JP2019516011A - アルミニウム、コバルト、鉄、及びニッケルのfcc材料、並びにそれを用いた製品 - Google Patents
アルミニウム、コバルト、鉄、及びニッケルのfcc材料、並びにそれを用いた製品 Download PDFInfo
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Abstract
Description
また、上記の新材料を付加製造によって製造することも可能である。本明細書で使用される場合、「付加製造(additive manufacturing)」とは、「Standard Terminology for Additively Manufacturing Technologies」と題するASTM F2792−12aで定義される「除去加工(subtractive manufacturing)法とは対照的に、材料を結合して3Dモデルデータから物体を、通常は層の上に層を、製造する方法」を意味する。新材料は、このASTM規格に記載されている任意の適切な付加製造技術、例えばバインダージェッティング、指向性エネルギー堆積法、材料押出、材料噴射、パウダーベッドフュージョン、又はシートラミネーション等によって製造されることができる。
上記の開示は、概ね、析出相をその中に有する新しいfcc材料を製造する方法を記載しているが、fcc固溶体構造から本質的になる材料を製造することも可能である。例えば、上記のように、インゴット、鍛造体、形状キャスティング、又は付加製造された本体の製造後、例えば上記の溶解工程(20)に関して記載される方法で材料を均質化することができる。適切な急速冷却により、任意の第2相粒子の析出を抑制/制限することができ、それにより本質的に第2相粒子を全く含まないfcc固溶体材料、即ち本質的にfcc固溶体構造からなる材料を実現することができる。
Claims (33)
- 4.4〜11.4重量%のAl、
4.9〜42.2重量%のCo、
4.6〜28.9重量%のFe、
44.1〜86.1重量%のNi、を含み、
残部が任意の付随元素及び不純物である組成物。 - 前記付随元素は、最大0.15重量%のC、最大0.15重量%のB、最大0.5重量%のHf、及び最大0.5重量%のZrを含む、請求項1に記載の組成物。
- 前記組成物は、4.9〜18.2重量%のCo、4.6〜17.3重量%のFe、及び57.4〜86.1重量%のNiを含む、請求項1に記載の組成物。
- 前記組成物は、6.8〜11.4重量%のAl、4.9〜12.5重量%のCo、4.8〜17.3重量%のFe、及び64.1〜83.5重量%のNiを含む、請求項1に記載の組成物。
- 前記組成物は、4.8〜10.4重量%のAl、5.4〜38.3重量%のCo、5.1〜26.3重量%のFe、及び49.0〜81.9重量%のNiを含む、請求項1に記載の組成物。
- 前記組成物は、5.4〜16.5重量%のCo、5.1〜15.7重量%のFe、及び63.8〜81.9重量%のNiを含む、請求項5に記載の組成物。
- 前記組成物は、7.5〜10.4重量%のAl、5.5〜11.3重量%のCo、5.3〜15.7重量%のFe、及び71.2〜78.7重量%のNiを含む、請求項1に記載の組成物。
- 請求項1〜7に記載の前記組成物のいずれかを含む合金本体。
- 前記合金本体は、航空宇宙又は自動車部品の形態である、請求項8に記載の合金本体。
- 前記航空宇宙又は自動車部品はタービンである、請求項9に記載の航空宇宙部品。
- 前記合金本体は、密度、延性、強度、破壊靭性、耐酸化性、耐疲労性、耐クリープ性及び耐高温性のうちの少なくとも2つの改善された組み合わせを含む、請求項8に記載の合金本体。
- 前記合金本体は、インゴットの形態である、請求項8に記載の合金本体。
- 前記合金本体は、圧延製品の形態である、請求項8に記載の合金本体。
- 前記合金本体は、押出品の形態である、請求項8に記載の合金本体。
- 前記合金本体は、鍛造品の形態である、請求項8に記載の合金本体。
- 前記合金本体は、形状キャスティング品の形態である、請求項8に記載の合金本体。
- 前記合金本体は、付加製造された製品の形態である、請求項8に記載の合金本体。
- (a)付加製造装置において原料を使用する工程であって、前記原料は、
4.4〜11.4重量%のAl、
4.9〜42.2重量%のCo、
4.6〜28.9重量%のFe、
44.1〜86.1重量%のNi、を含む、原料を使用する工程と、
(b)前記原料を使用して前記付加製造装置内で金属製品を製造する工程と、を含む、方法。 - 前記原料は粉末原料を含み、前記方法は、
(a)前記粉末原料の金属粉末を床に分散させ、及び/又は前記粉末原料の金属粉末を基材へ向かって、又は基材上へ噴霧する工程と、
(b)前記金属粉末の一部をその液相線温度を超えて選択的に加熱して、それにより溶融プールを形成する工程と、
(c)前記溶融プールを冷却し、それにより前記金属製品の一部を形成する工程であって、前記冷却する工程は、少なくとも100℃/秒の冷却速度で冷却する工程を含む、形成する工程と、
(d)前記金属製品が完成するまで工程(a)〜(c)を繰り返す工程であって、前記金属製品が金属マトリックスを含み、前記Al、Co、Fe、及びNiが前記マトリックスを構成する、繰り返す工程と、を含む、請求項18に記載の方法。 - 前記加熱する工程は放射線源による加熱することを含み、前記冷却速度は少なくとも1000℃/秒である、請求項19に記載の方法。
- 前記原料はワイヤ原料を含み、前記方法は、
(a)放射線源を使用してワイヤ原料の液相線点を超えて前記ワイヤ原料を加熱し、それにより溶融プールを形成する工程であって、前記溶融プールがAl、Co、Fe、及びNiを含む、形成する工程と、
(b)前記溶融プールを少なくとも1000℃/秒の冷却速度で冷却する工程と、
(c)前記金属製品が完成するまで工程(a)〜(b)を繰り返す工程であって、前記金属製品が金属マトリックスを含み、前記Al、Co、Fe、及びNiが前記マトリックスを構成する、繰り返す工程と、を含む、請求項18に記載の方法。 - 前記冷却速度は少なくとも1つの析出相を形成するのに十分である、請求項19〜21のいずれか一項に記載の方法。
- 前記少なくとも1つの析出相はL12及びB2のうちの少なくとも1つを含む、請求項22に記載の方法。
- 前記金属製品は少なくとも0.5体積%の前記析出相を含む、請求項22又は23のいずれか一項に記載の方法。
- 前記付加製造装置はバインダージェッティング装置を含む、請求項18に記載の方法。
- 前記付加製造装置は指向性エネルギー堆積装置である、請求項18に記載の方法。
- 前記指向性エネルギー堆積装置は電子ビーム装置又はプラズマアーク装置を備える、請求項26に記載の方法。
- 前記金属製品を加工する工程を含む、請求項18に記載の方法。
- 前記金属製品は、最終付加製造された本体であり、前記加工する工程は前記最終付加製造された本体の加工である、請求項28に記載の方法。
- 前記製造する工程は、
前記原料を使用して前記金属製品の一部を第1に製造する工程と、
前記原料を使用して前記金属製品の別の部分を第2に製造する工程と、を含み、
前記加工する工程は、少なくとも前記第1に又は第2に製造する工程の後に行われる、請求項28に記載の方法。 - 前記加工する工程は、前記第1に製造する工程と前記第2に製造する工程との間に行われる、請求項30に記載の方法。
- 前記加工する工程は熱間静水圧プレスを含む、請求項28〜31のいずれか一項に記載の方法。
- 前記加工する工程は、圧延、鍛造、及び押出のうちの1つ又は複数を含む、請求項28〜31のいずれか一項に記載の方法。
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2019
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CN109072347A (zh) | 2018-12-21 |
CA3016761A1 (en) | 2017-10-26 |
EP3445881A4 (en) | 2019-09-04 |
US10202673B2 (en) | 2019-02-12 |
US10480051B2 (en) | 2019-11-19 |
WO2017184771A1 (en) | 2017-10-26 |
US20190169718A1 (en) | 2019-06-06 |
US20170306458A1 (en) | 2017-10-26 |
EP3445881A1 (en) | 2019-02-27 |
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