與外周緣 抑成介面以密封該至少一孔口,及在凹部設有至少一門镶喪 :密封部以圍繞於各該至少一孔口,該至少一門鑲嵌部密封部 係與門鑲嵌部相異,並設計以與門鑲嵌部產生介面 嵌部與構架之間之密封部。 & 另一項實施例係提供一财置。該裝置包括有第—舱室, 於第-艙室内設有第-冷卻表面,第—基板支承係設置於 第-搶室内及設相支承第—基板,及第—夹頭至少部份設在 第一艙至内,該第一夾頭具有第二冷卻表面大致設在第一冷卻 表面之對侧,而第二基板支承係衍生自第H第二基板支 46 200922852 承係設計以支承第二基板,其中該第一夾頭係在加載位置與冷 卻位置之間移動自如,其中當位於冷卻位置時第二冷卻表面係 大致接觸第一基板之表面,而第一冷卻表面係大致接觸第二基 板之表面。 再一項實施例係提供一種裝置。該裝置包括有構成隔離式 艙室之構架,用以支承至少一基板,該隔離式艙室包括艙室壁 體及合併於艙室壁體用以加熱艙室壁體之至少一個加熱元件, 其中該艙室壁體係設計使艙室壁體表面積與隔離式艙室體積之 比例係最大化,藉此促成艙室壁體與隔離式艙室内氣體之間之 最適熱轉移。 須知實施例可單獨或以任何組合方式予以運用須知前述說 明僅用以闡述實施例。精於此藝者當可在不脫離本實施例之情 況下作成多項替代及變更態樣。因此本實施例擬用以涵蓋在本 案申請專利範圍内之所有替代,改良及變更態樣。 【圖式簡單說明】 第1A-1B圖係具有由不同透視方向顯示之實施例之特徵之 一基板加工搶模組之示意透視圖; 第1C-1E圖係該模組之另一方向之另一示意透視圖; 第1F圖係該模組之分解圖; 第2及第3圖係具有實施例特徵之基板加工工具之示意圖; 第4A-4B圖係分別為該模組之斷面圖及放大局部斷面圖; 第5A-5B圖係另一實施例之模組與基板運送裝置之另一斷 面圖; 47 200922852 第6圖係連接於另一實施例之加工工具之另一部份之模組 之立面圖; 第7A-7B圖分別為另一實施例之艙室模組之另一局部透視 圖與斷面圖; 第8A-8D圖係另一實施例之閥模組之不同示意透視圖; 第9圖係另一實施例之模組之部份之示意斷面圖; 第10A圖係另一實施例之艙室模組之分解透視圖,及第 圖係該模組之斷面圖; 第11 A- 11B圖分別顯不該模組在不同位置下之另一斷面 圖’第lie圖係該模組與基板之部份之局部斷面圖,第 圖係該模組在不同位置下之透視斷面圖; 第12A-12B圖係另一實施例之模組之另一斷面圖; 第13圖係另一實施例之模組之局部斷面圖; 第14A,14B圖顯示一實施例之兩種構造之加載互鎖室; 第14C圖顯示一實施例之加載互鎖室之頂面圖;Moving the door between the sealed states, in which the HUM, L/, and at least one driver are disposed on the outer side of the substrate transfer area to transfer the substrate through the opening into the recording board. The embodiment provides a semiconductor processing tool. == having a frame forming at least one of the compartments, the frame having at least one aperture disposed in the recess for accessing at least one of the apertures, and a separate door inlay coupled to the frame, the The door inlay has a design designed to fit the outer peripheral portion of the recess and has an inner groove with a single structure with the outer peripheral portion. 2 = less - the opening ' utilizes at least one k-port connected to the frame' The sealing portion is configured to seal the at least one opening with the outer peripheral edge, and at least one door is provided in the concave portion: a sealing portion surrounding each of the at least one opening, the at least one door inlaid portion sealing portion and the door inlay The parts are different and are designed to create a seal between the interface insert and the frame with the door inlay. & Another embodiment provides a wealth. The device includes a first chamber, a first cooling surface is disposed in the first chamber, a first substrate supporting system is disposed in the first chamber and the phase supporting substrate is disposed, and the first chuck is at least partially disposed In a compartment, the first chuck has a second cooling surface disposed substantially opposite the first cooling surface, and the second substrate support is derived from the Hth second substrate branch 46 200922852 to support the second substrate Wherein the first collet is movable between a loading position and a cooling position, wherein the second cooling surface substantially contacts the surface of the first substrate when in the cooling position, and the first cooling surface is substantially in contact with the second substrate surface. Yet another embodiment provides an apparatus. The apparatus includes a frame forming an isolated compartment for supporting at least one substrate, the isolated compartment including a cabin wall and at least one heating element incorporated in the compartment wall for heating the cabin wall, wherein the compartment wall system design The ratio of the wall surface area of the compartment to the volume of the isolated compartment is maximized, thereby facilitating optimal heat transfer between the chamber wall and the gas in the isolated compartment. It is to be understood that the embodiments may be used alone or in any combination. The foregoing description is only illustrative of the embodiments. It will be apparent to those skilled in the art that many alternatives and modifications can be made without departing from the embodiments. Therefore, the present embodiments are intended to cover all alternatives, modifications and variations in the scope of the application. BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1A-1B is a schematic perspective view of a substrate processing module having features of embodiments shown in different perspective directions; 1C-1E is another direction of the module. 1A is an exploded view of the module; 2 and 3 are schematic views of a substrate processing tool having the features of the embodiment; and 4A-4B are respectively a sectional view of the module and 5A-5B is another sectional view of the module and substrate transport device of another embodiment; 47 200922852 Fig. 6 is another part of the processing tool connected to another embodiment An elevational view of the module; Figures 7A-7B are another partial perspective and cross-sectional view of the compartment module of another embodiment; 8A-8D is a different embodiment of the valve module of another embodiment BRIEF DESCRIPTION OF THE DRAWINGS FIG. 9 is a schematic cross-sectional view of a portion of a module of another embodiment; FIG. 10A is an exploded perspective view of a compartment module of another embodiment, and FIG. Fig. 11A-11B shows another section of the module in different positions. A partial cross-sectional view of a portion of the substrate, a cross-sectional view of the module at different positions; and 12A-12B are another cross-sectional view of the module of another embodiment; A partial cross-sectional view of a module of another embodiment; 14A, 14B shows a load lock chamber of two configurations of an embodiment; and FIG. 14C shows a top view of a load lock chamber of an embodiment;
第14D及14E圖顯示一實施例之兩種構造之加載互鎖室之 前視圖; 第15圖係具有實施例之特徵之加載互鎖室; 第15A ’ 15B圖顯示一實施例之門驅動系統之一部份; 第16圖顯示具有實施例特徵之加工系統之斷面圖; 第16A圖係如第16圖所示之實施例之加載互鎖室之頂面 1SI · 團, 第16B及16C圖係如第16圖所示之實施例之加載互鎖室之 兩種構造之前視圖; 48 200922852 第17圖係具有實施例特徵之加載互鎖室之等距圖; 第18圖係一實施例之加載互鎖室/門介面之等距圖; 第19圖顯示一實施例之門位於第一位置之加載互鎖室/門 介面之斷面圖; 第20圖顯示一實施例之門位於第二位置之加載互鎖室/門 介面之斷面圖; 第21圖係第20圖之加載互鎖室/門介面之另一斷面圖; 第22圖係具有實施例特徵之加載互鎖室模組之一部份之示 意透視圖; 第23A-23C圖顯示一實施例之加載互鎖室模組; 第24圖係顯示實施例之特徵之圖; 第25圖顯示一實施例之加工工具與關連性流程表;及 第26圖顯示一實施例之關於基板生產率之圖。 【主要元件符號說明】 10 基板加工模組 12,13 閥 14 艙室 14A,14B 基板維持艙 16,18 基板運送開口 20,22 頂部與底部封蓋 22A,22B 支承架 24A,24B 基板冷卻表面 26 空隙 27冷卻區塊 30 骨架構架 32, 34 頂部與底部蓋體 36A,36B 真空埠口 49 200922852 37A,37B 排氣埠口 38A,38B,39A,39B 配對介面 40A, 40B 真空控制閥 42A, 42B 排氣閥 42VB 閥本體 44A 擴散器 54 氣埠 100 加載互鎖室模組 114A ,114B 加載互鎖室 120A ,120B 冷卻夾頭 121A ,121B 延伸部 124A 接觸面 150A ,152A 輻射翼片 152A 熱槽 600 常壓前端部 605 加載埠模組 610 加載互鎖真空室 620 真空後端部 625 運送艙 630 加工站 640 加載埠 650 匣盒 650A ,650B 埠口 651 擴散器/過濾器 660 微型環境 690 半導體工具站 691 控制器 710 基板加工工具 712 工具介面部 718 運送艙模組 750, 760,770 介面 780 基板運送裝置 1001 、1002導管 10100 加載互鎖室 10130,10120 常壓加載互鎖室門 10140 第一加載互鎖室 50 200922852 10150 第二加載互鎖室 10160 , 10161 真空加載互鎖室門 10200 , 10210 驅動模組 10200A ,10210A 上側驅動傳動器 10200B ,10210B 下側驅動傳動器 10230 密封接觸表面 20100 加載互鎖室 20101 常壓介面 20102 真空介面 20120 常壓門 20125 門驅動單元 20130 門鑲嵌部 20330 外侧凹部 20340 内槽部開口 20350 外周部 20360 内槽部 20400 背面 50110 基板轉移裝置 50111 上臂部 50112 ,50113前臂部 50116 , 50118 基板運送開口 50450 , 50451 加熱元件 50455 管線 50460 肘關節 50650A ,50650B 埠口 50710 真空艙室 50720 前端模組 50721 運送器 50725 加載埠 50790 加工工具 51Figures 14D and 14E show a front view of a load lock chamber of two configurations of an embodiment; Fig. 15 is a load lock chamber having the features of the embodiment; and Fig. 15A '15B shows a door drive system of an embodiment. Part 16; Figure 16 shows a cross-sectional view of a processing system having the features of the embodiment; Figure 16A is a top surface of the load lock chamber of the embodiment shown in Figure 16 1SI · Group, Figures 16B and 16C A front view of two configurations of the load lock chamber of the embodiment shown in Fig. 16; 48 200922852 Fig. 17 is an isometric view of the load lock chamber having the features of the embodiment; Fig. 18 is an embodiment An isometric view of the load lock chamber/door interface; Figure 19 shows a cross-sectional view of the load lock chamber/door interface of the door of the embodiment in a first position; Figure 20 shows a door of an embodiment in a second Sectional view of the load lock chamber/door interface; Fig. 21 is another sectional view of the load lock chamber/door interface of Fig. 20; Fig. 22 is a load lock chamber mold having the characteristics of the embodiment A schematic perspective view of a portion of the set; Figures 23A-23C show a load lock chamber of an embodiment Fig. 24 is a view showing the features of the embodiment; Fig. 25 is a view showing the processing tool and the related flow chart of an embodiment; and Fig. 26 is a view showing the productivity of the substrate in an embodiment. [Main component symbol description] 10 substrate processing module 12, 13 valve 14 compartment 14A, 14B substrate maintenance compartment 16, 18 substrate transport opening 20, 22 top and bottom cover 22A, 22B support frame 24A, 24B substrate cooling surface 26 gap 27 Cooling block 30 Skeleton frame 32, 34 Top and bottom cover 36A, 36B Vacuum port 49 200922852 37A, 37B Exhaust port 38A, 38B, 39A, 39B Mating interface 40A, 40B Vacuum control valve 42A, 42B Exhaust Valve 42VB Valve body 44A Diffuser 54 Air cylinder 100 Load lock chamber module 114A, 114B Load lock chamber 120A, 120B Cooling chuck 121A, 121B Extension 124A Contact surface 150A, 152A Radiation fin 152A Heat sink 600 Normal pressure Front end 605 loading 埠 module 610 loading interlocking vacuum chamber 620 vacuum rear end 625 transport compartment 630 processing station 640 loading 埠 650 匣 box 650A, 650B 埠 port 651 diffuser / filter 660 micro environment 690 semiconductor tool station 691 control 710 substrate processing tool 712 tool interface 718 transport module 750, 760, 770 interface 780 substrate transport device 100 1, 1002 conduit 10100 loading interlocking chamber 10130, 10120 atmospheric pressure loading interlocking chamber door 10140 first loading interlocking chamber 50 200922852 10150 second loading interlocking chamber 10160, 10161 vacuum loading interlocking chamber door 10200, 10210 driving module 10200A , 10210A Upper drive actuator 10200B , 10210B Lower drive drive 10230 Seal contact surface 20100 Load lock chamber 20101 Normal pressure interface 20102 Vacuum interface 20120 Normal pressure door 20125 Door drive unit 20130 Door inlay 20330 Outside recess 20340 Inner groove Opening 20350 outer peripheral portion 20360 inner groove portion 20400 rear surface 50110 substrate transfer device 50111 upper arm portion 50112, 50113 front arm portion 50116, 50118 substrate transport opening 50450, 50451 heating element 50455 line 50460 elbow joint 50650A, 50650B mouth 50710 vacuum chamber 50720 front end module 50721 carrier 50725 loading 埠50790 processing tool 51
Claims (1)
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| US93892207P | 2007-05-18 | 2007-05-18 |
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| TW097118332A TWI455861B (en) | 2007-05-18 | 2008-05-19 | Substrate processing tool, semiconductor processing tool, and substrate processing apparatus |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI713471B (en) * | 2014-10-23 | 2020-12-21 | 美商蘭姆研究公司 | A buffer station for thermal control of semiconductor substrates transferred therethrough and method of transferring semiconductor substrates |
| TWI729737B (en) * | 2015-04-24 | 2021-06-01 | 美商應用材料股份有限公司 | Wafer swapper |
| CN115241114A (en) * | 2022-08-17 | 2022-10-25 | 常熟市兆恒众力精密机械有限公司 | Crystal disc clamp |
| TWI810526B (en) * | 2020-02-14 | 2023-08-01 | 日商芝浦機械電子裝置股份有限公司 | Film forming device and method for removing water from film forming device |
| US12043898B2 (en) | 2020-02-14 | 2024-07-23 | Shibaura Mechatronics Corporation | Film formation apparatus and moisture removal method thereof |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6048154A (en) * | 1996-10-02 | 2000-04-11 | Applied Materials, Inc. | High vacuum dual stage load lock and method for loading and unloading wafers using a high vacuum dual stage load lock |
| US6688375B1 (en) * | 1997-10-14 | 2004-02-10 | Applied Materials, Inc. | Vacuum processing system having improved substrate heating and cooling |
| DE60012428T2 (en) * | 1999-06-14 | 2005-07-28 | Smc K.K. | pusher |
| US6558509B2 (en) * | 1999-11-30 | 2003-05-06 | Applied Materials, Inc. | Dual wafer load lock |
| JP2001319885A (en) * | 2000-03-02 | 2001-11-16 | Hitachi Kokusai Electric Inc | Substrate processing apparatus and semiconductor manufacturing method |
| US6918731B2 (en) * | 2001-07-02 | 2005-07-19 | Brooks Automation, Incorporated | Fast swap dual substrate transport for load lock |
| US7207766B2 (en) * | 2003-10-20 | 2007-04-24 | Applied Materials, Inc. | Load lock chamber for large area substrate processing system |
| JP4860167B2 (en) * | 2005-03-30 | 2012-01-25 | 東京エレクトロン株式会社 | Load lock device, processing system, and processing method |
-
2008
- 2008-05-19 TW TW097118332A patent/TWI455861B/en active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI713471B (en) * | 2014-10-23 | 2020-12-21 | 美商蘭姆研究公司 | A buffer station for thermal control of semiconductor substrates transferred therethrough and method of transferring semiconductor substrates |
| TWI729737B (en) * | 2015-04-24 | 2021-06-01 | 美商應用材料股份有限公司 | Wafer swapper |
| TWI810526B (en) * | 2020-02-14 | 2023-08-01 | 日商芝浦機械電子裝置股份有限公司 | Film forming device and method for removing water from film forming device |
| US12043898B2 (en) | 2020-02-14 | 2024-07-23 | Shibaura Mechatronics Corporation | Film formation apparatus and moisture removal method thereof |
| CN115241114A (en) * | 2022-08-17 | 2022-10-25 | 常熟市兆恒众力精密机械有限公司 | Crystal disc clamp |
| CN115241114B (en) * | 2022-08-17 | 2023-10-10 | 常熟市兆恒众力精密机械有限公司 | A wafer disc fixture |
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