JP2010528187A5 - - Google Patents

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JP2010528187A5
JP2010528187A5 JP2010509649A JP2010509649A JP2010528187A5 JP 2010528187 A5 JP2010528187 A5 JP 2010528187A5 JP 2010509649 A JP2010509649 A JP 2010509649A JP 2010509649 A JP2010509649 A JP 2010509649A JP 2010528187 A5 JP2010528187 A5 JP 2010528187A5
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alloy
solid
semi
aluminum
aluminum alloy
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JP2010509649A
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JP2010528187A (en
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Priority claimed from PCT/CA2008/001051 external-priority patent/WO2008144935A1/en
Publication of JP2010528187A publication Critical patent/JP2010528187A/en
Publication of JP2010528187A5 publication Critical patent/JP2010528187A5/ja
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Claims (13)

i) 0.010〜0.025質量%なる範囲のSr、
ii) ホウ素含有率で測定して、0.001〜0.005質量%のBなる範囲の量のTiB2
iii) TiB 2 においてBと化学量論的に結合した量を越えて、0.16%以下の過剰なTi、及び
iv) 1.2質量%までのSi、
を含むことを特徴とする、アルミニウム合金。
i) Sr in the range of 0.010 to 0.025 mass% ,
ii) TiB 2 in an amount ranging from 0.001 to 0.005% by weight B, as measured by boron content ;
Beyond B a stoichiometric binding amounts in iii) TiB 2, 0.16% or less of excess Ti, and
iv) Si up to 1.2% by weight,
An aluminum alloy comprising:
主としてアルミニウムと銅とを含む合金;主としてアルミニウムとマンガンとを含む合金;主としてアルミニウムとマグネシウムとを含む合金;主としてアルミニウム、マグネシウム及びケイ素を含む合金;及び主としてアルミニウム、マグネシウム、亜鉛及び銅を含む合金からなる群から選択される、請求項1記載のアルミニウム合金。 From alloys containing mainly aluminum and copper; alloys containing mainly aluminum and manganese; alloys containing mainly aluminum and magnesium; alloys containing mainly aluminum, magnesium and silicon; and alloys containing mainly aluminum, magnesium, zinc and copper 2. The aluminum alloy according to claim 1 , wherein the aluminum alloy is selected from the group consisting of: アルミニウム、マグネシウム及びケイ素を含む、請求項1〜2のいずれか1項に記載のアルミニウム合金。 The aluminum alloy according to any one of claims 1 to 2 , comprising aluminum, magnesium and silicon. 更に、0.010〜0.020質量%なる範囲のSr、及びホウ素含有率で測定して、0.002〜0.004質量%のBなる範囲の量のTiB2を含む、請求項記載のアルミニウム合金。 Furthermore, 0.010 to 0.020 wt% Scope of Sr, and as measured by its boron content, 0.002 to 0.004 mass% of B, including the range of TiB 2 in an amount comprised, according to claim 3, wherein the aluminum alloy. 造形カスト用の合金である、請求項1〜のいずれか1項に記載のアルミニウム合金。 The aluminum alloy according to any one of claims 1 to 4 , which is an alloy for modeling casting. ダイカスト用の合金である、請求項1〜のいずれか1項に記載のアルミニウム合金。 The aluminum alloy according to any one of claims 1 to 4 , which is an alloy for die casting. 前記合金が、半-固体カスト法を利用して製造された、合金鋳造品である、請求項1〜のいずれか1項に記載のアルミニウム合金。 The aluminum alloy according to any one of claims 1 to 4 , wherein the alloy is an alloy casting produced by using a semi-solid casting method. 質量%単位で表して、0.6〜0.8のSi、0.12までのFe、0.15〜0.40のCu、0.8〜1.2のMg、0.04〜0.10のCr、0.010〜0.025のSr、ホウ素含有率で測定して0.001〜0.005質量%のBTiB2においてBと化学量論的に結合した量を越えて、0.16%以下の過剰なTi、各々0.05未満であり、全体として0.15未満の偶発的な不純物、及び残部のAlなる組成を持つ、請求項1又は2記載のアルミニウム合金。 Expressed in mass%, measured as 0.6 to 0.8 Si, Fe up to 0.12, 0.15 to 0.40 Cu, 0.8 to 1.2 Mg, 0.04 to 0.10 Cr, 0.010 to 0.025 Sr, boron content 0.005 wt% of B, beyond B stoichiometric bound amount in Ti B 2, 0.16% or less of excess Ti, are each less than 0.05, as a whole less than 0.15 incidental impurities, and 3. The aluminum alloy according to claim 1, wherein the balance is Al. 半-固体法によって鋳造するための、請求項記載のアルミニウム合金。 9. Aluminum alloy according to claim 8 , for casting by a semi-solid process. 質量%単位で表して、0.6〜0.8のSi、0.12までのFe、0.15〜0.40のCu、0.8〜1.2のMg、0.04〜0.10のCr、0.010〜0.025のSr、ホウ素含有率で測定して0.001 to 0.005質量%のBTiB2においてBと化学量論的に結合した量を越えて、0.16%以下の過剰なTi、0.45質量%までのMn、但し全Mn+Feは0.55〜0.65質量%なる範囲にあり、各々0.05未満であり、全体として0.15未満の偶発的な不純物、及び残部のAlなる組成を持つ、請求項1記載のアルミニウム合金。 Expressed in mass%, measured as 0.6 to 0.8 Si, Fe up to 0.12, 0.15 to 0.40 Cu, 0.8 to 1.2 Mg, 0.04 to 0.10 Cr, 0.010 to 0.025 Sr, boron content To 0.005 mass% B , Ti B 2 beyond the amount stoichiometrically bound to B, 0.16% or less excess Ti, Mn up to 0.45 mass%, however, total Mn + Fe is 0.55 to 0.65 mass 2. The aluminum alloy according to claim 1, wherein said aluminum alloy has a composition of an incidental impurity of less than 0.05 and less than 0.15 as a whole, and a balance of Al. 完全な溶融状態において加工するための、請求項1記載のアルミニウム合金。   The aluminum alloy according to claim 1, for processing in a completely molten state. 液相線温度及び固相線温度を持つ、請求項1〜11のいずれか1項に記載のアルミニウム合金を加工する方法であって、
(1)該合金の液相線温度及び固相線温度の範囲内の半-固体を含む、合金を調製する工程、
(2)該合金を、該液相線温度以上の、高い合金の初期温度まで加熱して、該合金を十分に溶融する工程、
(3)該合金の温度を、該初期金属合金の高い温度から、該液相線温度未満であって、かつ該固相線温度を越える半-固体温度まで減じる工程、
(4)球状固体相が液相中に分散された状態にある該合金内に、半-固体構造を生成するのに十分な期間、該合金を該半-固体温度に維持する工程であって、該半-固体構造は、約50質量%未満の固相を含む工程、
(5)該金属合金の該半-固体構造中に存在する該液相の全てではなく少なくともその幾分かを除去して、該合金の、固体に富む半-固体構造を生成する工程であって、該除去工程は、該固体に富む半-固体構造が、約35〜約55質量%の固相を含むようになるまで、液相を除去する工程を含む工程、及び
(6)該固体に富む半-固体構造を持つ該合金を、所定形状に成形する工程、
を含むことを特徴とする、方法。
A method for processing an aluminum alloy according to any one of claims 1 to 11 , having a liquidus temperature and a solidus temperature,
(1) preparing an alloy comprising a semi-solid within the range of the liquidus temperature and solidus temperature of the alloy;
(2) heating the alloy to a high alloy initial temperature equal to or higher than the liquidus temperature to sufficiently melt the alloy;
(3) reducing the temperature of the alloy from a high temperature of the initial metal alloy to a semi-solid temperature below the liquidus temperature and above the solidus temperature;
(4) maintaining the alloy at the semi-solid temperature for a period of time sufficient to produce a semi-solid structure in the alloy in which a spherical solid phase is dispersed in the liquid phase, The semi-solid structure comprises less than about 50% by weight of a solid phase;
(5) removing at least some of the liquid phase present in the semi-solid structure of the metal alloy to produce a solid-rich semi-solid structure of the alloy. The removing step comprises removing the liquid phase until the solid-rich semi-solid structure contains about 35 to about 55 wt% solid phase; and
(6) forming the alloy having a semi-solid structure rich in the solid into a predetermined shape;
A method comprising the steps of:
溶融状態にある前記合金を、該合金内に半-固体状態を生成するのに十分な期間、所定温度に維持できる、請求項12記載の方法。 13. The method of claim 12 , wherein the alloy in a molten state can be maintained at a predetermined temperature for a period of time sufficient to produce a semi-solid state in the alloy.
JP2010509649A 2007-05-31 2008-05-29 Aluminum alloy formulations for reducing hot cracking susceptibility Ceased JP2010528187A (en)

Applications Claiming Priority (2)

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US94120707P 2007-05-31 2007-05-31
PCT/CA2008/001051 WO2008144935A1 (en) 2007-05-31 2008-05-29 Aluminum alloy formulations for reduced hot tear susceptibility

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EP (1) EP2152923A4 (en)
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CA (1) CA2687893A1 (en)
WO (1) WO2008144935A1 (en)

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