JP4261705B2 - Semi-molten forging of dissimilar metals - Google Patents
Semi-molten forging of dissimilar metals Download PDFInfo
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- JP4261705B2 JP4261705B2 JP30173099A JP30173099A JP4261705B2 JP 4261705 B2 JP4261705 B2 JP 4261705B2 JP 30173099 A JP30173099 A JP 30173099A JP 30173099 A JP30173099 A JP 30173099A JP 4261705 B2 JP4261705 B2 JP 4261705B2
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Description
【0001】
【発明の属する技術分野】
本発明は異種金属からなる部品の製造法、特に複雑な形状を有する部品の製造方法に関するものである。
【0002】
【従来の技術】
これまで、異種金属同士を接合,一体化する方法は、固相温度域、液相温度域あるいは固液共存温度域での接合法などが開示されている。例えば固相温度域では特開昭56−128688号公報において、接合する金属表面に微細な凹凸を形成した後、熱間静水圧処理を行い接合面強度を高める方法が開示されている。また、液相温度域では特開昭63−295077号公報において、接合する金属の一方の表面を溶融させた後、もう一方の金属を押しつけ冷却する方法が開示されている。さらに固液共存温度域では、文献(塑性加工連合講演会講演論文集VOL.48th PAGE.407‐408 1997)において、接合する一方の金属を固液共存温度域に加熱し、もう一方の金属を挿入後冷却する方法が開示されている。
【0003】
【発明が解決すべき課題】
しかしながら、特開昭56−128688号公報及び特開昭63−295077号公報では、複雑形状部品を異種金属を接合,一体化して製造する場合、予めそれぞれの金属体を最終形状を構成する形状に仕上げておく必要があり、その後異種金属を接合する方法を採らざるを得ず、製造コストの上昇につながる。また、文献ではフィン付き部品等ある特定形状の部品においては低コストでの製造が可能であるが、積極的に部品形状を創製するものではなく、他形状の部品に適用することは困難であり、また接合強度も不十分である。
本発明は、上記の点に鑑みてなされたもので、極めて単純な形状である2種類以上の異種金属素材を用いて、異種金属からなる複雑形状部品を歩留まり良くかつ少数回の鍛造工程で成形し、しかも接合面の強度を向上させることを目的とするものである。
【0004】
【課題を解決するための手段】
即ち本発明の要旨とするところは、
1) 固相率fSが0.3以上0.9未満となる温度域T0.3−0.9の重複しない高融点金属と低融点金属からなる鍛造部品の製造方法において、それぞれの金属に対して固相率fSが0.3以上0.9未満となる温度域T0.3−0.9の重複する単数の金属をインサート材として用い、高融点金属とインサート材を、それぞれの固相率fSが0.3以上0.9未満となる温度域T0.3−0.9の重複する温度に加熱、鍛造型内に挿入、鍛造して中間製品を製造した後、前記中間製品と低融点金属を、インサート材と低融点金属の固相率fSが0.3以上0.9未満となる温度T0.3−0.9の重複する温度に加熱、鍛造型内に挿入、鍛造して、一体化することを特徴とする半溶融鍛造方法
2) 固相率fSが0.3以上0.9未満となる温度域T0.3−0.9の重複しない高融点金属と低融点金属からなる鍛造部品の製造方法において、それぞれの金属に対して固相率fSが0.3以上0.9未満となる温度域T0.3−0.9が重複する融点の異なる複数のインサート材を用い、高融点金属材料と高融点インサート材を、それぞれの固相率fSが0.3以上0.9未満となる温度域T0.3−0.9の重複する温度に加熱、鍛造型内に挿入、鍛造して第1中間製品を製造し、前記第1中間製品と低融点インサート材を、高融点インサート材と低融点インサート材の固相率fSが0.3以上0.9未満となる温度域T0.3−0.9の重複する温度に加熱、鍛造型内に挿入、鍛造し第2中間製品を製造した後、前記第2中間製品と低融点金属を、低融点インサート材と低融点金属の固相率fSが0.3以上0.9未満となる温度域T0.3−0.9の重複する温度に加熱、鍛造型内に挿入、鍛造して一体化することを特徴とする半溶融鍛造方法
3) 高融点金属とインサート材及び中間製品と低融点金属の少なくとも1組の形状が異形状であることを特徴とする上記1)記載の半溶融鍛造方法
4) 高融点金属とインサート材及び中間製品と低融点金属の少なくとも1組の形状が同径であることを特徴とする上記1)記載の半溶融鍛造方法
5) 高融点金属とインサート材及び中間製品と低融点金属の少なくとも1組の形状が円筒状及び円柱状であり、円筒内径と円柱外径が実質的に同径であることを特徴とする上記1)記載の半溶融鍛造方法
6) 高融点金属と高融点インサート材、第1中間製品と低融点インサート材及び第2中間製品と低融点インサート材の少なくとも1組の形状が異形状であることを特徴とする上記2)記載の半溶融鍛造方法
7) 高融点金属と高融点インサート材、第1中間製品と低融点インサート材及び第2中間製品と低融点インサート材の少なくとも1組の形状が同径であることを特徴とする上記2)記載の半溶融鍛造方法
8) 高融点金属と高融点インサート材、第1中間製品と低融点インサート材及び第2中間製品と低融点インサート材の少なくとも1組の形状が円筒状及び円柱状であり、円筒内径と円柱外径が実質的に同径であることを特徴とする上記2)記載の半溶融鍛造方法
9) 高融点金属、インサート材の初期高さh0と高融点金属、インサート材の鍛造後高さhとの関係が、高融点金属、インサート材を加熱した際の固相率fSのうち一番小さいfsminとの関係において、
ln(h0/h)≧1.5×fsmin 2
を満たすような形状の高融点金属、インサート材を用いることを特徴とする請求項上記1)、3)〜5)の何れか1項に記載の半溶融鍛造方法
10) 中間製品、低融点金属の初期高さh0と中間製品、低融点金属の鍛造後の高さhとの関係が、中間製品、低融点金属を加熱した際の固相率fsのうち一番小さいfsminとの関係において、
ln(h0/h)≧1.5×fsmin 2
を満たすような形状の中間製品、低融点金属を用いることを特徴とする請求項上記1)、3)〜5)、9)の何れか1項に記載の半溶融鍛造方法
11) 高融点金属、高融点インサート材の初期高さh0と高融点金属、高融点インサート材の鍛造後高さhとの関係が、高融点金属、高融点インサート材を加熱した際の固相率fsのうち一番小さいfsminとの関係において、
ln(h0/h)≧1.5×fsmin 2
を満たすような形状の高融点金属、高融点インサート材を用いることを特徴とする上記2)、6)〜8)の何れか1項に記載の半溶融鍛造方法
12) 第1中間製品、低融点インサート材の初期高さh0と第1中間製品、低融点インサート材の鍛造後高さhとの関係が、第1中間製品、低融点インサート材を加熱した際の固相率fsのうち一番小さいfsminとの関係において、
ln(h0/h)≧1.5×fsmin 2
を満たすような形状の第1中間製品、低インサート材を用いることを特徴とする上記2)、6)〜8)、11)の何れか1項に記載の半溶融鍛造方法
13) 第2中間製品、低融点金属の初期高さh0と第2中間製品、低融点金属の鍛造後高さhとの関係が、第2中間製品、低融点金属を加熱した際の固相率fsのうち一番小さいfsminとの関係において、
ln(h0/h)≧1.5×fsmin 2
を満たすような形状の2中間製品、低融点金属を用いることを特徴とする上記2)、6)〜8)、11)、12)の何れか1項に記載の半溶融鍛造方法
14) 平均500mm/s以上の加工速度で成形することを特徴とする上記1)乃至13)の何れか1項に記載の半溶融鍛造方法
15) 予め200℃以上に加熱された鍛造型を用いて、平均200mm/s以上の加工速度で成形することを特徴とする上記1)乃至14)の何れか1項に記載の半溶融鍛造方法16) 成形終了後固相線温度以下となるまで最大鍛造荷重の50%以上の荷重を保持することを特徴とする上記1)乃至15)の何れか1項に記載の半溶融鍛造方法
にある。
【0005】
【発明の実施の形態】
鍛造品の部位の必要特性に応じて異なる成分を有する金属素材を用いるが、図1のグラフに示すように、高融点金属素材Aと低融点金属素材Bの固相率fsが 0.3以上0.9未満となる温度域T0.3-0.9 が重複しない場合、それぞれの金属素材に対して固相率fsが0.3以上0.9未満となる温度域T0.3-0.9 が重 複するような金属をインサート材として用いる。これは、後述するように、金属素材同士を健全に一体化するにはそれぞれの固相率fsが0.3以上0.9未満 となる温度域T0.3-0.9 に加熱した後、鍛造することが望ましいからである。異種金属は成分の異なる鋼同士でもよく、その他、鋳鉄、アルミニウム、マグネシウム、チタン等を使用することができる。インサート材は1種類あるいは2種類以上でも良い。
【0006】
次に加熱温度範囲を異種金属とインサート材の組合せにおいて、それぞれの固相率fsが0.3以上0.9未満となる温度域T0.3−0.9の重複する範囲に限定する理由を述べる。図2のグラフに示すように、異種金属素材あるいはインサート材の組合せのうち、融点の低い材料Eの固相率が0.3になる温度T E 0.3より加熱温度が高い場合、材料Eが加熱炉内で自立出来ず、鍛造型内に搬送できない。また異種金属素材あるいはインサート材の組合せのうち、融点の高い材料Dの固相率が0.9になる温度T D 0.9より加熱温度が低い場合、材料Dの液相成分が少なく、金属素材が鍛造により健全に一体化しない。そのため異種金属素材あるいはインサート材の組合せのうち、それぞれの固相率fsが0.3以上0.9未満となる温度域T0.3−0.9の重複する範囲の温度に加熱する。
【0007】
異種金属とインサート材の組合せにおいて、それぞれの固相率fsが0.3以上0.9未満となる温度域T0.3-0.9 の重複する範囲の温度が高い順に、順次加熱、鍛造を行う。これは2回目以降の加熱において、既に鍛造された異種金属あるいはインサート材の組合せのうち、固相率fsが0.3以上0.9未満となる温度域T0.3-0.9 の低い材料が加熱炉内で溶け落ちるのを防止するためである。
【0008】
異種金属、インサート材あるいは中間製品の形状は、例えば図3ないし図5(いずれも(a)は平面図、(b)は側面図)に示すように、一回目の鍛造を行った後、異形状であっても、同径形状であっても、円筒及び円柱であり円筒内径と円柱径が実質的に同径である場合でもよい。
【0009】
前記高融点金属とインサート材を鍛造して中間製品を得る工程、必要に応じて中間製品とインサート材を鍛造してさらに中間製品を得る工程、中間製品と低融点金属を鍛造して最終製品を得る工程において、高融点金属、インサート材、低融点金属のそれぞれの初期高さh0と高融点金属、インサート材、低融点金属のそれぞれ鍛造後高さhとの関係が、高融点金属、インサート材、低融点金属のそれぞれの組み合わせで加熱した際の固相率fsのうち一番小さいfsminとの関係において、
ln(h0/h)≧1.5×fsmin 2
を満たすような形状の高融点金属、インサート材、低融点金属を用いる各金属素材を用いるのは、各金属素材が十分な加工を受け、液相同士を十分に混合し一体化させるためである。
【0010】
鍛造時に平均500mm/秒以上の加工速度で成形するのは、これより遅い加工速度では鍛造型との接触により加熱された金属素材の温度が低下し、金属素材同士が十分に一体化しないからである。加工速度の上限は、本発明の効果を得るためには特に制限する必要はなく、設備能力に依存する。
【0011】
予め200℃以上に加熱された型を用いる場合には、鍛造型との接触による金属素材の温度低下が緩和されるため、鍛造時の加工速度は平均200mm/秒以上で十分である。加熱温度の上限は、本発明の効果を得るためには特に制限する必要はないが、金型の焼き戻し軟化を防止するため、500℃以下とすることが好ましい。
【0012】
成形終了後固相線温度以下となるまで最大鍛造荷重の少なくとも50%以上の荷重を保持させるのは、凝固収縮による鋳巣の発生を防止し、鍛造後の材質特性を向上させるためである。最大鍛造荷重の50%未満の荷重ではその効果は十分ではない。保持荷重の上限は、本発明の効果を得るためには特に制限する必要はなく、最大鍛造荷重の100%でも構わない。
【0013】
【実施例】
(実施例1)
実施例として、2種類の金属4A、4B及びインサート材4Cで構成される図6((a)は平面図、(b)は側面図)に示すような形状の鍛造品の鍛造を実施した。
素材には表1の化学成分を有する高融点材料である素材A、低融点材料である素材B及びインサート材料である素材Cを用いた。また示差熱分析により測定した固相線温度と液相線温度をそれぞれ表2に示した。
【0014】
【表1】
【0015】
【表2】
【0016】
鍛造素材として、図7に示すように、外径DA0、内径dA0、高さhA0の円筒形状である素材5Aと、外径DB0、高さhB0の円柱形状である素材5B、外径DC0、内径dC0、高さhC0の円筒形状である素材5Cを準備した。
【0017】
1回目の鍛造で素材5Aと素材5Cの鍛造を行い図8に示すように素材5Aと素材5Cからなる中間製品5Dを成形した後、2回目の鍛造で中間製品5Dと素材5Bの鍛造を行い図6に示す鍛造品1を成形した。表3に1回目の鍛造条件を、表4に2回目の鍛造条件を示す。加熱時における金属素材の固相率は、金属素材を加熱後速やかに水冷することにより組織を凍結、光学顕微鏡にて観察し、固相部分の面積率を測定することにより求めた。
【0018】
【表3】
【0019】
【表4】
【0020】
鍛造品の品質を評価するため、内部空孔有無の観察及び引張試験を実施した。内部空孔に関しては、鍛造品1の断面を切断,研磨し、光学顕微鏡にて空孔の有無を観察した。鍛造品1の図6に示す位置からφ6のサンプル42を切り出し、ねじ部を圧接することにより引張試験片を作製した。引張試験は常温で行った。表5に評価結果を示す。
【0021】
【表5】
【0022】
試験No.1〜4では、いずれの場合も鍛造品に内部空孔は見られず完全に一体化しており、引張強さが400MPa以上を示した。また破断位置は強度の低い金属Bの位置であった。
【0023】
1回目の鍛造での対数ひずみが小さい試験No.5、6では、素材Aと素材Cの一体化がやや不十分で、素材Aと素材Cの境界にわずかな空孔が見られ、引張試験では素材Aと素材Bの境界から破断した。
2回目の鍛造での対数ひずみが小さい試験No.7、8では、素材Bと素材Cの一体化がやや不十分で、素材Bと素材Cの境界にわずかな空孔が見られ、引張試験では素材Bと素材Cの境界から破断した。
【0024】
1回目の鍛造での加工速度が小さい試験No.9、10では、加工中に鍛造型との接触により温度低下が生じ、液相部分が減少したため、素材Aと素材Cの一体化がやや不十分であり、素材Aと素材Cの境界にわずかに空孔が見られ、引張試験では素材Aと素材Cの境界から破断した。
【0025】
1回目の鍛造後の荷重保持が小さい試験No.11では、素材Aと素材Cの境界に凝固収縮に伴う微細な鋳巣と思われる空孔が見られ、引張試験では素材Aと素材Cの境界から破断した。
【0026】
2回目の鍛造での加工速度が小さい試験No.12、13では、加工中に鍛造型との接触により温度低下が生じ、液相部分が減少したため、素材Bと素材Cの一体化がやや不十分であり、素材Bと素材Cの境界にわずかに空孔が見られ、引張試験では素材Bと素材Cの境界から破断した。
【0027】
2回目の鍛造後の荷重保持が小さい試験No.14では、素材Bと素材Cの境界に凝固収縮に伴う微細な鋳巣と思われる空孔が見られ、引張試験では素材Bと素材Cの境界から破断した。。
【0028】
1回目の鍛造で、素材Aの固相率が1.0となる温度に加熱した試験No.15では、素材Aと素材Cの一体化が不十分であり、素材Aと素材Cの境界に空孔が見られ、引張試験では素材Aと素材Cの境界から破断した。
【0029】
2回目の鍛造で、素材Aと素材Cからなる中間製品のうち素材Cの固相率が1.0となる温度に加熱した試験No.17では、素材Bと素材Cの一体化が不十分であり、素材Bと素材Cの境界に空孔が見られ、引張試験では素材Bと素材Cの境界から破断した。
【0030】
1回目の鍛造で、素材Bの固相率が0.1となる温度に加熱した試験No.16では、加熱炉内で金属素材Bが部分的に熔け落ち、鍛造型への搬送が出来なかった。
2回目の鍛造で、素材Aと素材Cからなる中間製品のうち素材Cの固相率の固相率が0.1となる温度に加熱した試験No.18では、加熱炉内で金属素材Cが部分的に熔け落ち、鍛造型への搬送が出来なかった。
したがって、試験No.16、18は鍛造品の引張試験を実施できなかった。
【0031】
(実施例2)
本発明外の実施例として、実施例1と同様に2種類の金属及びインサート材で構成される図6に示すような形状である鍛造品の鍛造を実施した。素材は実施例1で用いた表1と同じである。
鍛造素材として、図9に示すように、外径DA0、内径dA0、高さhA0の円筒形状である素材6Aと、外径DB0、高さhB0の円柱形状である素材6B、外径DC0、内径dC0、高さhC0の円筒形状である素材6Cを準備した。
【0032】
1回目の鍛造で素材6Bと素材6Cの鍛造を行い図10に示すように素材6Bと素材6Cからなる中間製品6Dを成形した後、2回目の鍛造で中間製品6Dと素材6Aの鍛造を行い第4図に示す鍛造品1を成形した。表6に1回目の鍛造条件を、表7に2回目の鍛造条件を示す。
鍛造品の品質を評価するため、実施例1と同様に、内部空孔有無の観察及び引張試験を実施した。表8に評価結果を示す。
【0033】
【表6】
【0034】
【表7】
【0035】
【表8】
【0036】
2回目の鍛造で、素材Bと素材Cからなる中間製品Dのうち素材Bの固相率が0.0となる温度に中間製品Dを加熱した試験No.19では、加熱炉内で金属素材Bが熔け落ち、鍛造型への搬送が出来なかった。したがって、試験No.19は鍛造品の引張試験を実施できなかった。
【0037】
2回目の鍛造で、素材Aの固相率が1.0となる温度に加熱した試験No.20では、素材Aと素材Cの一体化が不十分であり、素材Aと素材Cの境界に空孔が見られ、引張試験では素材Aと素材Cの境界から破断した。
【0038】
実施例2では、2回目の鍛造で、素材Bと素材Cからなる中間製品Dのうち素材Bの固相率が0.3以上0.9未満となる温度域T0.3-0.9 と素材Aの固相率が0.3以上0.9未満となる温度域T0.3-0.9 が無いため、健全な鍛造品を得ることは出来なかった。
【0039】
(実施例3)
本発明外の実施例として、図11((a)は平面図、(b)は側面図)に示すような形状をもつ2種類の金属で構成される鍛造品の鍛造を実施した。素材は実施例1で用いた表1の内、素材Aと素材Bである。表9に鍛造条件を示す。
【0040】
【表9】
【0041】
鍛造素材として、図12に示すように、外径DA0、内径dA0、高さhA0の円筒形状である素材8Aと、外径DB0、高さhB0の円柱形状である素材8Bを準備した。
鍛造品の品質を評価するため、実施例1と同様に、内部空孔有無の観察及び引張試験を実施した。表10に評価結果を示す。
【0042】
【表10】
【0043】
素材Bの固相率が0.0となる温度に素材Bを加熱した試験No.21では、加熱炉内で金属素材Bが熔け落ち、鍛造型への搬送が出来なかった。したがって、試験No.21は鍛造品の引張試験を実施できなかった。
素材Aの固相率が1.0となる温度に加熱した試験No.22では、素材Aと素材Bの一体化が不十分であり、素材Aと素材Bの境界に空孔が見られ、引張試験では素材Aと素材Bの境界から破断した。
【0044】
実施例3では、インサート材を用いておらず、素材Aの固相率が0.3以上0.9未満となる温度域T0.3-0.9 と素材Bの固相率が0.3以上0.9未満となる温度域T0.3-0.9 が無いため、健全な鍛造品を得ることは出来なかった。
【0045】
【発明の効果】
本発明では、融点の大きく異なる異種金属からなる鍛造品を成形する際、インサート材を加えて順次固液共存温度域に加熱して、鍛造,一体化させることにより、高歩留まりかつ少数回の鍛造工程で部位に応じた金属素材を用いた複雑形状部品を鍛造でき、自動車,機械用部品等を低コストで提供できる。
【図面の簡単な説明】
【図1】利用可能な素材の組合せと加熱温度範囲
【図2】加熱温度範囲
【図3】金属素材の組合せ方の例
【図4】金属素材の組合せ方の例
【図5】金属素材の組合せ方の例
【図6】鍛造品
【図7】鍛造に用いる金属素材
【図8】第1回目鍛造後の中間製品
【図9】鍛造に用いる金属素材
【図10】第1回目鍛造後の中間製品
【図11】鍛造品
【図12】鍛造に用いる金属素材
【符号の説明】
1A 高融点金属素材
1B 角柱である低融点金属素材
1C インサート材
1D 円柱である中間製品
2A 高融点金属素材
2B 同径の円柱である低融点金属素材
2C インサート材
2D 同径の円柱である中間製品
3A 高融点金属素材
3B 同径の内径を持つ円筒である低融点金属素材
3C インサート材
3D 同径の円柱である中間製品
41 鍛造品
42 引張試験片採取位置
4A 金属素材Aからなる部位
4B 金属素材Bからなる部位
4C 金属素材Cからなる部位
5A 鍛造に用いる金属素材A
5B 鍛造に用いる金属素材B
5C 鍛造に用いる金属素材B
5D 金属素材Aと金属素材Cからなる中間製品
6A 鍛造に用いる金属素材A
6B 鍛造に用いる金属素材B
6C 鍛造に用いる金属素材B
6D 金属素材Bと金属素材Cからなる中間製品
71 鍛造品
72 引張試験片採取位置
7A 金属素材Aからなる部位
7B 金属素材Bからなる部位[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a method for manufacturing a part made of a dissimilar metal, and particularly to a method for manufacturing a part having a complicated shape.
[0002]
[Prior art]
Up to now, as a method for joining and integrating dissimilar metals, a joining method in a solid phase temperature range, a liquid phase temperature range or a solid-liquid coexisting temperature range has been disclosed. For example, in the solid phase temperature range, Japanese Patent Application Laid-Open No. 56-128688 discloses a method of increasing the joining surface strength by forming hot irregularities on the metal surfaces to be joined and then performing hot isostatic pressing. In the liquid phase temperature range, Japanese Patent Application Laid-Open No. 63-295077 discloses a method in which one surface of a metal to be joined is melted and then the other metal is pressed and cooled. Furthermore, in the solid-liquid coexistence temperature region, one of the metals to be joined is heated to the solid-liquid coexistence temperature region in the literature (Volume of Plastic Processing Joint Lecture Vol. 48th PAGE. 407-408 1997). A method of cooling after insertion is disclosed.
[0003]
[Problems to be Solved by the Invention]
However, in Japanese Patent Application Laid-Open Nos. 56-128688 and 63-295077, when manufacturing complex-shaped parts by joining and integrating dissimilar metals, the respective metal bodies are preliminarily formed into shapes constituting the final shape. It is necessary to finish, and then a method of joining dissimilar metals must be adopted, leading to an increase in manufacturing cost. In addition, in the literature, it is possible to manufacture parts with specific shapes such as finned parts at a low cost, but they do not actively create part shapes and are difficult to apply to parts with other shapes. Also, the bonding strength is insufficient.
The present invention has been made in view of the above points, and by using two or more kinds of different metal materials having an extremely simple shape, complex shaped parts made of different metals are formed with a high yield and a small number of forging processes. And it aims at improving the intensity | strength of a joint surface.
[0004]
[Means for Solving the Problems]
That is, the gist of the present invention is that
1) In a method for manufacturing a forged part made of a high melting point metal and a low melting point metal that do not overlap each other in a temperature range T 0.3-0.9 in which the solid phase ratio fS is 0.3 or more and less than 0.9, On the other hand, an overlapping single metal having a temperature range T 0.3-0.9 in which the solid phase ratio fS is 0.3 or more and less than 0.9 is used as the insert material, and the refractory metal and the insert material are each fixed. After the intermediate product is manufactured by heating, inserting into a forging die and forging to an overlapping temperature in the temperature range T 0.3-0.9 where the phase ratio fS is 0.3 or more and less than 0.9, the intermediate product And the low melting point metal is heated to an overlapping temperature T 0.3-0.9 at which the solid phase ratio fS of the insert material and the low melting point metal is 0.3 or more and less than 0.9, and is inserted into the forging die. Semi-molten forging method characterized by forging and integrating 2) Solid phase ratio fS of 0.3 or more and 0.9 or less In the method for manufacturing a forged component made of a refractory metal and a low melting metal not overlapping temperature region T 0.3-0.9 serving as the solid phase rate fS is less than 0.3 to 0.9 for each metal A plurality of insert materials having different melting points with overlapping temperature ranges T 0.3-0.9 are used, and each of the high melting point metal material and the high melting point insert material has a solid phase ratio fS of 0.3 or more and 0.9. The first intermediate product is manufactured by heating to an overlapping temperature in the temperature range T 0.3-0.9 , being inserted into the forging die, and forging, and the first intermediate product and the low melting point insert are Heating to the overlapping temperature range T 0.3-0.9 where the solid phase ratio fS of the melting point insert material and the low melting point insert material is 0.3 or more and less than 0.9, insert into the forging die, forging (2) After manufacturing the intermediate product, the second intermediate product and the low melting point metal are mixed with the low melting point insert material and the low melting point metal. Heating to an overlapping temperature in the temperature range T 0.3-0.9 where the solid phase ratio fS of the melting point metal is 0.3 or more and less than 0.9, inserting into a forging die, forging and integrating. The semi-molten forging method 3) The semi-molten forging method 4) according to the above 1), wherein at least one of the shapes of the high melting point metal, the insert material, the intermediate product, and the low melting point metal is different. The semi-molten forging method according to 1) above, wherein at least one pair of shapes of the metal, the insert material, the intermediate product, and the low melting point metal has the same diameter 5) The high melting point metal, the insert material, the intermediate material, and the low melting point The semi-molten forging method 6) according to 1) above, wherein at least one pair of shapes of the metal is cylindrical and columnar, and the inner diameter of the cylinder and the outer diameter of the column are substantially the same. High melting point insert, first intermediate product and low melting point insert The semi-molten forging method according to 2) above, wherein the shape of at least one of the first and second intermediate products and the low-melting-point insert material is different, 7) the high-melting-point metal and the high-melting-point insert material, the first The semi-molten forging method according to 2) above, wherein at least one pair of the intermediate product and the low melting point insert material and the second intermediate product and the low melting point insert material have the same diameter. At least one set of the insert material, the first intermediate product and the low-melting-point insert material, and the second intermediate product and the low-melting-point insert material has a cylindrical shape and a cylindrical shape, and the cylindrical inner diameter and the cylindrical outer diameter are substantially the same diameter. thixoforging method 9) a refractory metal above 2), wherein that, the refractory metal and the initial height h 0 of the insert material, the relationship between the height h after forging the insert material, a refractory metal Heat the insert material In relation to the smallest fs min of solid fraction fS of time,
ln (h 0 /h)≧1.5×fs min 2
A semi-molten forging method according to any one of claims 1), 3) to 5), characterized in that a refractory metal and an insert material having a shape satisfying the above requirements are used. initial height h 0 and the intermediate products, the relationship between the height h after forging the low melting point metal, an intermediate product, the relationship between the smallest fs min of the solid phase rate fs upon heating the low melting point metal In
ln (h 0 /h)≧1.5×fs min 2
The intermediate product having a shape satisfying the above requirements, a low melting point metal is used, The semi-molten forging method according to any one of the above 1), 3) to 5), 9) 11) a high melting point metal The relationship between the initial height h 0 of the high melting point insert material and the height h after forging of the high melting point metal and high melting point insert material is the solid phase ratio fs when the high melting point metal and high melting point insert material are heated. In relation to the smallest fs min ,
ln (h 0 /h)≧1.5×fs min 2
The semi-molten forging method 12) according to any one of 2) and 6) to 8) above, wherein a refractory metal and a refractory insert material having a shape satisfying the above requirements are used. the initial height h 0 of the melting insert material first intermediate product, the relationship between the height h after forging of low melting insert material, the first intermediate product, of the solid phase rate fs upon heating the low-melting insert material In relation to the smallest fs min ,
ln (h 0 /h)≧1.5×fs min 2
A semi-molten forging method according to any one of 2), 6) to 8), 11) above, characterized in that a first intermediate product and a low insert material having a shape satisfying the above requirements are used. product, the initial height h 0 of the low-melting-point metal second intermediate product, the relationship between the height h after forging the metal having a low melting point, the second intermediate product, of the solid phase rate fs upon heating the low melting point metal In relation to the smallest fs min ,
ln (h 0 /h)≧1.5×fs min 2
The semi-molten forging method according to any one of 2), 6) to 8), 11), and 12) above, characterized in that a 2 intermediate product and a low melting point metal having a shape satisfying the requirements are used. The semi-molten forging method 15 according to any one of 1) to 13) above, wherein molding is performed at a processing speed of 500 mm / s or more, and average using a forging die heated to 200 ° C. or higher in advance. The semi-molten forging method 16 according to any one of 1) to 14) above, wherein the molding is performed at a processing speed of 200 mm / s or more. The semi-molten forging method according to any one of 1) to 15) above, wherein a load of 50% or more is maintained.
[0005]
DETAILED DESCRIPTION OF THE INVENTION
A metal material having different components is used depending on the required characteristics of the forged part. As shown in the graph of FIG. 1, the solid phase ratio f s of the high melting point metal material A and the low melting point metal material B is 0.3. If the temperature range T 0.3-0.9 comprising less than 0.9 or more non-overlapping temperature region T 0.3-0.9 to solid phase ratio f s for each metal material is less than 0.3 or more 0.9 duplicate Such a metal is used as an insert material. As will be described later, in order to integrate the metal materials in a sound manner, each solid fraction fs is heated to a temperature range T 0.3-0.9 where the solid phase ratio f s is 0.3 or more and less than 0.9, and then forged. This is because it is desirable. Different metals may be steels having different components, and cast iron, aluminum, magnesium, titanium, and the like can be used. One type or two or more types of insert materials may be used.
[0006]
Next, the heating temperature range is limited to the overlapping range of the temperature range T 0.3-0.9 in which the solid phase ratio f s is 0.3 or more and less than 0.9 in the combination of the dissimilar metal and the insert material. Give the reason. As shown in the graph of FIG. 2, when the heating temperature is higher than the temperature T E 0.3 at which the solid phase ratio of the material E having a low melting point is 0.3 in the combination of different metal materials or insert materials, the material E However, it cannot stand by itself in the heating furnace and cannot be transferred into the forging die. Further, in the combination of different metal materials or insert materials, when the heating temperature is lower than the temperature T D 0.9 at which the solid phase ratio of the material D having a high melting point becomes 0.9, the liquid phase component of the material D is small and the metal The material is not soundly integrated by forging. Therefore among the combinations of dissimilar metallic material or insert material, each of the solid phase ratio f s is heated to overlapping range of the temperature of the temperature range T 0.3-0.9 comprising less than 0.3 to 0.9.
[0007]
In the combination of the different metal and the insert material, heating and forging are sequentially performed in descending order of the temperature in the overlapping range of the temperature range T 0.3-0.9 where the solid phase ratio f s is 0.3 or more and less than 0.9. Which in the heating of the second and subsequent, among the combinations of the previously forged different metals or insert material, a low temperature region T 0.3-0.9 to solid phase ratio f s is less than 0.3 or more 0.9 material heating This is to prevent melting in the furnace.
[0008]
For example, as shown in FIGS. 3 to 5 (both (a) is a plan view and (b) is a side view), the shape of the dissimilar metal, insert material or intermediate product is different after the first forging. It may be a shape, the same diameter shape, or a cylinder and a column, and the cylinder inner diameter and the column diameter may be substantially the same.
[0009]
Forging the refractory metal and insert material to obtain an intermediate product, forging the intermediate product and insert material as necessary to obtain an intermediate product, forging the intermediate product and low melting point metal to produce a final product In the obtaining step, the relationship between the initial height h 0 of each of the high melting point metal, the insert material and the low melting point metal and the height h after forging of each of the high melting point metal, the insert material and the low melting point metal is In relation to the smallest f smin among the solid phase ratios f s when heated by a combination of a material and a low melting point metal,
ln (h 0 /h)≧1.5×f smin 2
The reason why each metal material using a high melting point metal, an insert material, and a low melting point metal satisfying the above conditions is used is that each metal material is sufficiently processed and the liquid phases are sufficiently mixed and integrated. .
[0010]
The reason for forming at a processing speed of 500 mm / sec or more on average during forging is that at a lower processing speed, the temperature of the metal material heated by the contact with the forging die is lowered and the metal materials are not sufficiently integrated with each other. is there. The upper limit of the processing speed is not particularly limited in order to obtain the effect of the present invention, and depends on the equipment capacity.
[0011]
When using a die that has been heated to 200 ° C. or higher in advance, since the temperature drop of the metal material due to contact with the forging die is alleviated, an average processing speed of 200 mm / second or more during forging is sufficient. The upper limit of the heating temperature is not particularly limited in order to obtain the effects of the present invention, but is preferably 500 ° C. or lower in order to prevent temper softening of the mold.
[0012]
The reason why the load of at least 50% of the maximum forging load is maintained until the temperature becomes below the solidus temperature after the completion of molding is to prevent the formation of a cast hole due to solidification shrinkage and improve the material properties after forging. The effect is not sufficient when the load is less than 50% of the maximum forging load. The upper limit of the holding load is not particularly limited in order to obtain the effect of the present invention, and may be 100% of the maximum forging load.
[0013]
【Example】
(Example 1)
As an example, forging of a forged product having a shape shown in FIG. 6 ((a) is a plan view and (b) is a side view) composed of two types of
The material used was material A, which is a high melting point material having the chemical components shown in Table 1, material B, which is a low melting point material, and material C, which is an insert material. The solidus temperature and liquidus temperature measured by differential thermal analysis are shown in Table 2, respectively.
[0014]
[Table 1]
[0015]
[Table 2]
[0016]
As the forging material, as shown in FIG. 7, a
[0017]
The forging of the
[0018]
[Table 3]
[0019]
[Table 4]
[0020]
In order to evaluate the quality of the forged product, the presence or absence of internal voids and a tensile test were performed. Regarding the internal voids, the cross section of the forged product 1 was cut and polished, and the presence or absence of voids was observed with an optical microscope. A sample of φ6 was cut out from the position shown in FIG. 6 of the forged product 1, and a tensile test piece was prepared by press-contacting the threaded portion. The tensile test was performed at room temperature. Table 5 shows the evaluation results.
[0021]
[Table 5]
[0022]
Test No. In all cases, the inner holes were not found in the forged product, and the tensile strength was 400 MPa or more. The breaking position was the position of metal B having low strength.
[0023]
Test No. with low logarithmic strain in the first forging In Examples 5 and 6, the integration of the material A and the material C was slightly insufficient, and a slight hole was observed at the boundary between the material A and the material C. In the tensile test, fracture occurred from the boundary between the material A and the material B.
Test No. with low logarithmic strain in the second forging 7 and 8, the integration of the material B and the material C was slightly insufficient, and a slight hole was observed at the boundary between the material B and the material C. In the tensile test, fracture occurred from the boundary between the material B and the material C.
[0024]
Test No. with low processing speed in the first forging. In Nos. 9 and 10, the temperature decreased due to contact with the forging die during processing, and the liquid phase portion was reduced. Therefore, the integration of the material A and the material C was slightly insufficient, and the boundary between the material A and the material C was slightly small. In the tensile test, fracture occurred from the boundary between the material A and the material C.
[0025]
Test No. with small load retention after the first forging. In No. 11, voids that appear to be fine voids due to solidification shrinkage were found at the boundary between the material A and the material C, and fractured from the boundary between the material A and the material C in the tensile test.
[0026]
Test No. 2 with low processing speed in the second forging. In Nos. 12 and 13, the temperature decreased due to contact with the forging die during processing, and the liquid phase portion was reduced. Therefore, the integration of the material B and the material C was slightly insufficient, and there was a slight gap between the material B and the material C. In the tensile test, fracture occurred from the boundary between the material B and the material C.
[0027]
Test No. with small load retention after the second forging. In No. 14, voids that appear to be fine voids due to solidification shrinkage were found at the boundary between the material B and the material C, and fractured from the boundary between the material B and the material C in the tensile test. .
[0028]
Test No. 1 was heated to a temperature at which the solid phase ratio of material A was 1.0 in the first forging. 15, the integration of the material A and the material C was insufficient, and voids were seen at the boundary between the material A and the material C, and fractured from the boundary between the material A and the material C in the tensile test.
[0029]
Test No. 2 was heated to a temperature at which the solid phase ratio of material C among the intermediate products made of material A and material C was 1.0 in the second forging. In No. 17, the integration of the material B and the material C was insufficient, and voids were observed at the boundary between the material B and the material C, and fractured from the boundary between the material B and the material C in the tensile test.
[0030]
Test No. 1 was heated to a temperature at which the solid fraction of material B was 0.1 in the first forging. In No. 16, the metal material B partially melted in the heating furnace, and could not be transferred to the forging die.
In the second forging, among the intermediate products made of material A and material C, test No. 1 was heated to a temperature at which the solid phase ratio of material C was 0.1. In No. 18, the metal material C partially melted in the heating furnace and could not be conveyed to the forging die.
Therefore, test no. 16 and 18 could not carry out the tensile test of the forged product.
[0031]
(Example 2)
As an example outside the present invention, forging of a forged product having a shape as shown in FIG. 6 composed of two kinds of metals and an insert material was carried out in the same manner as in Example 1. The material is the same as in Table 1 used in Example 1.
As the forging material, as shown in FIG. 9, a material 6A having a cylindrical shape with an outer diameter D A0 , an inner diameter d A0 and a height h A0 , and a
[0032]
The forging of the
In order to evaluate the quality of the forged product, as in Example 1, the presence or absence of internal vacancies and a tensile test were performed. Table 8 shows the evaluation results.
[0033]
[Table 6]
[0034]
[Table 7]
[0035]
[Table 8]
[0036]
Test No. 2 in which the intermediate product D was heated to a temperature at which the solid phase ratio of the material B among the intermediate products D made of the materials B and C was 0.0 in the second forging. In No. 19, the metal material B melted in the heating furnace and could not be transferred to the forging die. Therefore, test no. No. 19 could not carry out the tensile test of the forged product.
[0037]
Test No. 2 was heated to a temperature at which the solid phase ratio of material A was 1.0 in the second forging. In No. 20, the integration of the material A and the material C was insufficient, and voids were observed at the boundary between the material A and the material C, and fractured from the boundary between the material A and the material C in the tensile test.
[0038]
In Example 2, in the second forging, the temperature range T 0.3-0.9 in which the solid phase ratio of the material B of the intermediate product D made of the material B and the material C is 0.3 or more and less than 0.9 and the material A Since there was no temperature range T 0.3-0.9 where the solid phase ratio was 0.3 or more and less than 0.9, a sound forged product could not be obtained.
[0039]
(Example 3)
As an example outside the present invention, forging of a forged product having two shapes as shown in FIG. 11 ((a) is a plan view and (b) is a side view) was performed. The materials are Material A and Material B in Table 1 used in Example 1. Table 9 shows the forging conditions.
[0040]
[Table 9]
[0041]
As the forging material, as shown in FIG. 12, a
In order to evaluate the quality of the forged product, as in Example 1, the presence or absence of internal vacancies and a tensile test were performed. Table 10 shows the evaluation results.
[0042]
[Table 10]
[0043]
Test No. 1 in which material B was heated to a temperature at which the solid phase ratio of material B was 0.0. In No. 21, the metal material B melted down in the heating furnace and could not be transferred to the forging die. Therefore, test no. No. 21 could not carry out the tensile test of the forged product.
Test No. 1 was heated to a temperature at which the solid phase ratio of material A was 1.0. In No. 22, the integration of the material A and the material B was insufficient, and voids were observed at the boundary between the material A and the material B. In the tensile test, fracture occurred from the boundary between the material A and the material B.
[0044]
In Example 3, no insert material was used, the temperature range T 0.3-0.9 in which the solid phase ratio of the material A was 0.3 or more and less than 0.9, and the solid phase ratio of the material B was 0.3 or more and 0.00 . Since there was no temperature range T 0.3-0.9 that would be less than 9, a sound forged product could not be obtained.
[0045]
【The invention's effect】
In the present invention, when forming a forged product made of dissimilar metals having greatly different melting points, an insert material is added and sequentially heated to a solid-liquid coexistence temperature range, and forged and integrated, thereby achieving high yield and a small number of forgings. It is possible to forge complex shaped parts using metal materials according to the site in the process, and to provide automobiles, machine parts, etc. at low cost.
[Brief description of the drawings]
[Fig. 1] Combination of available materials and heating temperature range [Fig. 2] Heating temperature range [Fig. 3] Example of how to combine metal materials [Fig. 4] Example of how to combine metal materials [Fig. Example of combination [Fig. 6] Forged product [Fig. 7] Metal material used for forging [Fig. 8] Intermediate product after the first forging [Fig. 9] Metal material used for forging [Fig. 10] After the first forging Intermediate products [Fig. 11] Forged products [Fig. 12] Metal materials used for forging [Explanation of symbols]
1A high melting
5B Metal material B used for forging
Metal material B used for 5C forging
5D Intermediate product 6A consisting of metal material A and metal material C Metal material A used for forging
6B Metal material B used for forging
6C Metal material B used for forging
Claims (16)
ln(h0/h)≧1.5×fsmin 2
を満たすような形状の高融点金属、インサート材を用いることを特徴とする請求項1、3 〜5の何れか1項に記載の半溶融鍛造方法。The relationship between the initial height h 0 of the refractory metal and the insert material and the height h after forging of the refractory metal and the insert material is the most of the solid phase ratio f S when the refractory metal and the insert material are heated. In relation to a small f smin ,
ln (h 0 /h)≧1.5×f smin 2
Refractory metal shaped to satisfy the, thixoforging method according to any one of claims 1, 3-5, which comprises using an insert material.
ln(h ln (h 00 /h)≧1.5×f/H)≧1.5×f sminsmin 22
を満たすような形状の中間製品、低融点金属を用いることを特徴とする請求項1、3〜5、9の何れか1項に記載の半溶融鍛造方法。The semi-molten forging method according to any one of claims 1, 3 to 5, and 9, wherein an intermediate product and a low melting point metal having a shape satisfying the above conditions are used.
ln(h ln (h 00 /h)≧1.5×f/H)≧1.5×f sminsmin 22
を満たすような形状の高融点金属、高融点インサート材を用いることを特徴とする請求項2、6〜8の何れか1項に記載の半溶融鍛造方法。The semi-molten forging method according to any one of claims 2 and 6 to 8, wherein a refractory metal or a refractory insert material having a shape satisfying the above requirements is used.
ln(h ln (h 00 /h)≧1.5×f/H)≧1.5×f sminsmin 22
を満たすような形状の第1中間製品、低インサート材を用いることを特徴とする請求項2、6〜8、11の何れか1項に記載の半溶融鍛造方法。The semi-molten forging method according to any one of claims 2, 6 to 8, and 11, wherein a first intermediate product and a low insert material having a shape satisfying the above conditions are used.
ln(h ln (h 00 /h)≧1.5×f/H)≧1.5×f sminsmin 22
を満たすような形状の2中間製品、低融点金属を用いることを特徴とする請求項2、6〜8、11、12の何れか1項に記載の半溶融鍛造方法。The semi-molten forging method according to any one of claims 2, 6 to 8, 11, and 12, wherein two intermediate products and a low melting point metal having a shape satisfying the requirements are used.
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WO2011152556A1 (en) | 2010-06-04 | 2011-12-08 | 古河スカイ株式会社 | Method of joining aluminum alloys |
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WO2011152556A1 (en) | 2010-06-04 | 2011-12-08 | 古河スカイ株式会社 | Method of joining aluminum alloys |
US9174303B2 (en) | 2010-06-04 | 2015-11-03 | Furukawa-Sky Aluminum Corp. | Method of bonding aluminum alloy materials to each other |
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