TW201215500A - Coated article and method for making the same - Google Patents

Coated article and method for making the same Download PDF

Info

Publication number
TW201215500A
TW201215500A TW99134636A TW99134636A TW201215500A TW 201215500 A TW201215500 A TW 201215500A TW 99134636 A TW99134636 A TW 99134636A TW 99134636 A TW99134636 A TW 99134636A TW 201215500 A TW201215500 A TW 201215500A
Authority
TW
Taiwan
Prior art keywords
layer
substrate
target
transition layer
transition
Prior art date
Application number
TW99134636A
Other languages
Chinese (zh)
Inventor
Hsin-Pei Chang
Wen-Rong Chen
Huan-Wu Chiang
Cheng-Shi Chen
Jia Huang
Original Assignee
Hon Hai Prec Ind Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hon Hai Prec Ind Co Ltd filed Critical Hon Hai Prec Ind Co Ltd
Priority to TW99134636A priority Critical patent/TW201215500A/en
Publication of TW201215500A publication Critical patent/TW201215500A/en

Links

Landscapes

  • Physical Vapour Deposition (AREA)

Abstract

A coated article is provided. The coated article includes a substrate, a base layer formed on the substrate, an intermediate layer formed on the base layer, and a hard layer formed on the intermediate layer. The base layer is an aluminum, titanium, chromium or zirconium layer. The intermediate layer is an AtXyMez(CvN1-v) layer, where A is Al, Ti, Cr or Zr, X is W or Mo, Me is Rh or Pd. The hard layer is a XnMeg(CkN1-k) layer, where X is W or Mo, Me is Rh or Pd. A method for making the coated article is also provided.

Description

201215500 六、發明說明: 【發明所屬之技術領威】 [_本發明涉及-_膜件及該鍍膜件的製備方法。 [先前技術] 圃過渡金狀化物、魏物和錢化物具有高硬度、高抗 磨損性能和良好的化學穩定性等優異性能。因此,通常 將過渡金屬氮化⑱石反化物和碳氣化物以薄膜的形式錄 覆在刀具或模具表㈣成硬f塗層,减來提高刀具和 〇 模具的使用壽命。但是該類金屬氣化㈣膜在溫度大於 700艺時,硬度往铎會降低,而對於切削刀具,往往要求 硬質塗層在高的溫度下也能保持其硬度和耐磨性。 [0003] 中國專利申請20〇880022837·9揭示,在金屬氮化物膜系 中引入貴金屬Ru,Ru能溶解於金屬氮化物晶格中並有效 提高硬質塗層的失效溫度。 [0004] 但是在鍍膜件的製備過程中,由於膜層與基體間的熱膨 Q 脹係數相差較大’且不同膜層的'成份和晶體結構有明顯 的變化’膜層間存在不可避免的熱應力及晶格匹配所帶 來的内應力,這些應力在鍍膜件製備完成後往往不能消 除,使得膜層與基體間的結合力較差,薄膜在使用過程 中容易發生剝離,從而影響了此類鍍膜件的使用壽命及 其應用範圍。 【發明内容】 [0005] 有鑒於此,有必要提供一種有效解決上述問題的鍍膜件 099134636 表單編號A0101 第3頁/共13頁 0992060477-0 201215500 [0006] [0007] [0008] [0009] [0010] [0011] [0012] 另外’還有必要提供一種製備上述鍍膜件的方法β 一種鑛膜件’包括基材、形成於基材表面的打底層、形 成於打底層表面的過渡層及形成於過渡層表面的硬質層 ’該打底層為A1、Ti、Cr或Zr層;該過渡層為 A/yMe/Wv)層,其中〇.4StS0.8,0.35Sy$ 〇·65’〇.〇5$ zS 0.08,0.75 S(t + y + z) $1.05, 〇·75$ν$1.〇 ’其中a為打底層中的金屬A1、Ti、Cr或 Zr ’ X為W或Mo,Me為Rh或Pd ;該硬質層為 XnMeg(CkNi-k)層,其中〇. 35SnS0. 65,0. 〇5Sg$ 0.08,0.40g(n+g)s〇.7i,0.70盔kSl.O,其中χ為 過渡層中的金屬W或Mo,Me為過渡層t的金屬Rh或Pd。 一種鍍膜件的製備方法,其包括如下步驟: 提供一基材; 在該基材表面形成打底層,該打底層為Ai、Ti、Cr或Zr 層;201215500 VI. Description of the Invention: [Technology Leading to the Invention] [The present invention relates to a film member and a method of preparing the coated member. [Prior Art] The transitional gold compounds, Wei materials and money compounds have excellent properties such as high hardness, high abrasion resistance and good chemical stability. Therefore, the transition metal nitriding 18 stone inverse and carbon gas are usually recorded in the form of a film on the tool or mold table (4) into a hard f coating, which reduces the service life of the tool and the dies. However, when the temperature of the metal vaporized (four) film is higher than 700, the hardness will decrease, and for the cutting tool, the hard coating is required to maintain its hardness and wear resistance at a high temperature. [0003] Chinese Patent Application No. 20,880,028,837, discloses that a noble metal Ru is introduced into a metal nitride film system, and Ru can be dissolved in the metal nitride crystal lattice and effectively increase the failure temperature of the hard coating. [0004] However, in the preparation process of the coated parts, the thermal expansion coefficient between the film layer and the substrate differs greatly, and the composition and crystal structure of the different layers have obvious changes. The internal stress caused by stress and lattice matching, these stresses can not be eliminated after the preparation of the coated parts, so that the bonding force between the film layer and the substrate is poor, and the film is easily peeled off during use, thus affecting such coating. The service life of the piece and its application range. SUMMARY OF THE INVENTION [0005] In view of the above, it is necessary to provide a coated member that effectively solves the above problems. 099134636 Form No. A0101 Page 3 / Total 13 Page 0992060477-0 201215500 [0006] [0007] [0008] [0009] [ [0012] Further, it is also necessary to provide a method for preparing the above-mentioned coated member. [A mineral film member] comprises a substrate, a primer layer formed on the surface of the substrate, a transition layer formed on the surface of the primer layer, and formation. The hard layer on the surface of the transition layer is the A1, Ti, Cr or Zr layer; the transition layer is A/yMe/Wv) layer, wherein 〇.4StS0.8, 0.35Sy$ 〇·65'〇.〇 5$ zS 0.08,0.75 S(t + y + z) $1.05, 〇·75$ν$1.〇' where a is the metal A1, Ti, Cr or Zr in the bottom layer. X is W or Mo, and Me is Rh. Or Pd; the hard layer is XnMeg (CkNi-k) layer, wherein 〇. 35SnS0. 65,0. 〇5Sg$ 0.08, 0.40g(n+g)s〇.7i, 0.70 helmet kSl.O, where χ The metal W or Mo in the transition layer, Me is the metal Rh or Pd of the transition layer t. A method for preparing a coated member, comprising the steps of: providing a substrate; forming a primer layer on the surface of the substrate, the underlayer being an Ai, Ti, Cr or Zr layer;

在打底層的表面形成過渡層,該過渡層為 AtXyMez(CvNl_v)層,其中 ,〇.35SyS 0.65’0.05SzS0.08,0. 75S(t + y + z) $1. 〇5, 0· 75Sv$l. 〇 ’其中a為打底層中的金屬ai、Ti、Cr或 Zr ’ X為W或Mo,Me為Rh或Pd ; 在過渡層的表面形成硬質層,該硬質層為X Me (C N ) n g k 1 -ky 層’其中 0.35SnS0.65,0.05Sg$〇.〇8,〇.4〇s (n + g)S0· 71,0. 70SkSl. 0,其中X為過渡層中的金 屬W或Mo,Me為過渡層中的金屬Rh或Pd。 099134636 表單編號A0101 第4頁/共13頁 0992060477-0 201215500A transition layer is formed on the surface of the underlayer, which is an AtXyMez (CvNl_v) layer, wherein 〇.35SyS 0.65'0.05SzS0.08,0. 75S(t + y + z) $1. 〇5, 0· 75Sv$ l. 〇 'where a is the metal ai, Ti, Cr or Zr in the underlayer X is W or Mo, Me is Rh or Pd; a hard layer is formed on the surface of the transition layer, the hard layer is X Me (CN ) Ngk 1 -ky layer 'where 0.35SnS0.65, 0.05Sg$〇.〇8, 〇.4〇s (n + g)S0· 71,0. 70SkSl. 0, where X is the metal W in the transition layer or Mo, Me is the metal Rh or Pd in the transition layer. 099134636 Form No. A0101 Page 4 of 13 0992060477-0 201215500

DD

[_相較于f知技術,所述岐膜件在基㈣表面沉積金屬 作為打底層,再在打底層的表面沉積過渡層,再在過渡 層的表面沉積硬質層,膜系逐層過渡較好,膜層内部沒 有明顯的應力產生,這樣在施加外力的情況下,所鍍的 膜層不會因為内部的應力缺陷而導致其失效;且在過渡 層和硬質層中引入了 Rh或Pd,Rh或Pd可溶於過渡層和硬 質層中的金屬碳氮化物晶格中,在高溫狀態下金屬碳氮 化物發生晶型轉變,晶格發生畸變而產生畸變應力從而 對過渡層和硬質層的硬度起到辑化作用,從而有效提高 過渡層和硬質層的熱硬度及為諕下的财磨性,相應地提 向了所述鍍膜件的使用壽命和使黑溫度範圍。 【實施方式】 > [0014] 請參閱圖1 ’本發明一較佳實施方式的鍍膜件1〇包括基材 11、形成於基材11表面的打底層13、形成於打底層13表 面的過渡層15及形成於過渡層15表面的硬質層17。 [0015] 該基材11可為鋁合金、鎂合金、鈦合金或不銹鋼。 Ο [0016] 該打底層13可以磁控濺射的方式形成。該打底層13可為 AK鋁)、Ti (鈦)、Cr(鉻)或Zr(锆)層。該打底層13的 厚度可為100〜200nm。 [0017] 該過渡層15可以磁控濺射的方式形成。該過渡層15為 AtXyMez(CvNl v)層,其中 [0018] 〇. 4StS0. 8, [0019] 〇. 35SySO. 65, [0020] 〇.05SzS0.08, 0992060477-0 099134636 表單編號A0101 第5頁/共13頁 201215500 [0021] [0022] [0023] [0024] [0025] [0026] [0027] [0028] [0029] [0030] [0031] [0032] [0033] 099134636 〇. 75^(t + y + z)^l. 〇5 , 0. 75 S 1. 〇, 其中A可為所述打底層!3中的金屬A1、η、Cr或Zr,X可 為W (鶴)或Mo(翻)’ Me可為Rh(姥)或Pd(叙)。該過渡 層15的厚度可為1〇〇〜3〇〇ηιη。 該硬質層17可以磁控濺射的方式形成。該硬質層17為 ^(Cklk)層,其中 〇. 35SnS0. 65, 0. 05Sg$〇. 〇8, 〇. 4〇S(n+g)S〇. 7卜 7〇Sk$l. 0, 其中X可為所述過渡層15中的金屬w或M〇,Me可為所述過 渡層15中的金屬Rh或Pd。碑硬質層! 7的厚度可為3 〇 〇〜 600nm。 本發明一較佳實施方式的鍍膜件10妁製備方法,其包括 以下步驟: (a)提供一基材π,該基材u可為鋁合金、鎂合金鈦合 金或不錢鋼。 (b)將基材11放入無水乙醇中進行超聲波清洗以去除基 材11表面的汙潰’清洗時間可為5〜丨〇m丨n。 (c)對經上述處理後的基材丨丨的表面進行氬氣電漿清洗 以進-步去除基材11表面的油污,以及改善基材u表面 表單編號A0101 第6頁/共13頁 0992060477-0 201215500 與後續塗層的結合力。該電漿清洗的具體操作及工藝參 數可為:將基材11放入一磁控濺射鍍膜機(圖未示)的鍍 膜室内,將該鍍膜室抽真空至3. 0xl0_5Torr,然後向鍍 膜室内通入流量為50〜400sccm(標準狀態毫升/分鐘)的 氬氣(純度為99. 999%),並施加-300〜-600V的偏壓於 基材11,對基材11表面進行氬氣電漿清洗,清洗時間為5 〜10miη ° [0034] ❹ (d)採用磁控濺射法在經氬氣電漿清洗後的基材11上濺鍍 一打底層13,該打底層13可為A1、Ti、Cr或Zr層。賤錢 該打底層13在所述磁控濺射鍍膜機中進行。使用鋁靶、 鈦靶、鉻靶或鍅靶中的一種為靶材,以氬氣為工作氣體 ,氬氣流量可為100〜300sccm。滅鍍時對基材施加-100 〜-200V的偏壓,並加熱所述鍍膜室使基材11的溫度為 200〜500°C,鍍膜時間可為10〜30min。該打底層13的 厚度可為100〜200nm。 [0035] 〇 (e)繼續採用磁控濺射法在所述打底層13的表面濺鍍一過 渡層15。該過渡層15為、X Me (C N,)層,其中0.4S tS0.8,0.35Sy$0.65,0.05S z$ 0.08,0.75 S (t + y + z) SI. 05,0. 75SvSl. 0,其中A可為所述打底 層13中的金屬A1、Ti、Cr或Zr,X可為W或Mo,Me可為 Rh或Pd。濺鑛該過渡層15使用鎢le*與鉬乾中的一種、鍵 靶與鈀靶中的一種以及步驟(d)中使用的金屬靶,以氨氣 和乙炔為反應氣體,氨氣流量可為50〜200sccm,乙快 流量可為30〜200sccm,以氬氣為工作氣體,氣氣流量 可為100〜300sccm,鍍膜時間可為30〜60min。該過渡 099134636 表單編號A0101 第7頁/共13頁 0992060477-0 201215500 層15的尽度可為loo〜。 [0036] (〇繼續採用磁控濺射法在所述過渡層15的表面濺鍍一硬 質層17。該硬質層17為XnMeg(w_kM,其中〇 35“ ^0.65 > 〇.05^g^〇.〇8 > 0. 40^(n + g)^0. 71 - 〇. γ〇 SkSl. 〇,其中χ可為所述過渡層η中的金屬w或Μ〇,Me 可為所述過渡層15中的金屬Rh或pd。濺鍍該硬質層17使 用步驟(e)中使用的鎢靶與鉬靶中的一種、铑乾與鈀靶中 的一種,以氨氣和乙炔為反應氣體,氨氣流量可為5〇〜 200sccm,乙炔流量可為3〇〜20〇sccm,以氬氣為工作 氡體’氬氧流量可為1〇〇〜300's;cc:m.,:鑛膜時間可為3〇〜 60min。該硬質層π的厚度可為500〜700nm。 [0037] 本發明較佳實施方式鍍膜件1〇在基材π的表面沉積金屬 作為打底層13,再在打底層13的表面沉積過渡層15,再 在過渡層15的表面沉積硬質層17,膜系逐層過渡較好, 膜層内部沒有明顯的應力產生,填槔在施加外力的情況 下’所鍍的膜層不會因為内部的應力缺陷而導致其失效 ;且在過渡層15和硬質層17中引入了 Rh或Pd,Rh或Pd可 溶於過渡層15和硬質層17中的金屬碳氮化物晶格中,在 南溫狀態下金屬碳氮化物發生晶型轉變,晶格發生崎變 而產生畸變應力從而對過渡層15和硬質層丨7的硬度起到 強化作用,從而有效提高了過渡層15和硬質層17的熱硬 度及高溫下的耐磨性,相應地提高了所述鑛膜件1 〇的使 用壽命和使用溫度範圍。 【圖式簡單說明】 [0038] 圖1為本發明一較佳實施例鑛膜件的剖視圖。 099134636 表單編號A0101 第8頁/共13頁 0992060477-0 201215500 ‘ 【主要元件符號說明】 [0039] 鍍膜件:10 [0040] 基材:11 [0041] 打底層:13 [0042] 過渡層:15 [0043] 硬質層:17[_In contrast to the known technique, the ruthenium film is deposited on the surface of the base (4) as a primer layer, and then a transition layer is deposited on the surface of the primer layer, and then a hard layer is deposited on the surface of the transition layer. Well, there is no obvious stress generation inside the film layer, so that in the case of applying an external force, the plated film layer does not fail due to internal stress defects; and Rh or Pd is introduced in the transition layer and the hard layer, Rh or Pd is soluble in the metal carbonitride lattice in the transition layer and the hard layer. At high temperature, the metal carbonitride undergoes crystal transformation, the lattice is distorted and the distortion stress is generated to the transition layer and the hard layer. The hardness acts as a compensating effect, thereby effectively improving the thermal hardness of the transition layer and the hard layer and the curability of the underarm, and correspondingly increasing the service life of the coated member and the black temperature range. [Embodiment] Referring to Figure 1 , a coated member 1 of a preferred embodiment of the present invention includes a substrate 11, a primer layer 13 formed on the surface of the substrate 11, and a transition formed on the surface of the primer layer 13. The layer 15 and the hard layer 17 formed on the surface of the transition layer 15. [0015] The substrate 11 may be an aluminum alloy, a magnesium alloy, a titanium alloy or stainless steel. [0016] The underlayer 13 can be formed by magnetron sputtering. The primer layer 13 may be an AK aluminum, Ti (titanium), Cr (chromium) or Zr (zirconium) layer. The underlayer 13 may have a thickness of 100 to 200 nm. [0017] The transition layer 15 can be formed by magnetron sputtering. The transition layer 15 is an AtXyMez (CvNl v) layer, wherein [0018] St. 4StS0. 8, [0019] 35. 35SySO. 65, [0020] 〇.05SzS0.08, 0992060477-0 099134636 Form No. A0101 Page 5 [0012] [0023] [0028] [0028] [0030] [0032] [0033] [0033] 099134636 〇. 75^( t + y + z)^l. 〇5 , 0. 75 S 1. 〇, where A can be the bottom layer! The metal A1, η, Cr or Zr in 3, X may be W (crane) or Mo (turn)' Me may be Rh (姥) or Pd (descriptive). The transition layer 15 may have a thickness of 1 〇〇 to 3 〇〇 ηιη. The hard layer 17 can be formed by magnetron sputtering. The hard layer 17 is a layer of ^(Cklk), wherein 〇. 35SnS0. 65, 0. 05Sg$〇. 〇8, 〇. 4〇S(n+g)S〇. 7卜7〇Sk$l. 0, Wherein X may be the metal w or M〇 in the transition layer 15, and Me may be the metal Rh or Pd in the transition layer 15. The hard layer of the monument! The thickness of 7 can be 3 〇 600 ~ 600nm. A method for preparing a coated member 10 of a preferred embodiment of the present invention comprises the steps of: (a) providing a substrate π, which may be an aluminum alloy, a magnesium alloy titanium alloy or a steel. (b) The substrate 11 is placed in absolute ethanol for ultrasonic cleaning to remove the stain on the surface of the substrate 11. The cleaning time may be 5 to 丨〇m丨n. (c) performing argon plasma cleaning on the surface of the substrate ruthenium treated as described above to further remove oil stain on the surface of the substrate 11, and improving the surface of the substrate u. Form No. A0101 Page 6 of 13 0992060477 -0 201215500 Binding to subsequent coatings. The specific operation and process parameters of the plasma cleaning may be as follows: the substrate 11 is placed in a coating chamber of a magnetron sputtering coating machine (not shown), and the coating chamber is evacuated to 3. 0xl0_5 Torr, and then to the coating chamber. An argon gas (purity of 99.999%) having a flow rate of 50 to 400 sccm (standard state ml/min) was introduced, and a bias of -300 to -600 V was applied to the substrate 11, and argon gas was applied to the surface of the substrate 11. Slurry cleaning, cleaning time is 5~10miη ° [0034] ❹ (d) A layer of underlayer 13 is sputtered on the substrate 11 after argon plasma cleaning by magnetron sputtering, and the underlayer 13 can be A1 , Ti, Cr or Zr layer. The bottom layer 13 is carried out in the magnetron sputtering coater. One of an aluminum target, a titanium target, a chromium target or a ruthenium target is used as a target, and argon gas is used as a working gas, and the flow rate of the argon gas may be 100 to 300 sccm. When the plating is off, a bias of -100 to -200 V is applied to the substrate, and the coating chamber is heated to bring the temperature of the substrate 11 to 200 to 500 ° C, and the coating time may be 10 to 30 minutes. The underlayer 13 may have a thickness of 100 to 200 nm. [0035] 〇 (e) continues to sputter a transition layer 15 on the surface of the underlayer 13 by magnetron sputtering. The transition layer 15 is a layer of X Me (CN,), wherein 0.4S tS0.8, 0.35Sy$0.65, 0.05S z$ 0.08, 0.75 S (t + y + z) SI. 05,0. 75SvSl. 0, Wherein A may be the metal A1, Ti, Cr or Zr in the underlayer 13, X may be W or Mo, and Me may be Rh or Pd. Splashing the transition layer 15 uses one of tungsten le* and molybdenum, one of a bond target and a palladium target, and a metal target used in the step (d), using ammonia gas and acetylene as a reaction gas, and the ammonia gas flow rate can be 50~200sccm, the fast flow rate of B can be 30~200sccm, the working gas is argon gas, the gas flow rate can be 100~300sccm, and the coating time can be 30~60min. The transition 099134636 Form number A0101 Page 7 of 13 0992060477-0 201215500 Layer 15 can be loo~. [0036] (〇 continued to deposit a hard layer 17 on the surface of the transition layer 15 by magnetron sputtering. The hard layer 17 is XnMeg (w_kM, where 〇35" ^0.65 > 〇.05^g^ 〇.〇8 > 0. 40^(n + g)^0. 71 - 〇. γ〇SkSl. 〇, where χ may be the metal w or Μ〇 in the transition layer η, Me may be The metal Rh or pd in the transition layer 15. The hard layer 17 is sputtered using one of the tungsten target and the molybdenum target used in the step (e), one of the dry and palladium targets, and ammonia gas and acetylene as reaction gases. The flow rate of ammonia gas can be 5〇~200sccm, the flow rate of acetylene can be 3〇~20〇sccm, and the working volume of argon gas can be 1〇〇~300's; cc:m.,: film time The thickness of the hard layer π may be 500 to 700 nm. [0037] In the preferred embodiment of the present invention, the coated member 1 is deposited on the surface of the substrate π as the underlayer 13, and then underlying the underlayer 13 The surface layer is deposited with the transition layer 15, and then the hard layer 17 is deposited on the surface of the transition layer 15. The film layer is well transitioned layer by layer, and no obvious stress is generated inside the film layer, and the film is plated under the application of external force. The layer does not fail due to internal stress defects; and Rh or Pd is introduced into the transition layer 15 and the hard layer 17, and the metal carbonitride lattice of Rh or Pd soluble in the transition layer 15 and the hard layer 17 is introduced. In the south temperature state, the metal carbonitride undergoes a crystal transformation, and the crystal lattice undergoes a sag change to generate a distortion stress, thereby strengthening the hardness of the transition layer 15 and the hard layer 丨7, thereby effectively improving the transition layer 15 and The hot hardness of the hard layer 17 and the wear resistance at high temperature, correspondingly increase the service life and the temperature range of use of the mineral film member 1 [Schematic description] [0038] FIG. 1 is a preferred embodiment of the present invention. Cross-sectional view of the mineral film member of the embodiment 099134636 Form No. A0101 Page 8 of 13 0992060477-0 201215500 ' [Main component symbol description] [0039] Coated member: 10 [0040] Substrate: 11 [0041] Bottom layer: 13 [0042] Transition layer: 15 [0043] Hard layer: 17

099134636 表單編號A0101 第9頁/共13頁 0992060477-0099134636 Form No. A0101 Page 9 of 13 0992060477-0

Claims (1)

201215500 七、申請專利範圍: L —種鍍膜件’包括基材,其改良在於:該賴件還包括形 成於基材表面的打底層、形成於打底層表面的過渡層及形 成於過渡層表面的硬質層,該打底層為M、Ti、以或以 層;該過渡層為AtXyMez(c人V)層,其中〇.仏錢8 J 〇.35^y^〇.65 > 0.05^ z^ 0.08 . 0.75 ^(t + y + z) $1·〇5,〇·75$ν$1.〇,其中A為打底層中的金屬M、 Τι、Cr或Zr ’ X為W或Mo,Me為Rh或Pd ;該硬質層為 xnMeg(CkNl k)層,其中〇 35$η$〇. 65, U8 ’ 0·40%4)^·7Γ’ 〇 7〇客紅1〇,其令乂為 過渡層中的金屬W或Mo,Me為過渡層中的金屬Rh*pd。 2·如申請專利範圍第】項所述之鑛膜件,其中所述基材為紹 合金、鎂合金、鈦合金或不銹鋼。 3 .如申請專利範圍第!項所述之鑛膜件:其中所述打底層以 磁控濺射的方式形成,該打底層的厚度為100〜20〇nm。 4 .如申請專利範圍第w所述之鑛膜件:其中所述過渡層以 磁控濺射的方式形成,該過渡層;的厚度為1〇〇〜3〇〇nm。 5. 如申請專利範圍第!項所述之鑛膜禅:其中所述硬質層以 磁控濺射的方式形成,該硬質層的厚度為3〇〇〜6〇〇nm。 6. —種鍍膜件的製備方法,其包括如下步驟: 提供一基材; 在孩基材表面形成打底層,該打底層為A1、Ti、Cr或Zr 層; 在打底層的表面形成過渡層,該過渡層為 AtWhU 層,其中 0.4StS0.8,〇.35SyS 099134636 表單編號A0101 第10頁/共13頁 0992060477-0 201215500 0.65,0.05SzS0.08,0. 75S(t + y + z) SI. 05, 0.75SvS1.0,其中A為打底層中的金屬A1、Ti、Cr或 Zr,X為W或Mo,Me為Rh 或Pd ; 在過渡層的表面形成硬質層,該硬質層為X Me (C^N,,) n g k 1 -k 層,其中 0.35SnS0.65,0.05SgS0.08,0.40S (n + g)S0.71,0.70SkS1.0,其中X為過渡層中的金屬 W或Mo,Me為過渡層中的金屬Rh或Pd。201215500 VII. Patent application scope: L—a coated member ′ includes a substrate, and the improvement thereof comprises: forming a primer layer formed on a surface of the substrate, a transition layer formed on the surface of the primer layer, and a surface formed on the surface of the transition layer. a hard layer, the underlayer is M, Ti, or with a layer; the transition layer is an AtXyMez (c human V) layer, wherein 〇.仏钱8 J 〇.35^y^〇.65 > 0.05^ z^ 0.08 . 0.75 ^(t + y + z) $1·〇5,〇·75$ν$1.〇, where A is the metal M, Τι, Cr or Zr in the bottom layer. X is W or Mo, and Me is Rh. Or Pd; the hard layer is a xnMeg (CkNl k) layer, wherein 〇35$η$〇. 65, U8 '0·40%4)^·7Γ' 〇7〇客红1〇, which makes 乂 a transition layer The metal W or Mo, Me is the metal Rh*pd in the transition layer. 2. The mineral film member of claim 7, wherein the substrate is a sinter alloy, a magnesium alloy, a titanium alloy or a stainless steel. 3. If you apply for a patent scope! The mineral film member according to the invention, wherein the underlayer is formed by magnetron sputtering, and the underlayer has a thickness of 100 to 20 Å. 4. The mineral film member of claim w, wherein the transition layer is formed by magnetron sputtering, the transition layer; having a thickness of 1 〇〇 3 〇〇 nm. 5. If you apply for a patent scope! The mineral film zen: wherein the hard layer is formed by magnetron sputtering, and the thickness of the hard layer is 3 〇〇 6 6 〇〇 nm. 6. A method of preparing a coated member, comprising the steps of: providing a substrate; forming a primer layer on a surface of the substrate of the substrate, the underlayer being an A1, Ti, Cr or Zr layer; forming a transition layer on the surface of the underlying layer The transition layer is the AtWhU layer, where 0.4StS0.8, 〇.35SyS 099134636 Form No. A0101 Page 10 / Total 13 Page 0992060477-0 201215500 0.65, 0.05SzS0.08, 0. 75S(t + y + z) SI 05, 0.75SvS1.0, where A is the metal A1, Ti, Cr or Zr in the underlayer, X is W or Mo, Me is Rh or Pd; a hard layer is formed on the surface of the transition layer, the hard layer is X Me (C^N,,) ngk 1 -k layer, where 0.35SnS0.65, 0.05SgS0.08, 0.40S (n + g)S0.71, 0.70SkS1.0, where X is the metal W in the transition layer Or Mo, Me is the metal Rh or Pd in the transition layer. ❹ 099134636 .如申請專利範圍第6項所述之鍍膜件的製備方法,其中所 述形成打底層的步驟採用如下方式實現:採用磁控濺射法 ,使用鋁乾、鈦靶、鉻乾、鍅乾中的一種為靶材,以氬氣 為工作氣體,氬氣流量為100〜300sccm,基材偏壓為 -100〜-200V,加熱使基材的溫度為200〜500°C,鍍膜 時間為10〜30miη。 .如申請專利範圍第6項所述之鍍膜件的製備方法,其中所 述形成過渡層的步驟採用如下方式實現:採用磁控濺射法 \ ,使用鋁靶、鈦靶、鉻靶、锆靶中的一種、鎢靶與鉬靶中 的一種以及铑粗與纪把中的一種為把材,以氨氣和乙炔為 反應氣體,氨氣流量為50〜200sccm,乙炔流量為30〜 200sccm,以氬氣為工作氣體,氬氣流量為100〜 300sccm,基材偏壓為-100〜-200V,加熱使基材的溫度 為200〜500°C,鍍膜時間為30〜40min。 .如申請專利範圍第6項所述之鍍膜件的製備方法,其中所 述形成硬質層的步驟採用如下方式實現:採用磁控濺射法 ,使用鎢靶與鉬靶中的一種及铑靶與鈀靶中的一種為靶材 ,以氨氣和乙炔為反應氣體,氨氣流量為50〜200sccm, 乙炔流量為30〜200seem,以氬氣為工作氣體,氬氣流量 表單編號A0101 第11頁/共13頁 0992060477-0 201215500 為100〜300sccm,基材偏壓為-100--200V,加熱使基 材的溫度為200〜500°C,鍍膜時間為30〜60min。 099134636 表單編號A0101 第12頁/共13頁 0992060477-0The method for preparing a coated member according to claim 6, wherein the step of forming the underlayer is carried out by using a magnetron sputtering method, using an aluminum dry, a titanium target, a chrome dry, and a crucible. One of the dry targets is argon gas, the flow rate of argon gas is 100~300sccm, the substrate bias is -100~-200V, and the temperature of the substrate is 200~500°C. The coating time is 10~30miη. The method for preparing a coated member according to claim 6, wherein the step of forming the transition layer is carried out by using a magnetron sputtering method, using an aluminum target, a titanium target, a chromium target, and a zirconium target. One of the tungsten target and the molybdenum target, and one of the upset and the disc is a material, the ammonia gas and the acetylene are used as the reaction gas, the ammonia gas flow rate is 50 to 200 sccm, and the acetylene flow rate is 30 to 200 sccm. The argon gas is a working gas, the flow rate of the argon gas is 100 to 300 sccm, the substrate bias is -100 to -200 V, and the temperature of the substrate is 200 to 500 ° C by heating, and the coating time is 30 to 40 min. The method for preparing a coated member according to claim 6, wherein the step of forming a hard layer is performed by using a magnetron sputtering method, using one of a tungsten target and a molybdenum target, and a target One of the palladium targets is a target gas, ammonia gas and acetylene are used as reaction gases, ammonia gas flow rate is 50~200sccm, acetylene flow rate is 30~200seem, argon gas is used as working gas, argon gas flow form number A0101 page 11/ A total of 13 pages 0992060477-0 201215500 is 100~300sccm, the substrate bias is -100--200V, the substrate temperature is 200~500 °C, and the coating time is 30~60min. 099134636 Form No. A0101 Page 12 of 13 0992060477-0
TW99134636A 2010-10-11 2010-10-11 Coated article and method for making the same TW201215500A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
TW99134636A TW201215500A (en) 2010-10-11 2010-10-11 Coated article and method for making the same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TW99134636A TW201215500A (en) 2010-10-11 2010-10-11 Coated article and method for making the same

Publications (1)

Publication Number Publication Date
TW201215500A true TW201215500A (en) 2012-04-16

Family

ID=46786810

Family Applications (1)

Application Number Title Priority Date Filing Date
TW99134636A TW201215500A (en) 2010-10-11 2010-10-11 Coated article and method for making the same

Country Status (1)

Country Link
TW (1) TW201215500A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103935075A (en) * 2013-01-23 2014-07-23 深圳富泰宏精密工业有限公司 Shell and manufacturing method thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103935075A (en) * 2013-01-23 2014-07-23 深圳富泰宏精密工业有限公司 Shell and manufacturing method thereof
CN103935075B (en) * 2013-01-23 2018-07-03 深圳富泰宏精密工业有限公司 Housing and preparation method thereof

Similar Documents

Publication Publication Date Title
JP4850074B2 (en) Method for coating abrasives
CN101712215B (en) TiCN series nanometer gradient compound multi-layer coating and method for preparing same
WO2017156996A1 (en) Composite functional cutter coating for cutting titanium alloy and preparation method therefor
CN109402564B (en) AlCrSiN and AlCrSiON double-layer nano composite coating and preparation method thereof
TW200927479A (en) Structural material of diamond like carbon complex films and method of manufacturing the same
JP7382124B2 (en) Improved coating process
CN101698363B (en) TiN/(TiN+CrN)/CrAlN nano composite coating and preparation method thereof
US8372524B2 (en) Coated article
CN106244986A (en) Diamond-like carbon film of functionally gradient and preparation method thereof and goods
CN109097743A (en) A kind of superhard W-Cr-Al-Ti-N nanometer gradient multilayer film and preparation method thereof
CN102443772A (en) Coated article and its preparation method
US20130244054A1 (en) Composite material and method for improving fatigue properties of titanium alloy by coating metallic glass layer
TW201239110A (en) Coated article and method for making the same
CA2612881A1 (en) Coating system for high temperature stainless steel
TW201016861A (en) Cemented WC with diamond film
CN102465258A (en) Film-coated piece and preparation method thereof
Zhitomirsky et al. Vacuum arc deposition of metal/ceramic coatings on polymer substrates
TW201215500A (en) Coated article and method for making the same
CN110565051B (en) Diamond coated cutting tool with color layer, preparation method thereof and processing equipment
TW201213108A (en) Coated article and method for making the same
JP2974285B2 (en) Manufacturing method of coated carbide tool
JP2660180B2 (en) Coated carbide tool
CN109666890A (en) A kind of TiAlZr-Cr of carbide surface (Ti, Al, Zr, Cr) N Gradient Film
TW201221664A (en) Coated article and method for making the same
TW201240826A (en) Coating and method for manufacturing the coating