201200610 六、發明說明: 【發明所屬之技術領域】 本發明係關於一種氧化物蒸鍍材 蒸鍍法、離子電鍍法或高密度電漿輔 空蒸鍍法而製造透明導電膜之際所使 與使用此氧化物蒸鍍材所製造的透明 用以製造作爲太陽能電池之透明電極 在可見光區域之高透射率的透明導電 鏟材之改良。 【先前技術】 透明導電膜係具有高的導電性與 透射率。而且,活用此特性,該透明 陽能電池、液晶顯示元件、其他各種 進一步活用在近紅外線區域之反射吸 爲汽車或建築物之窗玻璃等所用之熱 抗靜電膜、冷凍展示櫃等之防霧用透 另外,於該透明導電膜中,一般 銻或氟作爲摻雜劑的氧化錫(Sn02 ) 錫作爲摻雜劑的氧化鋅(Ζ η Ο );含 雜劑的氧化銦(Ιη203 )等。尤其將錫 氧化銦膜,亦即ln203 - Sn系膜被稱 膜,由於容易地獲得低電阻之透明導 被廣泛使用。· ,其係於利用電子束 助蒸鍍法等之各種真 用的氧化物蒸鍍材、 導電膜,例如,關於 有用的低電阻且顯示 膜所使用的氧化物蒸 在可見光區域之高光 導電膜係被利用於太 受光元件之電極等, 收特性,亦可利用作 線式反射膜,或各種 明散熱體。 而言,廣泛利用含有 ;含有鋁、鎵、銦、 有錫、鎢、鈦作爲摻 作爲摻雜劑而含有的 爲ITO (氧化銦錫) 電膜,迄今工業上已 201200610 而且,此等透明導電膜之製造方法,一般使用真空蒸 鍍法、濺鍍法、塗布透明導電層形成用塗液之方法等。其 中,真空蒸鍍法或濺鍍法係於使用蒸氣壓低的材料之際或 於以精密的膜厚控制爲必要之際爲有效的手法,且因操作 爲非常簡便,在工業上爲有用。另外,若比較真空蒸鑛法 與濺鍍法時,由於真空蒸鑛法者能夠高速地進行成膜,具 有優異的量產性。 可是,一般而言,真空蒸鍍法係於1〇_3至10·2 Pa左右 之真空中,加熱蒸發源之固體或液體而暫時分解成氣體分 子或原子之後,再度在基板表面上使其冷凝作爲薄膜之方 法。另外,該蒸發源之加熱方式係各式各樣,一般爲電阻 加熱法(RH法)、電子束加熱法(EB法、電子束蒸鍍法)。 另外,習知係一邊將〇2氣等之反應氣體導入成膜室(腔) 內,且一邊進行蒸鍍之反應性蒸鏟法。 而且,使如ITO之氧化物膜堆積之情形,歷史上經常 利用該電子束蒸鍍法。亦即,一旦將ITO之氧化物蒸鍍材 (也稱爲ITO錠或ITO九)用於蒸發源,將反應氣體之〇2 氣導入成膜室(腔)內,利用電場而使從熱電子發生用燈 絲(主要爲W絲)跳出的熱電子加速而照射於ITO之氧化 物蒸鏟材時,所照射的部分將成爲局部的高溫,蒸發而堆 積於基板上。另外,藉由使用熱電子發射器或RF放電而使 電漿產生,利用此電漿而使蒸發物或反應氣體(02氣等) 活化,而能夠在低溫基板上製作低電阻膜之活化反應性蒸 201200610 鍍法(ARE法)亦爲有用於ITO成膜之方法。再者,最近 使用電漿槍之高密度電漿輔助蒸鍍法(HDPE法)也變得明 確爲有效於IT Ο成膜之手法,工業上已開始廣泛地使用(參 閱非專利文獻1: 「真空」、Vol. 44, No. 4,2001年,p. 43 5-439 )。於此方法中,使用電漿產生裝置(電漿槍)而 利用電弧放電,在電漿槍內所內藏的陰極與蒸發源之坩堝 (陽極)之間維持電弧放電。從陰極所釋出的電子藉磁場 所導引,集中而照射於經進料至坩堝的ITO氧化物蒸鍍材 之局部。從被此電子束照射而成爲局部高溫的部分,蒸發 物蒸發而堆積於基板。由於經氣化的蒸發物或經導入的〇2 氣係在此電漿內被活化,故能夠製作具有良好電特性的 IT Ο膜。另外,以此等各種真空蒸鍍法之另一分類法而言, 總稱伴隨蒸發物或反應氣體之離子化者爲離子電鏟法(IP 法),作爲獲得低電阻且高光透射率之ITO膜的方法爲有 效(參閱非專利文獻2 : 「透明導電膜之技術」、歐姆公 司、1999 年刊,ρ· 205-211)。 可是,不論透明導電膜所採用的任一種型式之太陽能 電池,在光所照射的表面側之電極上,該透明導電膜皆不 可少,習知係利用上述之IT 〇膜或摻雜有鋁、鎵的氧化鋅 (ZnO )膜。而且’於此等之透明導電膜中,尋求低電阻 或太陽光線之光透射率高等之特性。另外,此等之透明導 電膜之製造方法係利用上述之離子電鍍法或高密度電漿輔 助蒸鍍法等之真空蒸鍍法。 201200610 由於該電子束蒸鍍法、離子電鍍法或高密度電漿輔助 蒸鍍法等之真空蒸鍍法所用之氧化物蒸鍍材係使用小的尺 寸(例如’直徑爲10至50mm且高度爲10至50 mm左右 之圓柱形狀)之燒結體,利用一個氧化物蒸鏟材而能夠成 膜的膜量具有界限。而且,若氧化物蒸鍍材之消耗量變多 且殘留量變少時’將中斷成膜、空氣導入真空中之成膜室 而與未使用之氧化膜蒸鑛材進行交換,且具有再度進行成 膜室之抽真空的必要,成爲生產性惡化之主因。 另外’利用電子束蒸鍍法、離子電鍍法或高密度電漿 輔助蒸鍍法等之真空蒸鍍法而量產透明導電膜之情形下所 必要不可少的技術,可舉出上述氧化物蒸鍍材之連續供應 法,其一例係介紹於非專利文獻1。於此連續供應法中, 在圓筒狀之罩內側,圓柱狀之氧化物蒸鍍材相連接而被收 納,昇華面之高度也維持一定之狀態下,而變得依序擠出 氧化物蒸鏟材予以連續供應。而且,利用氧化物蒸鑛材之 連續供應法,而變得能夠實現因真空蒸鍍法所導致的透明 導電膜之大量生產。 而且,關於作爲原料使用的氧化物蒸鍍材,於專利文 獻1 (日本特開平8-104978號公報)中,介紹了 ITO之蒸 鍍材。實質上,已有人提出由銦、錫及氧所構成的 In203-Sn02系之粒狀,1粒子之體積爲0.01至0.5 cm3且 相對密度爲55%以上,另外,塡充於容器時之體積密度爲 2.5 g/cm3以下之ITO蒸鍍材。而且,也介紹了藉由作成上 201200610 述構造’經由電子束蒸鍍而能夠成膜安定的低電阻之IT〇 膜’利用效率成爲80%以上’再者,不會堵塞於供應機內 而可以獲得使其可連續供應的ΙΤΟ蒸鍍材。 還有’也於專利文獻2(日本特開2007-84881號公報) 中也介紹了由氧化銦與氧化錫所構成的ΙΤΟ蒸鍍材。於專 利文獻2中已記載的ΙΤΟ蒸鍍材係由密度爲4.9 g/cm3、直 徑爲3 0 mm、厚度爲40 mm之圓柱狀氧化物燒結體所構 成,記載在供應機內不會破損而能夠連續供應。 可是,使用上述專利文獻等所記載的習知ITO蒸鍍材 (氧化物蒸鏟材),利用電子束蒸鑛法、離子電鍍法或高 密度電漿輔助蒸鍍法等之各種真空蒸鍍法,而製造具有低 電阻且高光透射性的透明導電膜之情形,由於具有在成膜 時而將氧氣大量地導入成膜真空槽的必要(例如,參閱專 利文獻2之段落0007與段落0108等之記載),主要發生 如下所述之問題。 首先,透明導電膜與氧化物蒸鍍材之組成偏差變大, 透明導電膜之組成設計變得困難。一般而言,一旦導入成 膜真空槽之氧量變多時,因而使透明導電膜與氧化物蒸鍍 材之組成差容易變大。於成膜量產步驟中,由於成膜真空 槽內之氧量的變動也容易發生’受到此影響而使膜組成之 變動也變得容易發生,與膜特性之偏異有關。 另外,於使用氧氣之反應性蒸鍍成膜中,若氧量變多 時,不僅發生膜之密度降低,膜對基板的附著力也變弱等 201200610 之問題。由於若所蒸發的金屬氧化物在到達基板前被氧化 時能量會消失,故一旦氧化之比例變多時,變得難以獲得 緻密且對基板之高緊貼薄膜》 還有,在表面容易被氧化之金屬膜或有機物膜所覆蓋 之基板上形成透明導電膜之情形,一旦導入成膜真空槽之 氧量爲多時,於成膜前,基板表面將被氧化,因此變得無 法製造高性能之元件。成膜時之基板溫度越高,此傾向將 變得越顯著。例如,使光從與基板相反側之面射入而製造 欲進行能量轉換的太陽能電池之情形,由於具有在利用金 屬薄膜所形成的PIN元件之上形成透明導電膜的必要。於 進行氧導入量多的成膜中,元件容易受損而無法製造高性 能之元件。形成有機薄膜太陽能電池或形成頂部發光型的 有機電致發光元件之情形也爲同樣,在有機發光層上形成 透明導電膜之情形,於氧導入量多的狀況下,由於有機發 光層被氧化而受損,無法實現高性能之元件。 本發明係著眼於如此之問題點所進行者,其課題係以 添加有錫之氧化銦作爲主要成分,即使成膜時所導入的氧 量少,也提供一種能夠安定製造低電阻且在可見光區域具 有高光透射性之透明導電膜的氧化物蒸鍍材,合倂提供一 種使用此氧化物蒸鍍材所製造的透明導電膜。 【發明內容】 亦即,有關本發明之氧化物蒸鍍材,其特徵爲以氧化 銦作爲主要成分,由含錫之氧化物燒結體所構成,且錫之 201200610 含量爲以Sn/In原子數比計0.001至0.614 彩系統中之LM直爲54至75。 另外,有關以氧化銦作爲主要成分, 膜係使用上述氧化物蒸鍍材,由利用電子 電鍍法或高密度電漿輔助蒸鍍法所成膜的 電膜所構成,且錫之含量爲以Sn/In原子 0.614。 而且,由於有關CIE 1 976色彩系統中 75之本發明的氧化物蒸鍍材係具有最適之 此氧化物蒸鍍材,即使導入成膜真空槽之 使得利用真空蒸鍍法而製造低電阻且可見 射性的透明導電膜,並且,由於導入成膜| 能夠縮小膜與氧化物蒸鍍材之組成差,不 的之膜組成,也能夠量產時減低膜組成的 動。由於導入成膜真空槽之氧量少而成膜 因氧氣所造成的對基板之損害,便可能 件。尤其不會對基板造成損害而能夠安定 陽能電池之高性能薄膜。 【實施方式】 [用於實施發明之最佳形態] 以下,針對本發明之實施形態而詳加 (1 )氧化物蒸鍍材 本發明之氧化物蒸鑛材係具有以氧 ,在 CIE1976 色 含錫之透明導電 束蒸鍍法、離子 結晶性之透明導 數比計0.001至 之L *値爲5 4至 氧量,藉由採用 氧量少,也能夠 光區域中之高透 ί空槽之氧量少, 僅容易地獲得目 變動或特性的變 ,因而能夠減低 實現高性能之元 地製造有用於太 說明。 化銦作爲主要成 -10- 之 獲 多 到 荽 性 而 201200610 分,且錫之含有以Sn/In原子數比計0.001至0.614 的組成。而且,由於使用本發明之氧化物蒸鍍材而 空蒸鍍法所製得的透明導電膜之組成係極接近氧化 材之組成,氧化物蒸銨材之組成也成爲以氧化銦作J 成分,且成爲含有錫僅以Sn/In原子數比計0.001至 之比例。使其僅以上述比例含錫之理由係因能夠使^ 膜之移動率增加。膜組成,亦即氧化物蒸鑛材組成; 量(以Sn/In原子數比計)低於0.001之情形,無法^ 體濃度增加之效果(亦即移動率之增加效果)小且1 之膜。另外,若超過0.614的話,膜中之錫量將過: 電子移動之際的中性不純物散亂變大,無法獲得受; 率降低之影響的低電阻膜。爲了發揮更高的載體濃I 到低電阻膜之更佳的錫含量係以Sn/In原子數比計 至0.163,還有,其膜爲結晶膜。 可是,以氧化銦作爲主要成分之透明導電膜係 半導體,爲了使高的導電性與高的光透射性得以發j 適度之氧短缺成爲必要。亦即,膜中之氧量爲多且! 量爲少之情形,例如即使含有摻雜劑也不顯示導電'1 對顯示導電性而必要將氧短缺導入膜中;若氧短缺: 時’可見光之光吸收將變多而成爲著色的原因。因j 中具有最適之氧短缺的必要。膜中之氧係除了從原; 化物蒸鍍材予以供應之外,也藉由膜中捕捉成膜時 膜真空槽中的氧氣而予以供應。而且,若從氧化物 .比例 用真 蒸鍍 主要 0.6 14 化銦 錫含 :得載 ,電阻 ,於 移動 而得 0.040 型之 :且使 ,短缺 :。針 :過多 卜膜 -之氧 【入成 i鍍材 -11 - * 201200610 之供應量少時,具有使導入成膜真空槽中的氧量增多的必 要,一旦增多成膜真空槽中所導入的氧量時,將發生上述 之問題。因此’具有最適之氧量的氧化物蒸鍍材將成爲有 用。 而且,有關本發明之氧化物蒸鍍材,其最大之特徵係 利用在CIE1976色彩系統之L*値而規定。於此,所謂 CIE 1 976色彩系統係CIE (國際照明委員會)在1 976年所 推薦的色彩空間。由於係將顏色以由亮度L *與色彩指數 a-、b*所構成的均等色彩空間上之座標所表示者,也簡稱 爲CIELAB。顯示亮度之L*係在L* = 0時顯示黑色、在 L+ = 100時顯示白色的擴散色。另外,a*係以負値表示偏 綠、以正値表不偏洋紅,b係以負値表不偏藍、以正値表 示偏黃。 而且,以在CIE1976色彩系統之L*値所規定的有關本 發明之氧化物蒸鍍材的燒結體表面與燒結體內部之色調較 佳爲相同,但假設在最外表面與內部爲不同的氧化物蒸鍍 材之情形,於本發明中,係針對燒結體內部而決定L *値。 根據本發明人等所進行的實驗,氧化物蒸鏟材內部之 C値爲54至75之時,即使導入成膜真空槽之氧量少,也 能夠獲得兼具高導電性與在可見光區域之高透射率的透明 導電膜。另外,越帶白色,L*値越高;相反地,越帶黑色, L +値越低。而且,認爲氧化物蒸鍍材之L *値係與氧化物 蒸鑛材內之含氧量具有相關性,認爲値越大,含氧量越 -12- 201200610 多;L *値越小,含氧量越少。本發明人等係改變製造條件, 嚐試使用各種的L*値之氧化物蒸鍍材而利用真空蒸鍍法 製作透明導電膜之實驗後,L*値越大,導入成膜中之最適 氧量(爲了獲得低電阻且透明度高的膜之氧量)越少。此 係由於L *値越大的氧化物蒸鍍材,從氧化物蒸鏟材本身所 供應的氧量變得越多所致。另外,氧導入量越多,顯示膜 與氧化物蒸鑛材之組成差異越大之傾向。因而,L *値越 大,組成差異變得越小。 另外,有關本發明之氧化物蒸鍍材係具有導電性,氧 化物蒸鍍材之導電係數係視含氧量而定,也視密度、結晶 粒徑、鈽之摻雜劑效率而定。因而,氧化物蒸鍍材之導電 係數與L#値係不對應於1比1。 而且,從以氧化銦作爲主成分且含錫之有關本發明的 氧化物蒸鍍材,係於真空蒸鍍之際,主要以In203.x、Sn02_x 之形態而產生蒸發粒子,亦一邊與腔內之氧進行反應,一 邊吸收氧,到達基板所成膜。另外,蒸發粒子所具有之能 量係於到達基板而堆積於基板上之際,成爲物質移動之驅 動源,有助於膜之緻密化與對基板之附著力增強。而且, 由於氧化物蒸鍍材之L#値越小,氧化物蒸鍍材內之氧越 少,因而蒸發粒子之氧短缺變大,必須將多量之氧導入真 空槽中而於到達基板之前增多使其氧化反應之比例。但 是,由於蒸發粒子係因爲於飛行中進行氧化而消耗能量, 於增多氧所導入的反應性成膜中,獲得緻密且對基板之緊 •13- 201200610 貼力高的膜將變得困難》相反地,極力減少所導入的氧氣 之反應性蒸鑛成膜者,較容易地獲得高緊貼且高密度之 膜,本發明之氧化物蒸鑛材係能夠實現該者。 於此,若該L*値低於54時,由於氧化物蒸鍍材中之 氧量過少,爲了獲得低電阻且透明度高的膜之導入成膜真 空槽的最適氧導入量將變多,不僅膜與氧化物蒸鍍材之組 成差異變大,也發生於成膜中對基板之損害變大等之問題 故不佳。相反地,若該値超過75時,由於氧化物蒸鍍 材中所含之氧量過多,從氧化物蒸鍍材供應至膜中之氧變 得過多的結果,變得無法獲得具有最適之氧短缺的高導電 性膜。 可是,在介紹關於濺鍍法之發明的日本特開平 5 - 1 1 2 8 66號公報(參考公報)中介紹了含錫之氧化銦燒結 體的濺鍍靶,但依照在參考公報中所記載的製法所製造的 含錫之氧化銦燒結體之値係低至3 8至49之値(參閱比 較例3 )。因而,若將如此之燒結體作爲氧化物蒸鍍材使 用時,由於必須增多用以獲得最適膜之導入成膜真空槽的 氧量;而發生上述之問題,故未達成本發明之目的。 於此,上述L*値爲54至75之本發明的蒸鍍用氧化物 燒結體(氧化物蒸鍍材)係無法利用習知之製造ITO燒結 體的技術來進行製造。具有適合使用於利用真空蒸鍍法大 量生產之適度氧量(或是氧短缺量)之氧化物蒸鍍材能夠 利用如下之方法而製造。 -14- 201200610 亦即,以氧化銦作爲主要成分且含錫之氧化物燒結體 能夠以氧化銦與氧化錫之各粉末作爲原料,混合此等粉末 且進行成型而形成壓粉體,於高溫進行燒製,使其反應· 燒結而製造。氧化銦與氧化錫之各粉末並非特別者,可以 爲習知所用之氧化物燒結體用原料。另外,所使用的粉末 之平均粒徑爲1.5 μπι以下,較佳爲〇.1至1.1 μηι。 於製造上述氧化物燒結體之際的一般性原料粉末之混 合法係利用球磨機混合法,於製造本發明之燒結體之情形 也爲有效。球磨機係藉由將陶瓷等之硬質球(球徑10至 30 mm)與材料之粉置入容器中而使其旋轉,亦一邊磨碎 材料,一邊混合而製作微細之混合粉末的裝置。球磨機(粉 碎介質)係使用鋼、不銹鋼、耐綸等作爲罐體,且使用氧 化鋁、磁材質、天然二氧化矽、橡膠、胺甲酸酯等作爲內 襯。球可舉出以氧化鋁作爲主成分之氧化鋁球、天然矽石、 置入鐵芯之耐綸球、氧化銷球等。有濕式與乾式之粉碎方 法’廣泛利用於爲了獲得燒結體之原料粉末的混合·粉碎。 另外,球磨機混合以外之方法,珠磨機法或噴射磨機 法也爲有效。尤其,由於氧化錫粉末爲硬質材料,於使用 大的平均粒徑原料之情形、或必須於短時間內進行粉碎混 合之情形係非常有效。所謂珠磨機法係將70至90%的珠 (粉碎介質、珠徑0.005至3 mm)預先塡充於稱爲Vessel 之容器中,藉由以圓周轉速7至15 m/秒鐘而使容器中央之 旋轉軸旋轉而賦予珠運轉。在此,藉由利用泵來將原料粉 -15- 201200610 末等之被粉碎物混入液體的漿體送入其中,使珠撞擊而使 其微粉碎·分散。珠磨機之情形,若與被粉碎物合倂而縮 小珠徑的話,效率將提高。一般而言,珠磨機能夠實現以 接近球磨機之1千倍的加速度微粉碎與混合。如此構造的 珠磨機係以各式各樣之名稱來稱呼,例如,砂輪機、水化 機(Aquamizer)、磨碎機、珍珠磨機、Abex磨機、超黏 磨機(Ultra vi sco mill)、戴諾(DYNO)磨機、攪拌磨機、 環隙(Coball)磨機、釘碎(Spike)磨機' SC磨機等,於 本發明中,能夠使用其中任一種。另外,所謂噴射磨機係 從噴嘴而將以音速前後所噴射的高壓之空氣或蒸氣,作爲 超高速噴射而使其對原料粉末等之被粉碎物撞擊,藉由粒 子彼此之撞擊而粉碎成微粒之方法。 如上所述,首先以所欲之比例而將氧化銦粉末與氧化 錫粉末倒入球磨機用罐中,進行乾式或濕式之混合而調製 混合粉末。然後,爲了獲得本發明之氧化物燒結體,針對 該原料粉末之摻合比例,銦與錫之含量係以Sn/In原子數 比計成爲0.001至0.614的方式來調製。 將水及分散材·黏著劑等之有機物加入進行此方式所 調製的混合粉末中而製造漿體。漿體之黏度較佳爲150至 5000cp,更佳爲 400 至 3000cP。 藉由使用進行如此方式所獲得之漿體且利用噴霧乾燥 器等使其乾燥而能夠獲得造粒粉末。但是,爲了得到更均 勻且燒結性良好之燒結體,若進行藉以下之珠磨機所導致 16 - 201200610 的粉碎混合處理時,更爲有效。 亦即,將所獲得之漿體與珠置入珠磨機之容器中而進 行粉碎混合處理。珠材可舉出氧化锆、氧化鋁等,但基於 耐磨損性之觀點,較佳爲氧化锆。從粉碎效率之觀點,珠 之直徑較佳爲1至3 mm。通過次數可以爲1次,但較佳爲 2次以上,在5次以下可獲得充分之效果。另外,處理時 間較佳爲1 0小時以下,更佳爲4至8小時。 藉由進行如此·之處理,在漿體中之氧化銦粉末與氧化 錫粉末之粉碎·混合成爲良好。 接著,使用進行如此方式所處理的漿體而進行成形。 成形方法能夠採用鑄入成形法、加壓成形法中任一種。進 行鑄入成形之情形,將所獲得之漿體澆注至鑄入成型用模 具中而製造成形體。從珠磨機之處理起直到鑄入爲止的時 間較佳爲1 0小時以內。因而藉由進行此方式所獲得之漿體 能夠防止顯示搖變性。另外,進行加壓成形之情形,將聚 乙烯醇等之黏著劑等添加於所獲得之漿體中,視需要進行 水分調節後,利用噴霧乾燥器等使其乾燥而造粒。將所獲 得之造粒粉末塡充於既定大小之模具中,之後,使用加壓 機,以9.8至98 MPa( 100至1000 kg/cm2)之壓力進行單 軸加壓成形而作成成形體。此時之成形體的厚度係考量因 其後之燒製步驟所導致的收縮,較佳設定爲能夠獲得既定 大小之燒結體的厚度。 若使用由上述之混合粉末所製作的成形體的話,能夠 -17- 201200610 利用常壓燒結法而獲得本發明之氧化物燒結體。還有,利 用常壓燒結法進行燒製而獲得氧化物燒結體之情形下,係 成爲如下之方式。 首先’對於所獲得之成形體,於300至500 °C之溫度加 熱5至2 0小時左右’進行脫黏著劑處理。其後,使其升溫 而進行燒結’但爲了有效地使內部之氣泡缺陷向外部釋 出’升溫速度係設爲1 5 0 °C /小時以下,較佳設爲! 〇 〇。(: /小 時以下’更佳設爲8 0 °C /小時以下。燒結溫度係設爲丨丨5 〇 至1 3 0 0 °C ’較佳設爲1 2 0 0至1 2 5 0 °C ;燒結時間係設爲1 至2 0小時’較佳設爲2至5小時進行燒結。脫黏著劑處理 至燒結步驟重要爲在以每0.1 m3之爐內容積爲5公升/分鐘 以上之比例的氧導入爐內而進行。在該燒結步驟導入氧而 進行係因爲燒結體係於1150°C以上容易解離氧而容易達到 過剩之還原狀態,因而阻止此解離。在此步驟,一旦形成 過量地導入氧短缺的燒結體時,其後接著在氧量調整步 驟,將燒結體之氧短缺量調整至最適將變得困難。若在燒 製溫度超過i3〇oc之溫度進fr時’即使在如上述之氧氣環 境中’氧之解離也將變得頻繁’因而變得容易達到過量之 還原狀態’基於同樣的理由故不佳。另外,燒製溫度彳氏於 1 1 5 0°c之情形,由於溫度將過低而燒結不足,無法獲得足 夠強度之燒結體故不佳。 於燒結後’進行燒結體之氧量調整步驟。氧量調整步 驟重要爲在90 0至1 100°C ’較佳爲在950至105 Ot:之加熱 -18- 201200610 溫度進行’加熱時間1 〇小時以上。直到該氧量調整步驟之 加熱溫度爲止的冷卻係一邊持續氧導入且一邊進行冷卻, 以0.1至20°c/分鐘’較佳以2至1〇〇c/分鐘之範圍的降溫 速度進行降溫》 於燒結體之氧量調整步驟中,爐內氣體環境之控制也 特別重要’導入爐內之氣體重要爲在〇2/Ar = 40/6 0至90/1 0 之範圍內控制氧與氬之混合比(體積比),在以每〇.1 之爐內容積爲5公升/分鐘以上之比例而導入爐內。藉由精 密地調整如此之溫度與氣體環境、時間,能夠獲得有用於 作爲氧化物蒸鍍材而使用時之具有本發明所規定的該L* 値之燒結體。 在該氧量調整步驟之加熱溫度係在低於900°C之情 形,由於氧之解離·吸附的反應遲緩,直到燒結體內部均 句之還原處理需要時間故不佳;若在超過1100 °C之溫度進 行時,氧之解離將過度激烈,由於因該氣體環境所導致的 最適之還原處理係不可能故不佳。另外,若氧量調整步驟 之加熱時間低於1 〇小時的話,由於並不進行直到燒結體內 部之均勻還原處理故不佳。另外,若導入爐內之氣體的混 合比(〇2/Ar)低於40/60時,因氧之解離所導致的還原化 將成爲過度優勢,因而成爲L*値低於54之燒結體故不佳。 相反地,若導入爐內之氣體的混合比(〇2/Ar)超過90/10 時,氧化將成爲過度優勢,因而成爲値超過75之燒結 體故不佳。 -19- 201200610 爲了獲得本發明之氧化物蒸鍍材,如上述方式,重要 爲在利用氬氣而使氧氣精密地稀釋的氣體環境下,亦即在 精密地控制氧量的氣體環境下進行退火處理,環境氣體並 無必定爲氧與氬之混合氣體的必要。例如,即使使用氦或 氮等之其他惰性氣體以取代氬也爲有效。另外,即使使用 空氣以取代氬之情形下,若在其整體之混合氣體中精密地 固定控制氧含量的話也爲有效。但是,如習用之技術,一 般將氧氣導入利用空氣進行燒製的爐內,係由於無法精密 地控制爐中之氣體環境的氧含量故非有效。如本發明所提 案的方式,藉由導入與經精密地控制氧氣之含有比例的惰 性氣體之混合氣體而充滿爐內,能夠獲得具有最適之還原 狀態的氧化物蒸鍍材。 而且,結束氧量調整步驟之後,能夠以1 (TC /分鐘降溫 至室溫而在室溫從爐內取出。所獲得之燒結體能夠藉由硏 削成既定之尺寸等,進行加工而作成氧化物蒸鍍材。另外, 也考量燒結之收縮率,若使用燒製後成爲既定尺寸之大小 的成形體的話,即使不進行燒結後之硏磨加工,也能夠作 爲氧化物蒸鍍材而利用。 可是,已知利用一種濺鍍靶的製造法,作爲獲得高密 度燒結體的方法之熱加壓法爲有效。但是,將熱加壓法應 用於本發明的材料之情形,僅獲得L*値爲40以下之還原 性過強的燒結體。於如此之燒結體中,無法達成本發明之 目的。 -20- 201200610 另外,針對本發明之氧化物蒸鍍材,例如,使用直徑 10至50 mm且高度10至50 mm之圓柱狀的錠或九狀也爲 可能,即使粉碎如此之燒結體的1至1 〇 mm左右之顆粒形 狀也能夠利用。 另外,針對有關本發明之氧化物蒸鍍材,銦、錫、氧 以外之其他元素,亦可含有例如鎢、鉬、鋅、鎘、鈽等, 以不損害本發明之特性爲條件而被允許,但是,於金屬離 子之中,與氧化銦或氧化錫之蒸氣壓作一比較,其氧化物 之蒸氣壓極高的情形下,由於利用各種真空蒸鍍法使其蒸 發將變得困難,以不含有者較佳。與氧化銦或氧化錫作一 比較,例如,如鋁、鈦、矽之金屬,由於此等氧化物之蒸 氣壓極高,使其於氧化物蒸鍍材中含有之情形,使氧化銦 或氧化錫一起蒸發將變得困難。因此,殘存於氧化物蒸鍍 材中而高濃度化,最後由於造成妨礙氧化銦與氧化錫之蒸 發等之不良影響而不得使其含有。 而且,若採用本發明之氧化物蒸鍍材,利用各種真空 蒸鍍法而製造透明導電膜時,由於使上述氧化物蒸鍍材內 之氧含量已被最適調整,即使導入成膜真空槽之氧量少, 也能夠獲得最適之氧短缺的透明導電膜。因而,具有透明 導電膜與氧化物蒸鍍材間之組成差異小、也難以受到隨著 氧導入量變動所造成的特性偏異影響之優點。 (2 )透明導電膜 採用關於本發明之氧化物蒸鍍材,其係以氧化銦作爲 -21 - 201200610 主成分且藉由含有錫之燒結體所構成,錫之含量係以Sn/In 原子數比計爲0.001至0.614且在CIE1976色彩系統之r 値爲54至75,能夠利用電子束蒸鍍法、離子電鍍法或高 密度電漿輔助蒸鍍法等之各種真空蒸鍍法而製造含有錫之 氧化銦結晶膜(透明導電膜)。 藉由作成結晶膜,錫置換固溶在氧化銦之銦位置時, 能夠使高的移動率發揮。該結晶膜(透明導電膜)係亦可 藉由將成膜中之基板加熱至1 80°C以上而獲得;但亦可利用 於1 8 0°C以上將利用加熱或非加熱成膜所獲得之膜退火的 方法而獲.得。 而且,由於有關本發明之結晶性的透明導電膜能夠從 膜與氧化物蒸鍍材之組成差異小的氧化物蒸鍍材而製造, 且含有以Sn/In原子數比計爲0.001至0.614之錫的氧化銦 膜。若膜之錫含量(以Sn/Iri原子數比計)低於0.001的話, 載體濃度增加之效果(亦即移動率增加之效果)小且無法 獲得低電阻膜。另外,若超過0.614時,膜中之錫量將過 多且於電子移動之際的中性不純物散亂將變大,得不到受 移動率降低之影響的低電阻膜。爲了進一步獲得高載體濃 度的透明導電膜,更佳的錫含量係以Sn/In原子數比計爲 〇 · 〇 4 0至0 . 1 6 3 ’膜爲結晶膜。藉由得到如此之組成範圍的 結晶膜,.能夠實現如下之透明導電膜:載體濃度爲7.2x1 〇20 cm — 3以上、比電阻爲3.5xl〇_4Qcm以下。另外,關於本發 明之透明導電膜係在波長400至800 nm之膜本身的平均透 -22- 201200610 射率非常的高,爲90%以上。 以下,針對本發明之實施例而具體地加以說明。 〔實施例1至4〕 〔氧化物蒸鑛材之製作〕 將平均粒徑爲0.8 μιη之Ιη203粉末及平均粒徑爲1 μπι 之Sn02粉末作爲原料粉末,以S n/In原子數比計成爲0.048 之比例來調和此等之Ιη203粉末與Sn02粉末,且置入樹脂 製罐中,利用濕式球磨機進行混合。此時,使用硬質Zr02 球,將混合時間設爲20小時。 混合後,取出漿體而將聚乙烯醇之黏著劑添加於所獲 得之漿體中,利用噴霧乾燥器等使其乾燥而造粒。 使用此造粒物,以98 MPa( 1 ton/cm2)之壓力,進行 單軸加壓成形而獲得直徑30 mm、厚度40 mm之圓柱狀的 成形體。 接著,進行如下的方式來燒結所獲得之成形體。 亦即,在燒結爐內之空氣中,以3 00 °C之溫度條件加熱 1 〇小時左右而進行成形體之脫黏著劑處理後,在以每0 . 1 m3之爐內容積爲5公升/分鐘以上之比例而導入氧的氣體 環境’以1°C/分鐘之速度來升溫,在1 2 5 0°C燒結2小時(常 壓燒結法)。此時,於燒結後的冷卻之際,亦一邊導入氧, 一邊以1(TC/分鐘降溫至l〇〇〇t:。 接著’將導入氣體切換成氧與氬之混合氣體,於1000 °C 而加熱維持1 5小時(以後,將此步驟稱爲燒結體氧量調整 -23- 201200610 步驟)後,以1 〇 t /分鐘降溫至室溫。 而且,藉由使該混合氣體之氧與氬之混合比例改變而 能夠獲得各種的L*値之氧化物燒結體(氧化物蒸鍍材)。 亦即,有關實施例1之氧化物蒸鍍材係以氧氣/氬氣流 量比(亦即,體積比)爲「40/60」之條件來予以製造,有 關實施例2之氧化物蒸鍍材係以該體積比爲「60/40」之條 件來予以製造,有關實施例3之氧化物蒸鍍材係以該體積 比爲「8 0/2 0」之條件來予以製造,及有關實施例4之氧化 物蒸鍍材係以該體積比爲「90/10」之條件來予以製造。 還有,測定所獲得之氧化物燒結體(氧化物蒸鍍材) 之體積與重量而算出密度後,爲4.8至5.7 g/cm3。另外, 由根據該氧化物燒結體之斷裂面的掃瞄電子顯微鏡所獲得 之觀察,求出氧化物燒結體中之1 00個結晶粒徑的平均値 後’任一種皆爲3至10 μιη。另外,對於氧化物燒結體之 電子束照射面,利用四端子探針法電阻率.計以測定表面電 阻而算出比電阻爲1 kD cm以下。進一步對於全部之氧化物 燒結體’利用ICP發光分析法而進行組成分析後,得知具 有進料組成。另外,針對燒結體表面與燒結體內部,使用 色差計(BYK-GaradnerGmbH 公司製 Specrto Guide、 E-6834 ) ’測定在CiEi 9 7 6·色彩系統之L*値,顯示幾乎相 同的値。 將燒結體氧量調整步驟中所導入的混合氣體之氧氣/ 氬氣流量比(亦即,體積比)、與所獲得之氧化物燒結體 -24- 201200610 (氧化物蒸鍍材)之L +値顯示於以下之表1(a)、表1 (b )及表1 ( c )中。 表 1 ( a) 氧化物蒸鍍材之 Sn/In原子數比 燒結物氧量調整步驟中 之02/Ar流量比 氧化物蒸鍍材之1/値 最適氧混合量 實施例1 0.048 40/60 54 9 實施例2 0.048 60/40 62 8 實施例3 0.048 80/20 70 5 實施例4 0.048 90/10 75 2 比較例1 0.048 30/70 49 15 比較例2 0.048 100/0 79 0 比較例3 0.048 — 38 42 實施例5 0.102 40/60 55 8 實施例6 0.102 60/40 61 7 實施例7 0.102 80/20 69 4 實施例8 0.102 90/10 73 3 比較例4 0.102 30/70 50 15 比較例5 0.102 100/0 82 0 比較例6 0.102 — 49 42 實施例9 0.001 60/40 67 7 實施例1〇 0.009 60/40 65 7 實施例11 0.028 60/40 63 6 實施例12 0.163 60/40 60 6 實施例13 0.230 60/40 61 5 實施例14 0.614 60/40 62 5 比較例7 0.102 — 49 42 比較例8 0.102 100/0 79 0 -25- 201200610 表 1 ( b) 在最適氧混合量之膜特性 比電阻 (μΩοιη) 載體濃度 (cm'3) 電洞移動率 (cm2/V s ) 膜本身之可見光 區域之透射率(%) 實施例1 150 1.19χ1021 35 90 實施例2 150 1.3〇χ1021 32 90 實施例3 150 1.26x1021 33 90 實施例4 150 1.13χ1021 37 90 比較例1 190 9.14x1ο20 36 90 比較例2 230 7.76χ1020 35 90 比較例3 210 8.04x1020 37 90 實施例5 180 1.24χ1021 28 90 實施例6 180 1.29χ1021 27 90 實施例7 180 1.24x1021 28 90 實施例8 180 1.34χ1021 26. 90 比較例4 210 1.06χ1021 28 90 比較例5 310 7.75χ1020 26 90 比較例ό 220 1.14χ1021 25 90 實施例9 750 1.52χ1020 55 90 實施例10 675 1.82χ1020 51 90 實施例11 470 2.96χ1020 45 90 實施例12 350 7·14χ1020 25 90 實施例13 520 5.72χ1020 21 90 實施例14 780 4.71 χΙΟ20 17 90 比較例7 220 8.12Χ1020 35 90 比較例8 220 9·8〇χ1020 29 90 -26- 201200610 表 1 ( c) 在最適氧混合量之膜特件 氧化物蒸鍍材 之裂開 膜之結晶性 膜之Sn/In原子數比 膜對基板之附著力 實施例1 結晶膜 ' 0.048 強 未裂開 實施例2 結晶膜 0.048 強 未裂開 實施例3 結晶膜 0.048 強 未裂開 實施例4 結晶膜 0.048 強 未裂開 比較例1 結晶膜 0.075 弱 未裂開 比較例2 結晶膜 0.048 強 未裂開 比較例3 結晶膜 0.095 弱 裂開 實施例5 結晶膜 0.102 強 未裂開 實施例ό 結晶膜 0.102 強 未裂開 實施例7 結晶膜 0.102 強 未裂開 實施例8 結晶膜 0.102 強 未裂開 比較例4 結晶膜 0.122 弱 未裂開 比較例5 結晶膜 0.102 強 未裂開 比較例6 結晶膜 0.118 弱 裂開 實施例9 結晶膜 0.001 強 未裂開 實施例10 結晶膜 0.009 強 未裂開 實施例11 結晶膜 0.028 強 未裂開 實施例12 結晶膜 0.163 強 未裂開 實施例13 結晶膜 0.230 強 未裂開 實施例14 結晶膜 0.614 強 未裂開 比較例7 結晶膜 0.114 弱 裂開 比較例8 結晶膜 0.102 強 未裂開 〔透明導電膜之製作與膜特性評估、成膜評估〕 (1)將磁場偏向型電子束蒸鍍裝置用於透明導電膜之製 作。 真空排氣系統係由旋轉泵所導致的低真空排氣系統與 低溫泵所導致的高真空排氣系統所構成,可排氣直到 5 X 1 (Γ5 Pa。電子束係藉由燈絲之加熱而產生,經由在陰極-陽極間所外加的電場予以加速,在永久磁石之磁場中予以 彎曲後,照射於鎢製之坩堝內所設置的氧化物蒸鍍材。電 -27- 201200610 子束強度係藉由使對燈絲之外加電壓改變而能夠調整。另 外,若使陰極-陽極間的加速電壓改變時,能夠使電子束之 照射位置改變。 成膜係以下列之條件而實施。 將 Ar氣及 02氣導入真空室內而使壓力維持於 1.5x10 ·2 Pa。此時,評估使導入真空室內之Ar氣及02氣 之混合比例改變所獲得之透明導電膜的特性。將實施例1 至4之圓柱狀氧化物蒸鏟材直立配置於鎢製坩堝中,將電 子束照射於氧化物蒸鍍材圓形面之中央部,在厚度1.1 mm 之Corning 705 9玻璃基板上形成膜厚200 nm之透明膜。 設定電子槍之設定電壓爲9 kV、電流値爲150 mA,基板係 加熱至2 5 0 °C。 (2 )所獲得之薄膜(透明導電膜)之特性係利用以下之順 序進行評估。 首先,薄膜(透明導電膜)之表面電阻係利用四端子 探針法電阻率計 Loresta EP ( DIA Instruments公司製、 MCP-T3 60型)測定,且薄膜(透明導電膜)之膜厚係使用 接觸式表面粗糙度計(Tencor公司製)而從未成膜部分與 成膜部分之高低差測定而評估,算出「比電阻(μΩ cm )」。 進一步,使用電洞效果測定裝置(TOYO CORPORATION 製ResiTest),在室溫下利用van der Pauw法所獲得之膜 在室溫的「載子濃度(cm·3 )」、「電洞移動率(cm2/vs)」。 接著,利用分光光度計(日立製作所公司製、U-4000 ) -28- 201200610 而測定含有玻璃基板之膜(附膜L之玻璃基板B)之 率〔TL + b ( % )〕,利用同樣之方法而僅從測定的玻 板(玻璃基板B )之透射率〔TB( % )〕,利用〔TL+ B + TB (%)〕而算出膜本身之透射率。 另外,膜之結晶性係利用X線繞射測定而評估。 繞射裝置係使用X ’Pert PROMPD(PANalytical公司製 測定條件係利用廣域測定,使用CuKa線,利用電壓45 電流40 mA而進行測定。由X線繞射波峰之有無而評 之結晶性。此結果也顯示於表1 ( c )之「膜之結晶性 中。 接著,膜之組成(以Sn/In之原子數比計)係利用 發光分析法測定。另外,膜對基板之附著力係根據 C002 1而評估。評估係無膜剝離之情形視爲良好(強的 有膜剝離之情形視爲不足(弱的)。也將此等之結果 於表1 ( c )之「以Sn/In之原子數比計」與「膜對基 附著力」之各欄中。 各薄膜(透明導電膜)之比電阻與透射率係視於 中導入成膜真空槽之Ar氣與02氣之混合比例而定。丨 氣之混合比例〔〇2/ ( Ar + 02 ) ( % )〕以每1%而從 50%使其變化,將顯示最低比電阻的〇2氣之混合比例 最適氧混合量而定出。將此結果顯示於表1 (a)之「 氧混合量」之欄中。 利用較最適氧混合量爲少的氧量所製作的薄膜( 透射 璃基 X 1 00 X線 [)' kV、 估膜 」欄 ICP JIS 丨), 顯示 板的 成膜 塔〇2 〇至 作爲 最適 透明 -29- 201200610 導電膜)不僅導電性差且可見光區域之透射率也低。利用 最適氧混合量所製作的薄膜(透明導電膜)不僅導電性良 好,在可見光區域之透射率也高。 (3)使用實施例1至4之氧也物蒸鍍材而求得實施上述成 膜評估時之最適氧混合量、與此時之膜的比電阻、在可見 光區域(波長400至8 00 nm )之膜本身的平均透射率。 將此等之評估結果分別顯示於表1 ( b )之「比電阻 (μΩ(:η〇」與「膜本身之可見光區域的透射率(%)」欄 中〇 於使用實施例1至4之氧化物蒸鍍材的成膜之情形, 爲了獲得最低電阻且高透射性之透明導電膜,應該導入成 膜真空槽之最適氧混合量非常的少。此係由於各氧化物蒸 鍍材內含有最適之氧量所致。另外,在最適氧混合量所製 造的膜係顯示相同於氧化物蒸鑛材之組成,不僅顯示非常 低的比電阻且在可見光區域也顯示高的透射率。另外,膜 被確認爲方鐵錳礦(BUbyte)型構造之氧化銦結晶膜,對 基板之附著力也強而足以實用。 還有·,電子槍之設定電壓爲9 kV,電流値係設爲150 mA。觀察電子束照射60分鐘後的氧化物蒸鍍材,目視觀 察氧化物蒸鏟材中是否裂開或有無裂痕(氧化物蒸鍍材耐 久試驗)。實施例1至4之氧化物蒸鍍材即使連續使用也 未產生裂痕(「未裂開」之評估)。 如此之透明導電膜係作爲太陽能電池之透明電極可謂 -30- 201200610 非常的有用。 〔比較例1至2〕 於實施例1至4中,僅改變在燒結體氧量調整步驟之 導入氣體的混合比而製造氧化物燒結體。亦即,在比較例 1中,02/Ar流量比係設爲3 0/7 0 ;在比較例2中則設爲 1 0 0 / 0。針對所獲得之燒結體,同樣地評估密度、比電阻、 結晶粒徑、組成,與實施例1至4係同等。所獲得之氧化 物燒結體之表面與內部的顔色係同等,但測定其L *値後, 顯示如表1 ( a )之値。 接著,與實施例1至4同樣地實施成膜評估。 其結果也顯示於上表1(a)至(c)中。 比較例1係具有如下之特徵:爲顯示L*値較本發明之 規定範圍(54至75 )爲小的値(49 )之氧化物蒸鍍材;與 實施例1至4之氧化物蒸鍍材作一比較,在成膜時之最適 氧混合量較多(1 5 )。與實施例1至4作一比較,在最適 氧混合量之膜特性係透射率爲同等,但比電阻有些較高。 認爲此係主要原因爲膜之組成偏移大。再者,與實施例1 至4作一比較,比較例1之膜係較對基板之附著力爲弱。 認爲此係於成膜時稍多地導入氧之成膜所致。由於如此之 氧化物蒸鑛材,所獲得之膜組成偏異大而難以設計膜組 成。另外,由於必須將氧氣稍多地導入成膜真空槽中,一 旦在成膜之量產步驟使用時,受到真空槽內之氧濃度變動 的影響而使組成或特性的變動變大。因而,確認比較例1 201200610 之氧化物蒸鍍材並不適合於成膜量產。 另外,比較例2係顯示L *値較本發明之規定 的値(79)之氧化物蒸鍍材的例子。成膜時之最 量爲〇 %,膜之比電阻係較實施例1至4爲高。 由於從氧化物蒸銨材供應至膜中的氧過多,膜 多,能夠導入最適之氧短缺量。因而,確認即使 之氧化物蒸鍍材而成膜,也無法獲得此蒸鍍材之 原本所具有的高導電性之膜。 〔比較例3〕 接著,依據在日本特開平5-112866號公報(彥 所介紹的濺鍍靶之燒結體製作技術而製造含有錫 燒結體。 首先’將平均粒徑爲1 μιη以下之In2〇3粉末 徑爲1 μπι以下之Sn02粉末作爲原料粉末,使以 子數比計成爲如〇 _ 〇 4 8之比例來調和I n2 〇 3粉末與 末’且置入樹脂製罐中而利用濕式球磨機進行混名 使用硬質Z r Ο2球,將混合時間設爲2 0小時。混 出漿體,過濾、乾燥後進行造粒。 然後,使用所獲得之造粒粉末,施加1 96 t ο n / c m2 )之壓力而以低溫靜水壓加壓來實施成形 將所獲得之成形體置入燒結爐內,於空氣中,於 結5小時。 將所獲得之燒結體加工成直徑30 mm、厚度 範圍爲大 適氧混合 3忍爲此係 中的氧量 使用如此 組成發揮 〖考公報) 之氧化銦 及平均粒 Sn/In 原 I Sn02 ί。此時, 合後,取 MPa ( 2 ,進一步 1 520°C 燒 40 mm 大 -32- 201200610 小之圓柱狀。燒結體之密度爲6.0 g/cm3、比電阻爲 m Ω c m。另外,結晶粒徑爲1 2至1 5 μ m,組成係與進 成約略相同。所獲得之燒結體之表面與內部的顔色 等,但測定其L *値後’如表1 ( a )所示,爲極低的値(: 此係表示氧化物蒸鍍材中之氧量非常的少。 接著,與實施例1至4同樣地實施成膜評估。 其結果也顯示於上表1(a)至(c)中。 比較例3係顯示L +値較本發明之規定範圍(5 4 3 明顯爲小的値(3 8 )。與相同組成之實施例1至4的 物蒸鍍材作一比較,成膜時之最適氧混合量爲(42 ) 常的多。與實施例1至4作一比較,在最適氧混合量 特性的透射率係同等,但比電阻較高。認爲此係主要 爲膜之組成偏移爲大。再者,比較例3之膜係對基板 著力較實施例1至4爲弱。認爲此係由於成膜時爲稍 導入氧之成膜所致。由於如此氧化物蒸鍍材係所獲得 組成偏異大而難以設計膜組成。另外,由於必須將氧 多地導入成膜真空槽中,一旦在成膜之量產步驟使用 受到真空槽內之氧濃度變動的影響而使組成或特性的 變大。另外,以在與實施例1至4同樣的條件而實施 物蒸鍍材耐久試驗後,在連續成膜後之氧化物蒸鑛材 生裂痕(「裂開」之評估)。若使用如此之產生裂痕 化物蒸鍍材而進行連續成膜時,將發生成膜速度大 等之問題而無法安定地成膜》 0.6 料組 係同 I 8卜 75 ) 氧化 ,非 之膜 原因 之附 多地 之膜 氣稍 時, 變動 氧化 中產 的氧 變動 -33- 201200610 因而,確認比較例3之氧化物蒸鍍材並不適合於成膜 量產。 〔實施例5至8〕 於調和Ιη203粉末與311〇2粉末之際,除了使以Sn/In 原子數比計成爲如0.102之比例來調和以外,也以包含燒 結體氧量調整之條件而與實施例1至4完全同樣的條件而 製作實施例5至8之氧化物燒結體(氧化物蒸鑛材)。 亦即,有關實施例5之氧化物蒸鍍材係以氧氣/氬氣流 量比(亦即體積比)爲「40/60」之條件而予以製造,有關 實施例6之氧化物蒸鍍材係以該體積比爲「60/40」之條件 而予以製造,有關實施例7之氧化物蒸鍍材係以該體積比 爲^ 8 0/20」之條件而予以製造,及有關實施例8之氧化物 蒸鍍材係以該體積比爲^ 90/10」之條件而予以製造。 然後,針對所獲得之實施例5至8之氧化物燒結體(氧 化物蒸鍍材),同樣地評估密度、比電阻、結晶粒徑、組 成後,其中任一種皆與實施例1至4爲同等。另外,所獲 得之氧化物燒結體之表面與內部的顏色係同等。將測定其 L +値之結果顯示於上表1 ( a )中。 另外,與實施例1至4同樣地實施成膜評估。 其結果也顯示於上表1(a)至(c)中。 於使用實施例5至8之氧化物蒸鍍材的成膜中,爲了 獲得最低電阻且高透射性之透明導電膜而應該導入成膜真 空槽之最適氧混合量係與實施例1至4同樣地非常的少。 -34- 201200610 此係由於氧化物蒸鑛材內含有最適之氧量所致。另外,於 最適氧混合量所製造的膜係顯示與氧化物蒸鍍材相同的組 成,不僅顯示非常低的比電阻,即使在可見光區域也顯示 高的透射率。另外,全部的膜係成爲氧化銦之方鐵錳礦型 結晶構造之結晶膜,膜對基板之附著力也強而足以實用。 再者’即使實施例5至8之氧化物蒸鍍材連續使用,裂痕 也未產生。 如此之透明導電膜可謂非常有用作爲太陽能電池之透 明電極。 〔比較例4至5〕 於比較例1至2中,除了於使調和In2〇3粉末與Sn02 粉末之際的以Sn/In原子數比計成爲0.102以外,以與比較 例1至2同樣的條件而製作氧化物蒸鑛材。亦即,於比較 例 4中,燒結體氧量調整之條件係 〇2/Ar流量比設爲 3 0/7 0 ;於比較例5中設爲100/0。針對所獲得之燒結體, 同樣地評估密度、比電阻、結晶粒徑、組成,與實施例5 至8係同等。另外,所獲得之氧化物燒結體之表面與內部 的顏色係同等。測定其L*値後,顯示如表1 ( a )之値。 接著,與實施例1至4同樣地實施成膜評估。 其結果也顯示於表1(a)至(c)中。 比較例4係顯示L*値較本發明之規定範圍(54至75 ) 爲小的値(5 0 )之氧化物蒸鑛材,與使用實施例5至8之 氧化物蒸鍍材時作一比較,成膜時之最適氧混合量多至爲 -35- 201200610 (15 )。與實施例5至8作一比較,在最適 特性,透射率係約略同等,但比電阻稍高。 由於膜之組成偏移大,膜中含有過剩之錫。 4之膜,其對基板之附著力較實施例5至8 大組成偏移與低附著力之主要原因皆由於成 導入氧之成膜所致。由於所獲得之膜組成偏 計膜組成。另外,由於必須將氧氣稍多地導 中,一旦在成膜之量產步驟使用時,受到真 度變動的影響而顯著地變得容易受到組成或 因而,確認比較例4之氧化物蒸鍍材也不適名 另外,比較例5係顯示L *値較本發明之 的値(82 )之氧化物蒸鍍材的例子。成膜時 量爲〇%,但膜之比電阻較實施例5至8爲 由於從氧化物蒸鍍材供應至膜的氧過多而 多,未能導入最適之氧短缺量。因而,確認 之氧化物蒸鑛材而成膜,也未能得到發揮此 之組成本身所具有的高導電性之膜。 〔比較例6〕 於比較例3中,除了於使調和In2〇3粉5 之際的以Sn/In原子數比計成爲0.102以外, 同樣的條件而製作氧化物蒸鍍材。針對所獲 同樣地評估密度、比電阻、結晶粒徑、組成 3爲同等。另外,所獲得之燒結體之表面與 氧混合量之膜 認爲此原因係 再者,比較例 爲弱。如此之 膜時爲稍多地 移大而難以設 入成膜真空槽 空槽內之氧濃 特性的變動。 t於成膜量產。 規定範圍爲大 之最適氧混合 高。認爲此係 使膜中之氧量 即使使用如此 氧化物蒸鎪材 艮與Sn02粉末 以與比較例3 得之燒結體, ,但與比較例 內部的顏色係 -36- 201200610 同等,但測定其L *値後,顯示如表1 ( a )之値。 接著,與實施例1至4同樣地實施成膜評估。 其結果也顯示於表1(a)至(c)中。 比較例6也顯示L*値較本發明之規定範圍(54 3 爲小的値(49 )。與相同組成的實施例5至8之氧化 鍍材作一比較,成膜時之最適氧混合量爲(42),非 多。與相同組成之氧化物蒸鍍材的實施例5至8作一 t 在最適氧混合量之膜特性的透射率係同等,但與實施 至8之作一比較,比電阻較高。認爲此係主要原因爲 組成偏移大。再者,比較例6之膜係對基板之附著力 施例5至8爲弱。認爲此係由於成膜時爲稍多地導入 成膜所致。由於所獲得之膜組成偏異大,故如此之氧 蒸鍍材係難以設計膜組成。另外,由於必須將氧氣稍 導入成膜真空槽中,一旦在成膜之量產步驟而使用時 到真空槽內之氧濃度變動的影響而使組成或特性的變 大。另外,以在與實施例1至4同樣的條件而實施氧 蒸鍍材耐久試驗後,在連續成膜後之氧化物蒸鍍材中 裂痕(「裂開」之評估)。若使用如此之產生裂痕的 物蒸鍍材而進行連續成膜時,將發生成膜速度大幅變 之問題而無法安定地成膜。 由以上所述,確認比較例6之氧化物蒸鍍材也不 於成膜量產。 〔實施例9至1 4〕 75 ) 物蒸 常的 :較, 例 5 膜之 較實 氧之 化物 多地 ,受 動變 化物 產生 氧化 動等 適合 -37- 201200610 除了於使調和Iri2〇3粉末與Sn02粉末之際的摻合比 例’以S n /1 η原子數比計成爲〇 . 〇 〇〗(實施例9 )、〇 . 〇 〇 9 (實施例1 〇 )、0 . 〇 2 8 (實施例1 1 )、〇」6 3 (實施例1 2 )、 0.230(實施例13)及0.614(實施例14)的方式來使其改 變以外’以與實施例2同樣的條件(亦即,氧氣/氬氣流量 比爲「60/40」之條件)而製作實施例9至14之氧化物燒 結體(氧化物蒸鍍材)。 然後’針對所獲得之實施例9至1 4之氧化物燒結體(氧 化物蒸鍍材),同樣地評估密度、比電阻、結晶粒徑、組 成,任一種皆與實施例2爲同等。另外,所獲得之氧化物 燒結體之表面與內部的顏色係同等。將測定其L *値之結果 顯示於上表1(a)中。 另外,與實施例1至4同樣地實施成膜評估。 其結果也顯示於上表1(a)至(c)中。 使用實施例9至14之氧化物蒸鏟材的成膜之情形,爲 了獲得最低電阻且高透射性之透明導電膜,應該導入成膜 真空槽之最適氧混合量非常的少。此係由於氧化物蒸鍍材 內含有最適之氧量所致。另外,在最適氧混合量所製造的 膜係顯示與氧化物蒸鍍材相同的組成,不僅顯示非常低的 比電阻,且在可見光區域也顯示高的透射性。另外’全部 的膜被確認爲氧化銦之方鐵錳礦型結晶構造的結晶膜,對 基板之附著力也強而足以實用。另外,利用與實施例1至 4同樣的條件而實施氧化物蒸鍍材耐久試驗,實施例9至 -38- 201200610 I4之氧化物蒸鍍材即使連續使用也未產生裂痕。 如此之透明導電膜係作爲太陽能電池之透明電極可謂 非常的有用。 〔比較例7〕 接著,製造在日本特開平8 - 1 0497 8號公報(專利文獻 1 )所介紹的IT Ο氧化物蒸鍍材而進行同樣的評估。 亦即,使以Sn/In原子數比計成爲0.102的方式來將平 均粒徑爲1 μιη之氧化錫粉末摻入平均粒徑爲0.1 μιη之氧 化銦粉末中,且添加2質量%之醋酸乙烯系黏著劑。濕式 球磨機中,進行此等物質之1 6小時混合、乾燥及粉碎之 後,作成造粒粉末。進一步使用此造粒粉末,以低溫靜水 壓加壓施加49 MPa( 500 kg f/cm2)之壓力而作成圓柱狀之 成形體。於大氣中進行此成形體之燒結。燒結步驟係從室 溫起而以1 0小時升溫至60 0°C,再以4小時40分鐘使溫度 上升至1 45 0 °C爲止。然後,於1 450 °C保持1〇小時而獲得燒 結體。 將所獲得之燒結體加工成直徑3 0 mm、厚度40 mm大 小之圓柱狀而作成ITO氧化物蒸鍍材。燒結體之密度爲4.4 g/cm3、比電阻爲1.2 mDcm。另外,結晶粒徑爲12至16 μιη, 組成係與進料組成約略相同。所獲得之燒結體之表面與內 部的顏色係同等,但測定其L *値後,如表1 ( a )所示, 爲極低的値(49)。此係表示氧化物蒸鍍材中之氧量非常 的少。 -39- 201200610 接著,與實施例1至4同樣地實施成膜評估。 其結果也顯示於上表1(a)至(c)中。 如上所述,比較例7也明顯地顯示L *値較本發明之規 定範圍(54至75 )爲小的値(49 );與實施例5至8之氧 化物蒸鍍材作一比較,在成膜時之最適氧混合量爲(42 ), 非常的多。與實施例5至8作一比較,在最適氧混合量之 膜特性係透射率爲同等,但比電阻較高。認爲此係主要原 因爲膜之組成偏移大。再者,與實施例5至8作一比較, 比較例7之膜係較對基板之附著力爲弱。認爲此係於成膜 時稍多地導入氧之成膜所致。由於如此之氧化物蒸鏟材, 所獲得之膜組成偏異大而難以設計膜組成。另外,由於必 須將氧氣稍多地導入成膜真空槽中,一旦在成膜之量產步 驟使用時,受到真空槽內之氧濃度變動的影響而使組成或 特性的變動變大。另外,以在與實施例1至4同樣的條件 而實施氧化物蒸鍍材耐久試驗後,在連續成膜後之氧化物 蒸鍍材中產生裂痕(「裂開」之評估)。若使用如此之產 生裂痕的氧化物蒸鍍材而進行連續成膜時,將發生成膜速 度大幅變動等之問題而無法安定地成膜。 由以上所述,確認比較例7之氧化物蒸鍍材並不適合 於成膜量產。 〔比較例8〕 另外,製造在日本特開2007-84881號公報(專利文獻 2 )所介紹的IT Ο氧化物蒸鍍材而進行同樣的評估。 -40- 201200610 亦即,使以Sn/In原子數比計成爲0·102的方式來將平 均粒徑爲1 μιη以下之氧化錫粉末摻入平均粒徑爲1 μπι以 下之氧化銦粉末中,且添加2質量%之醋酸乙烯系黏著 劑。於使用硬質Zr02球之濕式球磨機中,進行此等物質之 18小時混合、乾燥及粉碎之後,作成造粒粉末。進一步使 用此造粒物,以低溫靜水壓加壓施加94 MPa ( 3 to n/cm2 ) 之壓力而作成圓柱狀之成形體。 將所獲得之成形體置入燒結爐內,在以每0.1 m3之爐 內容積爲5公升/分鐘之比例導入氧而形成氣體環境,在 11 00 °C常壓燒結2小時。此時,以l°c/分鐘升溫,於燒結 後之冷卻時係停止氧導入,以10 °c/分鐘降溫在到1000 °c» 使用立式綜合加工機而將所獲得之燒結體加工成直徑 3 0 mm、厚度40 mm大小之圓柱狀,測定體積與重量而算 出密度。 燒結體之密度爲4.8 g/cm3。另外,燒結體之表面與內 部的顔色係同等,但測定其L *値後,顯示L *値較本發明 之規定範圍(54至75 )爲大的値(79 )»此係表示氧化物 蒸鍍材中之氧量非常的多。 使用進行如此方式所製造的氧化物蒸鍍材而與實施例 1至4同樣地實施成膜評估。 雖然成膜時之最適氧混合量與比較例2同樣地爲〇 %,但膜之比電阻較實施例5至8爲高。認爲此係由於從 氧化物蒸鍍材供應至膜之氧過多而使膜中之氧量多,無法 -41- 201200610 導入最適之氧短缺量。因而,確認即使使用如此之氧化物 蒸鍍材而成膜,也無法獲得發揮此蒸鍍材組成所本來具有 的高導電性之膜。 〔產業上利用之可能性〕 藉由採用有關本發明之氧化物蒸鍍材,由於能夠在可見 光區域顯示高的光透射性,同時也利用真空蒸鍍法而製造 顯示高的導電性之透明導電膜,故具有作爲用以形成各種 太陽能電池之透明電極的氧化物蒸鍍材而所利用的產業上 之利用可能性。 【圖式簡單說明】 te 〇 【主要元件符號說明】 無。 -42-201200610 VI. Description of the Invention: [Technical Field] The present invention relates to an oxide vapor deposition material vapor deposition method, an ion plating method, or a high-density plasma auxiliary air vapor deposition method for producing a transparent conductive film. The transparency produced by using this oxide vapor-deposited material is used to manufacture a transparent conductive material which is a high transmittance of a transparent electrode of a solar cell in the visible light region. [Prior Art] The transparent conductive film has high conductivity and transmittance. Moreover, in order to utilize this characteristic, the transparent solar cell, the liquid crystal display element, and other various anti-static films used in the near-infrared region for absorption into the window glass of automobiles or buildings, and the anti-fog of the refrigerated display cabinet, etc. Further, in the transparent conductive film, tin oxide (Sn02), which is generally a dopant of tin or fluorine as a dopant, is used as a dopant of zinc oxide (ΖηΟ); a dopant-containing indium oxide (?n203) or the like. In particular, a tin indium oxide film, i.e., an ln203-Sn film, is referred to as a film, and is widely used because it is easy to obtain a low-resistance transparent guide. - It is used for various kinds of oxide vapor deposition materials and conductive films which are used for electron beam-assisted vapor deposition, etc., for example, high-light-conducting film which is useful in low-resistance and which is used for display film evaporation in the visible light region. It is used for electrodes such as solar light-receiving elements, and can be used as a line-type reflective film or various heat-dissipating bodies. In general, it contains ITO (Indium Tin Oxide) electric film containing aluminum, gallium, indium, tin, tungsten, and titanium as dopants. So far, the industry has been 201200610 and these transparent conductive As a method of producing the film, a vacuum deposition method, a sputtering method, a method of applying a coating liquid for forming a transparent conductive layer, and the like are generally used. Among them, the vacuum vapor deposition method or the sputtering method is effective when a material having a low vapor pressure is used or when a precise film thickness control is necessary, and is industrially useful because it is very simple in operation. Further, when the vacuum distillation method and the sputtering method are compared, the vacuum distillation method can form a film at a high speed, and has excellent mass productivity. However, in general, the vacuum evaporation method is performed in a vacuum of about 1 〇 3 to 10 · 2 Pa, and after heating a solid or liquid of an evaporation source to be temporarily decomposed into gas molecules or atoms, the vacuum deposition method is again performed on the surface of the substrate. The method of condensing as a film. Further, the evaporation source is heated in various ways, and is generally a resistance heating method (RH method) or an electron beam heating method (EB method or electron beam evaporation method). In addition, a reactive steaming method in which a reaction gas such as helium gas is introduced into a film forming chamber (cavity) while performing vapor deposition is known. Further, in the case where an oxide film such as ITO is deposited, the electron beam evaporation method is often used in history. That is, once the ITO oxide evaporation material (also referred to as ITO ingot or ITO 9) is used for the evaporation source, the argon gas of the reaction gas is introduced into the film forming chamber (cavity), and the electric field is used to make the thermal electrons. When the hot electrons jumping out of the filament (mainly W wire) are accelerated and irradiated onto the ITO oxide steaming material, the irradiated portion becomes a local high temperature and evaporates and deposits on the substrate. Further, by using a thermal electron emitter or RF discharge to generate plasma, the plasma or the reaction gas (02 gas or the like) is activated by the plasma, and the activation reactivity of the low-resistance film can be produced on the low-temperature substrate. Steaming 201200610 Plating (ARE method) is also a method for film formation of ITO. In addition, the high-density plasma-assisted vapor deposition method (HDPE method) using a plasma gun has recently become a technique effective for IT film formation, and has been widely used in the industry (see Non-Patent Document 1: " Vacuum", Vol. 44, No. 4, 2001, p. 43 5-439). In this method, an arc discharge is maintained using a plasma generating device (plasma gun) to maintain an arc discharge between a cathode contained in the plasma gun and a crucible (anode) of the evaporation source. The electrons released from the cathode are guided by a magnetic field and concentrated to be irradiated to a portion of the ITO oxide evaporation material that is fed to the crucible. The evaporate evaporates and deposits on the substrate from the portion where the electron beam is irradiated to a local high temperature. Since the vaporized vapor or the introduced helium gas system is activated in the plasma, an IT diaphragm having good electrical characteristics can be produced. In addition, in another classification method of various vacuum evaporation methods, the ionization method associated with the vaporized material or the reaction gas is an ion shovel method (IP method) as an ITO film which obtains low resistance and high light transmittance. The method is effective (see Non-Patent Document 2: "Technology of Transparent Conductive Film", Ohm Corporation, 1999, pp. 205-211). However, regardless of the solar cell of any type used in the transparent conductive film, the transparent conductive film is indispensable on the electrode on the surface side irradiated with light, and it is conventional to use the above-mentioned IT ruthenium film or doped with aluminum, Gallium zinc oxide (ZnO) film. Further, in such a transparent conductive film, characteristics such as low resistance or high light transmittance of solar rays are sought. Further, the method for producing such a transparent conductive film is a vacuum vapor deposition method using the above-described ion plating method or high-density plasma assisted vapor deposition method. 201200610 The oxide evaporation material used in the vacuum vapor deposition method such as the electron beam evaporation method, the ion plating method, or the high-density plasma-assisted vapor deposition method uses a small size (for example, 'the diameter is 10 to 50 mm and the height is The sintered body of a cylindrical shape of about 10 to 50 mm has a limit in the amount of film that can be formed by using one oxide steaming material. In addition, when the amount of consumption of the oxide vapor-deposited material is increased and the amount of the remaining is small, the film formation is interrupted, the air is introduced into the film forming chamber in the vacuum, and the unused oxide film is exchanged, and the film is formed again. The necessity of vacuuming the room becomes the main cause of deterioration in productivity. In addition, a technique which is indispensable in the case of mass production of a transparent conductive film by a vacuum vapor deposition method such as an electron beam evaporation method, an ion plating method, or a high-density plasma-assisted vapor deposition method, and the above-mentioned oxide evaporation may be mentioned. An example of the continuous supply method of a plating material is described in Non-Patent Document 1. In this continuous supply method, the cylindrical oxide evaporation material is connected and stored inside the cylindrical cover, and the height of the sublimation surface is maintained constant, and the oxide evaporation is sequentially performed. The shovel is supplied continuously. Further, by the continuous supply method of the oxide vapor-evaporated material, mass production of the transparent conductive film by the vacuum evaporation method can be realized. In addition, a vapor-deposited material of ITO is described in Patent Document 1 (JP-A-H08-104978). In essence, it has been proposed that the In203-Sn02 system consists of indium, tin and oxygen, and the volume of one particle is 0. 01 to 0. 5 cm3 and a relative density of 55% or more. In addition, the bulk density when filling the container is 2. ITO evaporation material below 5 g/cm3. In addition, it is also described that the utilization efficiency of the IT 〇 film which can form a film and stabilized by electron beam evaporation by the electron beam evaporation is 80% or more, and it is not blocked in the supply machine. A vapor-deposited material is obtained which allows it to be continuously supplied. Further, a vapor deposition material composed of indium oxide and tin oxide is also described in Patent Document 2 (JP-A-2007-84881). The tantalum vapor deposition material described in Patent Document 2 has a density of 4. A cylindrical oxide sintered body of 9 g/cm3, a diameter of 30 mm, and a thickness of 40 mm is constructed, and it is described that it can be continuously supplied without being damaged in the supply machine. However, various conventional ITO vapor deposition materials (oxide steaming materials) described in the above-mentioned patent documents and the like are used, and various vacuum vapor deposition methods such as electron beam evaporation, ion plating, or high-density plasma-assisted vapor deposition are used. In the case of producing a transparent conductive film having low electrical resistance and high light transmittance, it is necessary to introduce a large amount of oxygen into the film forming vacuum chamber at the time of film formation (for example, refer to paragraph 0007 and paragraph 0108 of Patent Document 2). It is noted that the following problems mainly occur. First, the composition deviation between the transparent conductive film and the oxide evaporation material becomes large, and the composition design of the transparent conductive film becomes difficult. In general, when the amount of oxygen introduced into the film forming vacuum chamber is increased, the difference in composition between the transparent conductive film and the oxide vapor deposition material tends to be large. In the film formation mass production step, fluctuations in the amount of oxygen in the film formation vacuum chamber are also likely to occur. The influence of the film composition is likely to occur, which is caused by the variation in film characteristics. Further, in the reactive vapor deposition film formation using oxygen, when the amount of oxygen is increased, not only the density of the film is lowered, but also the adhesion of the film to the substrate is weakened, etc., the problem of 201200610. Since the energy disappears when the evaporated metal oxide is oxidized before reaching the substrate, once the proportion of oxidation becomes large, it becomes difficult to obtain a dense and high adhesion film to the substrate. Also, the surface is easily oxidized. When a transparent conductive film is formed on a substrate covered with a metal film or an organic film, when the amount of oxygen introduced into the film forming vacuum chamber is large, the surface of the substrate is oxidized before film formation, so that it is impossible to manufacture high performance. element. This tendency becomes more pronounced as the substrate temperature at the time of film formation is higher. For example, in the case of producing a solar cell to be energy-converted by injecting light from the surface opposite to the substrate, it is necessary to form a transparent conductive film on the PIN element formed using the metal thin film. In the film formation in which the amount of oxygen introduction is large, the element is easily damaged and it is impossible to manufacture a high-performance element. In the case where an organic thin film solar cell or an organic electroluminescence device of a top emission type is formed, the transparent conductive film is formed on the organic light-emitting layer. In the case where the amount of oxygen introduction is large, the organic light-emitting layer is oxidized. Damaged, unable to achieve high performance components. The present invention has been made in view of such a problem, and the subject thereof is to use indium oxide added with tin as a main component, and to provide a low resistance in the visible light region even if the amount of oxygen introduced during film formation is small. An oxide evaporation material having a high light transmittance transparent conductive film, which is a transparent conductive film produced by using the oxide evaporation material. In other words, the oxide evaporation material of the present invention is characterized in that indium oxide is used as a main component and is composed of a sintered body containing tin oxide, and the content of tin 201200610 is the number of atoms of Sn/In. Ratio 0. 001 to 0. The LM in the 614 color system is straight from 54 to 75. Further, in the case where indium oxide is used as a main component, the film is formed using an oxide film formed by an electron plating method or a high-density plasma-assisted vapor deposition method, and the content of tin is Sn. /In atom 0. 614. Moreover, since the oxide evaporation material of the present invention relating to 75 of the CIE 1 976 color system has the most suitable oxide evaporation material, even if it is introduced into the film forming vacuum chamber, low resistance and visibility can be produced by vacuum evaporation. The transparent transparent conductive film and the film-forming method can reduce the difference in composition between the film and the oxide evaporation material, and the film composition can be reduced, and the film composition can be reduced in mass production. Since the amount of oxygen introduced into the film forming vacuum chamber is small, it is possible to damage the substrate due to oxygen. In particular, it does not damage the substrate and can stabilize the high performance film of the solar cell. [Embodiment] [Best Mode for Carrying Out the Invention] Hereinafter, the oxide evaporation material of the present invention is added to the oxide evaporation material of the present invention in an embodiment of the present invention. Tin transparent conductive beam evaporation method, ionic crystallographic transparent derivative ratio meter. 001 to L * 値 is 5 4 to the amount of oxygen, and by using a small amount of oxygen, it is also possible to reduce the amount of oxygen in the high-permeability groove in the light region, and it is easy to obtain the change of the mesh or the characteristic, thereby being able to reduce The realization of high-performance manufacturing is useful for illustration. Indium is used as the main -10- to get more than 006 and 201200610 points, and the tin content is calculated by the Sn/In atomic ratio. 001 to 0. The composition of 614. Further, since the composition of the transparent conductive film obtained by the air vapor deposition method using the oxide evaporation material of the present invention is very close to the composition of the oxidized material, the composition of the oxide evaporated ammonium material also becomes indium oxide as the J component. And it is tin-containing only in terms of Sn/In atomic ratio. 001 to the ratio. The reason why tin is contained only in the above ratio is because the mobility of the film can be increased. The composition of the membrane, that is, the composition of the oxide-vaporized ore; the amount (in terms of the atomic ratio of Sn/In) is less than 0. In the case of 001, the effect of increasing the bulk concentration (that is, the effect of increasing the mobility) is small and the film of 1 is not available. In addition, if it exceeds 0. In the case of 614, the amount of tin in the film will be too large: the neutral impurity which is scattered when the electron is moved becomes large, and the low-resistance film which is affected by the decrease in the rate cannot be obtained. In order to exert a higher carrier concentration I, a better tin content to the low-resistance film is based on the Sn/In atomic ratio to 0. 163. Further, the film is a crystalline film. However, a transparent conductive film-based semiconductor containing indium oxide as a main component is required to provide a moderate oxygen shortage for high conductivity and high light transmittance. That is, the amount of oxygen in the membrane is large and! In the case where the amount is small, for example, even if a dopant is contained, it does not show that the conductivity '1 pair exhibits conductivity, and it is necessary to introduce oxygen deficiency into the film; if oxygen is scarce: the light absorption of visible light is increased to cause coloring. Because of the need for the optimal oxygen shortage in j. The oxygen in the film is supplied from the original vapor deposition material as well as the oxygen in the film vacuum chamber at the time of film formation. Moreover, if from oxides. Proportion with true evaporation Mainly 0. 6 14 Indium Tin Contains: Load, resistance, and move to 0. Type 040: and make, shortage:. Needle: too much film-oxygen [into i-plating material-11 - * 201200610 When the supply is small, it is necessary to increase the amount of oxygen introduced into the film-forming vacuum chamber, and increase the amount of introduction into the film-forming vacuum chamber. In the case of oxygen, the above problems will occur. Therefore, an oxide evaporation material having an optimum amount of oxygen will be useful. Further, the most important feature of the oxide vapor-deposited material of the present invention is specified by the L*値 of the CIE 1976 color system. Here, the CIE 1 976 color system is the color space recommended by CIE (International Commission on Illumination) in 1976. Since the color is represented by a coordinate on the equal color space composed of the luminance L* and the color indices a-, b*, it is also simply referred to as CIELAB. The L* of the display brightness is displayed in black when L* = 0, and the white diffused color is displayed when L+ = 100. In addition, a* is indicated by negative 値 for greenish green, with positive 不 for non-biased, b for negative 値 without blue, and for positive for yellow. Further, the surface of the sintered body of the oxide-evaporated material according to the present invention specified by L*値 of the CIE1976 color system is preferably the same as the color of the inside of the sintered body, but it is assumed that the outermost surface is different from the inside. In the case of the vapor deposition material, in the present invention, L*値 is determined for the inside of the sintered body. According to the experiment conducted by the inventors of the present invention, when the C 内部 inside the oxide steaming material is 54 to 75, even if the amount of oxygen introduced into the film forming vacuum chamber is small, both the high conductivity and the visible light region can be obtained. High transmittance transparent conductive film. In addition, the more white, the higher the L*値; conversely, the more black, the lower the L +値. Moreover, it is considered that the L*値 system of the oxide evaporation material has a correlation with the oxygen content in the oxide vaporized material, and it is considered that the larger the enthalpy, the more the oxygen content is -12-201200610; the smaller the L*値The less oxygen is contained. The inventors of the present invention changed the production conditions, and tried to use various kinds of L*値 oxide-deposited materials to produce a transparent conductive film by vacuum evaporation, and the larger the L*値, the more suitable oxygen amount to be introduced into the film formation. The smaller the amount of oxygen (in order to obtain a film having low resistance and high transparency). This is because the amount of oxygen supplied from the oxide steaming material itself becomes larger due to the oxide evaporation material having a larger L*値. Further, the more the amount of oxygen introduced, the greater the difference in composition between the display film and the oxide-vaporized material. Therefore, the larger the L*値, the smaller the composition difference becomes. Further, the oxide vapor deposition material of the present invention has conductivity, and the conductivity of the oxide evaporation material depends on the oxygen content, and also depends on the density, the crystal grain size, and the dopant efficiency of the ruthenium. Therefore, the conductivity of the oxide evaporation material does not correspond to 1 to 1 for the L# system. Further, the oxide evaporation material of the present invention containing indium oxide as a main component and containing tin is based on vacuum deposition, mainly in In203. The form of x and Sn02_x generates evaporating particles, and also reacts with oxygen in the chamber to absorb oxygen and form a film on the substrate. Further, the energy of the evaporating particles is a driving source for the movement of the substance when it reaches the substrate and is deposited on the substrate, contributing to the densification of the film and the adhesion to the substrate. Further, since the smaller the L#値 of the oxide evaporation material, the less oxygen in the oxide evaporation material, the oxygen shortage of the evaporated particles becomes large, and it is necessary to introduce a large amount of oxygen into the vacuum chamber to increase before reaching the substrate. The ratio of its oxidation reaction. However, since the evaporating particles consume energy due to oxidation during flight, it is difficult to obtain a film that is dense and has a high adhesion to the substrate in the reactive film introduced by the increase in oxygen. In the ground, it is easier to obtain a highly adherent and high-density film by reducing the reactive vapor-forming film of the introduced oxygen, and the oxide-steamed metal of the present invention can achieve the same. Here, when the L*値 is less than 54, the amount of oxygen in the oxide vapor deposition material is too small, and the optimum oxygen introduction amount for introducing the film into the vacuum chamber in order to obtain a film having low resistance and high transparency is increased. The difference in the composition of the film and the oxide evaporation material becomes large, and the problem that the damage to the substrate becomes large in the film formation also occurs, which is not preferable. On the other hand, when the amount of oxygen contained in the oxide vapor deposition material is too large, the amount of oxygen supplied from the oxide vapor deposition material to the film becomes excessive, and the optimum oxygen cannot be obtained. A shortage of highly conductive films. However, a sputter target of a tin-containing indium oxide sintered body is described in Japanese Laid-Open Patent Publication No. Hei. No. Hei. No. Hei. No. 5 - 1 1 2 8 66 (reference publication), which is incorporated herein by reference. The tin-containing indium oxide sintered body produced by the method of the invention has a lanthanum as low as 38 to 49 (see Comparative Example 3). Therefore, when such a sintered body is used as an oxide vapor deposition material, the amount of oxygen introduced into the film forming vacuum chamber for obtaining an optimum film must be increased; and the above problems occur, and the object of the present invention is not achieved. Here, the vapor-deposited oxide sintered body (oxide-evaporated material) of the present invention having an L*値 of 54 to 75 is not manufactured by a conventional technique for producing an ITO sintered body. An oxide evaporation material suitable for use in a moderate amount of oxygen (or oxygen shortage) which is mass-produced by a vacuum deposition method can be produced by the following method. In the case of the sintered body containing tin oxide as a main component, the sintered body containing tin can be used as a raw material of each powder of indium oxide and tin oxide, and these powders are mixed and molded to form a green compact, which is subjected to high temperature. It is produced by firing and sintering and sintering. The respective powders of indium oxide and tin oxide are not particularly preferable, and may be a raw material for an oxide sintered body which is conventionally used. Further, the average particle diameter of the powder used was 1. 5 μπι or less, preferably 〇. 1 to 1. 1 μηι. The mixing of the general raw material powder at the time of producing the above oxide sintered body is also effective in the case of producing the sintered body of the present invention by a ball mill mixing method. The ball mill is a device in which a hard ball (a spherical diameter of 10 to 30 mm) such as ceramics and a powder of a material are placed in a container to be rotated, and the material is also ground while being mixed to prepare a fine mixed powder. The ball mill (pulverized medium) is made of steel, stainless steel, nylon or the like as a can body, and is made of an aluminum oxide, a magnetic material, natural cerium oxide, rubber, a urethane or the like as a lining. The ball may be an alumina ball containing alumina as a main component, a natural vermiculite, a nylon ball in which an iron core is placed, an oxidized pin ball, or the like. The wet and dry pulverization methods are widely used for obtaining and pulverizing the raw material powder of the sintered body. In addition, the bead mill method or the jet mill method is also effective in methods other than ball mill mixing. In particular, since the tin oxide powder is a hard material, it is very effective in the case of using a large average particle diameter raw material or in a case where it is necessary to carry out pulverization and mixing in a short time. The so-called bead mill system will be 70 to 90% of the beads (grinding medium, bead diameter 0. 005 to 3 mm) is preliminarily filled in a container called Vessel, and the bead is operated by rotating the rotating shaft in the center of the container at a peripheral rotation speed of 7 to 15 m/sec. Here, a slurry in which the material to be pulverized, such as the raw material powder -15-201200610, is mixed into the liquid is supplied thereto by the pump, and the beads are impacted to be finely pulverized and dispersed. In the case of a bead mill, if it is combined with the pulverized material to reduce the diameter of the bead, the efficiency will increase. In general, bead mills are capable of micro-grinding and mixing at an acceleration close to one thousand times that of a ball mill. The bead mill thus constructed is referred to by various names, for example, a grinder, an hydrating machine (Aquamizer), an attritor, a pearl mill, an Abex mill, an ultra-viscer mill (Ultra vi sco mill). ), a DYNO mill, a stirring mill, a Coball mill, a Spike mill 'SC mill, etc., in the present invention, any of them can be used. In addition, the jet mill blows high-pressure air or steam injected before and after the sound speed from the nozzle as a super-high-speed jet to impact the pulverized material such as the raw material powder, and pulverizes into particles by the collision of the particles. The method. As described above, the indium oxide powder and the tin oxide powder are first poured into a can for a ball mill at a desired ratio, and dry or wet mixing is carried out to prepare a mixed powder. Then, in order to obtain the oxide sintered body of the present invention, the content of indium and tin is 0. 001 to 0. 614 way to modulate. An organic substance such as water, a dispersion material, or an adhesive is added to the mixed powder prepared in this manner to produce a slurry. The viscosity of the slurry is preferably from 150 to 5,000 cp, more preferably from 400 to 3,000 cP. The granulated powder can be obtained by using the slurry obtained in this manner and drying it by a spray dryer or the like. However, in order to obtain a sintered body having more uniformity and good sinterability, it is more effective when the pulverization and mixing treatment of 16 - 201200610 is carried out by the following bead mill. Namely, the obtained slurry and beads are placed in a container of a bead mill to carry out pulverization and mixing treatment. The beads may be zirconia, alumina or the like, but zirconia is preferred from the viewpoint of abrasion resistance. The diameter of the beads is preferably from 1 to 3 mm from the viewpoint of pulverization efficiency. The number of passes can be one, but it is preferably two or more, and a sufficient effect can be obtained five or less times. Further, the treatment time is preferably 10 hours or less, more preferably 4 to 8 hours. By performing such treatment, the pulverization and mixing of the indium oxide powder and the tin oxide powder in the slurry are good. Next, molding is carried out using the slurry treated in this manner. The molding method can be either a casting molding method or a pressure molding method. In the case of casting, the obtained slurry is cast into a molding mold to produce a molded body. The time from the treatment of the bead mill to the time of casting is preferably within 10 hours. Therefore, the slurry obtained by performing this method can prevent the display from being shaken. Further, in the case of press molding, an adhesive such as polyvinyl alcohol or the like is added to the obtained slurry, and if necessary, moisture is adjusted, and then dried by a spray dryer or the like to be granulated. The obtained granulated powder is filled in a mold of a predetermined size, and then, a press machine is used to 9. A pressure of 8 to 98 MPa (100 to 1000 kg/cm2) is subjected to uniaxial press forming to form a molded body. The thickness of the formed body at this time is considered to be the shrinkage caused by the subsequent firing step, and is preferably set to a thickness at which a sintered body of a predetermined size can be obtained. When the molded body produced from the above mixed powder is used, the oxide sintered body of the present invention can be obtained by a normal pressure sintering method at -17 to 201200610. Further, in the case where the oxide sintered body is obtained by firing by a normal pressure sintering method, the following method is employed. First, the obtained molded body is heated at a temperature of 300 to 500 ° C for about 5 to 20 hours to carry out a debonding treatment. Thereafter, the temperature is raised and sintered. However, in order to effectively release the internal bubble defects to the outside, the temperature increase rate is set to 150 ° C / hour or less, preferably set to! 〇 〇. (: / hour or less 'more preferably set to 80 ° C / hour or less. Sintering temperature is set to 丨丨 5 〇 to 1 300 ° C ' is preferably set to 1 2 0 0 to 1 2 5 0 ° C The sintering time is set to 1 to 20 hours, preferably set to 2 to 5 hours for sintering. The debonding treatment to the sintering step is important to be in every 0. The oxygen content of the furnace of 1 m3 is 5 liters/min or more and the oxygen is introduced into the furnace. The introduction of oxygen in the sintering step is carried out because the sintering system easily dissociates oxygen at 1150 ° C or higher and easily reaches an excessive reduction state, thereby preventing the dissociation. In this step, once the sintered body in which the oxygen shortage is excessively introduced is formed, it is then difficult to adjust the oxygen shortage amount of the sintered body to the optimum in the oxygen amount adjusting step. If the firing temperature exceeds the temperature of i3〇oc into fr, 'even in the oxygen environment as described above, 'the dissociation of oxygen will become frequent' and thus it becomes easy to reach an excessive reduction state.] For the same reason, it is not good. . Further, in the case where the firing temperature is 195 ° C, the sintering is insufficient because the temperature is too low, and it is not preferable to obtain a sintered body having sufficient strength. After the sintering, the oxygen amount adjusting step of the sintered body is performed. The oxygen amount adjustment step is important to carry out a heating time of 1 Torr or more at a temperature of 90 to 1 100 ° C', preferably 950 to 105 Ot: -18 - 201200610. The cooling system up to the heating temperature of the oxygen amount adjusting step is cooled while continuing the introduction of oxygen, and is 0. 1 to 20 ° c / min ' is preferably cooled at a cooling rate in the range of 2 to 1 〇〇 c / min." In the oxygen amount adjustment step of the sintered body, the control of the gas atmosphere in the furnace is also particularly important 'introduction into the furnace The gas is important to control the mixing ratio (volume ratio) of oxygen to argon in the range of 〇2/Ar = 40/6 0 to 90/1 0, in each 〇. The inner volume of the furnace is introduced into the furnace at a ratio of 5 liters/min or more. By precisely adjusting such temperature and gas atmosphere and time, it is possible to obtain a sintered body having the L* 规定 defined by the present invention when used as an oxide vapor deposition material. In the case where the heating temperature of the oxygen amount adjusting step is lower than 900 ° C, the reaction of dissociation and adsorption of oxygen is slow, and it is not preferable until the reduction treatment inside the sintered body takes time; if it exceeds 1100 ° C When the temperature is carried out, the dissociation of oxygen will be excessively intense, and the optimum reduction treatment due to the gas environment is not preferable. Further, if the heating time of the oxygen amount adjusting step is less than 1 hr, it is not preferable because the uniform reduction treatment in the sintered body portion is not performed. Further, when the mixing ratio (〇2/Ar) of the gas introduced into the furnace is less than 40/60, the reduction by the dissociation of oxygen becomes an excessive advantage, and thus it becomes a sintered body having an L*値 lower than 54. Not good. On the contrary, if the mixing ratio (〇2/Ar) of the gas introduced into the furnace exceeds 90/10, the oxidation becomes an excessive advantage, and thus it becomes a poor sintered body of more than 75 Å. -19-201200610 In order to obtain the oxide evaporation material of the present invention, as described above, it is important to perform annealing in a gas atmosphere in which oxygen is precisely diluted by using argon gas, that is, in a gas atmosphere in which the oxygen amount is precisely controlled. For the treatment, the ambient gas is not necessarily required to be a mixed gas of oxygen and argon. For example, it is effective to use an inert gas such as helium or nitrogen instead of argon. Further, even in the case where air is used instead of argon, it is effective to precisely control the oxygen content in the entire mixed gas. However, as in the conventional technique, it is generally not effective to introduce oxygen into a furnace which is fired by air because the oxygen content of the gas atmosphere in the furnace cannot be precisely controlled. According to the mode proposed by the present invention, the furnace vapor-filled material having the optimum reduction state can be obtained by introducing a mixed gas of an inert gas having a ratio of oxygen contained in a precise control. Further, after the completion of the oxygen amount adjustment step, it can be taken out from the furnace at room temperature at a temperature of 1 (TC / min to room temperature). The obtained sintered body can be processed to be oxidized by dicing into a predetermined size or the like. In addition, the shrinkage ratio of the sintering is also considered. When a molded body having a predetermined size after firing is used, it can be used as an oxide vapor-deposited material without performing honing processing after sintering. However, it is known that a method of producing a sputtering target is effective as a hot press method for obtaining a high-density sintered body. However, when a hot press method is applied to the material of the present invention, only L*値 is obtained. It is an over-reducing sintered body of 40 or less. The object of the present invention cannot be achieved in such a sintered body. -20- 201200610 Further, for the oxide-evaporated material of the present invention, for example, a diameter of 10 to 50 mm is used. It is also possible to use a cylindrical ingot or a nine-shaped shape having a height of 10 to 50 mm, and it is possible to use a particle shape of about 1 to 1 〇 mm which pulverizes such a sintered body. The vapor deposition material, other elements other than indium, tin, and oxygen may contain, for example, tungsten, molybdenum, zinc, cadmium, tellurium, or the like, and are allowed to be present without impairing the characteristics of the present invention, but among metal ions, When the vapor pressure of the oxide is extremely high as compared with the vapor pressure of indium oxide or tin oxide, it is difficult to evaporate by various vacuum vapor deposition methods, and it is preferably not contained. Or tin oxide as a comparison, for example, metals such as aluminum, titanium, and antimony, because the vapor pressure of these oxides is extremely high, so that it is contained in the oxide evaporation material, so that indium oxide or tin oxide is evaporated together. Therefore, it is difficult to contain it because it remains in the oxide evaporation material and is highly concentrated, and it is not allowed to be contained because it adversely affects the evaporation of indium oxide and tin oxide. When the transparent conductive film is produced by various vacuum deposition methods, the oxygen content in the oxide vapor deposition material is optimally adjusted, and even if the amount of oxygen introduced into the film formation vacuum chamber is small, the maximum amount can be obtained. The transparent conductive film is in short supply of oxygen. Therefore, the difference in composition between the transparent conductive film and the oxide evaporation material is small, and it is also difficult to be affected by the characteristic deviation caused by the variation of the oxygen introduction amount. (2) Transparent conductive The film is made of an oxide evaporation material according to the present invention, which is composed of indium oxide as a main component of -21 to 201200610 and is composed of a sintered body containing tin, and the content of tin is 0 in terms of atomic ratio of Sn/In. 001 to 0. 614 and in the CIE 1976 color system, the r 値 is 54 to 75, and the tin-containing indium oxide crystal film can be produced by various vacuum evaporation methods such as electron beam evaporation, ion plating, or high-density plasma-assisted vapor deposition. (Transparent conductive film). When a crystal film is formed and tin is dissolved in the indium oxide indium position, a high mobility can be exhibited. The crystal film (transparent conductive film) can also be obtained by heating the substrate in the film formation to 180 ° C or higher; but it can also be used at 180 ° C or higher to obtain a film by heating or non-heating. Obtained by the method of film annealing. Got it. Further, the crystalline transparent conductive film of the present invention can be produced from an oxide evaporation material having a small difference in composition between the film and the oxide evaporation material, and contains 0 atomic ratio of Sn/In. 001 to 0. 614 tin indium oxide film. If the tin content of the film (in terms of Sn/Iri atomic ratio) is less than 0. In the case of 001, the effect of increasing the carrier concentration (i.e., the effect of increasing the mobility) is small and a low-resistance film cannot be obtained. In addition, if it exceeds 0. At 614, the amount of tin in the film is too large, and the neutral impurity which is scattered when the electrons move becomes large, and a low-resistance film which is affected by the decrease in the mobility is not obtained. In order to further obtain a transparent conductive film having a high carrier concentration, a more preferable tin content is 〇· 〇 40 to 0 in terms of the atomic ratio of Sn/In. The 1 6 3 ' film is a crystalline film. By obtaining a crystal film of such a composition range, The transparent conductive film can be realized as follows: the carrier concentration is 7. 2x1 〇20 cm — 3 or more, and the specific resistance is 3. 5xl〇_4Qcm or less. Further, the transparent conductive film of the present invention has a very high average transmittance of 90% or more in the film itself having a wavelength of 400 to 800 nm, which is 90% or more. Hereinafter, the embodiment of the present invention will be specifically described. [Examples 1 to 4] [Production of Oxide Steamed Material] The average particle diameter was 0. 8 μιη Ιη203 powder and Sn02 powder having an average particle diameter of 1 μπι as a raw material powder, and the atomic ratio of S n / In becomes 0. The Ι203 powder and the Sn02 powder were blended in a ratio of 048, placed in a resin can, and mixed by a wet ball mill. At this time, a hard Zr02 ball was used, and the mixing time was set to 20 hours. After mixing, the slurry is taken out, and an adhesive of polyvinyl alcohol is added to the obtained slurry, and dried by a spray dryer or the like to be granulated. Using this granulated product, a uniaxial compression molding was carried out at a pressure of 98 MPa (1 ton/cm2) to obtain a cylindrical molded body having a diameter of 30 mm and a thickness of 40 mm. Next, the obtained molded body was sintered in the following manner. That is, in the air in the sintering furnace, it is heated at a temperature of 300 ° C for about 1 hour to carry out the debonding treatment of the molded body, and then every 0. The gas atmosphere in which the internal volume of the furnace of 1 m3 is 5 liters/min or more and introduced with oxygen is heated at a rate of 1 °C/min and sintered at 1250 °C for 2 hours (normal pressure sintering method). At this time, in the case of cooling after sintering, oxygen is introduced, and the temperature is lowered by 1 (TC/min to l〇〇〇t:. Then, the introduced gas is switched to a mixed gas of oxygen and argon at 1000 °C. While heating is maintained for 15 hours (hereinafter, this step is referred to as a sintered body oxygen amount adjustment-23-201200610 step), the temperature is lowered to room temperature at 1 〇t / minute. Moreover, by making the mixed gas oxygen and argon The mixing ratio of the mixture is changed to obtain various oxide sintered bodies (oxide vapor deposition materials) of L*値. That is, the oxide evaporation material of the first embodiment is in an oxygen/argon flow ratio (that is, The volume ratio) was produced under the conditions of "40/60", and the oxide vapor deposition material of Example 2 was produced under the condition that the volume ratio was "60/40", and the oxide of Example 3 was steamed. The plating material was produced under the condition that the volume ratio was "80/200", and the oxide vapor-deposited material of Example 4 was produced under the condition that the volume ratio was "90/10". Yes, the volume and weight of the obtained oxide sintered body (oxide evaporation material) are measured. After the density, it is 4. 8 to 5. 7 g/cm3. Further, from the observation by a scanning electron microscope based on the fracture surface of the oxide sintered body, the average 値 of any one of the crystal grain sizes in the oxide sintered body was determined to be 3 to 10 μm. In addition, for the electron beam irradiation surface of the oxide sintered body, the four-terminal probe method resistivity is utilized. The specific resistance was calculated to be 1 kD cm or less by measuring the surface resistance. Further, after analyzing the composition of all the oxide sintered bodies by ICP luminescence analysis, it was found that the composition was present. Further, the surface of the sintered body and the inside of the sintered body were measured by a color difference meter (Specrto Guide, E-6834, manufactured by BYK-Garadner GmbH, Inc.), and L*値 in the CiEi 9 7 6 color system was measured to show almost the same flaw. The oxygen/argon flow ratio (i.e., volume ratio) of the mixed gas introduced in the sintered body oxygen amount adjusting step, and the obtained oxide sintered body-24-201200610 (oxide vapor-deposited material) L +値 is shown in Table 1(a), Table 1 (b) and Table 1 (c) below. Table 1 (a) Sn/In atomic ratio of oxide evaporation material 02/Ar flow ratio in the oxygen content adjustment step of the sintered oxide 1/値 of the oxide evaporation material The optimum oxygen mixing amount Example 1 0. 048 40/60 54 9 Example 2 0. 048 60/40 62 8 Example 3 0. 048 80/20 70 5 Example 4 0. 048 90/10 75 2 Comparative Example 1 0. 048 30/70 49 15 Comparative Example 2 0. 048 100/0 79 0 Comparative Example 3 0. 048 — 38 42 Example 5 0. 102 40/60 55 8 Example 6 0. 102 60/40 61 7 Example 7 0. 102 80/20 69 4 Example 8 0. 102 90/10 73 3 Comparative Example 4 0. 102 30/70 50 15 Comparative Example 5 0. 102 100/0 82 0 Comparative Example 6 0. 102 — 49 42 Example 9 0. 001 60/40 67 7 Example 1〇 0. 009 60/40 65 7 Example 11 0. 028 60/40 63 6 Example 12 0. 163 60/40 60 6 Example 13 0. 230 60/40 61 5 Example 14 0. 614 60/40 62 5 Comparative Example 7 0. 102 — 49 42 Comparative Example 8 0. 102 100/0 79 0 -25- 201200610 Table 1 (b) Membrane characteristics specific resistance (μΩοιη) in the optimum oxygen mixture. Carrier concentration (cm'3) Hole mobility (cm2/V s ) Visible light region of the film itself Transmittance (%) Example 1 150 1. 19χ1021 35 90 Example 2 150 1. 3〇χ1021 32 90 Example 3 150 1. 26x1021 33 90 Example 4 150 1. 13χ1021 37 90 Comparative Example 1 190 9. 14x1ο20 36 90 Comparative Example 2 230 7. 76χ1020 35 90 Comparative Example 3 210 8. 04x1020 37 90 Example 5 180 1. 24χ1021 28 90 Example 6 180 1. 29χ1021 27 90 Example 7 180 1. 24x1021 28 90 Example 8 180 1. 34χ1021 26. 90 Comparative Example 4 210 1. 06χ1021 28 90 Comparative Example 5 310 7. 75χ1020 26 90 Comparative example ό 220 1. 14χ1021 25 90 Example 9 750 1. 52χ1020 55 90 Example 10 675 1. 82χ1020 51 90 Example 11 470 2. 96χ1020 45 90 Example 12 350 7·14χ1020 25 90 Example 13 520 5. 72χ1020 21 90 Example 14 780 4. 71 χΙΟ20 17 90 Comparative Example 7 220 8. 12Χ1020 35 90 Comparative Example 8 220 9·8〇χ1020 29 90 -26- 201200610 Table 1 (c) Sn/In atom of the crystalline film of the cracked film of the film-specific oxide evaporation material in the optimum oxygen mixture amount Adhesion of the film to the substrate Example 1 Crystal film '0. 048 Strong Uncleared Example 2 Crystalline film 0. 048 Strong Uncleared Example 3 Crystalline film 0. 048 Strong Uncleared Example 4 Crystalline film 0. 048 Strong Uncleared Comparative Example 1 Crystalline film 0. 075 weak uncleared comparative example 2 crystalline film 0. 048 Strong Uncleared Comparative Example 3 Crystalline film 0. 095 weak cracking Example 5 crystalline film 0. 102 strong uncleared Example ό Crystalline film 0. 102 strong uncleared Example 7 crystalline film 0. 102 strong uncleared Example 8 crystalline film 0. 102 strong uncleared comparative example 4 crystalline film 0. 122 weak uncleared comparative example 5 crystalline film 0. 102 strong uncleared comparative example 6 crystalline film 0. 118 weak cracking Example 9 crystalline film 0. 001 Strong Uncleared Example 10 Crystalline film 0. 009 Strong Uncleared Example 11 Crystalline film 0. 028 Strong Uncleared Example 12 Crystalline film 0. 163 strong uncleared Example 13 crystalline film 0. 230 strong uncleared Example 14 crystalline film 0. 614 strong uncleared comparative example 7 crystalline film 0. 114 weak cracking Comparative Example 8 Crystal film 0. 102 Strong uncleared [Production of transparent conductive film and film property evaluation, film formation evaluation] (1) A magnetic field bias type electron beam evaporation device is used for the production of a transparent conductive film. The vacuum exhaust system consists of a low vacuum exhaust system caused by a rotary pump and a high vacuum exhaust system caused by a cryopump, which can be exhausted up to 5 X 1 (Γ5 Pa. The electron beam is heated by the filament The generation is accelerated by an electric field applied between the cathode and the anode, and is bent in a magnetic field of a permanent magnet, and then irradiated to an oxide evaporation material provided in a crucible made of tungsten. -27-201200610 The voltage can be adjusted by changing the voltage applied to the filament. When the acceleration voltage between the cathode and the anode is changed, the irradiation position of the electron beam can be changed. The film formation is carried out under the following conditions. 02 gas is introduced into the vacuum chamber to maintain the pressure at 1. 5x10 · 2 Pa. At this time, the characteristics of the transparent conductive film obtained by changing the mixing ratio of the Ar gas and the 02 gas introduced into the vacuum chamber were evaluated. The cylindrical oxide steaming materials of Examples 1 to 4 were placed upright in a crucible made of tungsten, and the electron beam was irradiated onto the central portion of the circular surface of the oxide evaporation material at a thickness of 1. A transparent film with a thickness of 200 nm was formed on a 1 mm Corning 705 9 glass substrate. Set the voltage setting of the gun to 9 kV, the current 値 to 150 mA, and the substrate heating to 250 °C. (2) The characteristics of the obtained film (transparent conductive film) were evaluated in the following order. First, the surface resistance of the film (transparent conductive film) was measured by a four-terminal probe method resistivity meter Loresta EP (manufactured by DIA Instruments, Inc., MCP-T3 60 type), and the film thickness of the film (transparent conductive film) was contacted. The surface roughness meter (manufactured by Tencor) was evaluated by measuring the difference between the film formation portion and the film formation portion, and the "specific resistance (μΩ cm)" was calculated. Further, using a hole effect measuring device (ResiTest manufactured by TOYO CORPORATION), the "carrier concentration (cm·3)" and "hole mobility (cm2) of the film obtained by the van der Pauw method at room temperature at room temperature. /vs)". Then, the rate (TL + b (%)) of the film containing the glass substrate (glass substrate B with film L) was measured by a spectrophotometer (U-4000, manufactured by Hitachi, Ltd.) -28-201200610, and the same was used. In the method, the transmittance of the film itself was calculated from the transmittance (TB (%)) of the measured glass plate (glass substrate B) by [TL + B + TB (%)]. Further, the crystallinity of the film was evaluated by X-ray diffraction measurement. In the diffraction apparatus, X 'Pert PROMPD was used (the measurement conditions by PANalytical Co., Ltd. were measured by wide-area measurement, and the CuKa line was used, and the measurement was performed using a voltage of 45 mA at 40 mA. The crystallinity was evaluated by the presence or absence of the X-ray diffraction peak. The results are also shown in "crystallinity of the film in Table 1 (c). Next, the composition of the film (in terms of the atomic ratio of Sn/In) is measured by luminescence analysis. Further, the adhesion of the film to the substrate is based on Evaluation of C002 1. Evaluation of the absence of film peeling is considered good (strong film peeling is considered insufficient (weak). The results of these are also shown in Table 1 (c) "by Sn/In In the respective columns of the atomic ratio and the film-to-substrate adhesion, the specific resistance and transmittance of each film (transparent conductive film) are based on the mixing ratio of Ar gas and 02 gas introduced into the film forming vacuum chamber. The mixing ratio of 丨 gas [〇2/ ( Ar + 02 ) ( % )] is changed from 50% per 1%, and the mixing ratio of 〇2 gas showing the lowest specific resistance is determined by the optimum oxygen mixing amount. This result is shown in the column of “oxygen blending amount” in Table 1 (a). A film prepared by mixing a small amount of oxygen (transmission glass base X 1 00 X line [) 'kV, estimated film column ICP JIS 丨), the film forming tower of the display panel 2 〇 to the optimum transparent -29- 201200610 Conductive film) is not only poor in conductivity but also low in transmittance in the visible light region. The film (transparent conductive film) produced by the optimum oxygen mixing amount is not only excellent in conductivity but also high in transmittance in the visible light region. (3) Using the oxygen-evaporated material of Examples 1 to 4, the optimum oxygen mixing amount at the time of performing the film formation evaluation described above, and the specific resistance of the film at this time, in the visible light region (wavelength 400 to 800 nm) The average transmittance of the film itself. The results of the evaluations are shown in Table 1 (b), "Specific Resistance (μη (:η〇) and "Transmittance (%) of the visible light region of the film itself"" in the use of Examples 1 to 4 In the case of film formation of an oxide evaporation material, in order to obtain a transparent conductive film having the lowest resistance and high transparency, the optimum oxygen mixing amount to be introduced into the film forming vacuum chamber is extremely small. This is because each oxide evaporation material contains In addition, the film system produced in the optimum oxygen mixture amount is the same as the composition of the oxide steamed material, and exhibits not only a very low specific resistance but also a high transmittance in the visible light region. The film was confirmed to be an indium oxide crystal film of a buckhamite type structure, and the adhesion to the substrate was strong enough to be practical. Further, the set voltage of the electron gun was 9 kV, and the current enthalpy was set to 150 mA. After the beam was irradiated for 60 minutes, the oxide evaporation material was visually observed for cracking or cracking in the oxide steaming material (the oxide evaporation material durability test). The oxide evaporation materials of Examples 1 to 4 were continuously used. Also not produced Rift ("Evaluation of Uncracked"). Such a transparent conductive film is very useful as a transparent electrode for a solar cell, -30-201200610. [Comparative Examples 1 to 2] In Examples 1 to 4, only the change was made. In the sintered body oxygen amount adjusting step, the mixing ratio of the introduced gas was used to produce an oxide sintered body. That is, in Comparative Example 1, the 02/Ar flow ratio was set to 30/70; in Comparative Example 2, The obtained sintered body was evaluated for density, specific resistance, crystal grain size, and composition in the same manner as in Examples 1 to 4. The surface and internal color of the obtained oxide sintered body were obtained. The results were the same, but after measuring L*値, the results are shown in Table 1 (a). Next, film formation evaluation was carried out in the same manner as in Examples 1 to 4. The results are also shown in Tables 1(a) to (c) above. Comparative Example 1 has the following features: an oxide evaporation material showing 値(49) which is smaller than the specified range (54 to 75) of the present invention; and oxidation with Examples 1 to 4. For comparison, the optimum oxygen mixing amount at the time of film formation is (1 5 ). Compared with Examples 1 to 4 The film properties of the optimum oxygen mixture amount are the same, but the specific resistance is somewhat higher. It is considered that the main cause is that the composition of the film is largely shifted. Furthermore, compared with Examples 1 to 4, comparison is made. The film system of Example 1 has a weaker adhesion to the substrate. It is considered that this is caused by a slight introduction of oxygen film formation at the time of film formation. Due to such an oxide-vaporized material, the obtained film composition is highly biased. It is difficult to design the film composition. In addition, since it is necessary to introduce oxygen slightly into the film forming vacuum chamber, once it is used in the mass production step of the film formation, the composition or characteristics are changed by the influence of the oxygen concentration fluctuation in the vacuum chamber. Therefore, it was confirmed that the oxide evaporation material of Comparative Example 1 201200610 is not suitable for film formation mass production. Further, Comparative Example 2 is an example of an oxide vapor-deposited material of 値(79) which is L*値 is more preferable than the present invention. The maximum amount of film formation was 〇%, and the specific resistance of the film was higher than that of Examples 1 to 4. Since the amount of oxygen supplied from the oxide-vaporized ammonium material to the membrane is too large, a large amount of membranes can be introduced, and an optimum oxygen shortage amount can be introduced. Therefore, it has been confirmed that even if the oxide deposited material is formed into a film, a film having high conductivity which is originally possessed by the vapor deposited material cannot be obtained. [Comparative Example 3] Next, a tin-containing sintered body was produced in accordance with the technique for producing a sintered body of a sputtering target described in Japanese Patent Publication No. Hei 5-112866. First, In2〇 having an average particle diameter of 1 μm or less was used. (3) Sn02 powder having a powder diameter of 1 μm or less is used as a raw material powder, and I n2 〇3 powder and final powder are blended in a ratio of 子_〇4 8 in a subratio to be placed in a resin can. The ball mill was mixed with a hard Z r Ο 2 ball, and the mixing time was set to 20 hours. The slurry was mixed, filtered, dried, and then granulated. Then, using the obtained granulated powder, 1 96 t ο n / was applied. The pressure of c m2 ) was applied by pressurization under a low temperature hydrostatic pressure, and the obtained molded body was placed in a sintering furnace and allowed to stand in air for 5 hours. The obtained sintered body was processed to have a diameter of 30 mm and a thickness range of a large oxygen mixture. 3 The amount of oxygen in this system was used. The composition was used to perform indium oxide and the average particle Sn/In original I Sn02 ί. At this time, after the combination, take MPa (2, further 1 520 ° C burn 40 mm large -32- 201200610 small cylindrical shape. The density of the sintered body is 6. 0 g/cm3, and the specific resistance is m Ω c m. Further, the crystal grain size is from 1 2 to 15 μm, and the composition is approximately the same as the composition. The surface of the obtained sintered body and the color of the inside, etc., but after measuring L * ' 'as shown in Table 1 ( a ), is extremely low 値 (: This means that the amount of oxygen in the oxide evaporation material is very high Next, film formation evaluation was carried out in the same manner as in Examples 1 to 4. The results are also shown in the above Tables 1 (a) to (c). Comparative Example 3 shows that L + 値 is within the prescribed range of the present invention ( 5 4 3 is obviously small 値 (3 8 ). Compared with the vapor-deposited materials of Examples 1 to 4 of the same composition, the optimum oxygen mixing amount at the time of film formation is (42) often. A comparison of 1 to 4 shows that the transmittance of the optimum oxygen mixing amount is the same, but the specific resistance is high. It is considered that the composition is mainly such that the composition of the film is shifted. Further, the film of the comparative example 3 is on the substrate. The strength is weaker than those of Examples 1 to 4. It is considered that this is caused by film formation with a slight introduction of oxygen at the time of film formation, and it is difficult to design a film composition because the composition obtained by the oxide evaporation material system is large. Since it is necessary to introduce oxygen into the film forming vacuum tank, once the mass production step of the film formation is used, the oxygen concentration in the vacuum tank is changed. The composition or the characteristic was increased by the ringing. Further, after the durability test of the vapor deposition material was carried out under the same conditions as in Examples 1 to 4, the oxide vaporized material was cracked after the continuous film formation ("cracking" "Evaluation". When continuous film formation is carried out using such a crack-forming vapor deposition material, a problem such as a large film formation rate is caused, and film formation cannot be stably performed. 6 The material group is the same as I 8 b 75 ) Oxidation, when the membrane gas of the membrane is slightly different, the oxygen in the oxidation oxidation is changed -33 - 201200610 Therefore, it is confirmed that the oxide evaporation material of Comparative Example 3 is not suitable. Mass production in film formation. [Examples 5 to 8] When the Ιη203 powder and the 311〇2 powder were blended, the ratio of the Sn/In atomic ratio was set to be 0. In addition to the ratio of 102, the oxide sintered bodies (oxide-steamed materials) of Examples 5 to 8 were produced under the same conditions as those of Examples 1 to 4 under the conditions of adjusting the amount of oxygen in the sintered body. That is, the oxide evaporation material of Example 5 was produced under the condition that the oxygen/argon flow ratio (i.e., volume ratio) was "40/60", and the oxide evaporation material of Example 6 was used. It is produced under the condition that the volume ratio is "60/40", and the oxide evaporation material of the seventh embodiment is produced under the condition that the volume ratio is 280/20", and the related embodiment 8 is The oxide evaporation material was produced under the condition that the volume ratio was 90/10/10. Then, with respect to the obtained oxide sintered bodies (oxide vapor-deposited materials) of Examples 5 to 8, the density, the specific resistance, the crystal grain size, and the composition were evaluated in the same manner, and any one of them was the same as Examples 1 to 4. Equivalent. Further, the surface of the obtained oxide sintered body was equivalent to the color inside. The results of measuring L + 値 are shown in Table 1 (a) above. Further, film formation evaluation was carried out in the same manner as in Examples 1 to 4. The results are also shown in Tables 1 (a) to (c) above. In the film formation using the oxide vapor-deposited materials of Examples 5 to 8, the optimum oxygen mixing amount to be introduced into the film forming vacuum chamber in order to obtain the transparent conductive film having the lowest electrical resistance and high transmittance is the same as in Examples 1 to 4. Very little land. -34- 201200610 This is due to the optimum oxygen content in the oxide steamed material. Further, the film system produced by the optimum oxygen mixing amount showed the same composition as the oxide vapor deposition material, and showed not only a very low specific resistance but also a high transmittance even in the visible light region. Further, all the film systems are crystal films of a perovskite-type crystal structure of indium oxide, and the adhesion of the film to the substrate is also strong enough to be practical. Further, even if the oxide evaporation materials of Examples 5 to 8 were continuously used, cracks did not occur. Such a transparent conductive film is very useful as a transparent electrode for a solar cell. [Comparative Examples 4 to 5] In Comparative Examples 1 to 2, except that the Sn/In atomic ratio was made to 0 when the In2〇3 powder and the Sn02 powder were blended. An oxide steamed material was produced under the same conditions as in Comparative Examples 1 to 2 except for 102. That is, in Comparative Example 4, the condition for adjusting the oxygen content of the sintered body was 〇2/Ar flow ratio was set to 3 0/70; and in Comparative Example 5, it was set to 100/0. The density, specific resistance, crystal grain size, and composition of the obtained sintered body were evaluated in the same manner as in Examples 5 to 8. Further, the surface of the obtained oxide sintered body was equivalent to the color inside. After measuring L*値, it is shown as Table 1 (a). Next, film formation evaluation was performed in the same manner as in Examples 1 to 4. The results are also shown in Tables 1 (a) to (c). Comparative Example 4 shows an oxide-vaporized ore material having a smaller 値(50) than L*値 in the specified range (54 to 75) of the present invention, and a case where the oxide-deposited materials of Examples 5 to 8 were used. In comparison, the optimum oxygen content during film formation is as high as -35 - 201200610 (15). In comparison with Examples 5 to 8, the transmittance is approximately the same at optimum characteristics, but slightly higher than the resistance. Due to the large compositional shift of the film, the film contains excess tin. The film of 4, the adhesion to the substrate was larger than that of Examples 5 to 8 due to the large compositional shift and low adhesion due to the formation of oxygen. The composition of the film obtained is biased due to the composition of the film. In addition, since oxygen must be slightly introduced, once it is used in the mass production step of film formation, it is significantly affected by the change in the degree of truth, and the composition is confirmed to be easily formed. Therefore, the oxide evaporation material of Comparative Example 4 was confirmed. In addition, Comparative Example 5 shows an example in which L*値 is an oxide vapor-deposited material of ruthenium (82) of the present invention. The amount of film formation was 〇%, but the specific resistance of the film was higher than that of Examples 5 to 8 due to the excessive supply of oxygen from the oxide evaporation material to the film, and the optimum oxygen shortage amount could not be introduced. Therefore, it was confirmed that the oxide-vaporized ore material was formed into a film, and a film having high conductivity which is exhibited by the composition itself was not obtained. [Comparative Example 6] In Comparative Example 3, the ratio of the Sn/In atomic ratio was set to 0 in addition to the blending of In2〇3 powder 5. An oxide vapor deposition material was produced under the same conditions except for 102. The density, specific resistance, crystal grain size, and composition 3 were evaluated in the same manner as obtained. Further, the film of the surface of the obtained sintered body and the amount of oxygen mixed was considered to be the reason, and the comparative example was weak. In such a film, it is slightly larger and it is difficult to set the fluctuation of the oxygen concentration characteristic in the film forming vacuum chamber. t is mass produced in film formation. The specified range is a large optimum oxygen mix. It is considered that the amount of oxygen in the film is the same as that of the Sn02 powder and the sintered body obtained in Comparative Example 3, but it is equivalent to the color system of the comparative example-36-201200610, but it is measured. After L *値, it is displayed as shown in Table 1 (a). Next, film formation evaluation was performed in the same manner as in Examples 1 to 4. The results are also shown in Tables 1 (a) to (c). Comparative Example 6 also shows that L*値 is smaller than the specified range of the present invention (54 3 is a small enthalpy (49). Compared with the oxidized plating materials of Examples 5 to 8 of the same composition, the optimum oxygen mixing amount at the time of film formation It is (42), not much. The transmittance of the film characteristics of the optimum oxygen mixing amount is the same as that of the examples 5 to 8 of the oxide evaporation material of the same composition, but compared with the implementation to 8 The specific resistance is high. It is considered that the main cause is that the composition shift is large. Furthermore, the adhesion of the film system of Comparative Example 6 to the substrate is weaker in Examples 5 to 8. It is considered that this is due to a slight increase in film formation. Since the film composition is greatly different in composition, it is difficult to design a film composition in such an oxygen evaporation material. In addition, since oxygen must be slightly introduced into the film vacuum chamber, once the film is formed, In the production step, the composition or the characteristic is increased by the influence of the fluctuation of the oxygen concentration in the vacuum chamber, and the oxygen vapor deposition material endurance test is carried out under the same conditions as in the first to fourth embodiments. Crack in the oxide evaporation material after the film ("evaluation of the crack"). If used When a vapor deposition material having a crack is formed and continuous film formation is performed, a problem that the film formation rate is largely changed and film formation cannot be stably formed. From the above, it was confirmed that the oxide evaporation material of Comparative Example 6 was not formed into a film. [Examples 9 to 14] 75) The product is usually steamed: compared with the case where the membrane is more solid than the oxygen, and the oxidative activity is affected by the change of the material. -37-201200610 In addition to the reconciliation of Iri2〇 3 The blending ratio of the powder to the Sn02 powder 'is 〇 in the atomic ratio of S n /1 η . 〇 〇〗 (Example 9), 〇. 〇 〇 9 (Example 1 〇), 0. 〇 2 8 (Example 1 1 ), 〇 ” 6 3 (Example 1 2 ), 0. 230 (Example 13) and 0. In the manner of 614 (Example 14), the oxidation of Examples 9 to 14 was carried out under the same conditions as in Example 2 (that is, the oxygen/argon flow ratio was "60/40"). Sintered body (oxide evaporation material). Then, the density, specific resistance, crystal grain size, and composition of the obtained oxide sintered bodies (oxygen vapor-deposited materials) of Examples 9 to 14 were evaluated in the same manner as in Example 2. Further, the surface of the obtained oxide sintered body was equivalent to the color inside. The results of measuring L*値 are shown in Table 1 (a) above. Further, film formation evaluation was carried out in the same manner as in Examples 1 to 4. The results are also shown in Tables 1 (a) to (c) above. In the case of film formation using the oxide steaming materials of Examples 9 to 14, in order to obtain a transparent conductive film having the lowest electrical resistance and high transmittance, the optimum oxygen mixing amount to be introduced into the film forming vacuum chamber is extremely small. This is due to the optimum amount of oxygen contained in the oxide evaporation material. Further, the film system produced by the optimum oxygen mixing amount showed the same composition as the oxide vapor deposition material, and showed not only a very low specific resistance but also a high transmittance in the visible light region. Further, all of the films were confirmed to be a crystal film of a perovskite-type crystal structure of indium oxide, and the adhesion to the substrate was also strong enough to be practical. Further, the oxide vapor deposition material endurance test was carried out under the same conditions as those of Examples 1 to 4, and the oxide vapor deposition materials of Examples 9 to 38-201200610 I4 were not cracked even if they were continuously used. Such a transparent conductive film is very useful as a transparent electrode of a solar cell. [Comparative Example 7] The IT Ο oxide vapor-deposited material described in Japanese Laid-Open Patent Publication No. Hei 08-1 0497 (Patent Document 1) was produced and the same evaluation was carried out. That is, the ratio of the atomic ratio of Sn/In is made 0. The method of 102 is to incorporate a tin oxide powder having an average particle diameter of 1 μη into an average particle diameter of 0. 1 μm of the indium oxide powder was added with 2% by mass of a vinyl acetate-based adhesive. In a wet ball mill, after mixing, drying and pulverizing these materials for 16 hours, a granulated powder is prepared. Further, this granulated powder was used to form a cylindrical molded body by applying a pressure of 49 MPa (500 kgf/cm2) under a low temperature hydrostatic pressure. The sintering of the shaped body is carried out in the atmosphere. The sintering step was carried out from room temperature to 70 ° C for 10 hours, and the temperature was raised to 1 450 ° C for 4 hours and 40 minutes. Then, it was kept at 1 450 ° C for 1 hour to obtain a sintered body. The obtained sintered body was processed into a cylindrical shape having a diameter of 30 mm and a thickness of 40 mm to prepare an ITO oxide vapor-deposited material. The density of the sintered body is 4. 4 g/cm3, specific resistance is 1. 2 mDcm. Further, the crystal grain size is 12 to 16 μm, and the composition is approximately the same as the composition of the feed. The surface of the obtained sintered body was equivalent to the inner color, but after measuring L * ,, as shown in Table 1 (a), it was an extremely low enthalpy (49). This means that the amount of oxygen in the oxide evaporation material is very small. -39-201200610 Next, film formation evaluation was carried out in the same manner as in Examples 1 to 4. The results are also shown in Tables 1 (a) to (c) above. As described above, Comparative Example 7 also clearly shows that L*値 is smaller than the specified range (54 to 75) of the present invention (49); compared with the oxide evaporation materials of Examples 5 to 8, The optimum oxygen mixing amount at the time of film formation is (42), which is very much. In comparison with Examples 5 to 8, the film properties of the optimum oxygen mixing amount were the same, but the specific resistance was high. This system is believed to be mainly due to the large offset of the composition of the film. Further, in comparison with Examples 5 to 8, the film of Comparative Example 7 was weaker than the adhesion to the substrate. It is considered that this is caused by a slight introduction of oxygen into the film at the time of film formation. Due to such an oxide steaming material, the obtained film composition is highly biased and it is difficult to design a film composition. Further, since a small amount of oxygen must be introduced into the film forming vacuum chamber, the composition or the characteristic fluctuation of the vacuum tank is affected by the fluctuation of the oxygen concentration in the vacuum chamber when it is used in the mass production step of the film formation. Further, after the oxide vapor deposition material endurance test was carried out under the same conditions as in Examples 1 to 4, cracks were formed in the oxide vapor deposition material after continuous film formation ("evaluation of "cracking"). When continuous deposition is carried out by using such a crack-producing oxide evaporation material, a problem such as a large fluctuation in the deposition rate occurs, and film formation cannot be performed stably. From the above, it was confirmed that the oxide vapor-deposited material of Comparative Example 7 was not suitable for film formation mass production. [Comparative Example 8] The IT Ο oxide vapor-deposited material described in JP-A-2007-84881 (Patent Document 2) was produced and evaluated in the same manner. -40-201200610, that is, a tin oxide powder having an average particle diameter of 1 μm or less is incorporated into an indium oxide powder having an average particle diameter of 1 μm or less so that the atomic ratio of Sn/In is 0·102. Further, a 2% by mass of a vinyl acetate-based adhesive was added. In a wet ball mill using a hard Zr02 ball, these materials were mixed, dried and pulverized for 18 hours to prepare a granulated powder. Further, this granulated product was applied to a cylindrical molded body by applying a pressure of 94 MPa (3 to n/cm2) under a low temperature hydrostatic pressure. The obtained shaped body is placed in a sintering furnace at a rate of 0. The furnace of 1 m3 was introduced into a gas atmosphere at a ratio of 5 liters/min. The mixture was sintered at normal pressure at 1100 °C for 2 hours. At this time, the temperature is raised at 1 ° C / min, the oxygen introduction is stopped during cooling after sintering, and the temperature is lowered to 1000 ° C at 10 ° C / min. The obtained sintered body is processed into a vertical composite machine. A cylindrical shape having a diameter of 30 mm and a thickness of 40 mm was measured for volume and weight to calculate density. The density of the sintered body is 4. 8 g/cm3. Further, the surface of the sintered body is equivalent to the color inside, but after measuring L*値, it is shown that L*値 is larger than the predetermined range (54 to 75) of the present invention. The amount of oxygen in the plating material is very large. Film formation evaluation was carried out in the same manner as in Examples 1 to 4 using the oxide evaporation material produced in this manner. Although the optimum oxygen mixing amount at the time of film formation was 〇% as in Comparative Example 2, the specific resistance of the film was higher than that of Examples 5 to 8. It is considered that this is because the amount of oxygen in the film is too large due to the excessive supply of oxygen from the oxide evaporation material to the membrane, and it is impossible to introduce an optimum oxygen shortage amount to -41 - 201200610. Therefore, it has been confirmed that a film having high conductivity which is originally possessed by the composition of the vapor deposition material cannot be obtained even if a film is formed using such an oxide vapor deposition material. [Probability of Industrial Use] By using the oxide evaporation material according to the present invention, it is possible to produce a transparent conductive material exhibiting high conductivity by vacuum deposition by exhibiting high light transmittance in a visible light region. The film has an industrial use possibility as an oxide vapor deposition material for forming transparent electrodes of various solar cells. [Simple description of the diagram] te 〇 [Description of main component symbols] None. -42-