TW201028287A - Metal clad body, circuit board and electronic part - Google Patents
Metal clad body, circuit board and electronic part Download PDFInfo
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- TW201028287A TW201028287A TW98131412A TW98131412A TW201028287A TW 201028287 A TW201028287 A TW 201028287A TW 98131412 A TW98131412 A TW 98131412A TW 98131412 A TW98131412 A TW 98131412A TW 201028287 A TW201028287 A TW 201028287A
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K3/00—Apparatus or processes for manufacturing printed circuits
- H05K3/0011—Working of insulating substrates or insulating layers
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K1/00—Printed circuits
- H05K1/02—Details
- H05K1/03—Use of materials for the substrate
- H05K1/0393—Flexible materials
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K2201/00—Indexing scheme relating to printed circuits covered by H05K1/00
- H05K2201/06—Thermal details
- H05K2201/068—Thermal details wherein the coefficient of thermal expansion is important
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K2203/00—Indexing scheme relating to apparatus or processes for manufacturing printed circuits covered by H05K3/00
- H05K2203/11—Treatments characterised by their effect, e.g. heating, cooling, roughening
- H05K2203/1105—Heating or thermal processing not related to soldering, firing, curing or laminating, e.g. for shaping the substrate or during finish plating
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K3/00—Apparatus or processes for manufacturing printed circuits
- H05K3/02—Apparatus or processes for manufacturing printed circuits in which the conductive material is applied to the surface of the insulating support and is thereafter removed from such areas of the surface which are not intended for current conducting or shielding
- H05K3/06—Apparatus or processes for manufacturing printed circuits in which the conductive material is applied to the surface of the insulating support and is thereafter removed from such areas of the surface which are not intended for current conducting or shielding the conductive material being removed chemically or electrolytically, e.g. by photo-etch process
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- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Laminated Bodies (AREA)
- Chemically Coating (AREA)
- Electroplating Methods And Accessories (AREA)
Abstract
Description
201028287 六、發明說明: 【發明所屬之技術領域】 本發明係關於金屬護面疊層體、電路基板以及電子零 件。尤其關於可縮小於藉由飩刻除去導體且在所形成之電 路基板安裝半導體元件之時由於焊料加熱所產生之熱變形 ,並且可提高連接信賴性的金屬護面疊層體、電路基板以 及電子零件。 ❺ 【先前技術】 近年來,多使用將半導體晶片直接搭載於薄膜配線板 之被稱爲COF ( Chip On Film )的方法。如此之安裝形式 雖然經常使用液晶畫面之1C驅動器之基板連接法,但是由 於訊號配線之微細化、半導體晶片之大型化,於安裝時所 產生之熱變形變大,半導體晶片和基板之連接信賴性則成 爲大問題。 φ 例如,矽晶片之熱膨脹係數爲3ppm/K,對此一般基板 之熱膨脹係數爲16〜6 Oppm/Κ,故於焊料加熱後下降至室 溫之時,由於熱膨脹差產生熱變形之情形則成爲大問題( 例如,參照專利文獻1 )。 [先前技術文獻] [專利文獻] [專利文獻1]日本特開2007-2625 63號公報 201028287 【發明內容】 [發明所欲解決之課題] 就以縮小該熱變形之方法而言,例如有使用低熱膨脹 係數之基板的方法。但是,電路基板因使用銅以作爲導體 ,故當縮小薄膜基材之熱膨脹係數之時,則有由於與銅之 熱膨脹係數(16ppm/K)之不同,產生基板之彎曲等之問 題,實質上無法解決。 本發明係鑑於上述之問題點而所硏究出,其目的在於 @ 提供可縮小於藉由蝕刻除去導體且在所形成之電路基板安 裝半導體元件之時由於焊料加熱所產生之熱變形,並且可 提高連接信賴性的金屬護面疊層體、電路基板以及電子零 件。 [用以解決課題之手段] 發明者針對上述以往之問題點精心硏究。其結果,判 明藉由使用在以蝕刻除去金屬層之後的熱處理中在平面方 © 向膨脹0.05〜0.4%之金屬護面叠層體,則可以縮小於將半 導體元件安裝於電路基板之時由於焊料加熱所產生之熱變 形。並且,熱處理係以軟化薄膜之溫度爲佳,爲將半導體 晶片直接搭載在電路基板之時的焊接。 該發明係藉由上述硏究成果而所創作出。 本發明之第1態樣所涉及之金屬護面疊層體爲具有薄 膜基材,和由銅(Cu)或銅(Cu)合金所構成之金屬層的 金屬護面疊層體,其特徵爲:以蝕刻除去上述金屬層之至 -6- 201028287 少一部份之後的熱處理中之上述金屬護面疊層體之平面方 向之尺寸變化率爲0.05〜0.4%。 本發明之第2態樣所涉及之金屬護面疊層體係在本發 明之第1態樣所涉及之金屬護面疊層體中,上述薄膜基材 之平面方向之線膨脹係數爲13〜6 0ppm/K。 本發明之第3態樣所涉及之金屬護面疊層體係在本發 明之第1或第2態樣所涉及之金屬護面疊層體中,在上述薄 φ 膜基材和上述金屬層之間形成有基底金屬層。 本發明之第4態樣所涉及之金屬護面疊層體係在本發 明之第3態樣所涉及之金屬護面疊層體中,上述基底金屬 層係由鎳(Ni)、鎳合金(Ni合金)、銅(Cu)、銅合金 (Cu合金)中之任一種所構成。 本發明之第5態樣所涉及之金屬護面疊層體係在本發 明之第1至第4態樣中之任一態樣所涉及之金屬護面疊層體 中,上述薄膜基材爲熱可塑性薄膜。 φ 本發明之第6態樣所涉及之金屬護面疊層體係在本發 明之第5態樣所涉及之金屬護面疊層體中,上述薄膜基材 係由從得到光學各向異性之溶融相的高分子、熱可塑性之 聚醯亞胺樹脂、聚醚醚酮(PEEK )樹脂、聚對苯二甲酸 乙二酯(PET )樹脂、聚萘二甲酸乙二酯(PEN )樹脂所 構成之群中選擇出之任一種類所構成。 本發明之第7態樣所涉及之金屬護面疊層體係在本發 明之第1至第4態樣中之任一態樣所涉及之金屬護面疊層體 中,上述薄膜基材係由非熱可塑性之聚醯亞胺樹脂所形成 201028287 本發明之第1態樣所涉及之電路基板,其特徵爲:使 用由本發明之第1至第7態樣中之任一態樣所涉及之金屬護 面疊層體而形成電路。 本發明之第1態樣所涉及之電路基板,其特徵爲:在 本發明之第1態樣所涉及之電路基板上直接搭載半導體元 件。 本發明之第2態樣所涉及之電子零件係在本發明之第1 @ 態樣所涉及之電子零件中,上述半導體元件之電極藉由凸 塊被連接於上述電路基板。 並且,在本說明書中,「尺寸變化率」係將尺寸變大 之側設爲正,尺寸變小之側設爲負。 [發明之效果] 若藉由本發明,則可以藉由使用以蝕刻除去金屬層之 後的熱處理中之金屬護面疊層體之平面方向之尺寸變化率 〇 爲0.05〜0.4% (由於熱處理而膨脹)之金屬護面疊層體’ 縮小於將半導體元件安裝於電路基板之時由於焊料加熱所 產生之熱變形。因此,藉由使用如此之金屬護面疊層體’ 則可以製作信賴性高之電路基板及電子零件。 【實施方式】 以下’針對該本發明之一實施型態,—面參照圖一面 說明。並且,以下所說明之實施型態係用以說明’並非限 [S } -8- 201028287 制本發明之範圍。因此,若爲該項技藝者可採用以與此均 等之要素置換該些各要素或全要素的實施型態,但該些實 施型態也包含在本發明之範圍內。 首先,針對可適用本發明之金屬護面疊層體予以說明 。第1圖係表示本發明之第1實施形態所涉及之金屬護面疊 層體的截面圖。 如第1圖所示般,本發明之第1實施型態所涉及之金屬 Φ 護面疊層體10具有薄膜基材11和被形成在薄膜基材11之面 1 la上的金屬層12。 本實施形態所渉及之金屬護面疊層體10具有下述般之 特徵。 金屬護面叠層體10係以蝕刻除去上述金屬層12之至少 一部份之後的熱處理中之金屬護面疊層體10之平面方向之 尺寸變化率爲0.05〜0.4%。再者,薄膜基材11之平面方向 之線膨脹係數爲13〜60ppm/K。 φ 藉由使用適用具有上述特徵之本發明的金屬護面疊層 體10,則可以縮小在電路基板安裝半導體元件之時由於焊 料加熱所產生之熱變形。再者.,藉由使用如此之金屬護面 疊層體10,則可以製作信賴性高之電路基板及電子零件。 接著,針對本發明之另外實施型態所涉及之金屬護面 疊層體予以說明。 第2圖係表示本發明之第2實施形態所涉及之金屬護面 疊層體的截面圖。如第2圖所示般,本發明之第2實施型態 所涉及之金屬護面疊層體20具有薄膜基材11和分別被形成 -9- 201028287 在薄膜基材11之兩面lla、lib上的金屬層12以及金屬層 12’。金屬護面疊層體20和金屬護面疊層體10之不同點係 金屬護面疊層體10爲依照薄膜基材11和金屬層12之順序被 疊層之兩層構造,對此金屬護面疊層體20爲依照金屬層 12’和薄膜基材11和金屬層12之順序而被疊層的3層構造。 再者,本發明之第2實施型態所涉及之金屬護面疊層體20 具有與上述金屬護面疊層體10相同之特徵和效果。 第3圖係表示本發明之第3實施形態所涉及之金屬護面 疊層體的截面圖。如第3圖所示般,本發明之第3實施型態 所涉及之金屬護面疊層體30具有薄膜基材11和被形成在薄 膜基材11之面11 a上的基底金屬層13,和被形成在基底金 屬層13之面13a上的金屬層12。金屬護面疊層體30和金屬 護面疊層體10之不同點係金屬護面叠層體10爲依照薄膜基 材11和金屬層12之順序被疊層之兩層構造,對此金屬護面 叠層體30爲依照薄膜基材11和基底金屬層13和金屬層12之 順序而被疊層的3層構造。再者,本發明之第3實施型態所 涉及之金屬護面疊層體30具有與上述金屬護面叠層體10相 同之特徵和效果。 並且,在第3圖中,雖然說明僅在薄膜基材11之單面 上形成基底金屬層13,接著在基底金屬層13上形成金屬層 12之時,但是即使爲分別在薄膜基材11之兩面上形成基底 金靥層13,接著在各個基底金屬層13上形成金屬層12’依 照金屬層12和基底金屬層13和薄膜基材11和基底金屬層13 和金屬層12之順序而被疊層之5層構造亦可。 201028287 接著,針對可適用本發明之金屬護面疊層體之金屬層 、基底金屬層、薄膜基材予以說明。可適用本發明之金屬 護面疊層體10、20、30之金屬層12、12’係由銅(Cu)或 銅合金(Cu合金)所構成。 再者,作爲可適用本發明之金屬護面疊層體30之基底 金屬層13,以由鎳(Ni)、鎳合金(Ni合金)、銅(Cu) 、銅合金(Cu合金)中之任一種所構成爲佳。再者,基底 φ 金屬層13之厚度以0.05至0.5微米厚度之範圍爲佳。 雖然可撓性電路基板使用耐熱性優之非熱可塑性聚醯 亞胺基材爲多,但是作爲可適用本發明之金屬護面疊層體 10、20、30之薄膜基材11,以使用溫度較高可撓性電路基 板容易軟化之熱可塑化樹脂之方式爲佳。該係因爲銅蝕刻 後。由於熱容易引起膨脹之故。 具體而言,可以適用液晶聚合物薄膜、聚醚醚酮( PEEK )、熱可塑性聚醯亞胺薄膜、聚酯薄膜等。再者’ φ 在聚酯薄膜中,雖然耐熱性比較低,但是聚萘二甲酸乙二 酯(PEN )、聚對苯二甲酸乙二酯(PET )可以適應。 於執行實際之Sn、SnAg系之焊接時,液晶聚醋、 PEEK、熱可塑性聚醯亞胺之耐熱性高爲佳。 接著,針對可適用本發明之金屬護面疊層體的電路基 板(配線基板),藉由蝕刻除去後之熱處理而膨脹的機構 ,以金屬護面叠層體30爲例予以說明。 製作金屬護面疊層體3 0係不使用接著劑,以將金屬直 接電鍍於薄膜基材11之方法來製作。此時,在電鍍皮膜殘 -11 - 201028287 留應力,藉由之後的熱處理,製作事先在平面方向收縮一 定量的金屬護面疊層體30。 即是,藉由無電解電鍍形成基底金屬層13之時,以電 鍍皮膜成爲拉伸應力的電鍍液、電鍍條件製作皮膜。接著 ,藉由加熱至薄膜之軟化溫度,使薄膜軟化,藉由電鍍皮 膜之應力,使金屬護面疊層體3 0在平面方向收縮。 於製作配線基板之時,藉由以蝕刻除去一部份之金屬 層12,除去電鍍皮膜之應力。因此,藉由再次加熱,解放 @ 薄膜基材11之收縮量。即是,可取得於焊料加熱時膨脹之 金屬護面叠層體30。 首先,針對可適用本發明之金屬護面疊層體之一製造 方法予以說明。在此,以直接將金屬電鍍於薄膜基材11而 製作金屬護面疊層體30之方法爲例予以說明。 首先,於電鍍之前,在薄膜基材Π表面執行粗化處理 (表面之粗化處理)。接著,執行無電解電鍍形成金屬層 之基底層(基底金屬層或是基底電鍍層)13(基底金屬層 @ 之形形成處理)。於形成基底金靥層13之時,以電鍍皮膜 之應力成爲拉伸應力之方式執行電鍍。 要形成持有拉伸應力之基底金屬層13,電鍍浴之pH從 弱酸性至中性,適合在60 °C以上之高溫實用性被析出的無 電解鎳-磷電鍍液。再者,適合析出之金屬皮膜之磷濃度 爲5 %以下之低濃度磷、5〜10%左右之中濃度磷皮膜。 電鍍皮膜(在此,爲基底金屬層13)之應力爲拉伸應 力或壓縮應力之判斷,可以僅對薄膜基材11之單面執行電 -12- 201028287 鍍,觀看電鍍後之金屬護面疊層體之彎曲方向而判斷。即 是,當電鍍皮膜置放成上方之時,若成爲凹狀’電鍍皮膜 則表示拉伸應力,若成凸狀,電鍍皮膜則表示壓縮應力。 依此,電鍍皮膜因對薄膜基材η產生收縮之力’故在 之後之熱處理中,當薄膜基材軟化時’由於電鍍皮膜之應 力,使得金屬護面疊層體3 0在平面方向收縮。 因此,藉由電鍍液之選定、電鍍條件’控制電鑛皮膜 φ 之應力,依據熱處理,使薄膜基材11軟化,依此可製作出 事先在平面方向收縮之金屬護面疊層體3〇。 作爲薄膜基材11之表面用之基底電鍍,使用無電解 鎳-磷電鍍液、無電解銅電鍍液等,在薄膜基材11之表面 以0.05至0.5微米厚度之範圍使基底金屬層13析出。 接著,執行熱處理(熱處理)。在此,熱處理係以金 屬護面疊層體30可以維持平坦形狀之方式負荷有張力之狀 態下執行,或者爲了防止明顯變形在可以維持重疊薄膜之 φ 靜止狀態的狀態下執行爲佳。即是,以在平坦支持板重疊 多片薄膜而執行加熱,或是在捲成捲筒狀之狀態執行加熱 爲佳。或是,即使以從加熱至冷卻金屬護面疊層體30可以 一貫維持平坦形狀之方式,對金屬護面疊層體30負荷張力 •而予以連續性加熱亦可。 藉由該熱處理薄膜軟化,金屬護面疊層體3 0依據電鍍 皮膜之應力,在平面方向收縮。收縮量越大,銅飽刻後之 焊料加熱時之膨脹量變大。 最後,在基底電鍍上,利用電鍍銅,形成1微米至20 -13- 201028287 微米厚度之上部金屬層12以當作導體(上部金屬層之形成 處理)。製作金屬護面疊層體30。 在上述金屬護面疊層體3 0之製作方法中,於形成基底 金屬層1 3之後,執行熱處理,最後形成上部金屬層1 2,但 是即使於形成基底金屬層13之後,接著形成上部金屬層12 ,最後執行熱處理亦可。 將收縮量設定成較大之時,則以僅形成基底金屬層13 之後執行熱處理之方式爲佳。僅無電解電鍍皮膜之側拉伸 應力大之故。 接著,針對可適用本發明之電路基板及電子零件予以 說明。第4圖係表示本發明之一實施形態所涉及之電路基 板的截面圖。在此,以使用第1圖所示之金屬護面疊層體 10而形成電路之電路基板爲例予以說明。 如第4圖所示般,電路基板40具有薄膜基材11和被疊 層在薄膜基材11之面11a上之形成電路的電路金屬層15。 就以該電路基板40之電路金屬層15之形成方法而言,例如 藉由扣除法,以成爲所欲配線圖案之方式,利用蝕刻除去 第1圖所示之金屬護面疊層體10之金屬層12不需要之金屬 部分,形成具有所欲配線圖案之電路金屬層15。 第5圖係表示本發明之一實施形態所涉及之電子零件 的截面圖。在此,以使用第4圖所示之電路基板40之電子 零件爲例予以說明。 如第5圖所示般,電子零件50係在第4圖所示之電路基 板4〇表面殘留半導體元件16之安裝部分而塗佈防焊劑17, 201028287 藉由凸塊18連接電路基板40之電路金屬層15和半導體元件 1 6之電極。 藉由使用可適用上述本發明的金屬護面疊層體10 ’則 可以縮小在電路基板40安裝半導體元件16之時由於焊料加 熱所產生之熱變形。因此,可以製作出信賴性高之電路基 板40及電子零件50。 接著,說明本發明較佳的幾個實施例。在此’針對依 φ 據銅蝕刻後之熱處理可適用本發明之金屬護面疊層體之平 面方向之尺寸變化率(膨脹率)之測量結果,以及使用可 適用本發明之金屬疊層體之電路基板和半導體晶片之連接 信賴性的實施例予以說明。 薄明 子說 分以 高予 的形 相情 融之 溶11 }之材 例性基 較異膜 比向薄 及各作 例學當 施光以 實成 } 之形膜 膜得薄 薄取物 物用合 合使聚 聚對晶 晶針液 液 ( ( Μ φ 。在此,就以高分子薄膜(液晶聚合物薄膜)而言’針對 使用KURARA (股)製作的VecsterCT之情形予以說明。並 且,薄膜厚度使用5 0微米厚度。 首先,將高分子薄膜浸泡在80°C之1〇規度(Normal) 之氫氧化鉀溶液15至30分鐘,溶解表面形成凹凸。接著’ 依照改質劑處理、鎳合金之無電解電鍍處理、熱處理、銅 之電鍍處理之順序施予各處理,製造出可適用本發明之金 屬護面疊層體30 (薄膜金屬護面疊層體)。. 改質劑處理係藉由奧野製藥工業(股)製作之OPC- -15- 201028287 3 50改質劑,洗淨高分子薄膜之表面。在此,使用奧野製 藥工業(股)之OPC-80觸媒,以作爲含有鈀之觸媒賦予液 ,使用OPC-500加速劑,以做爲活性化劑。 鎳合金之無電解電鑛處理係在薄膜兩面執行鎳-磷電 鍍。就以市售的鎳-磷電鍍液而言,使用奧野製藥工業( 股)製作之 TOP Nicoron LPH-LF。 皮膜應力使浴溫度、pH、次磷酸和金屬鎳之比率等變 更,製作出由不同基底電鍍皮膜(基底金屬層13)所構成 之薄膜金屬護面叠層體30 (從實施例1至實施例10之10種 類)。pH設爲5.6至6.3之範圍,在兩面形成0.1微米厚度之 基底電鍍層(基底金屬層13)。 電鍍皮膜(基底金屬層13)之應力之判定係僅執行單 面電鍍,觀看於電鍍後所產生之彎曲之方询,判斷爲拉伸 應力或壓縮應力。並且,於電鍍後電鍍皮膜側成爲凹之時 ,判斷爲拉伸應力,於成爲凸之時判斷爲壓縮應力。 熱處理係將薄膜金屬護面疊層體放入至熱處理槽,將 熱處理溫度在200°C至250°C保持10分鐘。 銅電鍍處理係以導體厚度(金屬層12之厚度)成爲8 微米之方式形成銅(金屬層12)。銅電鑛液使用下述。並 且,以使用荏原優吉莱特(股)製作之CU-BRITE TH-RIII 以作爲添加劑。並且,在所有實施例中,於兩面形成導體 (金屬層12 )。201028287 VI. Description of the Invention: TECHNICAL FIELD OF THE INVENTION The present invention relates to a metal facing laminate, a circuit substrate, and an electronic component. In particular, it is possible to reduce the thermal deformation of the conductor by the engraving of the conductor and the mounting of the semiconductor element on the formed circuit board, and to improve the connection reliability, the metal sheath laminate, the circuit board, and the electron Components.先前 [Prior Art] In recent years, a method called COF (Chip On Film) in which a semiconductor wafer is directly mounted on a thin film wiring board has been used. In such a mounting form, the substrate connection method of the 1C driver of the liquid crystal screen is often used. However, due to the miniaturization of the signal wiring and the enlargement of the semiconductor wafer, the thermal distortion generated during mounting becomes large, and the connection reliability of the semiconductor wafer and the substrate is increased. It becomes a big problem. φ For example, the thermal expansion coefficient of the germanium wafer is 3 ppm/K, and the thermal expansion coefficient of the general substrate is 16 to 6 Oppm/Κ, so when the solder is heated to fall to room temperature, the thermal deformation due to the difference in thermal expansion becomes A big problem (for example, refer to Patent Document 1). [Prior Art] [Patent Document 1] [Patent Document 1] JP-A-2007-2625 63-A Publication No. 201028287 [Problem to be Solved by the Invention] The method for reducing the thermal deformation is, for example, used. A method of a substrate having a low coefficient of thermal expansion. However, since the circuit board uses copper as a conductor, when the thermal expansion coefficient of the film substrate is reduced, there is a problem that the substrate is bent or the like due to the difference in thermal expansion coefficient (16 ppm/K) of copper. solve. The present invention has been made in view of the above problems, and an object thereof is to provide a thermal deformation which can be reduced by removing a conductor by etching and mounting a semiconductor element on a formed circuit substrate due to solder heating, and can be A metal facing laminate, a circuit board, and an electronic component that improve connection reliability. [Means for Solving the Problem] The inventors have carefully studied the above-mentioned problems. As a result, it has been found that by using a metal sheath laminate which is expanded by 0.05 to 0.4% in the plane direction during the heat treatment after the metal layer is removed by etching, it is possible to reduce the solder when the semiconductor element is mounted on the circuit board. Thermal deformation caused by heating. Further, the heat treatment is preferably a temperature of the softened film, and is a soldering when the semiconductor wafer is directly mounted on the circuit board. The invention was created by the above research results. A metal sheath laminate according to a first aspect of the present invention is a metal sheath laminate having a film substrate and a metal layer made of copper (Cu) or a copper (Cu) alloy, and is characterized by The rate of dimensional change in the planar direction of the metal facing laminate in the heat treatment after removing the metal layer to -6-201028287 by etching is 0.05 to 0.4%. In the metal sheath laminate according to the second aspect of the present invention, the linear expansion coefficient of the film substrate in the planar direction is 13 to 6 in the metal sheath laminate according to the first aspect of the present invention. 0ppm/K. A metal sheath laminate system according to a third aspect of the present invention, in the metal sheath laminate according to the first or second aspect of the present invention, in the thin φ film substrate and the metal layer A base metal layer is formed therebetween. According to a fourth aspect of the present invention, in a metal sheath laminate according to a third aspect of the present invention, the base metal layer is made of nickel (Ni) or a nickel alloy (Ni). Any of alloys, copper (Cu), and copper alloys (Cu alloys). A metal facing laminate system according to a fifth aspect of the present invention, wherein the film substrate is hot in any one of the first to fourth aspects of the present invention Plastic film. In the metal sheath laminate according to the fifth aspect of the present invention, the film substrate is obtained by obtaining optical anisotropy. Phase polymer, thermoplastic polyimine resin, polyetheretherketone (PEEK) resin, polyethylene terephthalate (PET) resin, polyethylene naphthalate (PEN) resin Any of the categories selected in the group. In the metal facing laminate according to any one of the first to fourth aspects of the present invention, the film substrate is composed of the metal substrate laminate according to the seventh aspect of the present invention. Non-thermoplastic polyimine resin is formed in the circuit board according to the first aspect of the present invention, which is characterized in that the metal involved in any of the first to seventh aspects of the present invention is used. The laminate is laminated to form an electrical circuit. A circuit board according to a first aspect of the present invention is characterized in that a semiconductor element is directly mounted on a circuit board according to a first aspect of the present invention. According to a second aspect of the invention, in the electronic component according to the first aspect of the invention, the electrode of the semiconductor element is connected to the circuit board by a bump. Further, in the present specification, the "dimension change rate" is such that the side where the size is increased is set to be positive, and the side where the size is decreased is set to be negative. [Effects of the Invention] According to the present invention, the dimensional change rate 〇 of the metal facing laminate in the heat treatment after the metal layer is removed by etching can be 0.05 to 0.4% (expanded by heat treatment) The metal facing laminate ' is reduced in thermal deformation due to solder heating when the semiconductor component is mounted on the circuit board. Therefore, by using such a metal facing laminate body, a circuit board and electronic components having high reliability can be produced. [Embodiment] Hereinafter, one embodiment of the present invention will be described with reference to the drawings. Further, the embodiments described below are intended to illustrate the scope of the invention not limited to [S } -8- 201028287. Therefore, those skilled in the art may adopt an embodiment in which the elements or all of the elements are replaced by equivalent elements, but such embodiments are also included in the scope of the present invention. First, a metal facing laminate to which the present invention is applicable will be described. Fig. 1 is a cross-sectional view showing a metal sheath laminate according to a first embodiment of the present invention. As shown in Fig. 1, the metal Φ sheath laminate 10 according to the first embodiment of the present invention has a film substrate 11 and a metal layer 12 formed on the surface 1 la of the film substrate 11. The metal facing laminate 10 of the present embodiment has the following features. The metal facing laminate 10 has a dimensional change ratio in the planar direction of the metal facing laminate 10 in the heat treatment after etching and removing at least a part of the metal layer 12 is 0.05 to 0.4%. Further, the linear expansion coefficient of the film substrate 11 in the planar direction is 13 to 60 ppm/K. φ By using the metal facing laminate 10 of the present invention having the above characteristics, it is possible to reduce the thermal deformation caused by the heating of the solder when the semiconductor element is mounted on the circuit board. Further, by using such a metal sheath laminate 10, a circuit board and electronic components having high reliability can be produced. Next, a metal facing laminate according to another embodiment of the present invention will be described. Fig. 2 is a cross-sectional view showing a metal sheath laminate according to a second embodiment of the present invention. As shown in Fig. 2, the metal facing laminate 20 according to the second embodiment of the present invention has a film substrate 11 and is formed on each of the surfaces 11a and 11b of the film substrate 11 by -9-201028287. Metal layer 12 and metal layer 12'. The metal facing laminate 20 and the metal facing laminate 10 are different in point. The metal facing laminate 10 is a two-layer structure in which the film substrate 11 and the metal layer 12 are laminated in this order. The surface laminate 20 has a three-layer structure in which the metal layer 12' and the film substrate 11 and the metal layer 12 are laminated in this order. Further, the metal sheath laminate 20 according to the second embodiment of the present invention has the same features and effects as those of the metal sheath laminate 10. Fig. 3 is a cross-sectional view showing a metal sheath laminate according to a third embodiment of the present invention. As shown in Fig. 3, the metal facing laminate 30 according to the third embodiment of the present invention has a film substrate 11 and a base metal layer 13 formed on the surface 11a of the film substrate 11. And a metal layer 12 formed on the face 13a of the base metal layer 13. The metal facing laminate 30 and the metal facing laminate 10 are different in point. The metal facing laminate 10 is a two-layer structure in which the film substrate 11 and the metal layer 12 are laminated in this order. The surface laminate 30 has a three-layer structure in which the film substrate 11 and the base metal layer 13 and the metal layer 12 are laminated in this order. Further, the metal facing laminate 30 according to the third embodiment of the present invention has the same features and effects as the above-described metal facing laminate 10. Further, in FIG. 3, although the base metal layer 13 is formed only on one surface of the film substrate 11, and then the metal layer 12 is formed on the base metal layer 13, even if it is separately on the film substrate 11, A base metal layer 13 is formed on both sides, and then a metal layer 12' is formed on each of the base metal layers 13 in accordance with the order of the metal layer 12 and the base metal layer 13 and the film substrate 11 and the base metal layer 13 and the metal layer 12. The five-layer structure of the layer is also possible. 201028287 Next, a metal layer, a base metal layer, and a film substrate to which the metal sheath laminate of the present invention can be applied will be described. The metal layers 12, 12' to which the metal facing laminates 10, 20, 30 of the present invention can be applied are composed of copper (Cu) or a copper alloy (Cu alloy). Further, as the base metal layer 13 to which the metal sheath laminate 30 of the present invention is applicable, any of nickel (Ni), nickel alloy (Ni alloy), copper (Cu), and copper alloy (Cu alloy) is used. One is better. Further, the thickness of the base φ metal layer 13 is preferably in the range of 0.05 to 0.5 μm. Although the flexible circuit substrate is made of a non-thermoplastic polyimide substrate having excellent heat resistance, the film substrate 11 to which the metal sheath laminates 10, 20, and 30 of the present invention can be applied is used at a temperature. A method of thermally plasticizing the resin in which the higher flexible circuit substrate is easily softened is preferred. This is because copper is etched. Because heat is easy to cause expansion. Specifically, a liquid crystal polymer film, polyetheretherketone (PEEK), a thermoplastic polyimide film, a polyester film, or the like can be applied. Further, in the polyester film, although the heat resistance is relatively low, polyethylene naphthalate (PEN) and polyethylene terephthalate (PET) can be accommodated. When performing actual Sn and SnAg welding, liquid crystal polyacetate, PEEK, and thermoplastic polyimine have high heat resistance. Next, a metal sheath laminate 30 will be described as an example of a mechanism in which a circuit board (wiring board) to which the metal sheath laminate of the present invention is applied is expanded by heat treatment after etching. The metal facing laminate 30 was produced by a method in which a metal was directly electroplated on the film substrate 11 without using an adhesive. At this time, stress is left on the plating film residue -11 - 201028287, and the metal sheath laminate 30 which has been contracted by a predetermined amount in the plane direction is produced by the subsequent heat treatment. In other words, when the underlying metal layer 13 is formed by electroless plating, a film is formed by plating solution in which the electroless plating film is subjected to tensile stress and plating conditions. Next, the film is softened by heating to the softening temperature of the film, and the metal facing laminate 30 is shrunk in the planar direction by the stress of the plating film. At the time of fabricating the wiring substrate, the stress of the plating film is removed by removing a portion of the metal layer 12 by etching. Therefore, the amount of shrinkage of the film substrate 11 is liberated by reheating. That is, the metal facing laminate 30 which is expanded when the solder is heated can be obtained. First, a method of manufacturing a metal facing laminate to which the present invention is applicable will be described. Here, a method of directly plating a metal onto the film substrate 11 to form the metal facing laminate 30 will be described as an example. First, a roughening treatment (surface roughening treatment) is performed on the surface of the film substrate before plating. Next, a base layer (base metal layer or base plating layer) 13 for forming a metal layer by electroless plating (formation treatment of the underlying metal layer @) is performed. At the time of forming the underlying gold layer 13, electroplating is performed in such a manner that the stress of the plating film becomes tensile stress. To form the base metal layer 13 holding the tensile stress, the pH of the plating bath is from weakly acidic to neutral, and it is suitable for an electroless nickel-phosphorus plating solution which is precipitated at a high temperature of 60 ° C or higher. Further, the phosphorus film having a phosphorus concentration suitable for precipitation is a low concentration of phosphorus of 5 % or less, and a concentration of a phosphorus film of about 5 to 10%. The stress of the plating film (here, the base metal layer 13) is judged by tensile stress or compressive stress, and only one side of the film substrate 11 may be subjected to electro--12-201028287 plating, and the metal sheath after plating may be viewed. Judging by the direction of the bend of the layer. That is, when the plating film is placed on the upper side, if it is in a concave shape, the plating film indicates tensile stress, and if it is convex, the plating film indicates compressive stress. According to this, the plating film is contracted by the film substrate η, so that in the subsequent heat treatment, when the film substrate is softened, the metal sheath laminate 30 shrinks in the planar direction due to the stress of the plating film. Therefore, the film substrate 11 is softened by the heat treatment by the selection of the plating solution and the plating conditions, and the metal substrate laminate 3 which has been previously shrunk in the planar direction can be produced. The base metal layer 13 is deposited on the surface of the film substrate 11 in a thickness of 0.05 to 0.5 μm using an electroless nickel-phosphorus plating solution, an electroless copper plating solution or the like as a substrate for the surface of the film substrate 11. Next, heat treatment (heat treatment) is performed. Here, the heat treatment is preferably performed in a state where the metal sheath laminate 30 can be loaded with tension in such a manner as to maintain a flat shape, or in order to prevent significant deformation from being performed in a state where the φ state of the superposed film can be maintained. That is, it is preferable to perform heating by superimposing a plurality of films on a flat support plate, or performing heating in a state of being wound into a roll. Alternatively, the metal facing laminate 30 may be subjected to continuous heating even if the flat surface of the metal facing laminate 30 is maintained in a uniform shape from the heating to the cooling of the metal facing laminate 30. By the softening of the heat-treated film, the metal facing laminate 30 shrinks in the planar direction in accordance with the stress of the plating film. The larger the amount of shrinkage, the larger the amount of expansion of the solder after the copper is saturated. Finally, on the substrate plating, an electroplated copper is used to form a metal layer 12 of a thickness of 1 μm to 20 -13 to 201028287 μm as a conductor (formation treatment of the upper metal layer). A metal facing laminate 30 is produced. In the above method of fabricating the metal facing laminate 30, after the underlying metal layer 13 is formed, heat treatment is performed to finally form the upper metal layer 12, but even after the underlying metal layer 13 is formed, an upper metal layer is formed. 12, the final implementation of heat treatment is also possible. When the amount of shrinkage is set to be large, it is preferable to perform heat treatment after forming only the underlying metal layer 13. Only the side of the electroless plating film has a large tensile stress. Next, a circuit board and an electronic component to which the present invention is applicable will be described. Fig. 4 is a cross-sectional view showing a circuit board according to an embodiment of the present invention. Here, a circuit board in which a circuit is formed using the metal facing laminate 10 shown in Fig. 1 will be described as an example. As shown in Fig. 4, the circuit board 40 has a film substrate 11 and a circuit metal layer 15 which is laminated on the surface 11a of the film substrate 11 to form an electric circuit. In the method of forming the circuit metal layer 15 of the circuit board 40, the metal of the metal sheath laminate 10 shown in FIG. 1 is removed by etching, for example, by a subtractive method to form a desired wiring pattern. The metal portion of layer 12 is not required to form a circuit metal layer 15 having the desired wiring pattern. Fig. 5 is a cross-sectional view showing an electronic component according to an embodiment of the present invention. Here, an electronic component using the circuit board 40 shown in Fig. 4 will be described as an example. As shown in FIG. 5, the electronic component 50 is coated with a solder resist 17 on the surface of the circuit board 4 on the surface of the circuit board 4 shown in FIG. 4, and the circuit is connected to the circuit board 40 by the bump 18. The metal layer 15 and the electrodes of the semiconductor element 16. By using the metal facing laminate 10' to which the above-described present invention can be applied, thermal deformation due to solder heating at the time of mounting the semiconductor element 16 on the circuit board 40 can be reduced. Therefore, the circuit board 40 and the electronic component 50 having high reliability can be produced. Next, preferred embodiments of the present invention will be described. Here, the measurement result of the dimensional change rate (expansion ratio) in the planar direction of the metal facing laminate of the present invention can be applied to the heat treatment after the copper etching according to the φ, and the use of the metal laminate to which the present invention is applicable An example of the connection reliability of the circuit board and the semiconductor wafer will be described. Bian Mingzi said that the composition of the high-prepared form is 11}, and the material base is thinner than the thin film and the various examples are applied to light the film to make a thin film. The polycondensation is applied to the liquid crystal solution (( Μ φ. Here, in the case of a polymer film (liquid crystal polymer film), the case of VecsterCT manufactured using KURARA) is described. 50 μm thickness. First, the polymer film is immersed in a potassium hydroxide solution at 80 ° C for 15 to 30 minutes to dissolve the surface to form irregularities. Then, according to the modifier treatment, the nickel alloy Each of the treatments of the electroless plating treatment, the heat treatment, and the copper plating treatment is applied to produce a metal sheath laminate 30 (film metal sheath laminate) to which the present invention is applicable. The modifier treatment is performed by OPC- -15- 201028287 3 50 modified by Okuno Pharmaceutical Co., Ltd. The surface of the polymer film is washed by the OPC-80 catalyst of Okuno Pharmaceutical Co., Ltd. as a palladium-containing material. Catalyst imparting liquid, accelerated with OPC-500 As an activator. Nickel alloy electroless ore processing is performed on both sides of the film by nickel-phosphorus plating. For the commercially available nickel-phosphorus plating solution, TOP Nicoron made by Okuno Pharmaceutical Co., Ltd. LPH-LF. The film stress changes the ratio of bath temperature, pH, hypophosphorous acid and metallic nickel to produce a thin film metal facing laminate 30 composed of different base plating films (base metal layer 13) (from the embodiment) 1 to 10 of the embodiment 10). The pH is set to a range of 5.6 to 6.3, and a base plating layer (base metal layer 13) having a thickness of 0.1 μm is formed on both sides. The stress of the plating film (base metal layer 13) is determined only by The single-sided electroplating is performed, and the bending caused by the plating is observed to determine the tensile stress or the compressive stress. Further, when the plating film side is concave after the plating, the tensile stress is judged to be a convex stress. It is judged to be a compressive stress. In the heat treatment, the film metal face laminate is placed in a heat treatment bath, and the heat treatment temperature is maintained at 200 ° C to 250 ° C for 10 minutes. The copper plating treatment is based on the thickness of the conductor (the thickness of the metal layer 12) Copper (metal layer 12) is formed in a manner of 8 micrometers. The copper electro-mineral liquid is used as follows. Further, CU-BRITE TH-RIII manufactured using 荏原优吉莱特(股) is used as an additive. And, in all the examples, A conductor (metal layer 12) is formed on both sides.
硫酸銅 120g/L 硫酸Copper sulfate 120g/L sulfuric acid
150 g/L 201028287 濃鹽酸 0.125mL/L (作爲氯離子) 並且,實施例9、實施例10係於銅電鍍後,在80°C執 行30分鐘之乾燥之後’執行200 °C以上之熱處理。此時之 電鍍皮膜之應力之判定’係觀看僅在單面形成導體之狀態 下的凹凸,判斷爲拉伸應力或壓縮應力。 再者,比較例1至比較例6,使用與賣施例1至實施例 10相同之薄膜基材11,同樣利用鹼溶液使表面粗化。 @ 在比較例1中,無電解電鍍液使用TOP Nicoron LPH- LF。再者,將pH設爲6.9,形成0.1微米厚度之鎳-磷之基 底電鍍層。之後的熱處理係將熱處理溫度設爲160t執行 10分鐘。之後,銅電鍍處理係以導體厚度成爲8微米之方 式形成銅。 在比較例2中,無電解電鍍液使用美國羅門哈斯( Rohm and Haas)公司製作之 OMNI-SHIELD 1 5 80。將 pH 設 爲9,形成0.1微米厚度之鎳-磷之基底電鍍層。之後的熱處 φ 理係將熱處理溫度設爲230°C執行10分鐘。之後,銅電鍍 處理係以導體厚度成爲8微米之方式形成銅。 在比較例3中,無電解電鍍液使用美國羅門哈斯( Rohm and Haas )公司製作之 OMNI-SHIELD 1 580。將 pH 設爲9,形成鎳-磷皮膜0.1微米厚度。之後,在80°C執行30 分鐘之乾燥之後,執行銅電鍍,接著執行熱處理。 比較例4至比較例6中,無電解電鍍液使用奧野製藥工 業(股)製造的TOP Nicoron NAC。將pH設爲4.6,形成 〇.1微米厚度之鎳-磷之基底電鍍層。之後的熱處理係將熱 -17- 201028287 處理溫度在比較例4中設爲240°C,在比較例5中設爲250°C . ,在比較例6中設爲260 °C,分別進行10分鐘。之後,銅電 鍍處理係以導體厚度成爲8微米之方式形成銅。 針對以上述般之條件所製作出之實施例1至實施例1 〇 以及比較例1至比較例6之薄膜金屬護面疊層體,除去導體 之後,藉由下述方法測量由於加熱所產生之平面方向之尺 寸變化率(膨脹率)。 利用與記載於IPC-TM-650 2.2.4之尺寸安定性之測量 @ 方法類似之方法,求出平面方向之變化率。在270mmx 290mm之薄膜金屬護面疊層體之四角形成劃線,製作4個 評估點A、B、C、D,測量AB間、BC間、CD間、DA間之 評估點距離,以當作初期値。 接著,藉由蝕刻除去除評估點區域以外之部分的所有 金屬。鈾刻使用氯化銅。之後,在假設焊料加熱溫度之 24 0°C下執行1分鐘之熱處理。在熱處理中,因高溫槽之熱 風不會對薄膜造成影響,故將薄膜放入金屬製之箱,在無 Θ 負荷狀態下執行熱處理。 於熱處理後,再次測量AB間、BC間、CD間、DA間之 評估點距離,求出自初期値變化量,並將薄膜金屬護面疊 層體之長邊方向、寬方向求出的變化量之平均平面方向之 尺寸變化率(膨脹率)。表1係表示由於銅蝕刻後之熱處 理所產生之平面方向之尺寸變化率(膨脹率)之測量結果 -18- 201028287 【1® 膨脹率 (%) 0.38 0.32 0.29 0.27 0.24 0.19 0.15 0.11 0.09 0.06 0.04 -0.02 r-H o 0.41 0.44 0.48 -R ^ 谶躍 n m |tf w 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 壓縮 壓縮 拉伸 拉伸 拉伸 熱處理溫度 (°C) 250 Ο Ο m <N Ο iri (N Ο (N Ο ΓΛ CN 240 220 240 Ο <N -1 230 230 240 Ο <N 260 處理工程 I_ 鹪 ϋ 1 勁 m & iRn> t 鹪 邀 Hi k 無電解電鏟—熱處理-銅電鍍 鹪 ipr Π57 滴 个 mil 勸 η & iwVn f m 衅 魃 壊 鹪 iDinfl ipr Π57 滴 个 tnu 勸 η 感 tRn> 个 m ίρΙΓ 駛 m 無電解電鍍—熱處理—銅電鍍 無電解電鍍^熱處理—銅電鍍 無電解電鍍熱處理θ銅電鍍 無電解電鍍—熱處理·—銅電鍍 mil 脚 魆 个 m Πο7 滴 t 鹪 m 駛 璀 無電解電鍍-銅電鍍-熱處理 無電解電鑛-熱處理-銅電鍍 鹪 iUmfl ipr 丄 ffin m m t 鹪 _ 邀 璀 mil w m 靈 TWK 个 鹪 顆 个 m m 駿 緘 摧 無電解電鍍—熱處理銅電鍍 無電解電鍍—熱處理—銅電鍍 無電解電鍍—熱處理-銅電鑛 in <5 ο in m v〇 \ό vo Ο 0\ ^0 m m vd Os VO OS Os VO rj- 寸’ I 無電解電鍍液 ! TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF OMNI-SHIELD1580 OMNI-SHIELD 1580 TOP Nicoron NAC TOP Nicoron NAC TOP Nicoron NAC 實施例1 實施例2 實施例3 實施例4 實施例5 實施例6 實施例7 實施例8 實施例9 實施例10 比較例1 比較例2 比較例3 比較例4 比較例5 比較例6 -19- 201028287 如表1所示般,實施例1至實施例10之平面方向之尺寸 . 變化率(膨漲率15)爲0.06〜0.38%。再者,比較例1至比 較例3之平面方向之尺寸變化率(膨脹率)爲-0.1〜0.04% 。再者,比較例4至比較例6之平面方向之尺寸變化率(膨 脹率)爲0.41〜0.48%。 接著,因試驗與半導體晶片之基板的連接信賴性,故 製作COF基板,執行溫度循環試驗。 製作藉由蝕刻除去金屬之電路基板,使用倒裝晶片接 @ 合器而連接於TEG晶片製作出電子零件。在此,使用在實 施例1至實施例10及比較例1至比較例6所製作之兩面基板 之薄膜金靥護面叠層體而製作出單面圖案。就以TEG晶片 而言,由日立超LSI系統使用JTEG Phase6_50,製作出適 合於此之配線基板。並且,JTEG Phase6_50之規格如下述 〇 晶片尺寸:16mmxl5.lmmxl5.lmm150 g/L 201028287 Concentrated hydrochloric acid 0.125 mL/L (as chloride ion) Further, Example 9 and Example 10 were subjected to copper plating and then dried at 80 ° C for 30 minutes, and then heat treatment at 200 ° C or higher was performed. At this time, the determination of the stress of the plating film was as follows. The unevenness in the state in which the conductor was formed only on one side was observed, and the tensile stress or the compressive stress was judged. Further, in Comparative Example 1 to Comparative Example 6, the same film substrate 11 as that of Example 1 to Example 10 was used, and the surface was also roughened by an alkali solution. @ In Comparative Example 1, the electroless plating solution used TOP Nicoron LPH-LF. Further, the pH was set to 6.9 to form a nickel-phosphorus base plating layer having a thickness of 0.1 μm. The subsequent heat treatment was performed by setting the heat treatment temperature to 160 t for 10 minutes. Thereafter, the copper plating treatment formed copper in such a manner that the conductor thickness became 8 μm. In Comparative Example 2, the electroless plating solution used OMNI-SHIELD 1 5 80 manufactured by Rohm and Haas Company of the United States. The pH was set to 9 to form a nickel-phosphorus base plating layer having a thickness of 0.1 μm. The subsequent heat φ system was performed by setting the heat treatment temperature to 230 ° C for 10 minutes. Thereafter, copper plating was performed to form copper so that the conductor thickness became 8 μm. In Comparative Example 3, the electroless plating solution was OMNI-SHIELD 1 580 manufactured by Rohm and Haas. The pH was set to 9 to form a nickel-phosphorus film having a thickness of 0.1 μm. Thereafter, after performing drying at 80 ° C for 30 minutes, copper plating was performed, followed by heat treatment. In Comparative Example 4 to Comparative Example 6, the electroless plating solution was TOP Nicoron NAC manufactured by Okuno Pharmaceutical Co., Ltd. The pH was set to 4.6 to form a nickel-phosphorus base plating layer having a thickness of 1 μm. In the subsequent heat treatment, the heat treatment temperature of -17-201028287 was 240 ° C in Comparative Example 4, 250 ° C in Comparative Example 5, and 260 ° C in Comparative Example 6, and 10 minutes each. . Thereafter, the copper plating treatment was performed to form copper so that the conductor thickness became 8 μm. With respect to the film metal sheath laminates of Examples 1 to 1 and Comparative Examples 1 to 6 produced under the above-described conditions, after the conductors were removed, the heat generation was measured by the following method. The dimensional change rate (expansion ratio) in the plane direction. The rate of change in the plane direction was obtained by a method similar to the measurement of the dimensional stability described in IPC-TM-650 2.2.4. A scribe line is formed at the four corners of the 270 mm x 290 mm film metal facing laminate, and four evaluation points A, B, C, and D are prepared, and the evaluation point distance between AB, BC, CD, and DA is measured to be regarded as Initially. Next, all the metals in the portion other than the evaluation point region are removed by etching. Chloride is used for uranium engraving. Thereafter, heat treatment was performed for 1 minute under the assumption that the solder heating temperature was 240 °C. In the heat treatment, since the hot air of the high temperature bath does not affect the film, the film is placed in a metal box and heat treatment is performed under no load. After the heat treatment, the distance between the evaluation points of AB, BC, CD, and DA was measured again, and the change from the initial enthalpy was determined, and the change in the longitudinal direction and the width direction of the film metal sheath laminate was determined. The dimensional change rate (expansion ratio) of the average plane direction of the quantity. Table 1 shows the measurement results of the dimensional change rate (expansion ratio) in the plane direction due to the heat treatment after copper etching. -18- 201028287 [1® Expansion ratio (%) 0.38 0.32 0.29 0.27 0.24 0.19 0.15 0.11 0.09 0.06 0.04 - 0.02 rH o 0.41 0.44 0.48 -R ^ nm 纳米 | tf w Tensile tensile stretching Tensile tensile stretching Tensile tensile stretching Compression Tensile stretching Tensile heat treatment temperature (°C 250 Ο Ο m <N Ο iri (N Ο (N Ο ΓΛ CN 240 220 240 Ο <N -1 230 230 240 Ο <N 260 Process Engineering I_ 鹪ϋ 1 劲力 m &iRn> t 鹪 invite Hi k electroless shovel - heat treatment - copper plating 鹪 ipr Π 57 drops mil persuasion η & iwVn fm 衅魃壊鹪iDinfl ipr Π57 drops a tnu persuade η sense tRn> m ίρΙΓ drive m electroless plating - heat treatment - copper Electroplating electroless plating ^ heat treatment - copper electroplating electroless plating heat treatment θ copper electroplating electroless plating - heat treatment · copper electroplating mil ankle m m Πο7 t t 鹪m 璀 璀 electroless plating - copper plating - heat treatment electroless mine - Heat treatment - copper plating 鹪iUm Fl ipr 丄ffin mmt 鹪_ Invitation mil wm 灵 TWK 鹪 mm mm 缄 缄 无 无 无 无 热处理 热处理 热处理 热处理 热处理 热处理 热处理 热处理 热处理 热处理 热处理 热处理 热处理 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无 无In mv〇\ό vo Ο 0\ ^0 mm vd Os VO OS Os VO rj- inch ' I electroless plating solution! TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF OMNI-SHIELD1580 OMNI-SHIELD 1580 TOP Nicoron NAC TOP Nicoron NAC TOP Nicoron NAC Implementation Example 1 Example 2 Example 3 Example 4 Example 5 Example 6 Example 7 Example 8 Example 9 Example 10 Comparative Example 1 Comparative Example 2 Comparative Example 3 Comparative Example 4 Comparative Example 5 Comparative Example 6 -19- 201028287 As shown in Table 1, the dimensions of the plane directions of Examples 1 to 10 are changed by a rate of expansion (expansion ratio 15) of 0.06 to 0.38%. Further, the dimensional change ratio (expansion ratio) in the plane direction of Comparative Example 1 to Comparative Example 3 was -0.1 to 0.04%. Further, the dimensional change ratio (expansion ratio) in the plane direction of Comparative Example 4 to Comparative Example 6 was 0.41 to 0.48%. Next, since the connection reliability with the substrate of the semiconductor wafer was tested, a COF substrate was produced and a temperature cycle test was performed. A circuit board on which metal was removed by etching was produced, and an electronic component was produced by connecting to a TEG wafer using a flip chip bonding apparatus. Here, a single-sided pattern was produced by using the film-metal enamel laminate of the double-sided substrates produced in Examples 1 to 10 and Comparative Examples 1 to 6. In the case of the TEG wafer, the Hitachi ultra-LSI system uses JTEG Phase 6_50 to fabricate a wiring board suitable for this. Moreover, the specifications of JTEG Phase6_50 are as follows: 晶片 Wafer size: 16mmxl5.lmmxl5.lmm
焊墊間距:50微米 H 焊墊數:479焊墊 凸塊尺寸:30微米xlOO微米 凸塊:金電鍍 高度10微米 爲了製作電路基板,藉由扣除法蝕刻薄膜護面疊層體 之後,藉由置換電鍍使Sn電鍍在銅表面析出0.5微米厚度 。之後,塗佈防焊劑而製作出電路基板。 電路基板和晶片之連接係利用倒裝晶片接合器執行晶 片之凸塊和電路基板之定位,並加熱至Sn之溶解溫度以上 -20- 201028287 而執行晶片和電路基板之接合。 執行溫度循環試驗,以作爲信賴性試驗。作爲溫度循 環試驗條件,重複在-55°C保持10分鐘之後,升溫至125°C 而保持10分鐘期間,又降溫至-55 °C。作爲連接電阻係每 1 〇〇循環測量晶片和電路基板之連接電阻,當從初期電阻 增加2 0 %之時,則視爲破斷。表2及第6圖表示至藉由溫度 循環試驗測量到破斷爲止循環數。Pad spacing: 50 microns H Number of pads: 479 pad bump size: 30 micron x lOO micron bumps: gold plating height 10 microns in order to make the circuit substrate, after subtracting the film protective layer laminate, by subtracting the method Displacement plating causes Sn plating to deposit a thickness of 0.5 microns on the copper surface. Thereafter, a solder resist is applied to form a circuit board. The connection between the circuit substrate and the wafer is performed by using a flip chip bonder to perform positioning of the bumps of the wafer and the circuit substrate, and heating to a temperature above the dissolution temperature of Sn -20-201028287 to perform bonding of the wafer and the circuit substrate. A temperature cycle test was performed as a reliability test. As a temperature cycling test condition, after repeating at -55 ° C for 10 minutes, the temperature was raised to 125 ° C for 10 minutes while the temperature was lowered to -55 ° C. The connection resistance of the wafer and the circuit board was measured every 1 〇〇 cycle as a connection resistance, and it was considered to be broken when the initial resistance was increased by 20%. Tables 2 and 6 show the number of cycles until the break was measured by the temperature cycle test.
m -21 - 201028287m -21 - 201028287
【CNS 循環數 (次) 1100 1900 2400 2600 2900 2800 2500 2100 1700 1100 900 600 400 800 650 450 膨脹率 (%) 0-38 0.32 0.29 0.27 0.24 0.19 0.15 0.11 0.09 0.06 0.04 -0.02 η 〇 0.41 0.44 0.48 鹅糴 •N H 鲣辉 鹪闼 li w 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 1 拉伸 拉伸 拉伸 壓縮 壓縮 拉伸 t: 拉伸 熱處理溫度 CC) 250 1_ ... 240 230 250 〇 230 240 220 240 200 230 230 240 Ο <Ν 260 處理工程 無電解電鍍—熱處理一銅電鍍 m _ Πρ7 箱 t mil ffil m 个 m 峨 毖 Μ ΙρΙΓ m 鹪 个 mi \ 脚 m 个 鹪 ϋ 毖 細 ipr m 無電解電鍍—熱處理一銅電鍍 m ΤΤΞΡ 徳 个 mil ffil 癒 个 m 邀 Iff m 無電解電鍍—熱處理—銅電鎪 鹪 |i Πρ7 箱 t tTTt 1 脚 艘 个 鹪 毖 ipr m 無電解電鍍-> 熱處理—銅電鍍 無電解電鑛—銅電鍍—熱處理 無電解電鍍-> 銅電鏟—熱處理 無電解電鎞-> 熱處理—銅電鍍 無電解電鍍一熱處理—銅電鍍 mi 1 W η 1RH、 t 鹪 iliiml Ιρ!Γ 个 鹪 衅 _ 壊 無電解電鏟—熱處理—銅電鍍 m 顆 个 will 棚 m 癒 t 鸛 壊 無電解電鑛—熱處理—銅電鍍 \〇 νο in ΓΟ ^0 cn cn OS Os VO VO ^0 〇\ — 寸· 無電解電鍍液 TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF OMNI-SHIELD 15 80 OMNI-SHIELD1580 TOP Nicoron NAC TOP Nicoron NAC TOP Nicoron NAC 實施例1 實施例2 實施例3 實施例4 實施例5 實施例6 實施例7 實施例8 實施例9 實施例10 比較例1 比較例2 比較例3 比較例4 比較例5 比較例6 -22- 201028287 如表2及第6圖所示般,可知於銅電鍍之後’在進行1 分鐘加熱溫度爲240 °C之加熱處理之後的平面方向之尺寸 變化率(膨脹率)爲〇.〇5 %〜0.4 %之實施例1至實施例1〇中 ,至破斷爲止之循環數大。即是,可知在進行1分鐘加熱 溫度爲240 °C之加熱處理之後的平面方向之尺寸變化率( 膨脹率)爲0.05 %〜0.4 %之實施例1至實施例10中,表示高 連接信賴性。再者,可知在進行1分鐘加熱溫度爲240 °C之 Φ 加熱處理之後的平面方向之尺寸變化率(膨脹率)爲0·1 % 〜0.3%之實施例3至實施例8中,表示更高連接信賴性。 另外,可知於執行1分鐘加熱溫度240 °C之加熱處理之 後的平面方向之尺寸變化率(膨脹率)小於0.05%之比較 例1至比較例3,以及於執行1分鐘加熱溫度240°C之加熱處 理之後的平面方向之尺寸變化率(膨脹率)大於0.4%之比 較例4至比較例6中,顯示出至破斷爲止之循環數變小,連 接信賴性低。 φ 接著,針對使用PEEK、熱可塑性聚醯亞胺、PET、 PEN、非熱可塑性聚醯亞胺,當作其他薄膜基材之情形予 以說明。 (PEEK之實施例以及比較例) 針對使用PEEK當作薄膜基材之情形予以說明。在此 ,針對使用_三菱樹脂(股)製作之IBUKI當作PEEK之情形 予以說明。並且,薄膜厚度使用50微米厚度。 首先,將PEEK浸泡在80°C之1〇規度(Normal)之氫 -23- 201028287 氧化鉀溶液15至30分鐘,溶解表面形成凹凸。接著’依照 改質劑處理、鎳合金之無電解電鍍處理、熱處理、銅之電 鍍處理之順序施予各處理,製造出薄膜金屬護面疊層體。 利用表3所示之電鏟液,形成0.1微米厚度之基底電鍍 層,利用表3所示之熱處理溫度,執行1 〇分鐘間之熱處理 〇 銅電鍍處理係以導體厚度成爲8微米之方式形成銅。 並且,在所有實施例中,於兩面形成導體。 @ 針對以上述般之條件所製作出之實施例1 1至實施例20 以及比較例7至比較例12之薄膜金屬護面叠層體,與高分 子薄膜(液晶聚合物薄膜)之情形相同,測量除去導體之 後由於加熱所產生之平面方向之尺寸變化率(膨脹率)。 再者,因試驗與半導體晶片之基板的連接信賴性,故製作 COF基板,執行溫度循環試驗。第3圖及第7圖表示藉由依 膨破 ^ 之 率量 化測 變所 寸而 尺驗 之試 向環 方循 面度 平溫 之由。 生藉果 產至結 所及量 理以測 處果之 熱結數 之量環 後測循 刻之之 餓 } 止 銅率爲 據脹斷 -24- 201028287[CNS cycle number (times) 1100 1900 2400 2600 2900 2800 2500 2100 1700 1100 900 600 400 800 650 450 Expansion rate (%) 0-38 0.32 0.29 0.27 0.24 0.19 0.15 0.11 0.09 0.06 0.04 -0.02 η 〇0.41 0.44 0.48 Goose • NH 鲣 鹪闼 w li w Tensile tensile stretching Tensile stretching stretching stretching stretching stretching compression stretching stretching t: stretching heat treatment temperature CC) 250 1_ ... 240 230 250 〇 230 240 220 240 200 230 230 240 Ο <Ν 260 treatment engineering electroless plating - heat treatment a copper plating m _ Πρ7 box t mil ffil m m 峨毖Μ ΙρΙΓ m 鹪 a mi \ foot m 鹪ϋ 毖 fine ipr m Electroless plating - heat treatment - copper plating m ΤΤΞΡ mil mil ffil more m invites Iff m electroless plating - heat treatment - copper electric 锼鹪 | i Π ρ7 box t tTTt 1 foot 鹪毖 鹪毖 ipr m electroless plating -> Heat treatment - copper electroplating electroless electrowinning - copper electroplating - heat treatment electroless plating - > copper electric shovel - heat treatment electroless electrolysis -> heat treatment - copper electroplating electroless plating - heat treatment - copper plating mi 1 W η 1RH, t 鹪ilii Ml Ιρ!Γ 鹪衅 壊 壊 壊 电解 — — 热处理 热处理 热处理 热处理 热处理 热处理 热处理 热处理 OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS OS ^0 〇\ — Inch · Electroless plating solution TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH- LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF TOP Nicoron LPH-LF OMNI-SHIELD 15 80 OMNI-SHIELD1580 TOP Nicoron NAC TOP Nicoron NAC TOP Nicoron NAC Example 1 Example 2 Example 3 Example 4 Example 5 Example 6 Example 7 Example 8 Example 9 Example 10 Comparative Example 1 Comparative Example 2 Comparative Example 3 Comparative Example 4 Comparative Example 5 Comparative Example 6 -22- 201028287 As shown in Table 2 and Figure 6, it is known that copper plating Then, in the example 1 to the first embodiment, the dimensional change rate (expansion ratio) in the plane direction after the heat treatment at a heating temperature of 240 ° C for 1 minute was 〇 〇 5% to 0.4%, to break The number of cycles until then is large. In other words, in Example 1 to Example 10 in which the dimensional change ratio (expansion ratio) in the planar direction after the heating treatment at a heating temperature of 240 ° C for 1 minute was 0.05% to 0.4%, it was found that high connection reliability was exhibited in Examples 1 to 10. . In addition, in Example 3 to Example 8, in which the dimensional change ratio (expansion ratio) in the plane direction after the Φ heat treatment at a heating temperature of 240 ° C for 1 minute was 0. 1% to 0.3%, it was found that High connection reliability. Further, it is understood that Comparative Example 1 to Comparative Example 3 in which the dimensional change ratio (expansion ratio) in the planar direction after the heat treatment at a heating temperature of 240 ° C for 1 minute was less than 0.05%, and the heating temperature of 240 ° C was performed for 1 minute. In Comparative Example 4 to Comparative Example 6 in which the dimensional change rate (expansion ratio) in the planar direction after the heat treatment was more than 0.4%, the number of cycles until the breakage was small, and the connection reliability was low. φ Next, the case of using PEEK, thermoplastic polyimine, PET, PEN, and non-thermoplastic polyimine as other film substrates will be described. (Examples and Comparative Examples of PEEK) A case where PEEK is used as a film substrate will be described. Here, the case where IBUKI made using Mitsubishi Resin Co., Ltd. is used as PEEK will be described. Also, the film thickness was 50 μm thick. First, the PEEK is immersed in a hydrogen -23-201028287 of a normal temperature of 80 ° C for 15 to 30 minutes to form a concave and convex surface. Then, each treatment was carried out in the order of the modifier treatment, the electroless plating treatment of the nickel alloy, the heat treatment, and the electroplating treatment of copper to produce a film metal sheath laminate. Using the electric shovel liquid shown in Table 3, a base plating layer having a thickness of 0.1 μm was formed, and heat treatment was performed for 1 〇 minutes using the heat treatment temperature shown in Table 3, and copper plating treatment was performed to form copper in such a manner that the conductor thickness became 8 μm. . Also, in all embodiments, the conductors are formed on both sides. The film metal sheath laminates of Examples 11 to 20 and Comparative Examples 7 to 12 produced under the above-described conditions were the same as those of the polymer film (liquid crystal polymer film). The dimensional change rate (expansion ratio) in the plane direction due to heating after the conductor was removed was measured. Further, since the test was reliable in connection with the substrate of the semiconductor wafer, a COF substrate was produced and a temperature cycle test was performed. Fig. 3 and Fig. 7 show the reason why the test is to measure the flatness of the ring by the rate of the expansion. Borrowing fruit to the end of the knot and measuring to measure the number of hot knots of the fruit ring after the test of the hungry } stop copper rate according to the expansion -24- 201028287
循環數 (次) 〇 in o 卜 o 2100 2200 2300 2000 Ο α\ 〇 卜 Ο Ό Ο m o Ο Ο <Ν ^Η ο 冢 ο ο 膨脹率 (%) 卜 〇 o as CN 〇 (N c5 1-H (N 〇 in o Ο Ο o Ο s o o o -0.02 寸 Ο JO ο ο § m N m 鲣s m 0 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸! 拉伸 壓縮 拉伸 拉伸 拉伸 熱處理溫度 ΓΟ , o o o (N o (N CS ο ο CN 1-Η § ο ^-Η s Ο (Ν ο <Ν ο ο (Ν 處理工程 个鹪 1 m iliiml Ipr a ^ 1 ιΐιιπτί TO 1 η 黑舔 1Rrt、 m 'Ο σ\ — 無電解電鍍液 TOPNicoronLPH-LF I _I OMNI-SHIELD 1580 I TOPNicoronNAC 廠商名 三菱樹脂 三菱樹脂 三菱樹脂 三菱樹脂 三菱樹脂 三菱樹脂 三菱樹脂 三菱樹脂 三菱樹脂 三菱樹脂 三菱樹脂 三菱樹脂 三菱樹脂 三菱樹脂 三菱樹脂 三菱樹脂 1 產品名 IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI 11 PEEK PEEK ω ω CU ω Pi u PQ ω CU m ω pu ω Cu w ω CU ω ω CU Ph W w pu ω ω Pn Dh ω ω ω w pu 〇Η 實施例11 實施例12 實施例13 實施例M 實施例15 實施例16 實施例Π 實施例18 實施例19 實施例20 比較例7 比較例8 比較例9 比較例10 比較例Π 比較例12 -25- 201028287 如表3及第7圖所示般,可知於銅電鍍之後,在進行1 分鐘加熱溫度爲240 °C之加熱處理之後的平面方向之尺寸 變化率(膨脹率)爲0.05%〜0.4%之實施例11至實施例20 中,至破斷爲止之循環數大。即是,可知在進行1分鐘加 熱溫度爲240 °C之加熱處理之後的平面方向之尺寸變化率 (膨脹率)爲0.05 %〜0.4%之實施例11至實施例20中,表 示高連接信賴性。 另外,可知於執行1分鐘加熱溫度240 t之加熱處理之 後的平面方向之尺寸變化率(膨脹率)小於0.05%之比較 例7至比較例9,以及於執行1分鐘加熱溫度240°C之加熱處 理之後的平面方向之尺寸變化率(膨脹率)大於0.4%之比 較例10至比較例12中,顯示出至破斷爲止之循環數變小, 連接信賴性低。 (PET、PEN之實施例以及比較例)Number of cycles (times) 〇in o 卜o 2100 2200 2300 2000 Ο α\ 〇 Ο Ό Ο Ο mo Ο Ο <Ν ^Η ο 冢ο ο Expansion rate (%) 〇 〇 as as CN 〇 (N c5 1- H (N 〇in o Ο Ο o Ο sooo -0.02 inch Ο JO ο ο § m N m 鲣sm 0 Tensile tensile stretching stretching stretching stretching stretching stretching stretching stretching tensile drawing Stretching and stretching heat treatment temperature ΓΟ , ooo (N o (N CS ο ο CN 1-Η § ο ^-Η s Ο (Ν ο < Ν ο ο (Ν processing project 鹪 1 m iliiml Ipr a ^ 1 ΐ ΐιιπτί TO 1 η 黑舔1Rrt, m 'Ο σ\ — Electroless plating solution TOPNicoronLPH-LF I _I OMNI-SHIELD 1580 I TOPNicoronNAC Manufacturer name Mitsubishi resin Mitsubishi resin Mitsubishi resin Mitsubishi resin Mitsubishi resin Mitsubishi resin Mitsubishi resin Mitsubishi resin Mitsubishi resin Mitsubishi Resin Mitsubishi resin Mitsubishi resin Mitsubishi resin Mitsubishi resin Mitsubishi resin Mitsubishi resin 1 Product name IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI IBUKI 11 PEEK PEEK ω ω CU ω Pi u PQ ω CU m ω pu ω Cu w ω CU ω ω CU Ph W w pu ω ω ω Pn Dh ω ω ω w pu 实施 Example 11 Example 12 Example 13 Example M Example 15 Example 16 Example 实施 Example 18 Example 19 Example 20 Comparative Example 7 Comparative Example 8 Comparative Example 9 Comparative Example 10 Comparative Example Π Comparative Example 12 -25- 201028287 As shown in Tables 3 and 7, it is understood that after the copper plating, the surface after the heat treatment at a heating temperature of 240 ° C for 1 minute is known. In the eleventh embodiment to the twenty-second embodiment, the dimensional change rate (expansion ratio) of the direction was 0.05% to 0.4%, and the number of cycles until the breakage was large. That is, it was found that heating at a heating temperature of 240 ° C for 1 minute was performed. In the embodiment 11 to the embodiment 20 in which the dimensional change rate (expansion ratio) in the planar direction after the treatment is 0.05% to 0.4%, the high connection reliability is shown. Further, it is understood that after the heat treatment of the heating temperature of 240 t for 1 minute is performed Comparative Example 7 to Comparative Example 9 in which the dimensional change rate (expansion ratio) in the planar direction was less than 0.05%, and the dimensional change ratio (expansion ratio) in the planar direction after the heat treatment at the heating temperature of 240 ° C for 1 minute was performed was more than 0.4. % comparison example 10 to comparison In Example 12, it was shown that the number of cycles until the breakage was small, and the connection reliability was low. (Examples of PET and PEN and comparative examples)
針對使用PET、PEN當作薄膜基材之情形予以說明。 H 在此,針對使用帝人杜邦薄膜(股)製作之Tetoron HSL 當作PET之情形予以說明。並且,薄膜厚度使用50微米厚 度。在此,針對使用帝人杜邦薄膜(股)製作之Te〇nex Q83當作PEN之情形予以說明。並且,薄膜厚度使用50微 米厚度。 首先,執行噴砂處理以作爲薄膜之粗化’施予砂墊層 加工,在薄膜表面形成凹凸。接著’依照改質劑處理、鎳 合金之無電解電鍍處理、熱處理、銅之電鍍處理之順序施 -26- 201028287 予各處理,製造出薄膜金屬護面疊層體。 利用表4所示之電鍍液,形成0.1微米厚度之基底電鍍 層,利用表4所示之熱處理溫度,執行10分鐘間之熱處理 〇 銅電鍍處理係以導體厚度成爲8微米之方式形成銅。 並且,在所有實施例中,於兩面形成導體。 針對以上述般之條件所製作出之實施例2 1至實施例30 φ 以及比較例13至比較例18之薄膜金屬護面疊層體,與高分 子薄膜(液晶聚合物薄膜)之情形相同,測量除去導體之 後由於加熱所產生之平面方向之尺寸變化率(膨脹率)。 再者,因試驗與半導體晶片之基板的連接信賴性,故製作 C OF基板.執行溫度循環試驗。 在此,因PET、PEN耐熱性低,故平面方向之尺寸變 化率(膨脹率)之測量中除去導體之後的加熱,於PET之 時在170°C執行1分鐘熱處理,於PEN之時在20(TC執行1分 ❹ 鐘加熱處理。再者,PET、PEN薄膜因耐熱性低,故執行 Sn電鑛和Bi電鍍I。再者,與晶片之接觸係利用大約150°C 之加熱而加以實施。 第4圖及第8圖表示藉由依據銅蝕刻後之熱處理所產生 之平面方向之尺寸變化率(膨脹率)之測量結果以及至藉 由溫度循環試驗而所測量之破斷爲止之循環數之測量結果 -27- 201028287The case where PET and PEN are used as a film substrate will be described. H Here, the case of using Tetoron HSL made by Teijin DuPont Film Co., Ltd. as PET is explained. Also, the film thickness was 50 μm thick. Here, the case where Te〇nex Q83 manufactured using Teijin DuPont Film Co., Ltd. is used as PEN will be described. Also, the film thickness was 50 μm thick. First, sand blasting is performed to apply a sanding layer as a roughening of the film to form irregularities on the surface of the film. Then, in accordance with the procedures of the modifier treatment, the electroless plating treatment of the nickel alloy, the heat treatment, and the copper plating treatment, each of the treatments was carried out to produce a film metal sheath laminate. Using the plating solution shown in Table 4, a base plating layer having a thickness of 0.1 μm was formed, and heat treatment was performed for 10 minutes by the heat treatment temperature shown in Table 4. The copper plating treatment was performed to form copper so that the conductor thickness became 8 μm. Also, in all embodiments, the conductors are formed on both sides. The film metal sheath laminates of Example 21 to Example 30 φ and Comparative Examples 13 to 18 produced under the above-described conditions were the same as those of the polymer film (liquid crystal polymer film). The dimensional change rate (expansion ratio) in the plane direction due to heating after the conductor was removed was measured. Furthermore, since the test was connected to the substrate of the semiconductor wafer, the COF substrate was fabricated and the temperature cycle test was performed. Here, since PET and PEN have low heat resistance, the heating after the conductor is removed in the measurement of the dimensional change rate (expansion ratio) in the planar direction is performed at 170 ° C for 1 minute at the time of PET, and at 20 minutes at PEN. (TC performs 1 minute of enthalpy heat treatment. Further, since PET and PEN films have low heat resistance, Sn electric ore and Bi plating I are executed. Further, contact with the wafer is performed by heating at about 150 °C. Fig. 4 and Fig. 8 show the measurement results of the dimensional change rate (expansion ratio) in the plane direction by the heat treatment after copper etching and the number of cycles up to the measurement by the temperature cycle test. Measurement results -27- 201028287
-28- 201028287 如表4及第8圖所示般,可知於銅電鍍之後,在進行1 分鐘加熱溫度爲170 r或200 °C之加熱處理之後的平面方向 之尺寸變化率(膨脹率)爲0.05%〜0.4%之實施例21至實 施例30中’至破斷爲止之循環數大。即是,可知在進行1 分鐘加熱溫度爲170 °C或200 °C之加熱處理之後的平面方向 之尺寸變化率(膨脹率)爲0.05 %〜0.4%之實施例21至實 施例30中,表示高連接信賴性。 另外’可知於執行1分鐘加熱溫度17(TC之加熱處理之 後的平面方向之尺寸變化率(膨脹率)小於0.05%之比較 例1 3至比較例1 5,以及於執行1分鐘加熱溫度200 °C之加熱 處理之後的平面方向之尺寸變化率(膨脹率)大於0.4%之 比較例16至比較例18中,顯示出至破斷爲止之循環數變小 ,連接信賴性低。 (熱可塑性聚醯亞胺之實施例及比較例) φ 針對使用熱可塑性聚醯亞胺當作薄膜基材之情形予以 說明。在此’針對使用三井化學當作熱可塑性聚醯亞胺之 情形予以說明。並且,薄膜厚度使用25微米厚度。 首先,將熱可塑性聚醯亞胺浸泡在80 °C之10規度( Normal )之氫氧化鉀溶液5至15分鐘,溶解表面形成凹凸 。接著,依照改質劑處理、鎳合金之無電解電鍍處理、熱 處理、銅之電鍍處理之順序施予各處理,製造出薄膜金屬 護面疊層體。 利用表5所示之電鍍液,形成0.1微米厚度之基底電鍍 -29- 201028287 層,利用表5所示之熱處理溫度,執行10分鐘間之熱處理 〇 銅電鍍處理係以導體厚度成爲8微米之方式形成銅。 並且,在所有實施例中,於兩面形成導體。 針對以上述般之條件所製作出之實施例31至實施例40 以及比較例19至比較例24之薄膜金屬護面疊層體,與高分 子薄膜(液晶聚合物薄膜)之情形相同,測量除去導體之 後由於加熱所產生之平面方向之尺寸變化率(膨脹率)。 @ 再者,因試驗與半導體晶片之基板的連接信賴性,故製作 COF基板’執行溫度循環試驗。第5圖及第9圖表示藉由依 據銅蝕刻後之熱處理所產生之平面方向之尺寸變化率(膨 脹率)之測量結果以及至藉由溫度循環試驗而所測量之破 斷爲止之循環數之測量結果。 S1 -30 - 201028287 e❿ r—1¾ 循環數 (次) 900 1000 1- 1200 1300 1 | 1400 1300 1200 1000 00 870 700 600 Ο 700 600 400 膨脹率 (%) 0.39 0.36 1- 0.33 1 1 0.28 1 1 0.25 0.20 0.15 0.11 0.08 0.06 0.43 0.48 0.50 0.02 -0.02 -0.08 埤躍 •N m m 〇 珉运 m g ϋ 丨拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 紧 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 拉伸 壓縮 壓縮 丨熱處理溫度 rc) 〇 290 (N 270 260 300 (N 280 〇 260 320 Ο cn cn 〇 〇 <N 280 處理工程 I_ I- 無電解電鍍 熱處理 —銅電鍍 無電解電鍍 -銅電鍍 —熱處理 無電解電鍍 —熱處理 —銅電鑛 無電解電鍍 —熱處理 —銅電鑛 m 'Ο I 無電解電鍍液 TOP Nicoron LPH-LF TOP Nicoron LPH-LF OMNI-SHIELD1580 1 廠商名 三井化學 1三井化學 丨三井化學 三井化學 三井化學 三井化學 三井化學 三井化學 三井化學 三井化學 三井化學 三井化學 三井化學 三井化學 三井化學 三井化學 產品名 I 丨 AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM 薄膜基材 ] 熱可塑PI 熱可塑PI 熱可塑PI 熱可塑PI 熱可塑PI 熱可塑pi 熱可塑PI 熱可塑PI 熱可塑PI 熱可塑PI 熱可塑PI 熱可塑PI 熱可塑PI 熱可塑pi 熱可塑PI 熱可塑PI 實施例31 實施例32 實施例33 實施例34 實施例35 實施例36 實施例37 實施例38 實施例39 實施例40 比較例19 比較例20 比較例21 比較例22 比較例23 比較例24 -31 - 201028287 如表5及第9圖所示般,可知於銅電鍍之後’在進行1 - 分鐘加熱溫度爲240 °C之加熱處理之後的平面方向之尺寸 變化率(膨脹率)爲0.05%〜0.4%之實施例31至實施例40 中,至破斷爲止之循環數大。即是,可知在進行1分鐘加 熱溫度爲24(TC之加熱處理之後的平面方向之尺寸變化率 (膨脹率)爲0.05%〜0.4%之實施例31至實施例40中’表 示高連接信賴性。 另外,可知於執行1分鐘加熱溫度240°C之加熱處理之 @ 後的平面方向之尺寸變化率(膨脹率)小於〇 . 〇 5 %之比較 例22至比較例24,以及於執行1分鐘加熱溫度240 °c之加熱 處理之後的平面方向之尺寸變化率(膨脹率)大於0.4 %之 比較例19至比較例21中,顯示出至破斷爲止之循環數變小 ,連接信賴性低。 (非熱可塑性聚醯亞胺之實施例及比較例) 針對使用非熱可塑性聚醯亞胺當作薄膜基材之情形予 © 以說明。在此,針對使用東麗、杜邦(股)製作之Kapton 1 00ΕΝ當作非熱可塑性聚醯亞胺之情形予以說明。 首先,將非熱可塑性聚醯亞胺浸泡在80°C之1〇規度(-28- 201028287 As shown in Tables 4 and 8, it is known that the dimensional change ratio (expansion ratio) in the plane direction after the copper plating is performed at a heating temperature of 170 r or 200 ° C for 1 minute is From 0.05% to 0.4% of Examples 21 to 30, the number of cycles until breaking was large. In other words, in Example 21 to Example 30, in which the dimensional change ratio (expansion ratio) in the plane direction after the heat treatment at 170 ° C or 200 ° C for 1 minute was performed was 0.05% to 0.4%, High connection reliability. In addition, it is known that the heating temperature 17 (the dimensional change rate (expansion ratio) in the plane direction after the heat treatment of TC is less than 0.05%, Comparative Example 1 3 to Comparative Example 15 is performed, and the heating temperature of 200 ° is performed for 1 minute). In Comparative Example 16 to Comparative Example 18 in which the dimensional change rate (expansion ratio) in the planar direction after the heat treatment of C was more than 0.4%, the number of cycles until the breakage was small, and the connection reliability was low. Examples and comparative examples of quinone imine) φ is described for the case where a thermoplastic polyimide is used as a film substrate. Here, the case of using Mitsui Chemical as a thermoplastic polyimide is described. The thickness of the film is 25 μm. First, the thermoplastic polyimide is immersed in a potassium hydroxide solution at 10 ° C for 10 to 15 minutes at 80 ° C to dissolve the surface to form irregularities. Then, according to the modifier The treatment, the electroless plating treatment of the nickel alloy, the heat treatment, and the copper plating treatment were sequentially applied to each other to produce a thin film metal sheath laminate. Using the plating solution shown in Table 5, a 0. 1 micron thick substrate plating -29- 201028287 layer, using the heat treatment temperature shown in Table 5, performing heat treatment for 10 minutes, copper plating treatment was performed in such a manner that the conductor thickness became 8 μm. And, in all the examples A conductor is formed on both sides. The film metal sheath laminates of Examples 31 to 40 and Comparative Examples 19 to 24 produced under the above-described conditions, and a polymer film (liquid crystal polymer film) In the same manner, the dimensional change rate (expansion ratio) in the plane direction due to heating after the conductor was removed was measured. @ Furthermore, since the connection reliability with the substrate of the semiconductor wafer was tested, the COF substrate was fabricated to perform a temperature cycle test. Fig. 5 and Fig. 9 show the measurement results of the dimensional change rate (expansion ratio) in the plane direction by the heat treatment after copper etching and the number of cycles up to the measurement by the temperature cycle test. Measurement results S1 -30 - 201028287 e❿ r—13⁄4 Cycle number (times) 900 1000 1- 1200 1300 1 | 1400 1300 1200 1000 00 870 700 600 Ο 7 00 600 400 Expansion ratio (%) 0.39 0.36 1- 0.33 1 1 0.28 1 1 0.25 0.20 0.15 0.11 0.08 0.06 0.43 0.48 0.50 0.02 -0.02 -0.08 ••N mm mg运mg ϋ 丨Stretching stretching drawing Stretching, Tensile, Tensile, Tensile, Tensile, Tensile, Tensile, Tensile, Compression, Heat Treatment, Temperature rc) 〇290 (N 270 260 300 (N 280 〇260 320 Ο cn cn 〇〇<N 280 treatment) Engineering I_ I- Electroless plating heat treatment - Copper plating electroless plating - Copper plating - Heat treatment Electroless plating - Heat treatment - Copper electroless electroless plating - Heat treatment - Copper electric ore m 'Ο I Electroless plating solution TOP Nicoron LPH-LF TOP Nicoron LPH-LF OMNI-SHIELD1580 1 Manufacturer name Mitsui Chemicals 1 Mitsui Chemicals Mitsui Chemicals Mitsui Chemicals Mitsui Chemicals Mitsui Chemicals Mitsui Chemicals Mitsui Chemicals Mitsui Chemicals Mitsui Chemicals Mitsui Chemicals Mitsui Chemicals Mitsui Chemicals Mitsui Chemicals Mitsui Chemicals Mitsui Chemicals Product Name I 丨AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM AURUM Film Substrate] Thermoplastic PI Heat PI Thermoplastic PI Thermoplastic PI Thermoplastic PI Thermoplastic pi Thermoplastic PI Thermoplastic PI Thermoplastic PI Thermoplastic PI Thermoplastic PI Thermoplastic PI Thermoplastic PI Thermoplastic pi Thermoplastic PI Thermoplastic PI Example 31 Example 32 Implementation Example 33 Example 34 Example 35 Example 36 Example 37 Example 38 Example 39 Example 40 Comparative Example 19 Comparative Example 20 Comparative Example 21 Comparative Example 22 Comparative Example 23 Comparative Example 24-31 - 201028287 Table 5 and As shown in Fig. 9, it can be seen that after the copper plating, the dimensional change rate (expansion ratio) in the plane direction after the heat treatment at a heating temperature of 240 ° C for 1 minute is 0.05% to 0.4%. In Example 40, the number of cycles until breaking is large. In other words, in Example 31 to Example 40 in which the heating temperature was 24 in 1 minute (the dimensional change rate (expansion ratio) in the planar direction after the heat treatment of TC was 0.05% to 0.4%, it was found that 'high connection reliability' was expressed. In addition, it can be seen that the dimensional change rate (expansion ratio) in the plane direction after performing the heating treatment at a heating temperature of 240 ° C for 1 minute is less than 〇 〇 5% of Comparative Example 22 to Comparative Example 24, and 1 minute of execution. In Comparative Example 19 to Comparative Example 21 in which the dimensional change rate (expansion ratio) in the planar direction after the heat treatment at a heating temperature of 240 ° C was more than 0.4%, the number of cycles until the breakage was small, and the connection reliability was low. (Examples and Comparative Examples of Non-Thermoplastic Polyimine) For the case of using non-thermoplastic polyimine as a film substrate, the description will be made here. For the purpose of using Toray and DuPont (shares) Kapton 100 00 is described as a non-thermoplastic polyimine. First, the non-thermoplastic polyimine is immersed in a temperature of 80 ° C (
Normal )之氫氧化鉀溶液5至15分鐘,溶解表面形成凹凸 。接著,依照改質劑處理、鎳合金之無電解電鍍處理、熱 處理、銅之電鍍處理之順序施予各處理,製造出薄膜金屬 護面疊層體。 利用表6所示之電鍍液’形成0.1微米厚度之基底電鍍 -32- 201028287 層,利用表6所示之熱處理溫度’執行ι〇分鐘間之熱處理 〇 銅電鍍處理係以導體厚度成爲8微米之方式形成銅。 並且,在所有實施例中,於兩面形成導體。 針對以上述般之條件所製作出之實施例4 1至實施例46 以及比較例25至比較例28之薄膜金屬護面疊層體,與高分 子薄膜(液晶聚合物薄膜)之情形相同,測量除去導體之 ^ 後由於加熱所產生之平面方向之尺寸變化率(膨脹率)。 Ό 再者,因試驗與半導體晶片之基板的連接信賴性,故製作 C OF基板,執行溫度循環試驗。表6及第10圖表示藉由依 據銅蝕刻後之熱處理所產生之平面方向之尺寸變化率(膨 脹率)之測量結果以及至藉由溫度循環試驗而所測量之破 斷爲止之循環數之測量結果。 -33- 201028287Normal potassium hydroxide solution for 5 to 15 minutes to form irregularities on the dissolved surface. Then, each treatment was carried out in the order of the modifier treatment, the electroless plating treatment of the nickel alloy, the heat treatment, and the copper plating treatment to produce a thin film metal sheath laminate. Using the plating solution shown in Table 6 to form a 0.1 μm thick base plating-32-201028287 layer, using the heat treatment temperature shown in Table 6 to perform the heat treatment of the 〇 〇 minute copper plating treatment with a conductor thickness of 8 μm The way to form copper. Also, in all embodiments, the conductors are formed on both sides. The film metal sheath laminates of Examples 41 to 46 and Comparative Examples 25 to 28 produced under the above-described conditions were the same as those of the polymer film (liquid crystal polymer film), and were measured. The rate of dimensional change (expansion ratio) in the plane direction due to heating after removal of the conductor. Furthermore, since the connection reliability of the test and the substrate of the semiconductor wafer was tested, a COF substrate was produced and a temperature cycle test was performed. Tables 6 and 10 show the measurement results of the dimensional change rate (expansion ratio) in the plane direction by the heat treatment after copper etching and the number of cycles up to the measurement by the temperature cycle test. result. -33- 201028287
-34- 201028287 如表6及第10圖所示般,可知於銅電鍍之後,在進行1 分鐘加熱溫度爲240 °c之加熱處理之後的平面方向之尺寸 變化率(膨脹率)爲0.05 %〜0.4%之實施例41至實施例46 中,至破斷爲止之循環數大。即是,可知在進行1分鐘加 熱溫度爲24 0 °C之加熱處理之後的平面方向之尺寸變化率 (膨脹率)爲0.05%〜0.4%之實施例41至實施例46中,表 不局連接信賴性。 I 另外,可知在進行1分鐘加熱溫度爲240 °C之加熱處理 之後的平面方向之尺寸變化率(膨脹率)小於0.05%之比 較例25至實施例88中,表示至破斷爲止之循環數小,連接 信賴性低。 如上述表1至表6及第6圖至第10圖所示般,可知當由 於銅蝕刻後之加熱所產生之平面方向之尺寸變化率(膨漲 率)爲0.05〜0.4%之時,連接信賴性高。再者,可知於執 行在通常電路基板所使用之Sn、SnAg系之焊接時,利用液 φ 晶聚酯(聚合物)、PEEK當作薄膜基材以取得高連接信 賴性。再者,也可知於不要求耐熱性之時,可以使用PET 、PEN。 由上述可知,藉由在由於利用鈾刻除去金屬層之後的 熱處理使得在平面方向膨脹〇.〇5〜0.4%之金屬護面疊層體 之電路基板,直接搭載半導體晶片(例如’藉由凸塊連接 電路基板之電極和半導體晶片),則可以製造連接信賴性 高之電子零件。 -35- 201028287 【圖式簡單說明】 H1Μ係表示本發明之第1實施形態所涉及之金屬護面 疊層體的截面圖。 第2匱[係表示本發明之第2實施形態所涉及之金屬護面 疊層體的截面圖。 第3圖係表示本發明之第3實施形態所涉及之金屬護面 疊層體的截面圖。 第4@係表示本發明之一實施形態所涉及之電路基板 @ 的截面圖。 胃5圖係表示本發明之—實施形態所涉及之電子零件 的截面圖。 第6圖係表示薄膜基材爲高分子薄膜(液晶聚合物薄 膜)之時的連接信賴性的曲線圖。 第7圖係表示薄膜基材爲PEEK之時的連接信賴性的曲 線圖。 第8圖係表示薄膜基材爲PET、PEN之時的連接信賴性 Θ 的曲線圖。 第9圖係表示薄膜基材爲熱可塑性聚醯亞胺之時的連 接信賴性的曲線圖。 第圖係表示薄膜基材爲非熱可塑性聚醯亞胺之時的 連接信賴性的曲線圖。 【主要元件符號說明】 10、20、30 :金屬護面疊層體 ] -36- 201028287-34- 201028287 As shown in Tables 6 and 10, it is understood that the dimensional change ratio (expansion ratio) in the plane direction after the heat treatment at a heating temperature of 240 ° C for 1 minute after copper plating is 0.05 %. In 0.4% of Examples 41 to 46, the number of cycles until breaking was large. In other words, in Example 41 to Example 46 in which the dimensional change ratio (expansion ratio) in the plane direction after the heat treatment at a heating temperature of 24 ° C for 1 minute was 0.05% to 0.4%, it was found that the table was not connected. Trustworthiness. In addition, in Comparative Example 25 to Example 88 in which the dimensional change ratio (expansion ratio) in the planar direction after the heating treatment at a heating temperature of 240 ° C for 1 minute was less than 0.05%, the number of cycles until breaking was shown. Small, the connection is low in reliability. As shown in the above Tables 1 to 6 and Figs. 6 to 10, it is understood that when the dimensional change rate (increase ratio) in the plane direction due to heating after copper etching is 0.05 to 0.4%, the connection is made. High reliability. Further, it is understood that liquid φ crystalline polyester (polymer) or PEEK is used as a film substrate to achieve high connection reliability when performing soldering of Sn or SnAg used in a usual circuit board. Further, it is also known that PET or PEN can be used when heat resistance is not required. From the above, it is known that the semiconductor substrate is directly mounted on the circuit substrate of the metal protective surface laminate which is expanded in the planar direction by the heat treatment after removing the metal layer by uranium engraving (for example, 'by the convex When the block is connected to the electrode of the circuit board and the semiconductor wafer, it is possible to manufacture an electronic component having high reliability. -35-201028287 [Brief Description of the Drawings] H1 is a cross-sectional view of a metal sheath laminate according to the first embodiment of the present invention. The second aspect of the present invention is a cross-sectional view showing a metal sheath laminate according to a second embodiment of the present invention. Fig. 3 is a cross-sectional view showing a metal sheath laminate according to a third embodiment of the present invention. The fourth embodiment is a cross-sectional view of the circuit board @ according to an embodiment of the present invention. The stomach 5 is a cross-sectional view showing an electronic component according to an embodiment of the present invention. Fig. 6 is a graph showing the connection reliability when the film substrate is a polymer film (liquid crystal polymer film). Fig. 7 is a graph showing the connection reliability when the film substrate is PEEK. Fig. 8 is a graph showing the connection reliability Θ when the film substrate is PET or PEN. Fig. 9 is a graph showing the connection reliability when the film substrate is a thermoplastic polyimide. The figure is a graph showing the connection reliability when the film substrate is a non-thermoplastic polyimide. [Description of main component symbols] 10, 20, 30: metal facing laminate] -36- 201028287
11: 12、 13 : 15 : 16 : 17 ·· 18 : 50 : 薄膜基材 1 2 ' ·’金屬層 基底金屬層 電路金屬層 半導體導元件 防焊劑 凸塊 電路基板 電子零件11: 12, 13 : 15 : 16 : 17 ·· 18 : 50 : Film substrate 1 2 ' ·' Metal layer Base metal layer Circuit metal layer Semiconductor conductive element Solder resist Bump Circuit board Electronic parts
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JP7117747B2 (en) * | 2016-09-29 | 2022-08-15 | 株式会社クオルテック | Electronic component manufacturing method |
CN110709239A (en) * | 2017-06-07 | 2020-01-17 | 株式会社旭电化研究所 | Flexible composite film and flexible circuit film using same |
KR102329838B1 (en) * | 2019-04-30 | 2021-11-22 | 도레이첨단소재 주식회사 | Flexible metal clad laminate film, article including the same and method of preparing the film |
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