TWI259851B - Method and device for manufacturing inner-surface coated cylindrical body and inner-surface coated cylindrical body manufactured thereby - Google Patents
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1259851 (1) 玫、發明說明 【發明所屬之技術領域】 本發明是關於在樹脂成形機機筒和漿料輸送用鋼管等 金屬筒體本體內表面上施加耐磨損性、耐腐蝕性優良的自 熔合金披覆層的內表面披覆筒體的製造技術。 【先前技術】 專利文獻1 :日本特開昭64-25989號公報 專利文獻2:日本特開平1 -96363號公報 以往,在鋼管等金屬筒體本體內周面上施加自熔合金 披覆層的內面披覆筒體爲眾所皆知。在專利文獻1 (曰本 特開昭64-25 9 89號公報)上揭示有:一種內面披覆層的形 成方法,即,利用在使筒體本體(管)旋轉得內周面上離 心力達到3 G以上的狀態下供給自熔合金粉末,以便在該 筒體本體內周面上形成一定厚度的粉末層,然後,將該筒 體本體加熱至前述粉末層呈燒結狀態的溫度,使上述的粉 末層附著在筒體內周面上之後停止旋轉,接著,利用加熱 筒體本體使其內周面溫度達到上述粉末的熔融溫度以上, 以使附著在筒體本體內周面上的粉末層熔融,以伴隨擴散 的形式下,來與母體金屬接合的方法,作爲這種內面披覆 筒體的製造方法。又,前述專利文獻2 (日本特開平1 -9 63 63號公報)上也揭示有:一種內面披覆層的形成方法 ’ β卩’利用:將與披覆層形成厚度相應量的自熔合金粉末 裝入筒體本體內後,一邊使該筒體本體旋轉使得內周面的 -7- 1259851 (2) 離心力達到2G以上、外周面的離心力處於7G以下,一邊 將筒體本體加熱到上述粉末的熔融溫度以上,以使附著在 筒體本體內周面上的粉末層熔融,利用以伴隨著擴散形式 ’來與母體金屬接合的方法。無論何種方法,均是利用將 分配在筒體本體內周面上的自熔合金粉末層加熱熔融,伴 隨著擴散形式與母體金屬接合,能夠形成與母體金屬接合 良好的緻密且接近無氣孔的自熔合金的內面披覆層,特別 是專利文獻2所記載的方法,是在使筒體本體旋轉狀態下 對粉末層進行熔融和凝固的一種離心鑄造方法,能利用使 離心力作用在形成於筒體本體內周面上的金屬熔液層,來 進一步減少氣孔,使所形成的自熔合金的內面披覆層成爲 硬度大,耐磨損性和耐腐蝕性優良的披覆層。 【發明內容】 〔發明所欲解決之課題〕 最近’爲使筒體本體上形成的內面披覆層的耐磨損性 進一步提高’一直希望進一步提高內面披覆層的硬度。爲 提高硬度,雖然認爲可以使用導入了碳化鎢等硬質微粒子 的自熔合金’但,已經判明未必能取得令人滿意的結果。 也就是說’在專利文獻1記載的方法中,利用導入碳化鎢 等硬質微粒子雖然能夠確保硬度獲得某種程度上的提高, 但與專利文獻2記載的方法相比,卻存在殘存氣孔量多的 缺點’另一方面,在專利文獻2記載的方法中,即使導入 碳化鎢等硬質微粒子也幾乎未發現內面披覆層表面在硬度 -8 - 1259851 (3) 上的提高。據說,這是因爲被廣泛採用的碳化鎢等 粒子的比重(与1 5 ),比熔接金屬相的比重(8〜9 多,從而使其自內面披覆層表面(內周面)向遠離 動,表面上不怎麼存在的緣故。而且,該硬質微粒 於內面披覆層的外徑側,也就是與母體金屬(筒體 的邊界區域,因此阻礙了伴隨內面披覆層向母體金 所産生的接合作用,導致粘接力降低,從而産生新 〇 鑒於上述情況,本發明的課題是提供一種利用 造法,至少能大幅度提高在筒體本體內周面上形成 合金內面披覆層的表面硬度的技術。 〔用以解決課題之手段〕 爲解決上記課題,申請專利範圍第1項之發明 種內面披覆筒體的製造方法,該方法包括在具有圓 周面的筒體本體的前述內周面上離心鑄造自熔合金 覆的製程,其特徵在於,利用以前述內周面位置上 〜50G離心力的旋轉速度進行前述離心鑄造,使鑄 在於自熔合金熔液內的硬質陶瓷微粒子中比重低於 液的熔接金屬相的微粒子,反離心聚集在離心鑄造 內徑側,在此狀態下使金屬熔液凝固,獲得前述低 粒子在內徑側聚集的內表面披覆層。如此由於低比 粒子形成在內徑側聚集的內面披覆層,所以該內面 的表面硬度變得極大,能夠製造耐磨損性優良的內 硬質微 )大得 方向移 子聚集 本體) 屬擴散 的問題 離心鑄 的自熔 ,是一 筒狀內 進行披 産生20 造中存 金屬熔 體系的 比重微 重的微 披覆層 面披覆 -9 - 1259851 (4) 筒體。而且由於能夠使硬質陶瓷微粒子在內面披覆層的內 徑側反離心聚集的結果,使得外徑側硬質陶瓷微粒子的濃 度降低,因此能夠提高韌性,同時由於妨礙伴隨著向母體 金屬擴散接合的因素減少,因此能提高與母體金屬的接合 力,從而能夠製造耐衝擊性、耐剝離性也優良的內面披覆 筒體。 申請專利範圍第2項之發明,是就申請專利範圍第1項 之發明,比前述內面披覆層內徑側聚集的前述熔接金屬相 比重低的微粒子,是屬於從自熔合金熔液析出的鉻系的硼 化物、碳化物、硼碳化物中任何物質的陶瓷微粒子。如此 ,作爲自熔合金直接使用鎳自熔合金、鈷自熔合金等廣泛 採用的自熔合金的條件下,能夠提高內面披覆層的表面硬 度。 申請專利範圍第3項之發明,是就申請專利範圍第1項 之發明,比前述內面披覆層內徑側聚集的前述熔接金屬相 比重低的微粒子,是屬於從自熔合金熔液析出的鉻系的硼 化物、碳化物、硼碳化物中任何物質的陶瓷微粒子,和作 爲前述自熔合金基本成分以外成分向前述自熔合金熔液中 導入的比重不超過前述鉻系陶瓷比重的硬質陶瓷微粒子。 如此可以使聚集於內徑側的硬質微粒子量增多,從而可以 進一步地提高其表面硬度。 申請專利範圍第4項之發明,是一種內面披覆筒體的 製造方法,該方法包括在具有圓筒狀內周面筒體本體的前 述內周面上離心鑄造自熔合金的披覆製程,其特徵在於, -10- (5) 1259851 前述離心鑄造在使Ο . 3〜3 Μ P a氣壓作用在金屬熔液層表 上的狀態下進行。一旦採用離心鑄造法形成自熔合金的 面披覆層,就會使披覆層內殘存的氣孔變得極爲微量, 且在該離心鑄造中由於金屬熔液表面受到0.3〜3 Μ P a氣 的作用並在該狀態下凝固,所以金屬熔液層中殘存的微 氣孔因受氣壓壓縮而體積減小,因而使得所獲的內面披 層內殘存氣孔所占的體積比例變得更加微少。因此,由 獲得的內面披覆層因氣孔所占體積而降低硬度的作用受 抑制的結果,與不加氣壓下離心鑄造的場合相比,其硬 增大,所以用此方法能夠製造耐磨損性優良的內面披覆 體。 申請專利範圍第5項之發明,是一種內表面披覆筒 的製造方法,該方法包括在具有圓筒狀內周面筒體本體 前述內周面上離心鑄造自熔合金的披覆製程,其特徵在 ,使金屬熔液層表面受0.3〜3MPa氣壓作用狀態下進行 述離心鑄造,同時在使前述金屬熔液層表面受前述氣壓 用的狀態下,使前述筒體本體的旋轉速度達到在前述內 面位置上産生10G以上離心力的旋轉速度。一旦金屬熔 層表面受到0.3〜3MP a氣壓作用的狀態下凝固,如上所 ,就會産生因壓縮金屬熔液層內氣孔而使體積減小的作 ,但在此情況下,加壓氣體有時會貫通金屬熔液層內的 孔,有時還會進一步貫通至金屬熔液與筒體本體的界面 ,一旦在這種狀態下進行凝固,就會産生比內面披覆層 存氣孔更大而且通到表面的孔,即針孔。爲了防止這種 面 內 而 壓 量 覆 於 到 度 筒 體 的 於 前 作 周 液 述 用 氣 處 殘 現 -11 - !259851 (6) 象發生,本發明中將前述筒體本體的旋轉速度設定爲能使 前述內周面位置上産生10G以上離心力的旋轉速度,以大 離心力作用在金屬熔液上,使包括金屬熔液層內厚度方向 的全部區域內均等産生壓縮應力,在使形成加壓氣體的壓 入α受壓行爲的波動獲得緩解的狀態下讓氣壓作用,以此 方法來防止加壓氣體的貫通。如此能夠形成幾乎沒有針孔 的內面披覆層。 申請專利範圍第6項之發明,是一種內表面披覆筒體 的製造方法,該方法包括在具有圓筒狀內周面筒體本體的 前述內周面上離心鑄造自熔合金的披覆製程,其特徵在於 ,在使金屬熔液層表面受0.3〜3 MPa氣壓作用的狀態下進 行前述離心鑄造,同時在使金屬熔液層表面受到前述氣壓 作用狀態下,使前述筒體本體的旋轉速度達到在前述內周 面位置上産生20〜5 0G離心力的旋轉速度,以此方式使存 在於鑄造中自熔合金熔液內硬質陶瓷微粒子中比重低於金 屬熔液熔接金屬相的微粒子,反離心聚集在離心鑄造體系 的內徑側,在此狀態下使金屬熔液凝固,獲得在內徑側聚 集了前述低比重微粒子的內表面披覆層。也就是說,本發 明是將技術方案1發明與技術方案4發明的特徵加以組合, 利用施加20〜5 0G離心力,使硬質微粒子聚集在內面披覆 層的內徑側,能夠提高表面硬度,同時利用使0.3〜3MP a 氣壓作用能使內面披覆層內殘存氣孔數量變得極微,如此 能夠提高硬度,可以製造具有更高硬度的內面披覆層的內 面披覆同體。 -12- 1259851 (7) 申請專利範圍第7項之發明,是就申請專利範圍第1至 6項之發明中,使前述離心鑄造中前述自熔合金熔液達到 的溫度,處於與該自熔合金的熔融一凝固有關的固相線至 '液相線的固液共存溫度區域內距離固相線側70 %位置處的 溫度以下。進行自熔合金的離心鑄造時,必須在被鑄造面 上形成自熔合金的金屬熔液層,此時金屬熔液溫度一旦增 高’就會因有助於硬度提高的金屬硼化物和金屬矽化物等 微粒子的熔化氧化消耗而使硬度降低,進而有混入氧化物 之虞。其中利用將金屬熔液溫度設定爲上述數値,能夠防 止硬質微粒子因熔化和氧化消耗而減少或氧化物混入,從 而能夠形成硬度高的披覆層。 申請專利範圍第8項之發明,是就申請專利範圍第1至 6項之發明中,前述離心鑄造中自熔合金熔液層在前述內 周面上的形成,是以向前述筒體本體內導入自熔合金粉末 ’在前述筒體本體旋轉下將該粉末加熱熔融的方式進行的 。自熔合金熔液層在筒體本體的內周面上的形成,雖然也 可以在筒體本體的外部製成金屬熔液後,以向筒體本體內 供給該金屬熔液的方式進行,但按照本發明,以粉末形式 向筒體本體內供給自熔合金,並在該位置將其加熱熔融的 方法,能使自熔合金的處理變得容易,而且所必須的設備 也簡化。 申請專利範圍第9項之發明,是就申請專利範圍第1至 6項之發明中,前述離心鑄造中自熔合金溶液層在前述內 周面上的形成,是以下述方式進行的:(1)在橫置的筒 -13- (8) 1259851 體本體內部,沿筒體軸線方向均等地配置與形成披覆層厚 度相當的量的自熔合金粉末,(2 )使筒體本體以其軸線 爲中心旋轉,使之達到在前述筒體本體的內周面位置上産 生3 G以上離心力的旋轉速度的情況下,也使筒體本體內 的粉末以遍及筒體本體圓周方向行進的形式黏貼在筒體本 體的內周面上,此時應使達到能夠産生3 G以上離心力的 旋轉速度所需的時間,不超過按以下實驗式(A )求出的 時間τ : r (秒)=3x105/D3 …(A ) (D是筒體的內徑,mm) 以便抑制沿筒體軸線方向均等配置的粉末在筒體軸線 方向上移動,藉此來形成一層沿筒體的軸線方向和圓周方 向幾乎沒有厚度偏差的粉末層並使其黏貼在筒體本體內周 面上,(3 )在繼續使筒體本體旋轉的情況下,加熱筒體 本體以使筒體全體同時升溫,並使筒體本體內的粉末同時 熔融。供給粉末時採用上述(1 ) 、( 2 )製程的場合下, 能夠在筒體本體內周面上形成沿筒體軸線方向的厚度偏差 極小的自熔合金粉末層,將該粉末層加熱熔融並使之凝固 時’能夠形成厚度偏差極小的自熔合金的內面披覆層。 申請專利範圍第10項之發明,是就申請專利範圍第1 至6項之發明中,前述離心鑄造中自熔合金溶液層在前述 內周面上的形成,是以向前述筒體本體內導入自熔合金粉 末’在前述筒體本體旋轉下將此粉末加熱熔融的方式進行 的’同時在減壓下進行前述筒體本體內粉末的熔融。按照 -14- 1259851 (9) 這種結構,能夠有效地從粉末熔融形成的金屬 去氣泡的同時,還能防止金屬熔液層氧化,能 氣孔極少而且有助於硬度提高的析出微粒子的氧 、氧化物混入也少的內面披覆層。 申請專利範圍第1 1項之發明,是一種內面披 它是一種在具有圓筒狀內周面的筒體本體的前述 形成了自熔合金的內面披覆層內面披覆筒體,其 ,其中鉻化合物系硬質陶瓷的微粒子在前述內面 的內徑側以高密度分佈,使鉻成分濃度達到20 水平,形成了硬度提高的硬質層。這種內面披覆 在內面披覆層表面(內周面)上具備硬度提高的 因此具有優良的耐磨損性。 申請專利範圍第1 2項之發明,是就申請專利 項之發明中,在前述內面披覆層內的外徑側,形 介裝物的顯微面積率在0 · 1 %以下的淸淨層。這種 非金屬介裝物少而具有優良的韌性,而且由於阻 向母體金屬的擴散導致接合的非金屬介裝物少而 體金屬的結合強度高,因此內面披覆層變成一種 良而且與母體金屬牢固接合的淸淨層支承表面硬 構,不僅耐磨損性優良,而且耐衝擊性和耐剝離 〇 申請專利範圍第1 3項之發明,是一種內面披 製造裝置’其中具有水平地支承筒體本體並使之 體支承旋轉裝置,向被該筒體支承旋轉裝置支承 液層內除 形成殘存 化消耗少 覆筒體, 內周面上 特徵在於 披覆層內 4 0質量% 筒體由於 硬質層, 範圍第11 成非金屬 淸淨層因 礙伴隨著 使得與母 由韌性優 質層的結 性也優良 覆筒體的 旋轉的筒 的筒體本 -15 - 1259851 (10) 體內供給與披覆層形成厚度相當的量自熔合金粉末的粉末 供給裝置,對被前述筒體支承旋轉裝置支承的筒體本體的 全部長度加熱的加熱裝置,前述筒體支承旋轉裝置能使前 述筒體本體以筒體本體內周面位置上産生20〜5〇(3離心力 的旋轉速度旋轉。在這種結構的製造裝置中,能夠向被前 述筒體支承旋轉裝置支承的筒體本體內供給與披覆層形成 厚度相當的量自熔合金粉末的粉末,使筒體本體旋轉以便 在內周面上形成自熔合金粉末層後,加熱熔融該自熔合金 粉末以形成金屬熔液層,進而進行使之凝固的這種離心禱 造,而且該離心鑄造以能使前述內周面位置上産生2 0〜 5 0G離心力的旋轉速度進行。因此,能夠使存在於鑄造中 自熔合金熔液中的硬質陶瓷微粒子內的、比重低於金屬熔 液熔接金屬相的微粒子反離心聚集在離心鑄造體系的內徑 側,在這種狀態下使金屬熔液凝固,如此就能夠獲得前述 低比重微粒子聚集在內徑側的內面披覆層,從而能夠製造 具有表面硬度極大的內面披覆層、耐磨損性優良的內面披 覆筒體。 申請專利範圍第14項之發明發明,是一種內面披覆筒 體的製造裝置,其中具有水平地支承筒體本體並使之旋轉 的筒體支承旋轉裝置,向被該筒體支承旋轉裝置支承的筒 體本體內供給與披覆層形成厚度相當的量自熔合金粉末的 粉末供給裝置,對被前述筒體支承旋轉裝置支承的筒體本 體的全部長度加熱的加熱裝置,和使0.3〜3MPa氣壓作用 在前述筒體本體的內表面上的加壓裝置。這種結構的製造 -16- (11) 1259851 裝置中,能夠向被前述筒體支承旋轉裝置支承的筒體本體 內供給與披覆層形成厚度相當的量自熔合金的粉末,使筒 體本體旋轉,以便在內周面上形成自熔合金粉末層,然後 利用加熱熔融該自熔合金粉末層來形成金屬熔液層,接著 進行使之凝固的這種離心鑄造,而且在該離心鑄造中,能 夠使自前述內周面上形成自熔合金熔液層至使這種金屬熔 液層凝固的過程,在前述金屬熔液層表面處於0.3〜3MPa 氣壓作用的狀態下經過,如此就能製造具有殘存的氣孔極 少、硬度大的內面披覆層、耐磨損性優良的內面披覆筒體 〇 申請專利範圍第15項之發明,是一種內面披覆筒體的 製造裝置,其中具有水平地支承筒體本體並使之旋轉的筒 體支承旋轉裝置,向被該筒體支承旋轉裝置支承的筒體本 體內供給與披覆層形成厚度相當的量自熔合金粉末的粉末 供給裝置,對被前述筒體支承旋轉裝置支承的筒體本體的 全部長度加熱的加熱裝置,和使0.3〜3MPa氣壓作用在前 述筒體本體內表面上的加壓裝置,前述筒體支承旋轉裝置 能使前述筒體本體以筒體本體內周面位置上産生10G以上 離心力的旋轉速度旋轉。這種結構的製造裝置中,能夠在 使前述筒體本體內的金屬溶液層表面受到0.3〜3MPa氣壓 作用的狀態下進行離心鑄造的同時,能使筒體本體此時在 筒體本體內周面位置上産生10G以上離心力的旋轉速度下 旋轉,因而能夠防止加壓氣體貫通金屬熔液層內的氣孔或 貫通金屬熔液層與筒體本體之間的界面,從而能形成幾乎 -17· 1259851 (12) 沒有針孔的內面披覆層。 申請專利範圍第i 2項之發明,是一種內面披覆筒體的 製造裝置,其中具有水平地支承筒體本體並使之旋轉的筒 體支承旋轉裝置,向被該筒體支承旋轉裝置支承的筒體本 體內供給與披覆層形成厚度相當的量自熔合金粉末的粉末 供給裝置’對被前述筒體支承旋轉裝置支承的筒體本體的 全部長度加熱的加熱裝置,和使0.3〜3MPa氣壓作用在前 述筒體本體內表面上的加壓裝置,前述筒體支承旋轉裝置 能使前述筒體本體以筒體本體內周面位置上産生20〜50G 離心力的旋轉速度旋轉。這種結構的製造裝置,能夠在使 前述筒體本體內的金屬溶液層表面受到0.3〜3MPa氣壓作 用的狀態下進行離心鑄造的同時,能使筒體本體此時在筒 體本體內周面位置上産生20〜50G離心力的旋轉速度下旋 轉,在〇·3〜3MPa氣壓作用下不僅能使內面披覆層內殘存 氣孔數量極爲微少而提高硬度,而且利用施加20〜50G離 心力使硬質微粒子反離心聚集在內面披覆層的內徑側而能 夠提高表面硬度,從而能夠製造具有硬度更高的內面披覆 層的內面披覆筒體。 申請專利範圍第1 7項之發明,是就申請專利範圍第1 3 至16項之發明中,前述加熱裝置具有能夠遍及筒體全長同 時對被前述筒體支承旋轉裝置支承的筒體的圓周方向的小 區間進行感應加熱的感應線圈。按照這種結構,能夠同時 而且迅速地對筒體本體全長加熱,因而能夠迅速地將自熔 合金粉末層加熱熔融。 -18- 1259851 (13) 綜上所述,本發明由於具有如此的結構,即利用離心 鑄造法在筒體本體內周面上形成自熔合金的內面披覆層時 ’能使筒體本體內周面位置處於2 0〜5 0 G離心力作用的狀 態或使金屬熔液層表面經受0 · 3〜3 Μ P a氣壓作用的狀態下 ’與已有方法形成的內面披覆層相比,使用同一自熔合金 能提局內面披覆層的表面硬度,具有能夠製造耐磨損性優 良的內面披覆筒體的效果。而且本發明製造的內面披覆筒 體具有優良的耐磨損性,將其用於樹脂成形機機筒和漿料 輸送用鋼管等上時,能夠獲得耐磨損性優良、使用壽命長 的樹脂成形機機筒和漿料輸送鋼管等製品。 【實施方式】 以下參照附圖說明本發明的實施方式。第1圖(a )、 (b)是顯示本發明實施方式中前述內面披覆筒體製造裝 置處於不同狀態下的示意性立體圖,第2圖(a ) 、 ( b ) 、(c) 、 (d)是顯示用第1圖的製造裝置在筒體本體的 內周面上形成自熔合金內面披覆層順序的示意斷面圖,1 是具有圓筒狀內周面的筒體本體。筒體本體1只要是金屬 制的皆可任選,其代表性實例可以舉出樹脂成形機機筒等 機筒和漿料輸送鋼管等各種鋼管。2是用於在筒體本體1內 周面上形成內面披覆層的自熔合金的粉末。作爲形成披覆 層的自熔合金,可以舉出廣泛採用的鎳自熔合金(例如 JIS,83 03的SFNi4等)和廣泛採用的鈷自熔合金(例如 JIS,8303的SFC〇3等)等。而且必要時還可以使用在這些 -19- 1259851 (14)1259851 (1) The present invention relates to the application of excellent wear resistance and corrosion resistance to the inner surface of a metal cylinder such as a resin molding machine barrel and a slurry conveying steel tube. A manufacturing technique for coating the inner surface of a self-fluxing alloy coating layer. [Patent Document 1] Japanese Laid-Open Patent Publication No. Hei. No. Hei. No. Hei. No. Hei. No. Hei. The inner cladding cylinder is well known. A method of forming an inner surface coating layer by using a centrifugal force on an inner circumferential surface of a cylindrical body (tube) is disclosed in Patent Document 1 (Japanese Unexamined Patent Publication No. Hei No. Hei No. Hei No. Hei No. Hei. When the self-fluxing alloy powder is supplied in a state of 3 G or more, a powder layer having a certain thickness is formed on the inner circumferential surface of the cylindrical body, and then the body of the cylinder is heated to a temperature at which the powder layer is in a sintered state, so that After the powder layer adheres to the circumferential surface of the cylinder body, the rotation is stopped, and then the inner peripheral surface temperature of the cylinder body is heated to a temperature higher than or equal to the melting temperature of the powder to melt the powder layer adhering to the inner circumferential surface of the cylinder body. A method of joining to a parent metal in the form of a diffusion, as a method of manufacturing such an inner coated cylinder. Further, the above-mentioned Patent Document 2 (Japanese Laid-Open Patent Publication No. Hei No. Hei. No. Hei. No. Hei. No. Hei. No. Hei. No. Hei. No. Hei. No. Hei. No. Hei. After the alloy powder is placed in the body of the cylinder, the body of the cylinder is rotated such that the centrifugal force of the inner peripheral surface of the -7-1259851 (2) reaches 2 G or more, and the centrifugal force of the outer peripheral surface is 7 G or less, and the cylinder body is heated to the above. Above the melting temperature of the powder, the powder layer adhering to the inner peripheral surface of the cylindrical body is melted, and a method of joining to the parent metal along with the diffusion form ' is used. In either method, the self-fluxing alloy powder layer distributed on the inner surface of the cylinder body is heated and melted, and the diffusion form is bonded to the parent metal to form a dense and nearly non-porous joint which is well bonded to the parent metal. The inner surface coating layer of the self-fluxing alloy, in particular, the method described in Patent Document 2 is a centrifugal casting method in which the powder layer is melted and solidified in a state in which the cylindrical body is rotated, and can be formed by using centrifugal force. The molten metal layer on the inner circumferential surface of the cylindrical body further reduces the pores, and the inner coating layer of the formed self-fluxing alloy becomes a coating layer having high hardness and excellent wear resistance and corrosion resistance. SUMMARY OF THE INVENTION [Problems to be Solved by the Invention] Recently, the wear resistance of the inner surface coating layer formed on the cylindrical body has been further improved. It has been desired to further increase the hardness of the inner surface coating layer. In order to increase the hardness, it is considered that a self-fluxing alloy into which hard particles such as tungsten carbide are introduced can be used. However, it has been found that satisfactory results may not be obtained. In other words, in the method described in Patent Document 1, although the hard microparticles such as tungsten carbide are introduced, the hardness can be improved to some extent. However, compared with the method described in Patent Document 2, the amount of residual pores is large. Disadvantages. On the other hand, in the method described in Patent Document 2, even if hard fine particles such as tungsten carbide are introduced, the surface of the inner cladding layer is hardly found to have an improvement in hardness of -8 to 129,851 (3). It is said that this is because the specific gravity (and 15) of particles such as tungsten carbide, which are widely used, is larger than the specific gravity of the welded metal phase (8 to 9 times, so that it is away from the surface (inner peripheral surface) of the inner cladding layer). The movement, the surface does not exist very much. Moreover, the hard particles on the outer diameter side of the inner cladding layer, that is, the parent metal (the boundary region of the cylinder, thus hindering the inner cladding layer to the parent gold The resulting bonding action causes a decrease in the bonding force, thereby generating a new one. In view of the above, an object of the present invention is to provide a method for at least greatly improving the formation of an inner surface of an alloy on a circumferential surface of a cylindrical body. The technique of the surface hardness of the layer. [Means for Solving the Problem] In order to solve the above problem, the method for manufacturing the inner surface coated cylinder of the invention of claim 1 includes a cylindrical body having a circumferential surface. The centrifugal casting of the self-fluxing alloy on the inner circumferential surface is characterized in that the centrifugal casting is performed at a rotational speed of 〜50 G centrifugal force at the inner circumferential surface position to cast the casting The fine ceramic particles in the molten alloy melt have a specific gravity lower than that of the molten metal phase of the liquid, and are centrifugally collected on the inner diameter side of the centrifugal casting. In this state, the molten metal is solidified, and the low particles are aggregated on the inner diameter side. Since the inner surface coating layer is formed on the inner diameter side due to the formation of the low specific particles, the surface hardness of the inner surface becomes extremely large, and the inner hard surface having excellent wear resistance can be manufactured. The direction shifting sub-aggregate body is a problem of diffusion. The self-melting of centrifugal casting is a micro-coated layer covering the surface of a cylindrically formed metal melting system. The micro-coating layer is covered by a -9 - 1259851 (4) body. Further, as a result of the centrifugal accumulation of the hard ceramic fine particles on the inner diameter side of the inner coating layer, the concentration of the outer diameter side hard ceramic fine particles is lowered, so that the toughness can be improved and the diffusion bonding to the parent metal is hindered. Since the factor is reduced, the bonding force with the parent metal can be improved, and the inner cladding cylinder excellent in impact resistance and peeling resistance can be manufactured. According to the invention of claim 2, in the invention of claim 1, the fine particles having a lower weight than the welded metal gathered on the inner diameter side of the inner cladding layer are precipitated from the molten alloy of the self-fluxing alloy. Ceramic microparticles of any of the chromium-based borides, carbides, and borocarbides. As described above, the surface hardness of the inner cladding layer can be improved under the condition that a self-fluxing alloy such as a nickel self-fluxing alloy or a cobalt self-melting alloy is widely used as the self-fluxing alloy. According to the invention of claim 3, in the invention of claim 1, the fine particles having a lower weight than the welded metal gathered on the inner diameter side of the inner cladding layer are precipitated from the molten alloy of the self-fluxing alloy. The ceramic fine particles of any of the chromium-based boride, the carbide, and the borocarbide, and the hard component which is introduced into the melt of the self-fluxing alloy as a component other than the basic component of the self-fluxing alloy, does not exceed the specific gravity of the chromium-based ceramic Ceramic microparticles. Thus, the amount of hard fine particles collected on the inner diameter side can be increased, so that the surface hardness can be further improved. The invention of claim 4 is a method for manufacturing an inner coated cylindrical body, which comprises a coating process for centrifugally casting a self-fluxing alloy on the inner circumferential surface of a cylindrical inner peripheral cylindrical body It is characterized in that -10-(5) 1259851 is subjected to centrifugal casting in a state where the pressure of Ο 3 3 Μ P a is applied to the molten metal layer. Once the surface coating of the self-fluxing alloy is formed by centrifugal casting, the pores remaining in the coating layer become extremely small, and in the centrifugal casting, the surface of the molten metal is subjected to 0.3 to 3 Μ P a gas. Since the action is solidified in this state, the micropores remaining in the molten metal layer are reduced in volume by the compression of the gas pressure, so that the volume ratio of the remaining pores in the obtained inner surface layer is made smaller. Therefore, as a result of suppressing the effect of lowering the hardness of the inner surface coating layer due to the volume occupied by the pores, it is harder than that in the case of centrifugal casting without air pressure, so that abrasion resistance can be produced by this method. An inner surface covering with excellent damage. The invention of claim 5 is a method for manufacturing an inner surface coated cylinder, the method comprising: a coating process for centrifugally casting a self-fluxing alloy on an inner circumferential surface of a cylindrical inner circumferential surface of a cylindrical body; It is characterized in that the surface of the molten metal layer is subjected to centrifugal casting under the action of a pressure of 0.3 to 3 MPa, and the rotation speed of the tubular body is achieved in a state in which the surface of the molten metal layer is subjected to the air pressure. A rotational speed of 10 G or more centrifugal force is generated at the inner surface position. Once the surface of the molten metal layer is solidified by a pressure of 0.3 to 3 MP a, as described above, a volume is reduced by compressing the pores in the molten metal layer, but in this case, the pressurized gas sometimes It will penetrate the hole in the molten metal layer, and sometimes penetrates further to the interface between the molten metal and the body of the cylinder. Once solidified in this state, it will be larger than the inner pore of the inner cladding layer. A hole that leads to the surface, that is, a pinhole. In order to prevent such an in-plane and the amount of pressure is applied to the liquid in the front cylinder, the rotation speed of the cylinder body is set to -11 - !259851 (6), in the present invention, the rotation speed of the cylinder body is set to The rotation speed at which the centrifugal force of 10 G or more is generated at the inner circumferential surface position is applied to the molten metal by a large centrifugal force, and compressive stress is uniformly generated in all the regions including the thickness direction of the molten metal layer to form a pressurized gas. The pressure in the pressure-inducing behavior of the pressure-inducing action is relieved, and the air pressure is applied in this way to prevent the penetration of the pressurized gas. This makes it possible to form an inner cladding layer having almost no pinholes. The invention of claim 6 is a method of manufacturing an inner surface cladding cylinder, the method comprising the coating process of centrifugally casting a self-fluxing alloy on the inner circumferential surface of a cylindrical inner circumferential cylinder body The centrifugal casting is carried out in a state where the surface of the molten metal layer is subjected to a gas pressure of 0.3 to 3 MPa, and the rotating speed of the cylindrical body is made while the surface of the molten metal layer is subjected to the air pressure. A rotation speed of 20 to 50 G centrifugal force is generated at the position of the inner circumferential surface, in such a manner that the fine particles having a lower specific gravity than the molten metal phase of the molten metal present in the molten metal in the molten alloy during casting are de-centrifuged. The inner surface side of the centrifugal casting system was collected, and in this state, the molten metal was solidified to obtain an inner surface coating layer in which the low specific gravity fine particles were collected on the inner diameter side. That is, the present invention combines the features of the first aspect of the invention and the fourth aspect of the invention, and by applying a centrifugal force of 20 to 50 G, the hard microparticles are collected on the inner diameter side of the inner coating layer, thereby improving the surface hardness. At the same time, the pressure of 0.3 to 3 MP a can be used to make the number of remaining pores in the inner coating layer extremely small, so that the hardness can be increased, and the inner surface of the inner coating layer having higher hardness can be manufactured. -12-1259851 (7) The invention of claim 7 is the invention in the invention of claim 1 to 6 wherein the temperature of the molten iron melt in the centrifugal casting is attained with the self-melting The melting-solidification-related solidus line of the alloy is below the temperature at the 70% position of the solidus side in the solid-liquid coexistence temperature region of the liquidus. When centrifugal casting of a self-fluxing alloy is carried out, it is necessary to form a molten metal layer of a self-fluxing alloy on the surface to be cast, and at this time, when the temperature of the molten metal is increased, it is caused by a metal boride and a metal telluride which contribute to an increase in hardness. The melting and oxidation of the fine particles are consumed to lower the hardness, and further, the oxide is mixed. By setting the temperature of the molten metal to the above number, it is possible to prevent the hard fine particles from being reduced by melting and oxidation, or to mix the oxides, thereby forming a coating layer having a high hardness. The invention of claim 8 is the invention of claim 1 to 6, wherein the formation of the molten alloy layer of the self-fluxing alloy on the inner circumferential surface in the centrifugal casting is performed in the cylinder body The introduction of the self-fluxing alloy powder is carried out by heating and melting the powder under the rotation of the cylindrical body. The formation of the molten metal layer of the self-fluxing alloy on the inner peripheral surface of the cylindrical body may be performed by supplying the molten metal to the inside of the cylindrical body after the molten metal is formed outside the tubular body, but According to the present invention, the self-fusing alloy is supplied to the body of the cylinder in the form of a powder, and the method of heating and melting the same in the position enables easy handling of the self-fusing alloy, and the necessary equipment is also simplified. The invention of claim 9 is the invention of claim 1 to 6, wherein the formation of the self-fluxing alloy solution layer on the inner peripheral surface in the centrifugal casting is performed in the following manner: (1) Inside the horizontal body 13-(8) 1259851 body, the self-fluxing alloy powder corresponding to the thickness of the coating layer is equally disposed along the axial direction of the cylinder, and (2) the body of the cylinder is When the axis rotates at the center so as to achieve a rotational speed of 3 G or more centrifugal force at the position of the inner circumferential surface of the cylindrical body, the powder in the cylindrical body is also adhered in the circumferential direction of the cylindrical body. On the inner peripheral surface of the cylindrical body, the time required to reach a rotational speed capable of generating a centrifugal force of 3 G or more is not more than the time τ obtained by the following experimental formula (A): r (second) = 3 x 105 /D3 (A) (D is the inner diameter of the cylinder, mm) so as to suppress the powder uniformly disposed along the axial direction of the cylinder from moving in the axial direction of the cylinder, thereby forming a layer along the axial direction and the circumferential direction of the cylinder Powder with almost no thickness deviation The last layer is adhered to the inner circumferential surface of the cylinder body, and (3) while the cylinder body is continuously rotated, the body of the cylinder is heated to simultaneously raise the temperature of the entire cylinder, and the powder in the cylinder body is simultaneously Melt. When the above-mentioned (1) and (2) processes are used for supplying the powder, a self-fluxing alloy powder layer having a small thickness variation along the axial direction of the cylinder can be formed on the inner circumferential surface of the cylindrical body, and the powder layer can be heated and melted. When it is solidified, it can form an inner coating layer of a self-fusing alloy having a very small thickness deviation. The invention of claim 10 is the invention of claim 1 to 6, wherein the formation of the self-fluxing alloy solution layer on the inner peripheral surface in the centrifugal casting is introduced into the body of the cylinder The self-fluxing alloy powder 'heats and melts the powder under the rotation of the cylindrical body' simultaneously while melting the powder in the cylindrical body under reduced pressure. According to the structure of No.-14-1259851 (9), it is possible to effectively remove bubbles from the metal formed by powder melting, and also prevent oxidation of the molten metal layer, which has few pores and contributes to the increase in hardness of precipitated fine particles of oxygen, An inner coating layer with less oxide incorporation. The invention of claim 11 is an inner surface coated with an inner surface of a cylindrical coating body having a cylindrical inner peripheral surface, wherein the inner surface of the inner surface of the cylindrical body having a cylindrical inner peripheral surface is covered with a self-fluxing alloy. In the case where the fine particles of the chromium compound-based hard ceramic are distributed at a high density on the inner diameter side of the inner surface, the chromium component concentration is 20 degrees, and a hard layer having an increased hardness is formed. Such an inner surface coating has an increased hardness on the inner surface of the inner cladding layer (inner peripheral surface) and thus has excellent wear resistance. According to the invention of claim 12, in the invention of the patent application, in the outer diameter side of the inner cladding layer, the microscopic area ratio of the shaped medium is less than 0.1%. Floor. The non-metallic medium has few toughness and excellent toughness, and since the diffusion of the parent metal causes the bonding of the non-metallic medium to be small and the bonding strength of the body metal is high, the inner cladding layer becomes a good and The cleansing layer supporting surface of the parent metal is firmly bonded, and is not only excellent in abrasion resistance, but also impact resistance and peeling resistance. The invention of claim 13 of the patent application is an inner face manufacturing device which has horizontally The cylindrical body is supported and supported by the rotating device, and the cylindrical body is supported by the rotating body in the supporting liquid layer, and the inner peripheral surface is characterized by a 40% by mass in the coating layer. Due to the hard layer, the 11th non-metallic ruthenium layer is in contact with the cylinder of the cylinder which is excellent in the knot-like property of the toughness-quality layer and is also excellent in the rotation of the cylinder. -15 - 1259851 (10) The coating layer forms a powder supply device for a self-fluxing alloy powder having a thickness corresponding to a thickness, and a heating device for heating the entire length of the cylindrical body supported by the cylindrical body supporting the rotating device The cylindrical support rotating device can rotate the cylindrical body body at a rotational speed of 3 to 5 〇 at a position on the inner circumferential surface of the cylindrical body. In the manufacturing apparatus of such a configuration, the cylindrical body can be rotated by the cylindrical body. The body supported by the device supplies a powder of a self-fluxing alloy powder in a thickness corresponding to the thickness of the coating layer, and the body of the cylinder is rotated to form a self-fluxing alloy powder layer on the inner circumferential surface, and the self-melting alloy powder is heated and melted. This centrifugal prayer is formed by forming a molten metal layer, and the centrifugal casting is performed at a rotational speed at which a centrifugal force of 20 to 50 G is generated at the inner circumferential surface position. The fine particles in the hard ceramic fine particles in the molten metal of the casting are less than the fine particles of the molten metal phase of the molten metal, and are centrifugally collected on the inner diameter side of the centrifugal casting system, and the molten metal is solidified in this state. The inner surface coating layer in which the low specific gravity fine particles are collected on the inner diameter side can be obtained, whereby the inner surface coating layer having excellent surface hardness and abrasion resistance can be manufactured. The invention of claim 14 is an apparatus for manufacturing an inner cladding cylinder, wherein the cylinder body supports a rotating device that horizontally supports and rotates the cylinder body, A powder supply device for supplying a self-fluxing alloy powder having a thickness corresponding to a thickness of the coating layer to the cylindrical body supported by the cylindrical body supporting the rotating device, and heating the entire length of the cylindrical body supported by the cylindrical body supporting rotating device a heating device and a pressurizing device for applying a gas pressure of 0.3 to 3 MPa on the inner surface of the cylindrical body. In the manufacturing of the structure - 16 - (11) 1259851, the rotating device can be supported by the cylindrical body The body of the cylinder is supplied with a powder of a self-fluxing alloy in a thickness corresponding to the thickness of the coating layer, and the body of the cylinder is rotated to form a self-fluxing alloy powder layer on the inner peripheral surface, and then the self-fluxing alloy powder layer is melted by heating. To form a molten metal layer, followed by centrifugal casting to solidify it, and in the centrifugal casting, a molten metal melt can be formed from the inner circumferential surface. The process of solidifying the molten metal layer to the surface of the molten metal layer is carried out under the action of a pressure of 0.3 to 3 MPa, thereby producing an inner coating layer having a small amount of residual pores and a large hardness. The invention relates to an inner surface coated cylinder which is excellent in abrasion resistance. The invention of claim 15 is an apparatus for manufacturing an inner cladding cylinder, which has a cylinder support for horizontally supporting and rotating the cylinder body. The rotating device supplies a powder supply device for the self-fluxing alloy powder in a thickness corresponding to the thickness of the coating layer to the cylindrical body supported by the cylindrical body supporting the rotating device, and the cylindrical body supported by the cylindrical body supporting the rotating device a heating device that heats all the lengths, and a pressing device that applies a pressure of 0.3 to 3 MPa on the inner surface of the cylindrical body, and the cylindrical supporting rotating device can generate the 10G of the cylindrical body at a position on the inner circumferential surface of the cylindrical body The rotation speed of the above centrifugal force is rotated. In the manufacturing apparatus of such a structure, the cylindrical body can be centrifugally cast in a state where the surface of the metal solution layer in the cylindrical body body is subjected to a pressure of 0.3 to 3 MPa, and the cylindrical body can be now in the inner circumference of the cylindrical body. When the position is rotated at a rotational speed of 10 G or more, it is possible to prevent the pressurized gas from penetrating through the pores in the molten metal layer or through the interface between the molten metal layer and the body of the cylinder, thereby forming almost -17·1259851 ( 12) The inner coating without pinholes. The invention of claim i is an apparatus for manufacturing an inner-faced cylindrical body, wherein a cylindrical body supporting a rotating device that horizontally supports and rotates the cylindrical body body is supported by the rotating body supporting the rotating body The inside of the cylindrical body is supplied with a powder supply device of a self-fluxing alloy powder in an amount corresponding to the thickness of the coating layer, and a heating device for heating the entire length of the cylindrical body supported by the cylindrical supporting rotating device, and 0.3 to 3 MPa is provided. A pressurizing device that acts on the inner surface of the cylindrical body by the air pressure, and the cylindrical supporting rotating device can rotate the tubular body at a rotational speed of 20 to 50 G centrifugal force at a position of a circumferential surface of the cylindrical body. In the manufacturing apparatus of such a structure, centrifugal casting can be performed in a state where the surface of the metal solution layer in the cylindrical body body is subjected to a pressure of 0.3 to 3 MPa, and the cylindrical body can be positioned at the circumferential surface of the cylindrical body at this time. Rotating at a rotational speed of 20~50G centrifugal force, under the pressure of 〇·3~3MPa, not only can the number of residual pores in the inner coating layer be extremely small, but the hardness can be increased, and the hard microparticles can be reversed by applying 20~50G centrifugal force. The inner surface side of the inner coating layer is centrifugally collected to increase the surface hardness, so that the inner surface coating cylinder having the inner surface coating layer having a higher hardness can be produced. The invention of claim 17 is the invention of claim 1 to 3, wherein the heating device has a circumferential direction of the cylindrical body supported by the cylindrical support rotating device over the entire length of the tubular body Inductive coil for induction heating between cells. According to this configuration, the entire length of the tubular body can be heated simultaneously and rapidly, so that the self-fusing alloy powder layer can be rapidly heated and melted. -18-1259851 (13) In summary, the present invention has such a structure that when the inner coating surface of the self-fluxing alloy is formed on the inner circumferential surface of the cylindrical body by centrifugal casting, the cylinder can be The position of the inner surface of the body is in a state of 20 0 to 50 G centrifugal force or the surface of the molten metal layer is subjected to a pressure of 0 · 3 〜 3 Μ P a , which is compared with the inner coating layer formed by the existing method. The same self-fluxing alloy can be used to extract the surface hardness of the inner surface coating layer, and has the effect of being able to produce an inner surface coating cylinder excellent in abrasion resistance. Further, the inner coated cylinder produced by the present invention has excellent wear resistance, and when it is used for a resin molding machine barrel and a steel pipe for slurry conveyance, it is possible to obtain an excellent wear resistance and a long service life. Resin molding machine barrel and slurry conveying steel pipe and other products. [Embodiment] Hereinafter, embodiments of the present invention will be described with reference to the drawings. Figs. 1(a) and 1(b) are schematic perspective views showing the state in which the inner facing cylindrical body manufacturing apparatus is in a different state according to the embodiment of the present invention, and Figs. 2(a), (b), (c), (d) is a schematic cross-sectional view showing a procedure for forming a self-fusing alloy inner surface coating layer on the inner circumferential surface of the cylindrical body by the manufacturing apparatus of Fig. 1, and 1 is a cylindrical body having a cylindrical inner circumferential surface. . The cylindrical body 1 is optional as long as it is made of a metal, and typical examples thereof include various steel tubes such as a barrel for a resin molding machine barrel and a slurry conveying steel tube. 2 is a powder of a self-fluxing alloy for forming an inner surface coating layer on the inner circumferential surface of the cylindrical body 1. Examples of the self-fluxing alloy forming the coating layer include widely used nickel self-fluxing alloys (for example, SFNi4 of JIS, 83 03, etc.) and widely used cobalt self-fluxing alloys (for example, JIS, SFC 3 of 8303, etc.). . And if necessary, you can also use these in -19- 1259851 (14)
自熔合金中導入自熔合金金屬彳谷液中析出的屬於鉻系的 硼化物、碳化物、硼碳化物中任何一種陶瓷的、比重同等 或處於其之下的、具體講比重在7以下的硬質陶瓷(例如 BN:比重 2.34' B4C:比重 2.47、Si3N4:比重 3.2、SiC :比重 3_21、V2O5:比重 3.36、V〇2:比重 4.34、TiB2: 比重 4·5、 V203 :比重 4.8 7、TiC :比重 4.94,TiB :比重 5.09、TiN :比重 5·43、V0 :比重 5.76, VC :比重 5.77、 ZrB2:比重 6.08、 ZrC:比重 6_73、NbB2:比重 6.97、或 其複合物等)的微粒子。 3是水平地支承筒體本體1並使之旋轉的筒體支承旋轉 裝置,本實施方式中具有支承筒體本體1下側的兩根承受 輥4、壓在筒體本體1上側的加壓輕5 (第1圖中省略)、旋 轉驅動上述兩根承受輥4的變速馬達6、以及利用該變速馬 達6來控制承受輥4的旋轉速度和加速度的控制裝置7等。 該變速馬達6和該控制裝置7,能夠使筒體本體1按照可使筒 體本體1的內周面位置受到20〜5 0G離心力作用的旋轉速 度旋轉。而且其結構能夠在不超過用上記實驗式(A )求 出的時間τ的短時間內將旋轉速度加速到産生3 g以上的 離心力。9是用於向被支承旋轉裝置3支承的筒體本體1內 供給與披覆層形成厚度相應量自熔合金粉末的粉末供給裝 置’本實施方式中具有從端部送出粉末的粉末供給管j 〇, 和保持該粉末供給管10並能在管軸方向移動的料斗台車工工 等。13是用於對被筒體支承旋轉裝置3支承的筒體本體 長加熱的加熱裝置,本實施方式中可以使用沿著筒體本體 -20- (15) 1259851 全長對筒體本體1圓周方向的小區間進行感應加熱的面加 熱形線圈的感應線圈。 以下說明採用上述結構的內面披覆筒體的製造裝置來 製造內面披覆筒體的方法。首先準備金屬制的筒體本體i, 查明適於披覆其內周面的表面粗糙度。這裏對筒體本體i 內周面的表面粗糙度並無特別限制,但最好選定爲5〜2 0 微米Ra左右。處於此範圍內的表面粗糙度,可以容易地採 用兼有淸潔內周面操作的內表面噴砂法來形成。在查明筒 體本體內周面的表面粗糙度處於5〜20微米Ra範圍內,並 向筒體本體1內供給自熔合金粉末並使其沿軸線均等配置 後’使筒體本體1局速旋轉以便使之沿圓周方向均等分佈 時的加速過程中,能夠抑制因粉末在筒體軸線方向移動所 造成的厚度不均的現象,這是其優點。據認爲這是因爲在 筒體本體1的內周面上存在一些適當的凹凸,在其吸引下 可以抑制粉末沿筒體軸線方向移動的緣故。筒體本體內周 面上表面粗糙度越高,對粉末沿筒體軸線方向移動傾向的 抑制效果越顯著,要利用這種抑制效果雖然應當像上述般 地將表面粗糙度設定在5微米Ra以上,但若將此値設定在 20微米R a以上則幾乎不能指望粉末移動的抑制效果更進一 步地增加。另一方面,粗面加工會導致成本提高。考慮到 這些因素,將表面粗糙度上限定爲20微米Ra爲佳。 接著將筒體本體1置於筒體支承旋轉裝置3上使之處於 橫置狀態下,對該橫置的筒體本體1的內部,進行沿筒體 軸線方向均等配置與披覆層形成厚度相當的量自熔合金粉 -21 - 1259851 (16) 末2的操作。具體講,將粉末供給裝置9的粉末供給管i 〇插 入筒體本體1內部,向筒體本體i內軸線方向的適當位置( 一處或多處)裝入預定量自熔合金粉末2(參照第2圖(a )),抽出粉末供給管1 〇,用適當的蓋子1 5堵住筒體本體 1的兩端’然後使筒體本體1以該筒體本體1內的粉末不會 沿者筒體本體的圓周方向舖開的速度緩緩旋轉。介由於這 種旋轉’使裝入筒體本體1內的粉末2在筒體本體1內的軸 線方向均等舖開,如此就能夠沿著軸線方向均等配置(參 照第2圖(b ))。按此方法在用粉末供給管10向筒體本體 1裝入自熔合金粉末時,由於允許沿著筒體軸線方向不均 等地裝入粉末,所以優點是粉末裝入操作容易。 其中,對筒體本體1內部沿筒體軸線方向均等配置與 披覆層形成厚度相當的量自熔合金粉末的操作,並不限於 上記的方法,也可以採用其他方法。例如,將粉末供給管 10插入筒體本體1內,採用一邊從其端部以一定流量噴出 粉末’ 一邊使料斗台車i〗沿筒體軸線方向以一定速度移動 的方法’也能向筒體本體1內沿筒體軸線方向均等配置粉 末。另外,作爲向筒體本體1內裝入粉末的粉末供給管10 ’也可以採用在其側面形成具有沿軸線方向延伸的狹縫狀 噴出口或沿軸線方向並排排列的多個孔所構成的噴出口的 供給管,利用關閉該噴出口或使之朝上的狀態向粉末供給 管10內沿軸線方向均等地裝入自熔合金粉末,將該粉末供 給管1 〇插入筒體本體1內,然後打開該噴出口或使之朝下 ’將粉末供給管10內的自熔合金粉末供給筒體本體1內的 -22· (17) 1259851 方法,也能沿軸線方向均等地配置粉末。 向筒體本體1內沿筒體軸線方向均等地配置自熔合金 粉末2後,介由於筒體支承旋轉裝置3使筒體本體1以其軸 線爲中心旋轉’使旋轉速度在筒體本體1內周面位置上産 生2 0〜5 0 G的離心力。利用這種旋轉作用,使被裝入筒體 本體1內的自熔合金粉末2沿筒體本體圓周方向均等地舖開 並黏貼在筒體本體內周面上(參照第2圖(c ))。如此, 沿筒體本體圓周方向均等舖開並黏貼在筒體本體內周面上 的粉末2’在內周面位置上産生3G以上離心力的旋轉速度 下’在筒體本體內周面上幾乎不移動而保持其位置,因而 能夠在筒體本體內周面上形成和維持均一壁厚的粉末層。 然而,在筒體本體1的加速過程中,當內周面位置産生1〜 2G左右離心力的旋轉速度下,雖然粉末一度黏貼在筒體 本體內周面上,但由於離心力産生的約束力小,在筒體本 體1內周面上紋理等微觀上的方向性的作用下,粉末會發 生左右位置移動,導致粉末沿筒體軸線方向移動,如此往 往使筒體軸線方向産生厚度不均的傾向。因此,從筒體本 體1開始旋轉至加速到預定旋轉速度期間,應當在短時間 內將旋轉速度加速到能使筒體本體的內周面位置産生3 G 以上的離心力,以便使這種沿筒體軸線方向的厚度不均幾 乎不産生(即使産生也應處於容許的範圍內)。具體講, 對於查明內周面的表面粗糙度處於5〜20微米Ra的筒體本 體1而言,應當在不超出由以下實驗式(A): r (秒)= 3χ105/ϋ3 …(A) -23- (18) 1259851 求出的時間τ的短時間內,對筒體本體1進行 使該筒體本體1的旋轉速度在上述短時間內達到産 3 G以上離心力的旋轉速度。這種方法能使筒體本f 面上形成和黏貼厚度沿筒體軸線方向偏差極小的自 粉末層。其中有關此實驗式(A )的根據詳見後述 使筒體本體1旋轉達到在內周面位置産生20〜 心力的預定旋轉速度後,使筒體本體1保持在該旋 下,在繼續旋轉的狀態下用加熱裝置13加熱筒體二 使筒體本體內的粉末2熔融後,保持在該熔融狀態 可以在筒體本體1的內周面上形成自熔合金的金屬 。這裏前述金屬熔液內的熔融狀態,不一定僅指粉 完全熔融的狀態,而且還指至少一部分粉末熔融, 之間以及能夠熔融附著在筒體本體內周面上的狀態 ,用加熱裝置1 3對筒體本體1的加熱溫度,可以選擇 貼在筒體本體內周面上的自熔合金粉末至少部分溶 致於粉末之間以及能夠熔融附著在筒體本體內周面 ,具體講可以選擇超過自熔合金狀態圖中固相線的 一方面筒體本體1的加熱溫度越高,粉末熔融 就越大,最後完全變成熔融狀態。雖然據認爲在粉 處於熔融狀態下能夠形成更加緻密而且沒有氣孔和 熔融附著披覆層,但根據本發明人等的發現,即使 一定完全熔融,也能形成緻密而無氣孔和針孔的熔 披覆層。而且粉末一旦處於完全熔融狀態下,雖然 的流動性能使披覆層厚度沿筒體軸線方向均等,因 加速, 生上述 豊1內周 熔合金 D / 50G 離 轉速度 隹體1以 。如此 熔液層 末全體 使粉末 。因此 能使黏 融,以 的溫度 溫度。 的比例 末完全 針孔的 粉末不 融附著 熔融層 而即使 -24- (19) 1259851 黏貼在筒體本體內周面上的粉末層有厚度上的不均也能獲 得修飾,但如上所述,若粉末層形成時幾乎處於沒有厚度 不均的狀態下,則沒有必要以完全熔融狀態來修正厚度的 不均。另一方面,一旦使粉末完全熔融,就必須提高筒體 本體1的加熱溫度,這當然會增大熱能的消耗,而且加熱 時間也會延長。而且一旦處於超過自熔合金的液相線溫度 的完全熔融狀態下,有助於提高自熔合金硬度的金屬硼化 物或金屬矽化物等粒子會由於熔化或氧化消耗而減少,因 而出現硬度降低或混入氧化物的缺點。考慮到這些因素, 筒體本體1加熱溫度的上限應當選擇使筒體本體內自熔合 金的溫度不超過與該自熔合金熔融有關的液相線溫度;更 理想爲使自熔合金溶液的到達溫度,低於從與該自熔合金 的熔融和凝固有關的液相線溫度至固液共存溫度內距固相 線7 0 %位置處的溫度。 對自熔合金粉末層加熱熔融時筒體本體1的旋轉速度 ,如上所述,確定爲産生2 0〜5 0 G離心力作用的旋轉速度 。然而以往知道’將筒體本體內面形成的自熔合金粉末層 熔融緻密化之際,利用使筒體本體1旋轉的離心力的作用 ’增加從自;丨谷合金溶液除去氣泡的效果,在上記的專利文 獻2記載的方法中,在2G以上離心力作用狀態下進行熔融 處理。然而,介由於離心力除去氣泡的效果,在離心力提 高至7〜8 G之前隨著離心力的增加而提高,但離心力即使 增加到該數値以上,氣泡的除去效果也幾乎不增加,因此 以往離心力充其量處於10G以下◦與此相比,本實施方式 -25 - (20) 1259851 中卻採用2 0〜5 0 G的離心力。介由于如此高G的離心力, 不僅氣泡的除去效果好,而且存在於金屬熔液中比重低於 熔接金屬相的硬質陶瓷微粒子也具有向內徑側反離心聚集 的效果,如此能夠大幅度提高表面層的硬度。也就是說’ 自熔合金熔液中的熔接金屬是Ni (比重8.9 ) 、Cr (比重 8.5 ) 、Co (比重8.85 )等,而合金熔液中存在的硬質陶 瓷微粒子是比重處於6〜7範圍內的從金屬熔液中析出的鉻 系的硼化物(CrB :比重6.2 )、碳化物(Cr3C2 :比重 6.68,Cr7C3:比重6.92)或由其複合而成的硼碳化物(比 重6〜7左右)等。這些硬質陶瓷微粒子的比重雖然低於熔 接金屬相,但其差別不大,所以在以往進行的3〜8 G左右 的離心力下,幾乎不能在金屬熔液層的內徑側反離心聚集 ,在20〜5 0 G的高G離心力下才能實現在內徑側反離心聚 集。 使筒體本體1內周面的自熔合金粉末在熔融狀態下保 持的時間,設定在10〜180秒鐘的範圍內爲佳。此時間低 於10秒鐘時,金屬熔液與母體金屬的擴散接合不充分,或 低比重陶瓷微粒子在內徑側聚集得不充分;反之若超過 1 8 0秒鐘,則金屬熔液中的硬質陶瓷微粒子因熔化或氧化 消耗而減少,存在不能提高硬度或混入氧化物的缺點。鑒 於這些情況,在加熱筒體本體1以使筒體本體內的粉末2熔 融並保持熔融狀態的情況下’把筒體本體1的加熱設定爲 在內部的自熔合金粉末的溫度超過與該自熔合金熔融有關 的固相線溫度,但卻不超過液相線的溫度,同時將前述熔 -26- (21) 1259851 融狀態下的保持時間選定在1 0〜1 80秒鐘爲佳。 將自熔合金粉末在熔融狀態下保持預定時間後,繼續 使筒體本體1在旋轉下轉移到冷卻階段,使筒體本體1內的 熔融自熔合金凝固。這種冷卻可以採用爐內冷卻或保溫冷 卻、或放冷、空冷等任何的冷卻方法,但若冷卻過快,凝 固的自熔合金披覆層就會因熱應力而産生裂紋。因此,應 當實驗求出不會産生裂紋、時間又儘可能短的冷卻制度。 綜上所述,使自熔合金在筒體本體內周面全體一度熔 融附著,能夠形成自熔合金披覆層,其後將筒體本體1從 裝置取出,如第2圖(d)所示,能夠製成在筒體本體1的 內周面上具有自熔合金內面披覆層21的內面披覆筒體20。 所獲得的自熔合金內面披覆層21,表面(內周面)的硬度 極高,而且沿筒體軸線方向和圓周方向的厚度偏差極小。 用顯微鏡對用以上製程獲得的內面披覆筒體20的內面 披覆層21的斷面進行觀察後發現,如第3圖示意所示,內 面披覆層21具有由表面層21a、中間層21b和邊界層21c所 構成的層狀結構。表面層21 a成爲白色交叉狀組織和黑色 交叉狀組織部分混合存在的組織,各交叉狀組織部分成爲 一種熔接金屬(基體金屬)內多數微粒子狀析出物精細分 佈的組織。這種表面層2 1 a如後述的實施例1〜4所示,顯 示出極高的硬度(例如818〜927Hv)。可以看到微粒子 狀析出物呈板狀、塊狀和斑點狀等,測定其化學成分後發 現,其金屬成分的大部分是鉻。因此可以認爲’這種表面 層2 1 a由於使鉻系的硼化物、碳化物、硼碳化物等鉻化合 •27- (22) 1259851 物系硬質陶瓷微粒子以高密度分佈而使其成爲提高了硬度 的硬質層,因而顯示高硬度。中間層21b成爲一種在基體 金屬內的微粒子狀析出物呈少量分散的組織,其硬度低於 表面層。邊界層2 1 c成爲一種在基體金屬內的共晶析出物 呈極少量分散的層狀組織,其硬度更低。可以認爲,這是 由於高G下進行離心鑄造的結果,基體金屬內所含的硬質 陶瓷微粒子等非金屬介裝物向內徑側移動,邊界層2 1 c幾 乎成爲由基體金屬組成的淸淨層的緣故。該邊界層2 1 c由 於是幾乎沒有非金屬介裝物的淸淨層,所以韌性優良,利 用中間層2 1 b形成相當於傾斜組成結構而很好地支承硬質 表面層21a,同時與母體金屬(筒體本體1)形成伴隨良好 擴散的接合。如此,內面披覆層2 1不僅表面(內周面)的 硬度極高,而且還具有適當韌性以及與母體金屬的良好接 合性等特性,其耐磨損性、耐衝擊性和耐剝離性等也優良 〇 上述的內面披覆層21的表面層21a,雖然鉻成分濃度 越高硬度就越高且耐磨損性越優良,但若硬度太高,製造 就有困難。因此,表面層21a的鉻成分濃度選定在20〜40 質量%左右爲佳。邊界層2 1 c非金屬介裝物越少韌性就越 好,而且與母體金屬伴隨擴散的接合特性也越好,具體而 言,非金屬介裝物的顯微面積率在0.1 %以下爲佳。 上述實施方式中,對旋轉中的筒體本體1加熱,以使 內部自熔合金粉末熔融時,筒體本體內成爲有空氣進入的 狀態,但本發明不限於這種結構,本發明可以在筒體本體 -28- 1259851 (23) 內處於減壓狀態下進行,如此能使披覆層內氣孔極小化, 或在無氧化氣氛狀態下進行’如此也可以使自熔合金氧化 極小化。第4圖是顯示用於在筒體本體內處於減壓狀態下 進行自熔合金粉末加熱操作的製造裝置的一個實例。這種 製造裝置中,安裝在筒體本體1一端的蓋子15A與連接管 25連接,此連接管25利用旋轉接頭26與配管27連接,該配 管A上連接有開關閥28和真空泵29。其他結構與第1圖所 示的製造裝置相同。在使用第4圖的製造裝置的場合,如 第2圖(a )所示,向筒體本體1內供給自熔合金粉末2後, 如第4圖所示,在筒體本體1的兩端安裝蓋子1 5和1 5 A,將 筒體本體1兩端封閉的同時使內部與真空泵29連通,啓動 真空泵29以使筒體本體1內處於減壓狀態下,與上述的實 施方式同樣地使筒體本體1旋轉,讓20〜5 0 G離心力作用 於筒體本體1的內周面位置上,在該狀態下進行自熔合金 粉末的加熱熔融和凝固。如此能形成具有極高硬度表面層 的內面披覆層。另外,由於在加熱熔融時筒體本體1內處 於減壓下’所以金屬熔液內氣泡的除去效果高,能夠形成 殘存氣孔極小的內面披覆層。另外,不使用真空栗29而是 將其連接到供給惰性氣體的裝置上,使筒體本體1內充滿 惰性氣體,形成無氧化氣體氣氛,在該狀態下進行自熔合 金粉末的加熱熔融和凝固’也能使自熔合金的氧化極小化 。以上說明的各實施方式中’在筒體本體1的內周面上形 成自熔合金粉末層的時刻’筒體本體的內周面位置處已經 處於2 0〜5 0 G離心力的作用下’但本發明並不限於這種情 -29- (24) 1259851 況,也可以在自熔合金粉末層形成時,以對內周面位置施 加3 G以上適當離心力的旋轉速度使筒體本體1旋轉,在該 狀態下加熱熔融粉末層以形成金屬熔液後,再提高筒體本 體1的旋轉速度,作用以2 0〜5 0 G的離心力,在該狀態下 使之凝固。 第5圖是顯示在本發明其他實施方式中使用的內面披 覆筒體製造裝置。追種實施方式的製造裝置,與第4圖所 示的實施方式同樣,安裝在筒體本體1一端的蓋子15A與 連接管25連接,此連接管25利用旋轉接頭2 6與具有開關閥 28的配管27連接,但與第4圖所示的實施方式不同,該配 管27上連接具有壓力調節閥31和壓縮機32的加壓裝置。這 種加壓裝置的結構,能使筒體本體1內至少受0.3〜3 MPa氣 壓的作用。另外,也可以使用加壓鋼瓶來代替壓縮機3 2。 在這種場合,製成加壓鋼瓶與筒體本體1 一起旋轉的結構 ,可以省略旋轉接頭26。在使用加壓鋼瓶的場合,採用封 入了氮氣等惰性氣氛的加壓鋼瓶爲佳。其他結構與第1圖 的實施方式相同。 以下說明使用第5圖所示製造裝置的內面披覆筒體的 製造方法。本實施方式中也是向筒體本體1內供給自熔合 金粉末2 (參照第2圖(a )),然後用蓋子15和15 A封閉筒 體本體1的兩端,使筒體本體1緩緩旋轉,讓粉末2沿軸線 方向均等舖開。至此爲止的製程,與使用第1圖所示製造 裝置的場合相同。 在筒體本體1內沿筒體軸線方向配置自熔合金粉末2之 -30- (25) 1259851 後,利用筒體支承旋轉裝置3加速,直到在筒體本體1的內 周面上産生3G以上的離心力,理想爲産生10G以上離心力 的預定旋轉速度爲止,進而保持該旋轉速度。如此一來, 被裝入筒體本體1內的自熔合金粉末2就會沿著筒體本體圓 周方向均等舖開,黏貼在筒體本體內周面上。在這種場合 ,使筒體本體1向預定旋轉速度加速時,筒體本體1內周面 上形成的粉末層在筒體軸線方向幾乎不産生厚度偏差(即 使産生也處於容許範圍內),當加速到使內周面位置短時 間內産生3 G以上離心力的旋轉速度時,具體講,對內周 面表面的表面粗糙度爲5〜20微米Ra的筒體本體1而言,對 筒體本體1進行加速,使該筒體本體1的旋轉速度,在不超 過由以下實驗式(A ): r (秒)=3x105/D3 …(A ) 求出的時間r的短時間內達到産生上述3 G以上離心 力的旋轉速度。如此,能夠在筒體本體1內周面上形成和 黏貼上厚度沿筒體軸線方向上的偏差極小的自熔合金粉末 層。 達到産生3 G以上離心力的預定旋轉速度後,在該旋 轉速度下保持筒體本體1,在繼續旋轉的條件下,利用加熱 裝置1 3來加熱筒體本體1,以使筒體本體1內粉末2熔融後 保持熔融狀態。如此可以在筒體本體1的內周面上形成自 熔合金的熔液層。這種場合下,可以適當選擇用加熱裝置 1 3對筒體本體1加熱的溫度,使黏貼在筒體本體內周面 上的自熔合金粉末至少部分熔融,如此能使粉末相互之間 -31 - (26) 1259851 以及粉末在筒體本體內周面上熔融附著。具體講,可以選 擇超過自熔合金狀態圖中固相線的溫度。 在筒體本體1內形成金屬熔液層後,啓動壓縮機32使 筒體本體1內的金屬熔液表面處於0.3〜3MPa氣壓的作用下 。如此,殘存在金屬熔液內的氣孔在氣壓作用下被壓縮至 其體積減小,變得極爲細微。這裏將作用在金屬熔液表面 上的氣壓定在0 · 3〜3 Μ P a的理由是,低於此範圍時,氣孔 體積的減小效果小,而在超過此範圍的氣壓下,因氣壓增 大不僅使設備成本大幅度提高,而且氣孔體積的減小效果 也幾乎不再提高。將筒體本體1內周面的自熔合金粉末保 持在熔融狀態並處於0.3〜3MPa氣壓作用下的時間,處於 10〜180秒鐘範圍內爲佳。如此設定的理由是,此時間小 於1 0秒鐘時,與金屬熔液母體金屬的擴散接合不充分,或 氣孔壓縮引起體積減小的效果不充分,另一方面,若超過 180秒鐘,會有:金屬熔液中的硬質陶瓷微粒子就會因熔 化或氧化消耗而減少,從而不能提高硬度或産生混入氧化 物的弊端。 將自熔合金粉末在熔融狀態下保持預定的時間並以 〇 · 3〜3 Μ P a氣壓對其作用後,在保持該狀態下轉移到冷卻 階段,使筒體本體1內的熔融自熔合金凝固。利用以上方 法能夠形成殘存氣孔極少、硬度大的內面披覆層。 採用上記第5圖的製造裝置的內面披覆製程中,將筒 體本體1內周面上的粉末加熱熔融並對其內面施加〇_3〜 3 MPa氣壓的期間,施加在筒體本體1上的旋轉速度,如上 -32- (27) 1259851 所述,定爲在內周面上産生3 G以上離心力作用的旋轉速 度。這是因爲,在內周面上産生3G以上離心力作用的旋 轉速度下,筒體本體1的內周面上能夠沿圓周方向均等分 配粉末,同時分配後能夠阻止粉末沿圓周方向和軸線方向 移動,保持其位置,而且加熱熔融産生的金屬熔液能夠在 圓周方向保持一定厚度的緣故。也就是說,當作用在筒體 本體1內周面上的離心力處於3 G以上時,能夠形成厚度均 一的內面披覆層。 如上所述,爲了形成均一厚度的內面披覆層,雖然可 以將筒體本體1設定在使該內周面上作用3 G以上離心力的 旋轉速度下,但設定爲使筒體本體內周面位置産生10G以 上離心力的旋轉速度爲佳。如此,當使10G以上的離心力 作用在筒體本體1內周面上的金屬熔液層,在金屬熔液層 內包括厚度方向的全部區域內就會均等産生壓縮應力,加 壓氣體壓入口之類受壓行爲的波動將轉變成處於緩解的狀 恶下,在0.3〜3MPa氣壓對該金屬溶液層表面座生作用的 期間,能夠防止加壓氣體貫通金屬熔液層內的氣孔或貫通 金屬熔液層與筒體本體之間界面的現象出現。如此能夠形 成幾乎沒有針孔的內面披覆層。 此外,在使筒體本體內的金屬熔液層表面處於〇·3〜 3 MPa氣壓作用的狀態下進行離心鑄造時,也可以事先使 同體本體以在筒體本體內周面位置座生20〜50G離心力的 旋轉速度下旋轉。如此,使筒體本體內的金屬熔液層表面 處於0.3〜3 MPa氣壓作用的狀態下進行離心鑄造時’若使 -33- (28) 1259851 該金屬熔液層處於20〜5 0G離心力的作用下,不僅會因內 面披覆層內殘存的氣孔數量極微而能提高硬度,而且利用 施加20〜50G的離心力,還能使硬質微粒子反離心聚集在 內面披覆層的內徑側,從而可以提高表面硬度,因而能夠 製造具有硬度更高的內面披覆層的內面披覆筒體。 在使用第5圖的製造裝置的上記實施方式中,利用對 方疋轉中的同體本體1加熱使內部的自熔合金粉末溶融之際 ,筒體本體內成爲空氣進入的狀態,但本發明並不限於 這種結構,也可以使筒體本體內在處於減壓狀態下進行以 實現披覆層內的氣孔極小化,或在無氧化氣氛的狀態下進 行以實現自熔合金的氧化極小化。第6圖是顯示可以使筒 體本體內處於減壓狀態下進行自熔合金粉末加熱熔融操作 的製造裝置1個實例的示意圖。這種製造裝置中的旋轉接 頭26,不僅利用配管27與具有壓力調節閥31和壓縮機32的 加壓裝置相連接,而且還利用配管27 A與開關閥28 A和真 空泵29A相連接。其他結構與第5圖所示的製造裝置相同 。在使用第6圖所示製造裝置的場合,向筒體本體1內供給 自给合金粉末後’在筒體本體1的兩端安裝蓋子15和15A ’將筒體本體1的兩端關閉,首先啓動真空泵29A使筒體 本體1內處於減壓狀態下,與上記的實施方式同樣使筒體 本體1旋轉,使筒體本體1的內周面位置處於3 G以上離心 力作用下,在該狀態下進行自熔合金粉末的加熱熔融。進 而當形成熔融層後,停止真空泵29A,啓動壓縮機32使筒 體本體內的金屬熔液層的表面承受0.3〜3MPa氣壓的作用 -34- (29) 1259851 ,在該狀態下保持預定的時間後,進行冷卻和凝固。如此 能夠形成殘存氣孔更少的內面披覆層。其中,也可以與惰 性氣體供給裝置連接以代替真空泵29A,使筒體本體1內 充滿惰性氣體,形成無氧化氣體氣氛’在該狀態下進行自 熔合金粉末的加熱熔融,如此能夠實現自熔合金氧化的極 小化。 上記的各實施方式中,可以使用遍及筒體本體全長同 時對筒體本體1圓周方向的小區間進行感應加熱的直線狀 感應線圈(面加熱型線圈),作爲加熱筒體本體1的加熱 裝置1 3。採用這種結構的感應線圈的加熱裝置1 3能夠在短 時間內對筒體本體1全長均一加熱,由於筒體本體1以高速 旋轉,所以具有能在短時間內對筒體本體1全體均一加熱 的優點。然而,對筒體本體1的全長加熱的加熱裝置13 ’ 並不限於這種裝置,可以作適當變更’例如也可以使用設 置得大體沿著全長包圍筒體本體同時對筒體本體全體感應 加熱的多線圈形式的感應線圏。 以下說明爲導出上記實驗式(A )進行的實驗。 (1 ) 實驗1The self-fusing alloy is introduced into the self-fluxing alloy metal strontium solution, and any one of the chromium-based borides, carbides, and borides is equal or under the specific gravity, specifically, the specific gravity is 7 or less. Hard ceramics (for example, BN: specific gravity 2.34' B4C: specific gravity 2.47, Si3N4: specific gravity 3.2, SiC: specific gravity 3_21, V2O5: specific gravity 3.36, V〇2: specific gravity 4.34, TiB2: specific gravity 4·5, V203: specific gravity 4.8, TiC : Microparticles having a specific gravity of 4.94, TiB: specific gravity of 5.09, TiN: specific gravity of 5.43, V0: specific gravity of 5.76, VC: specific gravity of 5.77, ZrB2: specific gravity of 6.08, ZrC: specific gravity of 6_73, NbB2: specific gravity of 6.97, or a composite thereof. 3 is a cylindrical body supporting rotation device that horizontally supports and rotates the cylindrical body 1. In the present embodiment, the two receiving rolls 4 that support the lower side of the cylindrical body 1 are pressed against the upper side of the cylindrical body 1. 5 (omitted in FIG. 1), a shift motor 6 that rotationally drives the two receiving rolls 4, and a control device 7 that controls the rotational speed and acceleration of the receiving roller 4 by the shift motor 6. The shift motor 6 and the control device 7 are capable of rotating the tubular body 1 at a rotational speed at which the inner circumferential surface of the cylindrical body 1 is subjected to a centrifugal force of 20 to 50 G. Further, the structure can accelerate the rotational speed to a centrifugal force of 3 g or more in a short time not exceeding the time τ obtained by the above experimental formula (A). 9 is a powder supply device for supplying a self-fluxing alloy powder having a thickness corresponding to the thickness of the coating layer to the inside of the cylindrical body 1 supported by the supporting rotating device 3. In the present embodiment, the powder supply pipe j is fed from the end portion. 〇, and a hopper trolley worker or the like that holds the powder supply pipe 10 and is movable in the tube axis direction. 13 is a heating device for heating the length of the cylindrical body supported by the cylindrical support rotating device 3. In the present embodiment, the circumferential direction of the cylindrical body 1 can be used along the entire length of the tubular body -20-(15) 1259851. The induction coil of the surface heating coil that inductively heats the small section. Next, a method of manufacturing the inner cladding cylinder by the apparatus for manufacturing the inner cladding cylinder of the above configuration will be described. First, the metal body i of the metal is prepared, and the surface roughness suitable for covering the inner peripheral surface thereof is ascertained. Here, the surface roughness of the inner peripheral surface of the cylindrical body i is not particularly limited, but is preferably selected to be about 5 to 20 μm Ra. The surface roughness within this range can be easily formed by the inner surface blasting method which has the operation of the chamfer inner peripheral surface. After the surface roughness of the inner circumferential surface of the cylindrical body is found to be in the range of 5 to 20 μm Ra, and the self-fluxing alloy powder is supplied into the cylindrical body 1 and uniformly arranged along the axis, the cylindrical body 1 is made to have a local velocity. In the acceleration process when rotating so as to be evenly distributed in the circumferential direction, it is possible to suppress the phenomenon of uneven thickness due to the movement of the powder in the axial direction of the cylinder, which is an advantage. This is considered to be because there are some irregularities on the inner peripheral surface of the cylindrical body 1, and the suction of the powder in the axial direction of the cylinder can be suppressed. The higher the surface roughness of the inner surface of the cylinder body, the more significant the effect of suppressing the tendency of the powder to move along the axial direction of the cylinder. To use this suppression effect, the surface roughness should be set to 5 μRa or more as described above. However, if the enthalpy is set to 20 μm or more, it is hardly expected that the effect of suppressing the movement of the powder is further increased. On the other hand, rough surface processing leads to increased costs. In view of these factors, it is preferable to limit the surface roughness to 20 μm Ra. Next, the cylindrical body 1 is placed on the cylindrical support rotating device 3 so as to be in a horizontal state, and the inside of the horizontally cylindrical body 1 is uniformly disposed in the axial direction of the tubular body to be equal to the thickness of the coating layer. The amount of self-melting alloy powder-21 - 1259851 (16) at the end of the 2 operation. Specifically, the powder supply tube i of the powder supply device 9 is inserted into the inside of the cylindrical body 1, and a predetermined amount of self-fluxing alloy powder 2 is loaded into an appropriate position (one or more) in the axial direction of the cylindrical body i (refer to In Fig. 2(a)), the powder supply pipe 1 is pulled out, and the both ends of the cylindrical body 1 are blocked by a suitable cover 15 and then the cylindrical body 1 is not covered by the powder in the cylindrical body 1. The speed at which the cylindrical body is spread in the circumferential direction is gradually rotated. Since the powder 2 inserted into the cylindrical body 1 is evenly spread in the axial direction of the cylindrical body 1 by this rotation, it can be equally arranged along the axial direction (refer to Fig. 2(b)). According to this method, when the self-fluxing alloy powder is charged into the cylindrical body 1 by the powder supply tube 10, since the powder is allowed to be unevenly distributed in the axial direction of the cylinder, there is an advantage that the powder loading operation is easy. Here, the operation of uniformly arranging the self-fluxing alloy powder in the cylinder body 1 in the axial direction of the cylinder in a thickness corresponding to the thickness of the coating layer is not limited to the above method, and other methods may be employed. For example, the powder supply pipe 10 is inserted into the tubular body 1 and the hopper hopper i is moved at a constant speed in the cylinder axis direction while discharging the powder at a constant flow rate from the end portion thereof. 1 The powder is uniformly disposed along the axial direction of the cylinder. In addition, as the powder supply tube 10' in which the powder is placed in the cylindrical body 1, a slit having a slit-like discharge port extending in the axial direction or a plurality of holes arranged side by side in the axial direction may be formed on the side surface thereof. The supply pipe of the outlet is uniformly filled with the self-fluxing alloy powder in the axial direction of the powder supply pipe 10 by closing the discharge port or facing upward, and the powder supply pipe 1 is inserted into the cylindrical body 1, and then It is also possible to arrange the powder evenly in the axial direction by opening the discharge port or causing the self-fluxing alloy powder in the powder supply pipe 10 to be supplied to the inside of the cylindrical body 1 by the method of -22·(17) 1259851. After the self-fluxing alloy powder 2 is uniformly disposed in the cylindrical body 1 in the direction of the cylinder axis, the cylindrical body 1 is rotated about the axis thereof by the cylindrical body supporting the rotating device 3, so that the rotational speed is within the cylindrical body 1 A centrifugal force of 20 to 50 G is generated at the circumferential position. By this rotation, the self-fluxing alloy powder 2 placed in the cylindrical body 1 is evenly spread in the circumferential direction of the cylindrical body and adhered to the inner peripheral surface of the cylindrical body (see Fig. 2(c)). In this way, the powder 2' which is uniformly spread in the circumferential direction of the tubular body and adhered to the circumferential surface of the cylindrical body body 2' produces a centrifugal force at a centrifugal force of 3 G or more at the inner circumferential surface position, which is hardly on the inner circumference of the cylindrical body. By moving and maintaining its position, it is possible to form and maintain a powder layer of uniform wall thickness on the inner peripheral surface of the cylindrical body. However, in the acceleration process of the tubular body 1, when the inner circumferential surface position generates a centrifugal force of about 1 to 2 G centrifugal force, although the powder is once adhered to the inner circumferential surface of the cylinder body, the binding force due to the centrifugal force is small. Under the action of microscopic directionality on the inner circumferential surface of the cylindrical body 1, the powder moves to the left and right positions, and the powder moves in the axial direction of the cylinder. This tends to cause uneven thickness in the axial direction of the cylinder. Therefore, during the rotation from the cylinder body 1 to the acceleration to the predetermined rotation speed, the rotation speed should be accelerated in a short time so that the centrifugal force of the inner circumferential surface of the cylinder body can generate 3 G or more, so that the cylinder can be made The thickness unevenness in the body axis direction hardly occurs (it should be within an allowable range even if it is generated). Specifically, for the cylinder body 1 in which the surface roughness of the inner peripheral surface is 5 to 20 μm Ra, it should not exceed the following experimental formula (A): r (second) = 3 χ 105 / ϋ 3 ... (A -23- (18) 1259851 In a short time of the obtained time τ, the cylindrical body 1 is subjected to a rotational speed at which the rotational speed of the tubular body 1 reaches a centrifugal force of 3 G or more in the short time. This method enables the formation and adhesion of the self-powder layer having a thickness which is extremely small along the axial direction of the cylinder on the f-face of the cylinder. In the case where the cylindrical body 1 is rotated to a predetermined rotational speed of 20 to a heart force at the inner circumferential surface position, the cylindrical body 1 is held in the rotation and continues to rotate. In the state where the cylindrical body 2 is heated by the heating device 13, the powder 2 in the cylindrical body is melted, and the molten metal can be formed on the inner peripheral surface of the cylindrical body 1 in the molten state. Here, the molten state in the molten metal does not necessarily mean only a state in which the powder is completely melted, and also refers to a state in which at least a part of the powder is melted, and can be melted and adhered to the circumferential surface of the cylindrical body, and the heating device 13 is used. The heating temperature of the cylindrical body 1 can be selected to be at least partially dissolved between the powders and adhered to the circumferential surface of the body of the cylinder, and can be selected to exceed In the self-fluxing alloy state diagram, on the one hand, the higher the heating temperature of the cylindrical body 1 is, the larger the powder is melted, and finally the molten state is completely formed. Although it is considered that the powder can be formed to be denser and has no pores and a molten adhesion coating layer in the molten state, according to the findings of the present inventors, even if it is completely melted, it is possible to form a dense and non-porous and pinhole melting. Covered layer. Moreover, once the powder is in a completely molten state, although the flow property is such that the thickness of the coating layer is equal along the axial direction of the cylinder, due to the acceleration, the inner circumference of the crucible 1 is melted at the D / 50G speed of the crucible 1 . Thus, the entire layer of the melt layer is powdered. Therefore, it can be fused to the temperature and temperature. At the end of the ratio, the powder of the completely pinhole does not adhere to the molten layer, and even if the thickness of the powder layer adhered to the inner surface of the body of the cylinder body - 24 - (19) 1259851 can be modified, as described above, If the powder layer is formed in a state where there is almost no thickness unevenness, it is not necessary to correct the thickness unevenness in a completely molten state. On the other hand, once the powder is completely melted, it is necessary to increase the heating temperature of the cylindrical body 1, which of course increases the consumption of heat energy, and the heating time is also prolonged. Moreover, once in a completely molten state exceeding the liquidus temperature of the self-fluxing alloy, particles such as metal boride or metal telluride which contribute to increase the hardness of the self-melting alloy may be reduced due to melting or oxidation consumption, thereby causing a decrease in hardness or Disadvantages of mixing oxides. In consideration of these factors, the upper limit of the heating temperature of the barrel body 1 should be selected such that the temperature of the self-fluxing alloy in the body of the cylinder does not exceed the liquidus temperature associated with the melting of the self-fluxing alloy; more preferably, the arrival of the self-fluxing alloy solution The temperature is lower than the temperature from the liquidus temperature associated with the melting and solidification of the self-fusing alloy to the 70% position of the solidus line within the solid-liquid coexistence temperature. The rotational speed of the cylindrical body 1 when the self-fluxing alloy powder layer is heated and melted is determined to be a rotational speed at which a centrifugal force of 20 to 50 G is generated as described above. However, it has been known in the past that when the self-fluxing alloy powder layer formed on the inner surface of the cylinder body is melted and densified, the effect of removing the air bubbles from the silicon alloy solution by increasing the centrifugal force of the cylindrical body 1 is increased. In the method described in Patent Document 2, the melting treatment is performed under a centrifugal force of 2 G or more. However, the effect of removing the bubbles by the centrifugal force increases as the centrifugal force increases before the centrifugal force is increased to 7 to 8 G. However, even if the centrifugal force increases above the number, the effect of removing the bubbles hardly increases, so that the centrifugal force at the time is at best In the present embodiment -25 - (20) 1259851, a centrifugal force of 20 to 50 G is used. Due to the centrifugal force of such a high G, not only the effect of removing bubbles is good, but also the hard ceramic particles having a specific gravity lower than that of the molten metal phase in the molten metal have the effect of centrifugally collecting toward the inner diameter side, so that the surface can be greatly improved. The hardness of the layer. That is to say, the fusion metal in the molten metal melt is Ni (specific gravity 8.9), Cr (specific gravity 8.5), Co (specific gravity 8.85), etc., and the hard ceramic microparticles present in the alloy melt are in the range of 6 to 7. A chromium-based boride (CrB: specific gravity 6.2), a carbide (Cr3C2: specific gravity 6.68, Cr7C3: specific gravity: 6.92) precipitated from the molten metal, or a boron carbide compounded by the composite (about 6 to 7 specific gravity) )Wait. Although the specific gravity of these hard ceramic fine particles is lower than that of the welded metal phase, the difference is not large. Therefore, under the centrifugal force of about 3 to 8 G which has been conventionally performed, it is almost impossible to centrifugally concentrate on the inner diameter side of the molten metal layer. The high-G centrifugal force of ~50 G can achieve reverse centrifugal concentration on the inner diameter side. The time during which the self-melting alloy powder on the inner peripheral surface of the cylindrical body 1 is maintained in a molten state is preferably set in the range of 10 to 180 seconds. When the time is less than 10 seconds, the diffusion bonding of the molten metal to the parent metal is insufficient, or the low specific gravity ceramic fine particles are insufficiently aggregated on the inner diameter side; if it is more than 180 seconds, the molten metal is in the molten metal. Hard ceramic fine particles are reduced by melting or oxidation consumption, and there is a disadvantage that hardness cannot be increased or oxides are mixed. In view of these circumstances, in the case where the cylindrical body 1 is heated so that the powder 2 in the cylindrical body is melted and maintained in a molten state, the heating of the cylindrical body 1 is set such that the temperature of the self-fluxing alloy powder inside exceeds the self. The solidus temperature of the molten alloy is melted, but does not exceed the temperature of the liquidus, and the holding time of the melted -26-(21) 1259851 is preferably selected from 10 to 180 seconds. After the self-fluxing alloy powder is held in a molten state for a predetermined time, the cylindrical body 1 is continuously transferred to the cooling stage under rotation to solidify the molten self-melting alloy in the cylindrical body 1. This cooling may be carried out by any cooling method such as cooling in the furnace or cooling, or cooling, air cooling, etc., but if the cooling is too fast, the solidified self-fluxing alloy coating may be cracked by thermal stress. Therefore, it is necessary to experimentally find a cooling system that does not cause cracks and that is as short as possible. As described above, the self-fluxing alloy is once melted and adhered to the entire circumference of the cylindrical body, and a self-fluxing alloy coating layer can be formed, and then the cylindrical body 1 is taken out from the apparatus as shown in Fig. 2(d). The inner surface covering cylinder 20 having the self-fusing alloy inner surface coating layer 21 on the inner circumferential surface of the cylindrical body 1 can be formed. The inner surface of the self-fluxing alloy coating layer 21 has an extremely high hardness on the surface (inner peripheral surface), and the thickness deviation in the axial direction of the cylinder and the circumferential direction is extremely small. When the cross section of the inner cladding layer 21 of the inner cladding cylinder 20 obtained by the above process was observed with a microscope, it was found that, as schematically shown in Fig. 3, the inner cladding layer 21 had the surface layer 21a. A layered structure composed of the intermediate layer 21b and the boundary layer 21c. The surface layer 21a is a structure in which a white cross-shaped structure and a black cross-shaped structure are mixed, and each of the intersecting-like structures becomes a finely distributed structure of a plurality of fine-particle precipitates in a weld metal (base metal). Such a surface layer 2 1 a exhibits an extremely high hardness (e.g., 818 to 927 Hv) as shown in Examples 1 to 4 to be described later. It can be seen that the fine particles precipitated in a plate shape, a block shape, and a spot shape, and the chemical composition thereof was measured, and it was found that most of the metal components were chromium. Therefore, it can be considered that the surface layer 2 1 a is improved by high-density distribution of chromium-based borides, carbides, borides, and the like. The 27-(22) 1259851 hard ceramic fine particles are distributed at a high density. A hard layer of hardness, thus showing high hardness. The intermediate layer 21b is a structure in which fine particles of precipitates in the base metal are dispersed in a small amount, and the hardness thereof is lower than that of the surface layer. The boundary layer 2 1 c becomes a layered structure in which a eutectic precipitate in the base metal is dispersed in a very small amount and has a lower hardness. It is considered that this is because the centrifugal casting at high G results that the non-metallic filler such as hard ceramic fine particles contained in the base metal moves toward the inner diameter side, and the boundary layer 2 1 c becomes almost a matrix composed of the base metal. The sake of the net layer. Since the boundary layer 2 1 c is a clean layer having almost no non-metallic media, the toughness is excellent, and the intermediate layer 2 1 b is formed to form a structure corresponding to the inclined structure to support the hard surface layer 21a well, and the parent metal (The barrel body 1) forms a joint with good diffusion. Thus, the inner surface coating layer 2 1 has not only the surface (internal peripheral surface) but also has excellent toughness and good adhesion to the parent metal, and its abrasion resistance, impact resistance and peeling resistance. The surface layer 21a of the inner surface coating layer 21 described above is also excellent in hardness, and the higher the chromium component concentration, the higher the hardness and the more excellent the abrasion resistance. However, if the hardness is too high, it is difficult to manufacture. Therefore, the chromium component concentration of the surface layer 21a is preferably about 20 to 40% by mass. The less the toughness of the boundary layer 2 1 c non-metallic media, the better the bonding property with the diffusion of the parent metal, in particular, the microscopic area ratio of the non-metallic media is preferably 0.1% or less. . In the above embodiment, the rotating main body 1 is heated to melt the inner self-fluxing alloy powder, and the inside of the cylinder body is in a state in which air enters. However, the present invention is not limited to this configuration, and the present invention can be used in the cylinder. The body body -28-1259851 (23) is carried out under reduced pressure, so that the pores in the coating layer can be minimized, or in the absence of an oxidizing atmosphere. Thus, the oxidation of the self-fluxing alloy can be minimized. Fig. 4 is a view showing an example of a manufacturing apparatus for performing a self-fluxing alloy powder heating operation under a reduced pressure state in the cylindrical body. In the manufacturing apparatus, the cover 15A attached to one end of the tubular body 1 is connected to the connecting pipe 25, and the connecting pipe 25 is connected to the pipe 27 by a rotary joint 26 to which an on-off valve 28 and a vacuum pump 29 are connected. The other structure is the same as that of the manufacturing apparatus shown in Fig. 1. When the manufacturing apparatus of Fig. 4 is used, as shown in Fig. 2(a), after the self-fusing alloy powder 2 is supplied into the cylindrical body 1, as shown in Fig. 4, at both ends of the cylindrical body 1. The lids 15 and 15A are attached, and the inside of the cylinder main body 1 is closed, and the inside is connected to the vacuum pump 29, and the vacuum pump 29 is activated to depressurize the inside of the cylinder main body 1, and the same as in the above-described embodiment. The cylindrical body 1 is rotated, and a centrifugal force of 20 to 50 G is applied to the inner peripheral surface of the cylindrical body 1, and in this state, the self-melting alloy powder is heated and melted and solidified. This makes it possible to form an inner cladding layer having an extremely high hardness surface layer. Further, since the inside of the cylindrical body 1 is under reduced pressure during heating and melting, the effect of removing bubbles in the molten metal is high, and an inner coating layer having a small remaining pore can be formed. Further, instead of using the vacuum pump 29, it is connected to a device for supplying an inert gas, and the inside of the cylindrical body 1 is filled with an inert gas to form an atmosphere of no oxidizing gas, and in this state, heating, melting and solidification of the self-fluxing alloy powder are performed. 'Also can minimize the oxidation of the self-fluxing alloy. In each embodiment described above, 'the time at which the self-fusing alloy powder layer is formed on the inner peripheral surface of the cylindrical body 1' is already at the position of the inner peripheral surface of the cylindrical body at the centrifugal force of 20 to 50 G. The present invention is not limited to the case of the case -29-(24) 1259851, and the cylindrical body 1 may be rotated at a rotational speed of 3 G or more by applying an appropriate centrifugal force to the inner circumferential surface position when the self-fluxing alloy powder layer is formed. After the molten powder layer is heated in this state to form a molten metal, the rotation speed of the cylindrical body 1 is increased, and the centrifugal force of 20 to 50 G is applied to solidify the mixture in this state. Fig. 5 is a view showing an inner-coated cylindrical body manufacturing apparatus used in another embodiment of the present invention. In the manufacturing apparatus of the embodiment, the cover 15A attached to one end of the tubular body 1 is connected to the connection pipe 25 by the rotary joint 26 and the switch valve 28, as in the embodiment shown in Fig. 4 . Although the piping 27 is connected, unlike the embodiment shown in Fig. 4, the piping 27 is connected to a pressurizing device having a pressure regulating valve 31 and a compressor 32. The structure of the pressurizing device enables the cylinder body 1 to be subjected to at least a gas pressure of 0.3 to 3 MPa. Alternatively, a pressurized steel cylinder may be used instead of the compressor 3 2 . In this case, the structure in which the pressurized cylinder is rotated together with the cylindrical body 1 can be omitted, and the rotary joint 26 can be omitted. In the case of using a pressurized cylinder, a pressurized cylinder in which an inert atmosphere such as nitrogen is sealed is preferred. The other structure is the same as that of the embodiment of Fig. 1. Next, a method of manufacturing the inner coated cylinder using the manufacturing apparatus shown in Fig. 5 will be described. In the present embodiment, the self-melting alloy powder 2 is also supplied into the cylindrical body 1 (see Fig. 2(a)), and then both ends of the cylindrical body 1 are closed by the covers 15 and 15 A, so that the cylindrical body 1 is slowly lowered. Rotate to allow the powder 2 to spread evenly along the axis. The process up to this point is the same as the case of using the manufacturing apparatus shown in Fig. 1. After the -30-(25) 1259851 of the self-fluxing alloy powder 2 is disposed in the cylindrical body 1 in the axial direction of the cylinder, the cylinder is supported by the rotating device 3 to accelerate until the inner circumferential surface of the cylindrical body 1 is 3 G or more. The centrifugal force is preferably a predetermined rotational speed at which a centrifugal force of 10 G or more is generated, and the rotational speed is maintained. As a result, the self-fluxing alloy powder 2 loaded into the cylindrical body 1 is uniformly spread along the circumferential direction of the cylindrical body and adhered to the inner peripheral surface of the cylindrical body. In this case, when the cylindrical body 1 is accelerated at a predetermined rotational speed, the powder layer formed on the inner circumferential surface of the cylindrical body 1 hardly causes thickness deviation in the axial direction of the cylinder (even within the allowable range even when generated). When the rotational speed of the centrifugal force of 3 G or more is generated in a short time in the inner circumferential surface position, specifically, the cylindrical body 1 having a surface roughness of 5 to 20 μm on the inner circumferential surface is applied to the cylindrical body 1 is accelerated so that the rotation speed of the cylindrical body 1 reaches the above-mentioned 3 in a short time not exceeding the time r obtained by the following experimental formula (A): r (second) = 3x105 / D3 (A) The rotational speed of the centrifugal force above G. In this manner, the self-fluxing alloy powder layer having a thickness which is extremely small in the axial direction of the cylinder can be formed and adhered to the inner circumferential surface of the cylindrical body 1. After reaching a predetermined rotational speed at which a centrifugal force of 3 G or more is generated, the cylindrical body 1 is held at the rotational speed, and the cylindrical body 1 is heated by the heating device 13 under the condition of continued rotation so that the powder in the cylindrical body 1 is made. 2 After melting, it remains in a molten state. Thus, a molten layer of a self-fluxing alloy can be formed on the inner peripheral surface of the cylindrical body 1. In this case, the temperature at which the tubular body 1 is heated by the heating device 13 can be appropriately selected so that the self-fluxing alloy powder adhered to the inner peripheral surface of the cylindrical body is at least partially melted, so that the powders can be mutually-31 - (26) 1259851 and the powder is fused to the inner surface of the cylinder body. Specifically, the temperature of the solidus line in the self-fluxing alloy state diagram can be selected. After the molten metal layer is formed in the cylindrical body 1, the compressor 32 is started to cause the molten metal surface in the cylindrical body 1 to be under the pressure of 0.3 to 3 MPa. Thus, the pores remaining in the molten metal are compressed under the action of the gas pressure to a reduced volume and become extremely fine. Here, the reason why the gas pressure acting on the surface of the molten metal is set to 0 · 3 to 3 Μ P a is that, below this range, the effect of reducing the pore volume is small, and at a pressure exceeding the range, the gas pressure is The increase not only greatly increases the cost of the equipment, but also the effect of reducing the pore volume is hardly increased. It is preferable that the self-fluxing alloy powder on the inner peripheral surface of the cylindrical body 1 is maintained in a molten state at a pressure of 0.3 to 3 MPa, preferably in the range of 10 to 180 seconds. The reason for this setting is that when the time is less than 10 seconds, the diffusion bonding with the molten metal metal is insufficient, or the effect of reducing the volume due to the pore compression is insufficient. On the other hand, if it exceeds 180 seconds, There are: the hard ceramic particles in the molten metal are reduced by melting or oxidation, so that the hardness or the incorporation of oxides cannot be increased. After the self-fluxing alloy powder is held in a molten state for a predetermined period of time and is acted upon by a pressure of 〇·3 〜 3 Μ P a , it is transferred to a cooling stage while maintaining the state, so that the molten solid alloy in the cylindrical body 1 is made. solidification. By the above method, it is possible to form an inner surface coating layer having few residual pores and high hardness. In the inner surface coating process of the manufacturing apparatus of the fifth drawing, the powder on the inner peripheral surface of the cylindrical body 1 is heated and melted, and a pressure of 〇3 to 3 MPa is applied to the inner surface thereof, and applied to the cylindrical body. The rotation speed at 1 is as described above in the -32-(27) 1259851, and the rotation speed at which the centrifugal force of 3 G or more is generated on the inner peripheral surface is determined. This is because, on the inner peripheral surface, at the rotational speed at which the centrifugal force of 3 G or more is generated, the inner peripheral surface of the cylindrical body 1 can equally distribute the powder in the circumferential direction, and at the same time, the powder can be prevented from moving in the circumferential direction and the axial direction after the distribution. The position is maintained, and the molten metal produced by heating and melting can maintain a certain thickness in the circumferential direction. In other words, when the centrifugal force acting on the inner circumferential surface of the cylindrical body 1 is at least 3 G, an inner coating layer having a uniform thickness can be formed. As described above, in order to form the inner surface coating layer having a uniform thickness, the cylindrical body 1 can be set at a rotational speed at which a centrifugal force of 3 G or more is applied to the inner peripheral surface, but the inner peripheral surface of the cylindrical body is set. The rotational speed at which the position generates a centrifugal force of 10 G or more is preferable. In this manner, when a centrifugal force of 10 G or more is applied to the molten metal layer on the inner peripheral surface of the cylindrical body 1, the compressive stress is uniformly generated in all the regions including the thickness direction in the molten metal layer, and the pressurized gas is pressurized. The fluctuation of the pressure-like behavior will be transformed into a relief-like state. During the period of 0.3~3 MPa pressure on the surface of the metal solution layer, it is possible to prevent the pressurized gas from penetrating through the pores in the molten metal layer or through the molten metal. The phenomenon of the interface between the liquid layer and the body of the cylinder occurs. This makes it possible to form an inner coating layer having almost no pinholes. Further, when centrifugal casting is performed in a state where the surface of the molten metal layer in the cylindrical body body is at a pressure of 〇3 to 3 MPa, the body of the same body may be previously placed in the circumferential position of the cylindrical body. Rotate at a rotational speed of ~50G centrifugal force. In this way, when the surface of the molten metal layer in the body of the cylinder is subjected to centrifugal casting under the action of a pressure of 0.3 to 3 MPa, the effect of the -35- (28) 1259851 molten metal layer on the centrifugal force of 20 to 50 G is obtained. In addition, not only the amount of pores remaining in the inner coating layer is extremely small, but also the hardness can be increased, and by applying a centrifugal force of 20 to 50 G, the hard microparticles can be centrifugally collected on the inner diameter side of the inner coating layer. The surface hardness can be increased, and thus it is possible to manufacture an inner coated cylinder having a higher hardness inner coating layer. In the above-described embodiment using the manufacturing apparatus of FIG. 5, when the internal self-fluxing alloy powder is melted by the heating of the body 1 in the other side, the inside of the cylinder body enters the air, but the present invention The inside of the cylindrical body is not limited to this configuration, and the pores in the coating layer may be minimized or may be performed in an oxidizing atmosphere to minimize oxidation of the self-fluxing alloy. Fig. 6 is a schematic view showing an example of a manufacturing apparatus which can perform a self-melting alloy powder heating and melting operation in a state where the cylindrical body is under a reduced pressure. The rotary joint 26 in the manufacturing apparatus is connected not only to the pressurizing means having the pressure regulating valve 31 and the compressor 32 by the piping 27, but also to the switching valve 28A and the vacuum pump 29A by the piping 27A. The other structure is the same as that of the manufacturing apparatus shown in Fig. 5. When the manufacturing apparatus shown in Fig. 6 is used, after the self-feeding alloy powder is supplied into the cylindrical body 1, 'the cover 15 and 15A are attached to both ends of the cylindrical body 1', and both ends of the cylindrical body 1 are closed, first started. When the inside of the cylindrical body 1 is in a reduced pressure state, the vacuum pump 29A rotates the tubular body 1 in the same manner as the above-described embodiment, and the inner circumferential surface position of the cylindrical body 1 is subjected to a centrifugal force of 3 G or more, and is performed in this state. The self-melting alloy powder is heated and melted. Further, after the molten layer is formed, the vacuum pump 29A is stopped, and the compressor 32 is started to cause the surface of the molten metal layer in the body of the cylinder to withstand the pressure of 0.3 to 3 MPa - 34 - (29) 1259851, and maintained in this state for a predetermined period of time. After that, it is cooled and solidified. In this way, it is possible to form an inner coating layer with less residual pores. In place of the vacuum pump 29A, the cylinder body 1 may be filled with an inert gas to form an atmosphere of no oxidizing gas. In this state, the self-melting alloy powder is heated and melted, so that the self-fluxing alloy can be realized. Minimization of oxidation. In each of the above-described embodiments, a linear induction coil (surface heating type coil) that inductively heats the cells in the circumferential direction of the cylindrical body 1 over the entire length of the cylindrical body can be used as the heating device 1 for heating the cylindrical body 1. 3. The heating device 13 of the induction coil having such a configuration can uniformly heat the entire length of the cylindrical body 1 in a short time, and since the cylindrical body 1 is rotated at a high speed, it is possible to uniformly heat the entire cylinder body 1 in a short time. The advantages. However, the heating device 13' that heats the entire length of the tubular body 1 is not limited to such a device, and may be appropriately changed. For example, it is also possible to use a body that is generally provided to surround the tubular body along the entire length while inductively heating the entire body of the cylinder. Inductive coils in the form of multiple coils. The following is an experiment for deriving the above experimental formula (A). (1) Experiment 1
作爲筒體本體1,準備了以下形狀的筒體本體樣品A 、B 和 C。 樣品A :外徑125毫米X內徑44毫米X長度1250毫米 材料:SCM410 內周面:噴砂加工(內周面粗糙度20微米Ra) -35- (30) 1259851 樣mB·外徑125毫米χ內徑44毫米χ長度125〇毫米 材料·· S C Μ 4 1 0 內周面:噴砂加工(內周面粗糙度5微米Ra ) f永品C.外徑125毫米X內徑44毫米x長度1250毫米 材料:S C Μ 4 1 0 內周面:珩磨加工(內周面粗糙度0.5微米R a) 在以下條件下,用第1圖、第2圖所示的裝置分別對這 些樣品A、B和C的內周面進行了自熔合金披覆加工。 自熔合金粉末:霍加納海綿鐵粉(Hoganas)#1355-20As the cylindrical body 1, cylindrical body samples A, B, and C of the following shapes were prepared. Sample A: outer diameter 125 mm X inner diameter 44 mm X length 1250 mm Material: SCM410 Inner peripheral surface: sandblasting (internal circumferential surface roughness 20 μm Ra) -35- (30) 1259851 sample mB · outer diameter 125 mm χ Inner diameter 44 mm χ length 125 〇 mm material ·· SC Μ 4 1 0 Inner circumferential surface: sandblasting (internal circumferential surface roughness 5 μm Ra) f permanent product C. outer diameter 125 mm X inner diameter 44 mm x length 1250 Millimeter material: SC Μ 4 1 0 Inner circumferential surface: honing processing (internal circumferential surface roughness 0.5 μm R a) These samples A and B are respectively used in the apparatus shown in Fig. 1 and Fig. 2 under the following conditions. The inner peripheral surface of C was subjected to self-fluxing alloy coating. Self-fluxing alloy powder: Hogana sponge iron powder (Hoganas) #1355-20
固相線溫度:970°C 液相線溫度:1 0 7 0 °C 粉末的裝入:在筒體本體1內的一處裝入2.5千克粉末 。然後使筒體本體以70轉/分鐘速度旋轉,藉以使粉末沿 著軸線方向均一分散在筒體本體1之內。 筒體本體的加速:用表1所示的時間使筒體本體1從靜 止狀態加速到350轉/分鐘(産生3G離心力作用的旋轉速度 )。達到該旋轉速度後,保持該旋轉速度。 筒體本體的加熱:將筒體本體1加熱到105 0 °C。以此 使內部的粉末升溫到大體相同的溫度下,使粉末變成部分 熔融狀態。然後在此溫度下保持30秒鐘。 筒體本體的冷卻:放置冷卻。 利用以上操作在各樣品筒體本體的內周面上形成了內 面披覆層。測定了這些內面披覆層的厚度和軸線方向上的 厚度偏差率。用表1和第7圖的曲線顯示其結果。 -36- 1259851 (31) 厚度偏差率 (%) (N 凝 νη cn 壊 披覆層厚度 I (mm) (Ν cs CN (Ν 至3G的加 速時間 νη (Ν v〇 <N CN 內面加 工方法 噴砂 噴砂 噴砂 噴砂 ί行磨 內面粗糙度 (pmRa) d 筒體本 體樣品 < < PQ OQ U 試驗 編號 試驗1 試驗2 試驗3 試驗4 試驗5 -37- 1259851 (32) 表1和第7圖的曲線說明,加速時間越短厚度偏差率越 小,而且筒體本體內周面的粗糙度越大厚度偏差率越小。 因此可以確認,加大內周面粗糙度能有效防止披覆層沿軸 線方向的偏厚。 (2 ) 實驗2 作爲筒體本體1,準備了以下形狀的筒體本體樣品D 、丑和F。 樣品D:外徑125毫米X內徑27毫米X長度1250毫米 材料:SCM410 內周面:噴砂加工,內周面粗糙度5微米Ra 樣品E:外徑125毫米X內徑35毫米X長度1250毫米 材料:SCM410 內周面··噴砂加工,內周面粗糙度5微米Ra 樣品F:外徑125毫米X內徑44毫米X長度1250毫米 材料·· SCM410 內周面:噴砂加工,內周面粗糙度5微米Ra 在以下條件下,用第1圖、第2圖所示的裝置分別對這 些樣品D、E和F的內周面進行了自熔合金披覆加工。 使用自熔合金粉末:霍加納海綿鐵粉(Hoganas)#1355-2〇Solidus temperature: 970 ° C Liquidus temperature: 1 0 7 0 ° C Powder loading: 2.5 kg of powder was placed in one place in the body 1 of the cylinder. Then, the body of the cylinder was rotated at a speed of 70 rpm so that the powder was uniformly dispersed in the body 1 of the cylinder in the axial direction. Acceleration of the barrel body: The barrel body 1 was accelerated from the stationary state to 350 rpm (the rotational speed at which 3G centrifugal force was generated) with the time shown in Table 1. After the rotation speed is reached, the rotation speed is maintained. Heating of the barrel body: The barrel body 1 is heated to 105 ° C. Thereby, the internal powder is heated to substantially the same temperature to make the powder partially melted. It is then held at this temperature for 30 seconds. Cooling of the barrel body: placement to cool. By the above operation, an inner cladding layer was formed on the inner peripheral surface of each sample cylinder body. The thickness of the inner cladding layer and the thickness deviation ratio in the axial direction were measured. The results are shown by the curves of Tables 1 and 7. -36- 1259851 (31) Thickness deviation rate (%) (N condensing νη cn 壊 coating thickness I (mm) (Ν cs CN (Ν to 3G acceleration time νη (Ν v〇<N CN inner surface processing Method Sandblasting sandblasting sandblasting sanding roughness (pmRa) d cylinder body sample << PQ OQ U test number test 1 test 2 test 3 test 4 test 5 -37- 1259851 (32) Table 1 and The graph of Fig. 7 shows that the shorter the acceleration time, the smaller the thickness deviation rate, and the smaller the roughness of the inner circumferential surface of the cylinder body, the smaller the thickness deviation rate. Therefore, it can be confirmed that the inner peripheral surface roughness can be increased to effectively prevent the coating. The layer was thicker in the axial direction. (2) Experiment 2 As the cylinder body 1, the cylindrical body samples D, ugly and F of the following shapes were prepared. Sample D: outer diameter 125 mm X inner diameter 27 mm X length 1250 mm Material: SCM410 Inner peripheral surface: Sandblasting, inner peripheral surface roughness 5 μm Ra Sample E: outer diameter 125 mm X inner diameter 35 mm X length 1250 mm Material: SCM410 Inner peripheral surface · Sandblasting, inner peripheral surface roughness 5 micron Ra sample F: outer diameter 125 mm X inner diameter 44 mm X length 1250 mm material·· Inner surface of SCM410: sandblasting, inner peripheral surface roughness 5 μm Ra Under the following conditions, the inner peripheral surfaces of these samples D, E and F were self-melted by the devices shown in Fig. 1 and Fig. 2, respectively. Alloy coating processing. Self-fluxing alloy powder: Hoganas sponge powder (Hoganas) #1355-2〇
固相線溫度:9 7 0 °C 液相線溫度:1 0 7 0 QC 粉末的裝入:在筒體本體i內的一處裝入表2所示數量 的粉末。然後使筒體本體i以7 〇轉/分鐘速度旋轉2 〇秒,藉 -38- (33) 1259851 以使粉末沿著軸線方向均一分散在筒體本體1之內。 筒體本體的加速:用表2所示的時間使筒體本體1從靜 止狀態加速到表2所示的旋轉速度(産生3 G離心力作用的 旋轉速度)。達到該旋轉速度後’保持該旋轉速度。 筒體本體的加熱:將筒體本體1加熱到1〇2〇 °C。以此 使內部的粉末升溫到大體相同的溫度下’使粉末變成部分 熔融狀態。然後在此溫度下保持60秒鐘。 筒體本體的冷卻:放置冷卻。 利用以上操作在各樣品同體本體的內周面上形成了內 面披覆層。測定了這些內面披覆層的厚度和軸線方向上的 厚度偏差率。用表2和第8圖的曲線顯示其結果。 -39- (34)1259851 厚度偏差率 (%) 摧 vn (N 壊 yn 壊 披覆層厚度 (mm) (N (Ν (N (N (Ν (Ν (N (Ν 旋轉速度 (rpm) 450 450 390 390 390 350 350 1 350 至3G的加 速時間 in 〇 〇 (Ν 粉末供給量 (千克) rH ο (Ν 〇 Η 〇 (Ν νη (Ν tn (Ν (Ν 筒體內徑 i 1 (mm) ν〇 m in cn m 客 筒體本 體樣品 Q Q ω (Jh 試驗編號 試驗ό 試驗7 試驗8 試驗9 試驗10 試驗11 試驗12 試驗13 -40 _ (35) 1259851 表2和第8圖的曲線說明,加速時間越短厚度偏差率越 小,而且厚度偏差率隨著內徑增大而增大,爲了將厚度偏 差率抑制至數値變小,必須縮短加速時間。而且在第8圖 的曲線內,畫出了顯示幾乎不産生厚度偏差的曲線3 5,該 曲線35是用以下實驗式(A)獲得的。 τ (秒)=3x105/D3 …(A ) (D是筒體的內徑,mm) 因此,對於內周面粗糙度處於5微米Ra以上的筒體本 體進行自熔合金披覆時,將粉末沿著軸線方向在筒體本體 內均等配置後,若使筒體本體達到産生3G以上離心力的 旋轉速度所需的時間,設定在不超過由上記實驗式(A ) 求出的時間r的數値,則能夠形成厚度沿筒體軸線方向幾 乎沒有偏差的披覆層。 實施例 [實施例1〜4 ] (1 )準備了以下形狀的筒體本體1和自熔合金粉末。 筒體本體:外徑125毫米X內徑44毫米X長度1250毫米 材料:S C Μ 4 1 0 內周面:噴砂加工,內周面(粗糙度20微米Ra) 自熔合金粉末:霍加納海綿鐵粉(Hoganas ) #1560Solidus temperature: 9 7 0 °C Liquidus temperature: 1 0 7 0 QC Loading of powder: The amount of powder shown in Table 2 was placed at one place in the body i of the cylinder. Then, the cylinder body i was rotated at a speed of 7 rpm for 2 sec seconds, and -38-(33) 1259851 was used to uniformly disperse the powder in the cylinder body 1 along the axial direction. Acceleration of the cylinder body: The cylinder body 1 was accelerated from the stationary state to the rotational speed shown in Table 2 (rotation speed at which 3 G centrifugal force was applied) with the time shown in Table 2. After the rotation speed is reached, the rotation speed is maintained. Heating of the barrel body: The barrel body 1 is heated to 1 〇 2 ° C. Thereby, the internal powder is heated to substantially the same temperature to make the powder into a partially molten state. It is then held at this temperature for 60 seconds. Cooling of the barrel body: placement to cool. With the above operation, an inner coating layer was formed on the inner peripheral surface of the same body of each sample. The thickness of the inner cladding layer and the thickness deviation ratio in the axial direction were measured. The results are shown by the curves of Table 2 and Figure 8. -39- (34)1259851 Thickness deviation rate (%) Destroy vn (N 壊yn 壊 coating thickness (mm) (N (N (N (N (Ν (N (Ν (rpm) (R) 390 390 390 350 350 1 350 to 3G acceleration time in 〇〇 (Ν powder supply (kg) rH ο (Ν 〇 〇(Ν νη (Ν tn (Ν (Ν barrel inner diameter i 1 (mm) ν〇 m in cn m Passenger cylinder body sample QQ ω (Jh test number test ό test 7 test 8 test 9 test 10 test 11 test 12 test 13 -40 _ (35) 1259851 The curves of Table 2 and Figure 8 illustrate the acceleration time The shorter the thickness deviation rate is, the smaller the thickness deviation rate increases as the inner diameter increases. In order to suppress the thickness deviation rate to a small number, the acceleration time must be shortened. Also, in the graph of Fig. 8, A curve 35 showing almost no thickness deviation is obtained, which is obtained by the following experimental formula (A): τ (sec) = 3x105 / D3 (A) (D is the inner diameter of the cylinder, mm) When the inner body surface roughness is 5 micrometers Ra or more, the body of the cylinder is coated with a self-fluxing alloy, and the powder is placed along the axis direction in the cylinder. After the body is uniformly disposed, if the cylinder body reaches the time required to generate a rotational speed of 3 G or more centrifugal force, and the number of times r is not exceeded by the time r obtained by the above experimental formula (A), the thickness can be formed along the tube. A coating layer having almost no deviation in the body axis direction. Examples [Examples 1 to 4] (1) A cylindrical body 1 and a self-fluxing alloy powder of the following shapes were prepared. The cylinder body: outer diameter 125 mm X inner diameter 44 Mm X Length 1250 mm Material: SC Μ 4 1 0 Inner circumference: Sandblasted, inner circumferential surface (roughness 20 μm Ra) Self-fluxing alloy powder: Hoganas sponge iron powder (Hoganas ) #1560
固相線溫度:980°C 液相線溫度:1200°C 1259851 (36) (2 )粉末的供給和粉末層的形成 將筒體本體1置於第1圖所示的製造裝置上,在該筒體 本體1內的一處裝入2.5千克粉末。然後用蓋子15將筒體本 體G的兩端封閉後,使該筒體本體1以70轉/分鐘速度旋轉 20秒鐘。藉以使粉末沿著軸線方向均一分散在筒體本體1 之內。Solidus temperature: 980 ° C Liquidus temperature: 1200 ° C 1259851 (36) (2) Supply of powder and formation of powder layer The cylindrical body 1 is placed on the manufacturing apparatus shown in Fig. 1, where A portion of the inside of the cylinder body 1 was charged with 2.5 kg of powder. Then, both ends of the cylindrical body G were closed by a cover 15, and the cylindrical body 1 was rotated at a speed of 70 rpm for 20 seconds. Thereby, the powder is uniformly dispersed in the cylindrical body 1 along the axial direction.
接著將筒體本體1的旋轉加速到內周面分別處於26 G (實施例1 ) 、3 4 G (實施例2 ) 、4 2 G (實施例3 )和5 0 G (實施例4 )離心力作用下的旋轉速度,達到該旋轉速度 後,保持該旋轉速度。此時的加速度定爲在2秒鐘內離心 力從〇達到3 G的加速度。 (3 )粉末的加熱熔融和凝固 將筒體本體1加熱到1 05 0 °C。以此使內部的粉末也升 溫到大體相同的溫度下,使粉末變成部分熔融狀態。將筒 體本體1加熱到105(TC後,在該溫度下保持3〇秒鐘,然後停 止加熱’放冷。藉此使筒體本體1內面的金屬熔液層凝固 ’從而在筒體本體的內周面上形成內面披覆層。 (4 )內面披覆層的硬度測定 獲得的內面披覆層厚度爲2毫米。測定了這種內面披 覆層深度0.5毫米位置、1.〇毫米位置和1<5毫米位置處的硬 度。其結果示於表3之中。 -42 - (37) 1259851 [比較例1〜3 ] 使用與實施例1同一形狀的筒體本體1和自熔合金粉末 ,除粉末層加熱時在筒體本體1的內周面上施加4 G、1 〇 G 和1 8 G的離心力之外,其餘與實施例1在同一條件下形成 了內面披覆層。對所獲的內面披覆層與實施例1〜4同樣測 定了硬度。其結果也示於表3之中。 表3 離心力 硬度 (Hv5) 硬度測定位置 (距表面的深度m m ) 平均 0.5 1.0 1.5 比較例1 4 650 560 473 561 比較例2 10 781 560 480 607 比較例3 18 792 565 490 616 實施例1 26 818 584 502 629 實施例2 34 857 841 549 725 實施例3 42 874 857 6 13 769 實施例4 50 927 532 465 637 表3的結果說明,提高離心力下離心鑄造的實施例1〜 4,與離心力低的比較例相比,內面披覆層的表面硬度極 高。因此可以確認,使用同一自熔合金,採用本發明能夠 提高內面披覆層的表面硬度。將實施例2形成的內面披覆 層的斷面切開進行顯微觀察後發現,如第3圖所示,具有 -43- (38) 1259851 二層結構’表面層21a形成一種硬質陶瓷微粒子極多的組 _ °可以認爲如此的結構才能大幅度地提高硬度。 [實施例5〜7 ] (1 )準備了以下形狀的筒體本體1和自熔合金粉末。 筒體本體:外徑125毫米X內徑44毫米X長度1250毫米 材料:SCM410 內周面:噴砂加工(內周面粗糙度20微米R a) 自熔合金粉末:霍加納海綿鐵粉(Η 〇 g a n a s )# 1 5 6 0Then, the rotation of the cylindrical body 1 is accelerated to the inner peripheral surface at 26 G (Example 1), 3 4 G (Example 2), 4 2 G (Example 3), and 50 G (Example 4) centrifugal force, respectively. The rotational speed under the action, after reaching the rotational speed, maintains the rotational speed. The acceleration at this time is set to an acceleration of the centrifugal force from 〇 to 3 G in 2 seconds. (3) Heating, melting and solidification of the powder The body 1 of the cylinder was heated to 1,050 °C. Thereby, the internal powder is also heated to substantially the same temperature to cause the powder to become partially molten. After the cylinder body 1 is heated to 105 (TC, it is kept at this temperature for 3 sec, then the heating is stopped and the cooling is performed. Thereby the molten metal layer on the inner surface of the cylindrical body 1 is solidified) so that the body is in the cylinder body The inner surface of the inner peripheral surface is formed with a coating layer. (4) The hardness of the inner surface coating layer is 2 mm, and the thickness of the inner surface coating layer is 0.5 mm. The hardness at the 〇mm position and the 1<5 mm position. The results are shown in Table 3. -42 - (37) 1259851 [Comparative Examples 1 to 3] The cylindrical body 1 having the same shape as that of Example 1 was used. The self-fluxing alloy powder was subjected to the centrifugal force of 4 G, 1 〇 G, and 18 G on the inner peripheral surface of the cylindrical body 1 when the powder layer was heated, and the inner surface was formed under the same conditions as in Example 1. The hardness of the obtained inner coating layer was measured in the same manner as in Examples 1 to 4. The results are also shown in Table 3. Table 3 Centrifugal hardness (Hv5) Hardness measurement position (depth from the surface mm) Average 0.5 1.0 1.5 Comparative Example 1 4 650 560 473 561 Comparative Example 2 10 781 560 480 607 Comparative Example 3 18 792 565 490 616 Example 1 26 818 584 502 629 Example 2 34 857 841 549 725 Example 3 42 874 857 6 13 769 Example 4 50 927 532 465 637 The results of Table 3 illustrate Examples 1 to 4 of centrifugal casting under increased centrifugal force Compared with the comparative example with low centrifugal force, the surface hardness of the inner surface coating layer was extremely high. Therefore, it was confirmed that the surface hardness of the inner surface coating layer can be improved by using the same self-fluxing alloy. The cross section of the inner cladding layer was cut and microscopically observed. As shown in Fig. 3, the surface layer 21a having a -43-(38) 1259851 two-layer structure formed a very large group of hard ceramic particles. It is considered that such a structure can greatly increase the hardness. [Examples 5 to 7] (1) The cylindrical body 1 and the self-fluxing alloy powder of the following shapes were prepared. The cylindrical body: outer diameter 125 mm X inner diameter 44 Mm X Length 1250 mm Material: SCM410 Inner circumference: Sandblasting (internal circumferential surface roughness 20 μm R a) Self-fluxing alloy powder: Hogana sponge iron powder (Η 〇ganas ) # 1 5 6 0
固相線溫度:980°C 液相線溫度:1 2 0 0 °C (2 )粉末的供給和粉末層的形成 將筒體本體1置於第5圖所示的製造裝置上,在該筒體 本體1內一處裝入2.5千克粉末。然後用蓋子15、15 A將筒 體本體G的兩端封閉後,使該筒體本體1以70轉/分鐘速度 旋轉20秒鐘。藉以使粉末沿軸線方向均一分散在筒體本體 1之內。Solidus temperature: 980 ° C Liquidus temperature: 1 2 0 0 ° C (2) Supply of powder and formation of powder layer The cylinder body 1 is placed on the manufacturing apparatus shown in Fig. 5, in which the cylinder 2.5 kg of powder was placed in one body of the body 1. Then, both ends of the cylindrical body G were closed by the covers 15, 15 A, and the cylindrical body 1 was rotated at a speed of 70 rpm for 20 seconds. Thereby, the powder is uniformly dispersed in the cylindrical body 1 in the axial direction.
接著將筒體本體1的旋轉加速到內周面分別處於10G 離心力作用下的旋轉速度’達到該旋轉速度後’保持該旋 轉速度。此時的加速度定爲在2秒鐘內離心力從〇達到3 G 的加速度。 (3 )粉末的加熱熔融和凝固 -44- 1259851 (39) 將筒體本體1加熱到1 05 〇 °C。以此使內部的粉末也升 溫到大體相同的溫度下,使粉末變成部分熔融狀態。將筒 體本體1加熱升溫到105 Ot後,啓動壓縮機3 2,使筒體本體 1內處於〇.3MPa (實施例5 ) 、〇 · 6 Μ P a (實施例6 )和 l.OMPa (實施例7 )氣壓的作用下,在該溫度下保持15秒 鐘,然後停止加熱並將其放冷。以此方式使筒體本體1內面 的金屬溶液層凝固,在筒體本體的內周面上形成內面披覆 層。 (4 )內面披覆層的硬度測定 獲得的內面披覆層厚度爲2毫米。測定了這種內面披 覆層深度0.5毫米、1.0毫米和1.5毫米位置處的硬度。結果 示於表4之中。 [比較例4]Then, the rotation of the cylindrical body 1 is accelerated until the rotational speed of the inner peripheral surface under the action of 10 G centrifugal force 'after reaching the rotational speed' maintains the rotational speed. The acceleration at this time is set to an acceleration of the centrifugal force from 〇 to 3 G in 2 seconds. (3) Heating, melting and solidification of the powder -44 - 1259851 (39) The cylinder body 1 is heated to 10 〇 °C. Thereby, the internal powder is also heated to substantially the same temperature to cause the powder to become partially molten. After heating the cylinder body 1 to 105 Ot, the compressor 3 2 is started, so that the inside of the cylinder body 1 is at MPa3 MPa (Example 5), 〇·6 Μ P a (Example 6), and 1.0 MPa ( Example 7) Under the action of air pressure, it was kept at this temperature for 15 seconds, then the heating was stopped and allowed to cool. In this way, the metal solution layer on the inner surface of the cylindrical body 1 is solidified, and an inner surface coating layer is formed on the inner peripheral surface of the cylindrical body. (4) Hardness measurement of the inner coating layer The inner coating layer was obtained to have a thickness of 2 mm. The hardness of the inner cladding layer at positions of 0.5 mm, 1.0 mm, and 1.5 mm was measured. The results are shown in Table 4. [Comparative Example 4]
使用與實施例5同一形狀的筒體本體1和自熔合金粉末 ,除粉末層加熱時在筒體本體1內施加0氣壓外,其餘與實 施例5在同一條件下形成了內面披覆層。對所獲的內面披 覆層與實施例5〜7同樣測定了硬度。其結果也示於表4之 中〇 -45 - (40) 1259851 表4 氣壓 (MPa) 硬度 (Hv5) 硬度測定位置 (距表面的丨朱度m m ) 平均 0.5 1.0 i 1.5 比較例4 0 78 1 560 480 607 實施例5 0.3 792 652 600 681 實施例6 0.6 825 748 620 73 1 實施例7 1.0 841 766 680 762 表4的結果說明,使筒體本體1內的金屬熔液層處於 0.3 MPa以上氣壓作用下離心鑄造的實施例5〜7,與無氣壓 作用的比較例4相比,其表面硬度增大。因此可以確認, 使用同一自熔合金,採用本發明能夠提高內面披覆層的表 面硬度。Using the cylindrical body 1 and the self-fluxing alloy powder having the same shape as in Example 5, the inner coating layer was formed under the same conditions as in Example 5 except that 0 atmosphere was applied to the cylindrical body 1 when the powder layer was heated. . The hardness of the obtained inner facing layer was measured in the same manner as in Examples 5 to 7. The results are also shown in Table 4 〇-45 - (40) 1259851 Table 4 Pressure (MPa) Hardness (Hv5) Hardness measurement position (丨 度 度 mm from the surface) Average 0.5 1.0 i 1.5 Comparative Example 4 0 78 1 560 480 607 Example 5 0.3 792 652 600 681 Example 6 0.6 825 748 620 73 1 Example 7 1.0 841 766 680 762 The results of Table 4 illustrate that the molten metal layer in the barrel body 1 is at a pressure of 0.3 MPa or more. Examples 5 to 7 of centrifugal casting under action exerted an increase in surface hardness as compared with Comparative Example 4 in which no air pressure was applied. Therefore, it was confirmed that the same self-fluxing alloy can be used, and the surface hardness of the inner cladding layer can be improved by the present invention.
[實施例8J 使用與實施例2同一形狀的筒體本體1和自熔合金粉末 ’將此筒體本體1置於第5圖所示的製造裝置上,對粉末加 熱熔融時除使筒體本體1的內周面處於l.OMPa氣壓作用之 外’其餘在與實施例2同一條件(因此加熱熔融時,筒體 本體1的內周面處於3 4 G離心力作用下的條件)下形成了 內面披覆層。對所獲的內面披覆層與實施例2同樣測定了 硬度。其結果與實施例2的結果一倂示於表5之中。 -46- 1259851 (41) 表5 氣壓 (MPa) 硬度 (Hv5) 硬β (距表_ ^測定位置 S的深度mm) 平均 0.5 1.0 1.5 實施例2 0 857 841 549 725 實施例8 1.0 900 912 796 869 表5的結果說明,使筒體本體1的內周面位置經受34G 離心力作用,同時受l.OMPa氣壓作用下進行離心鑄造的實 施例8,與無氣壓作用的實施例2相比,其內面披覆層的硬 度更高。因此可以確認,利用使金屬熔液層經受高G離心 力作用的同時經受高氣壓作用,能夠進一步提高內面披覆 層的表面硬度。 對實施例8形成的內面披覆層斷面切開後進行了顯微 鏡觀察,結果發現這種場合下也形成如第3圖所示的三層 結構,表面層2 1 a變成一種硬質陶瓷微粒子極多的組織。 這種表面層2 1 a和邊界層2 1 c的化學成分測定結果示於表6 中。而且在表6中也列出了加熱處理前自熔合金粉末(霍 加納海綿鐵粉(Hog anas ) # 1 5 60 )的化學成分。其中,表 6中的成分濃度爲質量%。 -47 - (42) 1259851 表6 C Si _J Cr Fe Ni _^面層21a 0.39 6.03 28.32 7.45 59.81 邊界層2 1 c 0.00 4.83 4.26 32.07 58.84 粉末 0.73 4.38 14.72 3.24 餘量 表6的結果說明,表面層21a中鉻成分濃度增高,而邊 界層2 1 c中鉻成分濃度卻降低。這是因爲離心鑄造時利用 賦予高G離心力,使金屬熔液中析出的鉻化合物系硬質陶 瓷微粒子聚集在表面層內的緣故。 【圖式簡單說明】 第1圖(a) 、 (b)是顯示本發明實施方式中前述內 面披覆筒體製造裝置處於不同動作狀態下的示意性立體圖 〇 第2圖(a) 、 (b) 、 (c) 、 (d)是顯示用第1圖的 裝置在筒體本體內周面上形成樹脂披覆層製程的斷面示意 圖。 第3圖是顯示內面披覆層斷面結構的斷面示意圖。 第4圖是顯示本發明其他實施方式關於的內面披覆筒 體製造裝置的示意性立體圖。 第5圖是顯示本發明另一實施方式中前述內面披覆筒 體製造裝置的示意性立體圖。 第6圖是顯示本發明又一實施方式中前述內面披覆筒 -48 - 1259851 (43) 體製造裝置的示意性立體圖。 第7圖是顯示實驗1獲得的、筒體本體內周面的表面粗 縫度和加速時間與披覆層軸線方向厚度偏差率之間關係的 曲線。 第8圖是顯示實驗2獲得的、筒體本體內徑和加速時間 與披覆層軸線方向厚度偏差率之間關係的曲線。 【圖號說明】 1、 體本體 2、 自熔 合 金 粉 末 3、 筒體 支 承 旋 轉裝置 4、 承受 輥 5 > 加壓 輥 6、 變速 馬 達 7、 控制 裝 置 9、 粉末供給裝置 10、 粉 末 供 給 管 1卜 料 斗 台 車 13、 加 熱 裝 置 15、 15 A : 蓋 子 20、 內 面 披 覆 筒體 21、 內 面 披 覆 層 25、 連 接 管 2 6、 旋 轉 接 頭 -49 - 1259851 (44) 27、 28、 29、 3 1、 32、 配管 28A :開關閥 真空泵 壓力調節閥 壓縮機[Example 8J Using the cylindrical body 1 and the self-fluxing alloy powder of the same shape as in Example 2] This cylindrical body 1 was placed on the manufacturing apparatus shown in Fig. 5, and the body of the cylinder was removed while heating and melting the powder. The inner peripheral surface of 1 is outside the pressure of 1.0 MPa. The rest is formed under the same conditions as in the embodiment 2 (so that the inner peripheral surface of the cylindrical body 1 is under the action of centrifugal force of 34 G when heated and melted). Covered with a layer. The hardness of the obtained inner coating layer was measured in the same manner as in Example 2. The results are shown in Table 5 together with the results of Example 2. -46- 1259851 (41) Table 5 Air pressure (MPa) Hardness (Hv5) Hard β (depth from the table _ ^ measured position S mm) Average 0.5 1.0 1.5 Example 2 0 857 841 549 725 Example 8 1.0 900 912 796 869 The results of Table 5 show that Example 8 in which the inner circumferential surface position of the cylindrical body 1 was subjected to 34 G centrifugal force while being subjected to centrifugal casting under a pressure of 1.0 MPa was compared with Example 2 without air pressure. The inner coating has a higher hardness. Therefore, it was confirmed that the surface hardness of the inner cladding layer can be further improved by subjecting the molten metal layer to a high G centrifugal force while being subjected to a high gas pressure. The inner cladding layer formed in Example 8 was cut in a cross section and observed under a microscope. It was found that a three-layer structure as shown in Fig. 3 was also formed in this case, and the surface layer 21 a became a hard ceramic microparticle. More organizations. The chemical composition measurement results of the surface layer 2 1 a and the boundary layer 2 1 c are shown in Table 6. Further, the chemical composition of the self-fluxing alloy powder (Hog anas #1 5 60 ) before heat treatment is also listed in Table 6. Here, the concentration of the components in Table 6 is % by mass. -47 - (42) 1259851 Table 6 C Si _J Cr Fe Ni _^ surface layer 21a 0.39 6.03 28.32 7.45 59.81 Boundary layer 2 1 c 0.00 4.83 4.26 32.07 58.84 Powder 0.73 4.38 14.72 3.24 Balance Table 6 results, surface layer The concentration of chromium in 21a is increased, while the concentration of chromium in boundary layer 2 1 c is decreased. This is because the chromium compound-based hard ceramic fine particles which are precipitated in the molten metal are concentrated in the surface layer by centrifugal force during the centrifugal casting. BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 (a) and (b) are schematic perspective views showing a state in which the inner cladding cylinder manufacturing apparatus according to the embodiment of the present invention is in a different operation state, Fig. 2(a), ( b), (c), and (d) are schematic cross-sectional views showing a process of forming a resin coating layer on the inner circumferential surface of the cylindrical body by the apparatus of Fig. 1. Figure 3 is a schematic cross-sectional view showing the cross-sectional structure of the inner cladding layer. Fig. 4 is a schematic perspective view showing an apparatus for manufacturing an inner cladding cylinder according to another embodiment of the present invention. Fig. 5 is a schematic perspective view showing the apparatus for manufacturing an inner facing cylindrical body according to another embodiment of the present invention. Fig. 6 is a schematic perspective view showing the above-described inner surface coated cylinder -48 - 1259851 (43) body manufacturing apparatus in still another embodiment of the present invention. Fig. 7 is a graph showing the relationship between the surface roughness and the acceleration time of the circumferential surface of the cylinder body obtained in Experiment 1, and the thickness deviation ratio in the axial direction of the coating layer. Fig. 8 is a graph showing the relationship between the inner diameter and the acceleration time of the cylinder body and the thickness deviation ratio in the axial direction of the coating layer obtained in Experiment 2. [Description of the figure] 1. Body body 2, self-fluxing alloy powder 3, cylinder supporting rotating device 4, receiving roller 5 > Pressurizing roller 6, variable speed motor 7, control device 9, powder supply device 10, powder supply tube 1 hopper trolley 13, heating device 15, 15 A: cover 20, inner cladding cylinder 21, inner cladding layer 25, connecting pipe 26, rotary joint -49 - 1259851 (44) 27, 28, 29 , 3 1, 32, Piping 28A: On-off valve vacuum pump pressure regulating valve compressor
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CN102407310A (en) * | 2011-09-30 | 2012-04-11 | 陈留军 | Method for casting hydraulic oil cylinder body |
CN102560477A (en) * | 2012-01-12 | 2012-07-11 | 自贡市巨光硬面材料有限公司 | Manufacturing process of pipe fitting with corrosion and abrasion-resistant inner wall |
US9649686B2 (en) | 2012-02-22 | 2017-05-16 | General Electric Company | Casting preforms and methods of use thereof |
CN102747365A (en) * | 2012-06-20 | 2012-10-24 | 北京科技大学 | Preparation method for steel pipe having wear-resistant and corrosion-resistant lining layer |
CN104190901A (en) * | 2014-07-28 | 2014-12-10 | 宁国市大泉机械有限公司 | Machining method of seamless steel tube |
CN104805435A (en) * | 2015-04-24 | 2015-07-29 | 中国人民解放军装甲兵工程学院 | Preparation method of metal protective coating for inner wall surface of inner bore part |
CN106735228B (en) * | 2017-01-06 | 2019-02-22 | 昆山中士设备工业有限公司 | A kind of manufacturing method of plastic molding press machine barrel |
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