TW201527584A - Method for removing deposits on the walls of a processing chamber - Google Patents
Method for removing deposits on the walls of a processing chamber Download PDFInfo
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- TW201527584A TW201527584A TW103134935A TW103134935A TW201527584A TW 201527584 A TW201527584 A TW 201527584A TW 103134935 A TW103134935 A TW 103134935A TW 103134935 A TW103134935 A TW 103134935A TW 201527584 A TW201527584 A TW 201527584A
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- processing chamber
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- 238000000034 method Methods 0.000 title claims abstract description 27
- 238000004140 cleaning Methods 0.000 claims abstract description 33
- 229910052751 metal Inorganic materials 0.000 claims abstract description 22
- 239000002184 metal Substances 0.000 claims abstract description 22
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 6
- 229910002804 graphite Inorganic materials 0.000 claims abstract description 5
- 239000010439 graphite Substances 0.000 claims abstract description 5
- 239000007789 gas Substances 0.000 claims description 24
- 238000009736 wetting Methods 0.000 claims description 15
- 238000005530 etching Methods 0.000 claims description 10
- 238000000576 coating method Methods 0.000 claims description 8
- 239000012159 carrier gas Substances 0.000 claims description 7
- 239000011248 coating agent Substances 0.000 claims description 7
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 6
- 150000002902 organometallic compounds Chemical class 0.000 claims description 5
- 238000000151 deposition Methods 0.000 claims description 4
- 229910052733 gallium Inorganic materials 0.000 claims description 3
- 239000011261 inert gas Substances 0.000 claims description 3
- 229910052757 nitrogen Inorganic materials 0.000 claims description 3
- 230000000694 effects Effects 0.000 claims description 2
- 229910052738 indium Inorganic materials 0.000 claims description 2
- KZBUYRJDOAKODT-UHFFFAOYSA-N Chlorine Chemical compound ClCl KZBUYRJDOAKODT-UHFFFAOYSA-N 0.000 claims 1
- IOVCWXUNBOPUCH-UHFFFAOYSA-M Nitrite anion Chemical compound [O-]N=O IOVCWXUNBOPUCH-UHFFFAOYSA-M 0.000 claims 1
- 150000002826 nitrites Chemical class 0.000 claims 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 7
- 239000010410 layer Substances 0.000 description 23
- 239000000460 chlorine Substances 0.000 description 10
- 239000000758 substrate Substances 0.000 description 6
- ZAMOUSCENKQFHK-UHFFFAOYSA-N Chlorine atom Chemical compound [Cl] ZAMOUSCENKQFHK-UHFFFAOYSA-N 0.000 description 4
- 229910052801 chlorine Inorganic materials 0.000 description 4
- 229910001338 liquidmetal Inorganic materials 0.000 description 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 4
- 239000002356 single layer Substances 0.000 description 4
- 229910052799 carbon Inorganic materials 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- GYHNNYVSQQEPJS-UHFFFAOYSA-N Gallium Chemical compound [Ga] GYHNNYVSQQEPJS-UHFFFAOYSA-N 0.000 description 2
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 230000008021 deposition Effects 0.000 description 2
- 238000010926 purge Methods 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- 238000005406 washing Methods 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- BLRPTPMANUNPDV-UHFFFAOYSA-N Silane Chemical compound [SiH4] BLRPTPMANUNPDV-UHFFFAOYSA-N 0.000 description 1
- -1 Silizium nitrile Chemical class 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 229910052797 bismuth Inorganic materials 0.000 description 1
- 150000001805 chlorine compounds Chemical class 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000005137 deposition process Methods 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 description 1
- 239000013067 intermediate product Substances 0.000 description 1
- 229910052741 iridium Inorganic materials 0.000 description 1
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 239000010955 niobium Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 229910052756 noble gas Inorganic materials 0.000 description 1
- 230000003071 parasitic effect Effects 0.000 description 1
- 238000002161 passivation Methods 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 229910000077 silane Inorganic materials 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- 239000003039 volatile agent Substances 0.000 description 1
Classifications
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/4401—Means for minimising impurities, e.g. dust, moisture or residual gas, in the reaction chamber
- C23C16/4405—Cleaning of reactor or parts inside the reactor by using reactive gases
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- C11D2111/20—
-
- C11D2111/24—
Abstract
Description
本發明係有關一種自CVD反應器之處理室壁,尤其自塗SiC石墨部件移除沈積物之方法,其中將該處理室加熱至清洗溫度並在一段清洗時間內向該處理室導入特定言之含有第VII主族元素之清洗氣體。 The present invention relates to a method for removing deposits from a processing chamber wall of a CVD reactor, particularly a self-coated SiC graphite component, wherein the processing chamber is heated to a cleaning temperature and introduced into the processing chamber for a period of cleaning time. A cleaning gas for the element of the VII main group.
US 2013/0005118 A1、US 8,334,166 B2及US 7,842,588 B2揭露沈積III-V族半導體層於例如由III-V族單晶構成之基板上。該等基板亦可由相應之晶格匹配矽構成。將TMGa或TMAl隨NH3、PH3或AsH3一同導入CVD反應器之處理室以沈積III-V族層。為了在沈積過程結束並自處理室取出基板後對該等基板進行清洗,將Cl2作為清洗氣體隨惰性氣體如氬氣或氮氣一同導入處理室。由此實現在介於550℃與1050℃之溫度下進行的蝕刻過程,在此期間,形成於處理室壁特別是塗SiC石墨部件上之寄生覆層主要轉變成揮發性氯化物,其由載氣流帶離處理室。 US 2013/0005118 A1, US Pat. No. 8,334,166 B2 and US Pat. No. 7,842,588 B2 disclose the deposition of a Group III-V semiconductor layer on a substrate composed, for example, of a Group III-V single crystal. The substrates may also be formed by corresponding lattice matching iridium. TMGa or TMAl is introduced into the processing chamber of the CVD reactor along with NH 3 , PH 3 or AsH 3 to deposit a III-V layer. In order to clean the substrates after the deposition process is completed and the substrate is removed from the processing chamber, Cl 2 is introduced as a purge gas into the processing chamber along with an inert gas such as argon or nitrogen. Thereby an etching process is carried out at a temperature between 550 ° C and 1050 ° C, during which the parasitic coating formed on the walls of the processing chamber, in particular the SiC-coated graphite component, is mainly converted into volatile chlorides, which are carried by The gas stream is taken away from the processing chamber.
DE 10 2011 056 538 A1揭露一種藉H2脈衝導入HCl以清洗處理室之方法。清洗時形成中間產物鎵。 DE 10 2011 056 538 A1 discloses a method of introducing a HCl by H 2 pulse to clean a processing chamber. The intermediate product gallium is formed during cleaning.
US 2004/0244817 A1描述一種使用多組分蝕刻劑清洗渦輪葉片之方法。該蝕刻劑例如含有NH4Cl或金屬組分鋁或鉻。 US 2004/0244817 A1 describes a method of cleaning a turbine blade using a multi-component etchant. The etchant contains, for example, NH 4 Cl or a metal component of aluminum or chromium.
DE 10 2012 101 438 A1及US 2011/0223710 A1分別描述一種藉由導入清洗氣體來清洗處理室之方法,其中該清洗氣體直接接觸位於表面之覆層。 DE 10 2012 101 438 A1 and US 2011/0223710 A1 each describe a method of cleaning a processing chamber by introducing a cleaning gas, wherein the cleaning gas directly contacts the coating on the surface.
US 2011/0268880 A1及US 5,976,396各描述一種採用多組分蝕刻劑的蝕刻方法。該等多組分蝕刻劑直接接觸待清洗之壁。 US 2011/0268880 A1 and US 5,976,396 each describe an etching process using a multi-component etchant. The multi-component etchant directly contacts the wall to be cleaned.
SiN層主要作為鈍化層應用於HEMT結構,而沈積SiN層須向處理室導入矽烷(SiH4)。其與被導入處理室的NH3共同形成SiN。矽亞硝酸鹽(Siliziumnitrit)不僅形成於基板表面,亦在處理室壁表面特別是處理室底部上形成一層。處理室壁由塗碳化矽(SiC)石墨構成。以氯氣為清洗氣體無法清洗處理室壁,因為SiN將成為含氯蝕刻氣體之蝕刻障壁。 The SiN layer is mainly applied as a passivation layer to the HEMT structure, and the SiN layer is deposited to introduce silane (SiH 4 ) into the processing chamber. It forms SiN together with NH 3 introduced into the processing chamber. Silizium nitrile is formed not only on the surface of the substrate but also on the surface of the treatment chamber wall, particularly on the bottom of the treatment chamber. The chamber wall is composed of carbon coated bismuth (SiC) graphite. The treatment chamber wall cannot be cleaned with chlorine as a purge gas because SiN will become an etch barrier for chlorine-containing etching gases.
本發明之目的在於提供一種能清洗處理室並能改良處理室清洗效果之方法。 It is an object of the present invention to provide a method which is capable of cleaning a processing chamber and improving the cleaning effect of the processing chamber.
申請專利範圍所給出之本發明為用以達成該目的之解決方案。 The invention as set forth in the scope of the patent application is a solution for achieving this object.
本發明首先且主要提出如下方案:導入該清洗氣體前用金屬潤濕待清洗之壁。較佳在升高溫度下實施之,其中潤濕階段的溫度可高於550℃。特定言之,基座溫度或處理室溫度在潤濕階段可自一較低溫度不斷上升至例如1150℃之最高溫度。由此經歷一段溫度斜坡,在此期間同時向處理室導入含金屬的氣態起始材料,該起始材料在壁上形成金屬凝結物。該含金屬起始材料較佳為一有機金屬化合物,其隨一載氣如氫氣、氮氣或一稀有氣體一同被導入處理室。該有機金屬化合物在上述升高溫度下分解,其中在壁上凝結一較薄的液態金屬膜。根據本發明之一較佳方案,送入處理室之金屬的量至少能在待清洗之壁上形成一閉合金屬膜,尤其能形成一金屬膜的至少一單層。該金屬特別可採用鋁、鎵或銦。該等金屬之氣態載體可採用TMAl、TMGa、TEGa或TMIn。此處亦可在較低溫度下開始導入該有機金屬化合物,其中基座溫度或處理室壁之溫度不斷上升至最高值。自下方被加熱的基座可用作熱源以加熱處理室壁。基座以熱輻射方式為處理室其餘的 壁加熱,使得該等壁所達到的最終溫度低於基座表面之溫度。在處理室所有的壁達到能使含金屬氣體如有機金屬化合物熱解成金屬之溫度之前,即已可開始該含金屬氣體之導入。根據第一方案,在於一較短的停止沖洗期間實施過潤濕階段後,視情況在降低的總氣體壓力下沖洗處理室。而後將清洗氣體隨載氣一同導入處理室。該清洗氣體較佳採用Cl2。但亦可使用第VII主族之其他元素或其他蝕刻氣體或第VII主族元素之化合物如HCl。例如在介於500℃與1000℃之溫度下實施蝕刻步驟。潤濕步驟及接下來的清洗步驟可作為步驟序列依次反覆實施。根據該方法之一方案,在潤濕步驟後施覆一較薄III-V族層於液態金屬層上。該液態金屬層僅需具有一單層之厚度。但其亦可具有數個單層之厚度。藉由隨該含金屬氣體如TMAl一同導入NH3,直接沈積一III-V族層如AlN層於該金屬膜上。其層厚大致處於30nm範圍。在該AlN層上可沈積一GaN層。此點可藉由同時導入NH3與TMGa而實現。該GaN層較佳具有最高達500nm之層厚。停止沖洗一段較短時間並酌情降低處理室總壓力後,藉由導入清洗氣體如Cl2及載氣來實施清洗步驟。在上述溫度斜坡達到其高於1000℃,特定言之高於1200℃的最大值之前,即已可開始NH3之導入。事實表明,用金屬特別是液態鋁潤濕SiN覆層能使該反應性液態金屬施加影響於(打開)SiN鍵,從而使得SiN層或該金屬所形成之合金能透過氯之添加而轉變成揮發性化合物,再由載氣流運走該揮發性化合物。在第二方案中亦可依次反覆實施步驟序列。但此方案較佳係依次反覆實施III-V族塗佈過程及接下來藉由導入清洗氣體而實現的清洗過程。 The invention first and mainly proposes a solution for wetting the wall to be cleaned with metal before introducing the cleaning gas. It is preferably carried out at elevated temperatures wherein the temperature of the wetting stage can be above 550 °C. In particular, the susceptor temperature or process chamber temperature may be ramped from a lower temperature to a maximum temperature of, for example, 1150 ° C during the wetting phase. This results in a temperature ramp during which a metal-containing gaseous starting material is simultaneously introduced into the processing chamber, which forms a metal condensate on the wall. The metal-containing starting material is preferably an organometallic compound which is introduced into the processing chamber along with a carrier gas such as hydrogen, nitrogen or a noble gas. The organometallic compound decomposes at the elevated temperature described above, wherein a thinner liquid metal film is condensed on the wall. According to a preferred embodiment of the present invention, the amount of metal fed into the processing chamber can form at least a closed metal film on the wall to be cleaned, in particular at least a single layer of a metal film. The metal may specifically be aluminum, gallium or indium. The gaseous carrier of the metals may be TMAl, TMGa, TEGa or TMIn. It is also possible here to start introducing the organometallic compound at a lower temperature, in which the temperature of the susceptor or the wall of the treatment chamber is continuously increased to the highest value. The base heated from below can be used as a heat source to heat the chamber walls. The susceptor heats the remaining walls of the processing chamber in a thermally radiated manner such that the final temperature reached by the walls is lower than the temperature of the susceptor surface. The introduction of the metal-containing gas can be started before all the walls of the processing chamber reach a temperature at which the metal-containing gas such as the organometallic compound is pyrolyzed into a metal. According to a first variant, the treatment chamber is flushed under reduced total gas pressure, as appropriate, after a wetting phase has been carried out during a short stop flush. The cleaning gas is then introduced into the processing chamber along with the carrier gas. The cleaning gas is preferably Cl 2 . However, other elements of the VII main group or other etching gases or compounds of the VII main group elements such as HCl may also be used. The etching step is carried out, for example, at a temperature between 500 ° C and 1000 ° C. The wetting step and the subsequent washing step can be carried out in turn as a sequence of steps. According to one aspect of the method, a thinner III-V layer is applied to the liquid metal layer after the wetting step. The liquid metal layer only needs to have a thickness of a single layer. However, it may also have a thickness of several single layers. A III-V layer such as an AlN layer is directly deposited on the metal film by introducing NH 3 along with the metal-containing gas such as TMAl. The layer thickness is approximately in the range of 30 nm. A GaN layer may be deposited on the AlN layer. This can be achieved by simultaneously introducing NH 3 and TMGa. The GaN layer preferably has a layer thickness of up to 500 nm. After the rinsing is stopped for a short period of time and the total pressure of the processing chamber is lowered as appropriate, the washing step is carried out by introducing a cleaning gas such as Cl 2 and a carrier gas. The introduction of NH 3 can already be started before the above temperature ramp reaches its maximum above 1000 ° C, in particular above 1200 ° C. It has been shown that the wetting of the SiN coating with a metal, in particular liquid aluminum, enables the reactive liquid metal to exert an influence on the (opening) of the SiN bond, so that the SiN layer or the alloy formed by the metal can be converted to volatilized by the addition of chlorine. The compound is then transported away from the volatile compound by a carrier gas stream. In the second variant, the sequence of steps can also be carried out in succession. However, this solution preferably repeats the III-V coating process and the subsequent cleaning process by introducing a cleaning gas.
下面參照圖1闡述本發明之實施例。 An embodiment of the present invention will now be described with reference to FIG.
圖1係以時間為橫軸、以總壓力及基座溫度為縱軸之流程圖。時標間距為15分鐘。 Figure 1 is a flow chart with time as the horizontal axis and total pressure and susceptor temperature as the vertical axis. The time scale interval is 15 minutes.
圖1所示之清洗過程係在200℃左右的升高溫度下開始。先向處理室饋入惰性氣體或氫氣。將處理室壓力調節至100mbar。而後經歷一段溫度斜坡。溫度達到550℃時向處理室導入TMAl,其在高溫的基座表面分解,其中形成液態鋁及氣態甲烷。氣態甲烷由載氣運走。剩餘的鋁將被SiN污染之處理室壁的表面潤濕,從而形成至少一濃度為100%之單層(100%-ige Monolage)。 The cleaning process shown in Figure 1 begins at an elevated temperature of about 200 °C. An inert gas or hydrogen gas is first fed to the process chamber. The chamber pressure was adjusted to 100 mbar. Then go through a temperature ramp. When the temperature reached 550 ° C, TMAl was introduced into the processing chamber, which decomposed on the surface of the high temperature substrate, in which liquid aluminum and gaseous methane were formed. Gaseous methane is carried away by the carrier gas. The remaining aluminum will be wetted by the surface of the SiN contaminated processing chamber wall to form at least one monolayer (100%-ige Monolage) at a concentration of 100%.
大約過7分鐘並且在溫度達到約1050℃後,向處理室導入NH3並藉由饋入相應量之載氣來將處理室壓力提高至200mbar。沈積一層厚度約為30nm之AlN後,用TMGa代替TMAl導入處理室以沈積一約500nm厚之GaN層。停止沖洗一段時間並待處理室壓力下降後實施蝕刻步驟,其中在950℃左右之溫度下向處理室導入氯。其間處理室內壓力為100mbar。 After about 7 minutes and after the temperature reached about 1050 ° C, NH 3 was introduced into the process chamber and the process chamber pressure was increased to 200 mbar by feeding a corresponding amount of carrier gas. After depositing a layer of AlN having a thickness of about 30 nm, TMGa was used instead of TMAl to introduce a processing chamber to deposit a GaN layer of about 500 nm thick. The etching step is performed after the rinsing is stopped for a while and the pressure of the chamber to be treated is lowered, wherein chlorine is introduced into the processing chamber at a temperature of about 950 °C. The chamber pressure during this time was 100 mbar.
再停止沖洗一段時間後,在較低的處理室壓力下藉由導入TMAl及NH3再度沈積一AlN層並藉由導入TMGa及NH3再度沈積一GaN層。在此,AlN之層厚約為30nm或小於30nm,例如10nm,GaN之層厚約為500nm或小於500nm,例如150nm。 After stopping the rinsing for a period of time, an AlN layer was deposited again by introducing TMAl and NH 3 under a lower processing chamber pressure and a GaN layer was deposited again by introducing TMGa and NH 3 . Here, the layer thickness of AlN is about 30 nm or less, for example 10 nm, and the layer thickness of GaN is about 500 nm or less, for example, 150 nm.
再停止沖洗一段時間後再實施一蝕刻步驟,其中向處理室導入Cl2。 After the rinsing is stopped for a while, an etching step is performed in which Cl 2 is introduced into the processing chamber.
最後實施回火步驟,其中僅向處理室導入H2及NH3。 Finally, a tempering step is carried out in which only H 2 and NH 3 are introduced into the treatment chamber.
III-V族塗佈步驟及接下來的蝕刻步驟可作為處理步驟序列依次反覆實施直至無殘留地移除SiN覆層。 The III-V coating step and the subsequent etching step can be carried out sequentially as a sequence of processing steps until the SiN coating is removed without residue.
在一未圖示實施例中,僅需用液態鋁潤濕塗碳化矽處理室壁之SiN覆層並在該潤濕步驟後立即向處理室導入Cl2,便可完成處理室之清洗或III-VI族層之沈積。此處亦可循環反覆實施清洗步驟序列,其中每個步驟序列皆包括潤濕步驟與蝕刻步驟。 In an unillustrated embodiment, it is only necessary to wet the SiN coating of the carbonized niobium processing chamber wall with liquid aluminum and introduce Cl 2 into the processing chamber immediately after the wetting step to complete the cleaning of the processing chamber or III. - deposition of the VI family layer. The sequence of cleaning steps can also be performed cyclically and repeatedly, wherein each step sequence includes a wetting step and an etching step.
所有已揭露特徵(自身即)為發明本質所在。故本申請之揭露內容亦包含相關/所附優先權檔案(在先申請副本)所揭露之全部內容,該等檔案所述特徵亦一併納入本申請之申請專利範圍。附屬項採用可選並列措辭對本發明針對先前技術之改良方案的特徵予以說明,其目的主要在於在該等請求項基礎上進行分案申請。 All the revealed features (ie, themselves) are the essence of the invention. Therefore, the disclosure of the present application also contains all the contents disclosed in the related/attached priority file (copy of the prior application), and the features described in the files are also included in the scope of the patent application of the present application. The sub-items illustrate the features of the prior art improvements of the prior art using optional side-by-side wording, the main purpose of which is to make a divisional application on the basis of the claims.
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US5976396A (en) * | 1998-02-10 | 1999-11-02 | Feldman Technology Corporation | Method for etching |
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WO2011112587A1 (en) * | 2010-03-09 | 2011-09-15 | First Solar, Inc. | Deposition chamber cleaning system and method |
US20130005118A1 (en) | 2011-07-01 | 2013-01-03 | Sung Won Jun | Formation of iii-v materials using mocvd with chlorine cleans operations |
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