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JP4883400B2 - Casting parts - Google Patents
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JP4883400B2 - Casting parts - Google Patents

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JP4883400B2
JP4883400B2 JP2006261849A JP2006261849A JP4883400B2 JP 4883400 B2 JP4883400 B2 JP 4883400B2 JP 2006261849 A JP2006261849 A JP 2006261849A JP 2006261849 A JP2006261849 A JP 2006261849A JP 4883400 B2 JP4883400 B2 JP 4883400B2
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layer
hardness
coating
casting
thickness
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JP2008080353A (en
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謙一 井上
史明 本多
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Proterial Ltd
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Hitachi Metals Ltd
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Priority to EP07018412.2A priority patent/EP1918421B1/en
Priority to KR1020070096546A priority patent/KR100987685B1/en
Priority to US11/860,951 priority patent/US7744056B2/en
Priority to CN200710154372XA priority patent/CN101152780B/en
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Description

本発明は、ダイカストおよび鋳造に使用される金型、もしくは鋳抜きピンや、ダイカストの射出機に使用されるピストンリング等の、溶融金属に接して使用される鋳造用部材に関するものである。   The present invention relates to a casting member used in contact with a molten metal, such as a die used for die casting and casting, or a casting pin, or a piston ring used for an injection machine for die casting.

溶融金属の鋳造による成形に用いられる鋳造用部材には、従来、熱間ダイス鋼、高速度鋼、ステンレス鋼等の鋼が用いられてきた。鋳造による成形で最も多く用いられる被成形金属はアルミニウム合金であるが、金型等の鋳造用部材に使用されている上記鉄鋼材料の場合、アルミニウム合金と接触する部分では、これらの鉄鋼材料がアルミニウム合金溶湯によって溶損し、アルミニウム合金溶湯中の鉄含有量を増化し、鋳造品の品質を低下させる。さらに、これら金型等の溶損は操業上種々の不都合を発生させる。   Conventionally, steels such as hot die steel, high-speed steel, and stainless steel have been used for casting members used for forming molten metal by casting. The metal to be molded most frequently used in molding by casting is an aluminum alloy. However, in the case of the above steel materials used for casting members such as molds, these steel materials are aluminum in the portion that comes into contact with the aluminum alloy. It melts with the molten alloy, increases the iron content in the molten aluminum alloy, and lowers the quality of the cast product. Furthermore, the melting damage of these molds and the like causes various inconveniences in operation.

上記の対策としては、深い硬化処理層が得られ、かつ処理の価格も非常に安価であることから、その作業面への窒化処理が多く用いられてきた。しかし、鋳造品の高強度化により、被成形材として高融点アルミニウム合金の使用が増大してきたことから、窒化処理では、高温において処理層中のNがアルミニウム溶湯中に容易に拡散してしまうため、処理層の消滅による、耐溶損性の低下が生じ、急速に溶損現象が進む。   As the above countermeasure, since a deep hardened layer is obtained and the cost of the treatment is very low, nitriding treatment on the work surface has been often used. However, due to the increased strength of cast products, the use of high-melting-point aluminum alloys has increased as a material to be molded. Therefore, in nitriding, N in the treated layer easily diffuses into the molten aluminum at high temperatures. As a result of the disappearance of the treatment layer, the resistance to melt damage is reduced, and the melt damage phenomenon proceeds rapidly.

上記問題点を解決するために、溶融金属と反応し難いセラミックスを物理蒸着法(以下PVD法とも記す)により作業面に被覆した金型の適用が増加している。例えば、金型母材に浸炭もしくは窒化処理を施した後、PVD法にてTiC、TiNといった被覆層を適用する手法(特許文献1)、金型表面にTi中間層を被覆し、次いでTiAlNを被覆する手法(特許文献2)が提案されている。また、被覆層にCrNを適用する手法も提案されている(特許文献3,4)。
特開昭61−033734号公報 特開平07−112266号公報 特開平10−137915号公報 特開2001−11599号公報
In order to solve the above problems, there is an increasing use of a mold in which a work surface is coated with a ceramic that is difficult to react with a molten metal by a physical vapor deposition method (hereinafter also referred to as a PVD method). For example, after carburizing or nitriding the mold base material, a method of applying a coating layer such as TiC or TiN by the PVD method (Patent Document 1), coating the Ti intermediate layer on the mold surface, then TiAlN A coating method (Patent Document 2) has been proposed. A method of applying CrN to the coating layer has also been proposed (Patent Documents 3 and 4).
JP 61-033734 A JP 07-112266 A Japanese Patent Laid-Open No. 10-137915 JP 2001-11599 A

近年の鋳造サイクルの高速化により、アルミニウム合金の溶湯温度は比較的高温の状態で鋳造されるため、鋳造用金型といった接溶湯部材の使用環境はいっそう苛酷になっている。つまり、鋳造時の溶融金属による金型やその他部材の熱膨張と、被加工材凝固後の離型剤塗布による収縮、または被加工材の凝固収縮による金型、部材のたわみが顕著に発生するようになってきた。その結果、特許文献1〜4に提案されている組成の被覆層では、使用中に被覆層の剥離が発生し、この剥離部を経路として溶融金属が部材内部に浸透、表面処理層直下の母材中の鉄と反応して合金を形成する。そして、表面被覆層直下が、この合金形成により膨張すると、処理層が一気に剥離してしまい、溶損が急速に進む現象が認められた。   Due to the recent increase in the speed of the casting cycle, the molten metal temperature of the aluminum alloy is cast at a relatively high temperature, so that the use environment of the molten metal member such as a casting mold becomes more severe. In other words, the thermal expansion of molds and other members due to molten metal during casting, and shrinkage due to the application of a release agent after solidification of the work material, or deflection of the mold and members due to solidification shrinkage of the work material occurs significantly. It has become like this. As a result, in the coating layer having the composition proposed in Patent Documents 1 to 4, peeling of the coating layer occurred during use, and the molten metal penetrated into the member through this peeling portion as a route, and the mother layer just below the surface treatment layer. Reacts with iron in the material to form an alloy. And when the surface coating layer directly expanded due to the formation of this alloy, the treatment layer was peeled off at once, and a phenomenon in which the melting loss rapidly progressed was observed.

また、軽量化が要求されるハードディスク、パーソナルコンピュータ、携帯電話等の筐体には、近年、アルミニウム合金やマグネシウム合金のダイカスト製品が適用されるようになり、鋳造製品の薄肉化されている。鋳造製品の薄肉化を達成するためには、金型内への溶湯射出速度を早くする必要があり、上記提案の被覆層では、溶湯による摩耗に対し、十分な耐摩耗性を有していない。つまり、金型で説明すれば、湯口付近の溶湯が高速で進入する部位において、流体による摩耗が発生してしまうため、金型修正サイクル、金型寿命の低下、鋳造品の形状不良を招くこととなる。   In recent years, die casting products made of aluminum alloy or magnesium alloy have been applied to housings such as hard disks, personal computers, and mobile phones that are required to be lighter, and cast products have been made thinner. In order to reduce the thickness of the cast product, it is necessary to increase the injection speed of the molten metal into the mold, and the proposed coating layer does not have sufficient wear resistance against wear due to the molten metal. . In other words, if explained with a mold, wear due to fluid occurs at a site where the molten metal near the gate enters at a high speed, resulting in a mold correction cycle, a decrease in mold life, and a defective shape of the cast product. It becomes.

本発明は、ダイカスト金型や鋳抜きピンといった、その作業面が高温の溶融金属に接して使用される鋳造用部材において、上記の問題を解消した鋳造用部材を提供することを目的とする。   An object of the present invention is to provide a casting member that solves the above-mentioned problems in a casting member such as a die-casting die or a casting pin that is used in contact with a high-temperature molten metal.

本発明者らは、上記の用途であるような鋳造用部材における、不具合の発生機構に着目し、上記部材の作業面(接溶湯面)に適用する被覆層の耐溶損性、耐摩耗性に及ぼす被覆層の組成、層構造ならびに成膜条件の影響について詳細な検討を行った。   The present inventors pay attention to the failure occurrence mechanism in the casting member that is the above-mentioned use, and in the melting resistance and wear resistance of the coating layer applied to the working surface (welded surface of the molten metal) of the member. The effects of the composition of the coating layer, the layer structure, and the film formation conditions were examined in detail.

その結果、母材表面から被加工材に接する作業面にかけて役割を担う被覆層を、その硬さ分布によって分類のされる複合層とし、更にはそれら層間の厚さ関係をも調整することで、鋳造用部材として極めて良好な耐溶損性、耐摩耗性が得られることを見いだした。この結果により、例えばアルミニウム合金のダイカスト鋳抜きピンにおいては、鋳造品の凝固収縮時に発生するピンのたわみによる被覆層の剥離による溶損や、高速の溶湯が衝突した場合の摩耗が十分に抑制され、鋳造用部材として著しく寿命が向上するということを確認した。   As a result, the coating layer that plays a role from the base material surface to the work surface in contact with the workpiece is a composite layer classified by its hardness distribution, and further by adjusting the thickness relationship between those layers, As a casting member, it has been found that extremely good resistance to melting and abrasion can be obtained. As a result, for example, in an aluminum alloy die-cast die-cast pin, melt damage due to peeling of the coating layer due to deflection of the pin that occurs during solidification shrinkage of the cast product, and wear when a high-speed molten metal collides are sufficiently suppressed. It was confirmed that the service life of the casting member was significantly improved.

すなわち、本発明の第1発明は、金属を母材とする鋳造用部材の、その少なくとも作業面に物理蒸着法による被覆層を有した鋳造用部材であって、該被覆層は、最表層にa層、母材直上にc層、a層とc層の間にb層の少なくとも3層が被覆されており、a層、b層、c層は同金属系化合物であり、硬さ記号HV0.025による各層の硬さが、
2500>(a層の硬さ)>1000、
3500>(b層の硬さ)>2300、
2500>(c層の硬さ)>1000かつ、
(500+a層の硬さ)<(b層の硬さ)、
(500+c層の硬さ)<(b層の硬さ)であり、
層厚にてb層<c層であり、被覆層の層厚の合計が5〜15μmであることを特徴とする鋳造用部材である。
That is, the first invention of the present invention is a casting member having a coating layer formed by physical vapor deposition on at least a work surface of a casting member made of a metal as a base material, and the coating layer is formed on the outermost layer. a layer, c layer directly above the base material, and at least three layers of b layer are coated between the a layer and c layer, and the a layer, b layer, and c layer are the same metal-based compound, and the hardness symbol HV0 The hardness of each layer according to .025
2500> (hardness of layer a)> 1000,
3500> (b layer hardness)> 2300,
2500> (hardness of c layer)> 1000 and
(500 + a layer hardness) <(b layer hardness),
(500 + c layer hardness) <(b layer hardness),
The casting member is characterized in that the layer thickness is b layer <c layer, and the total thickness of the coating layers is 5 to 15 μm.

なお、本発明の上記最表層であるa層ならびに母材直上のc層は、金属元素部分がTiもしくはCrを主体とする窒化物、炭化物、炭窒化物のいずれかからなり、最表層a層と母材直上のc層の間に被覆するb層は、金属元素部分がTi、Crから選んだ1種もしくは2種を主体とする窒化物、炭化物、炭窒化物のいずれかであることが望ましい。または、a層ならびにc層は、金属元素部分がCrを主体とする窒化物、炭化物、炭窒化物のいずれかからなり、b層は、金属元素部分がCrおよびAlを主体とする窒化物、炭化物、炭窒化物のいずれかであることが望ましい。 The a layer which is the outermost layer of the present invention and the c layer immediately above the base material are composed of a nitride, carbide or carbonitride mainly composed of Ti or Cr, and the outermost layer a layer. and b layer covering between the c layer directly preform is either a nitride, carbide, carbonitride of a metal element portion Ti, mainly one or two chosen C r or al It is desirable. Alternatively, the a layer and the c layer are composed of any one of a nitride, carbide, and carbonitride in which the metal element portion is mainly composed of Cr, and the b layer is a nitride in which the metal element portion is mainly composed of Cr and Al, It is desirable to be either carbide or carbonitride.

そして、最表層であるa層の層厚が1〜5μm、b層の層厚は1〜5μm、母材直上であるc層の層厚が2〜7μmであることが望ましい。   It is desirable that the outermost layer a has a layer thickness of 1 to 5 μm, the b layer has a layer thickness of 1 to 5 μm, and the c layer immediately above the base material has a layer thickness of 2 to 7 μm.

更に、被覆層が形成された母材は、その母材最表面から25μmの深さにおける硬さが、母材最表面から500μmの深さにおける硬さに比べ、硬さ記号HV0.2にて100以上高いことが望ましい。   Further, the base material on which the coating layer is formed has a hardness symbol HV0.2 that has a hardness at a depth of 25 μm from the outermost surface of the base material compared to a hardness at a depth of 500 μm from the outermost surface of the base material. It is desirable that it is 100 or more.

従来のTiN、TiCN、CrNが被覆された鋳造用部材は、近年における使用環境の過酷化に対し、十分な寿命が得られなくなってきた。本発明の表面被覆層構造を適用した鋳造用部材を使用することにより、金型の耐溶損性、耐摩耗性の改善が達成できるため、寿命を飛躍的に向上させることが可能である。   Conventional casting members coated with TiN, TiCN, and CrN have been unable to obtain a sufficient life against the severe use environment in recent years. By using the casting member to which the surface coating layer structure of the present invention is applied, it is possible to achieve improvement in the mold resistance and wear resistance of the mold, so that the life can be drastically improved.

鋳造用部材の作業面に被覆される硬質皮膜は、その接する溶湯に対してだけの特性に注視して検討すればよいものではなく、母材との相性も当然に考慮した、トータル的な特性の検討が必要である。よって、本発明での皮膜は、その溶湯に接する最表面にとっての要求特性と、母材に対しての要求特性の両方を、最大限に付与できるための複合被覆層としている。そして、本発明の最表層は、鋳造用部材に耐溶損性、耐摩耗性を付与することが主な役割であり、その存在は極めて重要である。そのため、これらの特性を高い次元でバランスよく有する皮膜であることが必要である。   The hard coating on the working surface of the casting member does not have to be examined only by paying attention to the characteristics only for the molten metal that comes into contact with it. It is necessary to consider this. Therefore, the coating film according to the present invention is a composite coating layer that can impart both the required characteristics for the outermost surface in contact with the molten metal and the required characteristics for the base material to the maximum extent. The outermost layer of the present invention has a main role of imparting melt resistance and wear resistance to the casting member, and its presence is extremely important. Therefore, it is necessary that the film has these characteristics in a high dimension and in a well-balanced manner.

本発明者らの検討結果によると、最表層のa層、母材直上のc層、a層とc層の間に存在するb層といったように、金型作業面には少なくとも3層が、物理蒸着法で被覆されるものである。そして、その3層の境界は、各々が有する硬さ特性によって分類がされるものであって、各層の硬さは硬さ記号HV0.025で、
2500>(a層の硬さ)>1000、
3500>(b層の硬さ)>2300、
2500>(c層の硬さ)>1000かつ、
(500+a層の硬さ)<(b層の硬さ)、
(500+c層の硬さ)<(b層の硬さ)
となる構造にすることが、被覆層の密着性を向上させるために極めて重要であると確認された。なお、硬さ記号HV0.025とは、JIS−Z−2244で指定のされるビッカース硬さ試験方法においての、試験荷重0.2452Nによる硬さ値である。
According to the examination results of the present inventors, at least three layers on the mold work surface, such as the outermost layer a layer, the layer c immediately above the base material, and the layer b existing between the layer a and the layer c, It is coated by physical vapor deposition. And the boundary of the three layers is classified according to the hardness characteristics that each has, and the hardness of each layer is a hardness symbol HV0.025,
2500> (hardness of layer a)> 1000,
3500> (b layer hardness)> 2300,
2500> (hardness of c layer)> 1000 and
(500 + a layer hardness) <(b layer hardness),
(Hardness of 500 + c layer) <(Hardness of b layer)
In order to improve the adhesion of the coating layer, it has been confirmed that it is extremely important to make the structure as follows. The hardness symbol HV0.025 is a hardness value with a test load of 0.2452N in the Vickers hardness test method specified by JIS-Z-2244.

硬質材料は、比較的軟質な物質ほど、鋳造製品である被加工材への攻撃性が低く、熱サイクルや部材のたわみによる被覆層中のクラックも発生し難い。そして、更に物理蒸着法の場合は、被覆物質の密着性も良好となる。そのため、最表層には、ある程度の硬さは必要でありながらも、比較的軟質な物質のa層を適用することは、被加工材への攻撃性が低下、つまり被覆層が被加工材を引掻くことで発生する突発的なカジリが抑制できる。また、クラックの発生しづらい軟質の物質で被覆層を覆ってしまう構造となるため、クラックを起点とした剥離や溶損が抑えられ、結果として被覆層全体の密着性も向上することとなる。このとき、同様にある程度の硬さは必要でありながらも、母材直上のc層へも軟質な物質を適用する理由は、母材である金型材と被覆層の本質的な密着性を向上させるためである。   As the hard material is a relatively soft substance, the aggressiveness to the work piece that is a cast product is lower, and cracks in the coating layer due to thermal cycle and bending of the member are less likely to occur. Further, in the case of physical vapor deposition, the adhesion of the coating material is also improved. Therefore, although a certain degree of hardness is required for the outermost layer, applying a layer of a relatively soft substance reduces the aggression on the workpiece, that is, the covering layer reduces the workpiece. Sudden galling caused by scratching can be suppressed. In addition, since the coating layer is covered with a soft material that does not easily generate cracks, peeling and melting damage starting from the cracks can be suppressed, and as a result, the adhesion of the entire coating layer can be improved. At this time, although a certain degree of hardness is required, the reason for applying a soft substance to the c layer immediately above the base material is to improve the essential adhesion between the base mold material and the coating layer. This is to make it happen.

一方、b層は、硬さ2300HV0.025を越える比較的硬質な物質であり、耐摩耗性を向上させることを目的とし被覆されるが、上述の軟質物質とは逆に、高硬度な物質ほど密着性に劣る。このとき、b層を、軟質なa層とc層で挟み込むことで、b層は容易に剥離しなくなることが認められ、更に鋳造用部材の溶湯による摩耗が激しい部位においては、最表層のa層が優先的に摩耗するが、その下から硬質のb層が出現するため、必要な部位において被覆層が耐摩耗性を向上させる機能を発揮すると確認された。   On the other hand, the b layer is a relatively hard substance having a hardness exceeding 2300HV0.025 and is coated for the purpose of improving the wear resistance. Poor adhesion. At this time, it is recognized that the b layer is not easily peeled by sandwiching the b layer between the soft a layer and the c layer. Further, in a portion where the wear due to the molten metal of the casting member is severe, the outermost layer a The layer wears preferentially, but since a hard b layer appears from below, it was confirmed that the coating layer exhibited a function of improving the wear resistance at a necessary site.

各層の厚みに関しては、硬質なb層をc層より厚くすると、上記のような硬さの関係であっても、各層が持つ特性のバランスが崩れ、b層の密着性が低下する。そのため、b層とc層の層厚は、b層<c層の関係である。また、被覆層全体の膜厚は、5μm未満であると、鋳造用部材として十分な耐溶損性が得られなくなり、また15μmを越えて被覆すると密着性が極端に低下するため、被覆層の層厚は合計が5〜15μmとする。更には7〜12μmとすることが良い。   Regarding the thickness of each layer, if the hard b layer is made thicker than the c layer, the balance of the characteristics of each layer is lost and the adhesion of the b layer is deteriorated even in the above-described hardness relationship. Therefore, the layer thickness of the b layer and the c layer has a relationship of b layer <c layer. Also, if the film thickness of the entire coating layer is less than 5 μm, sufficient melt resistance cannot be obtained as a casting member, and if the coating layer exceeds 15 μm, the adhesiveness is extremely reduced. The total thickness is 5 to 15 μm. Furthermore, it is good to set it as 7-12 micrometers.

本発明の鋳造用部材の被覆方法については、物理蒸着法を規定している。これは、硬質材料を被覆する母材への熱影響、金型に発生する熱歪みや変形等を抑制する目的であり、例えば母材である熱間ダイス鋼や高速度鋼等の焼戻し温度以下で成膜でき、皮膜に圧縮応力を残留させることができるためである。物理蒸着法の種類については特に限定を設けないが、アークイオンプレーティング法もしくはスパッタリング法といった、被覆母材側にBias電圧を印可する物理蒸着法であることが望ましい。   The physical vapor deposition method is prescribed | regulated about the coating method of the member for casting of this invention. This is for the purpose of suppressing the thermal effect on the base material that coats the hard material, thermal distortion and deformation generated in the mold, for example, below the tempering temperature of the hot die steel or high-speed steel that is the base material. This is because the film can be formed and the compressive stress can remain in the film. Although there is no particular limitation on the type of physical vapor deposition method, it is desirable to be a physical vapor deposition method such as an arc ion plating method or a sputtering method in which a Bias voltage is applied to the coating base material side.

母材の金属材質については、特段に定めるものではなく、例えば上記の通りの、熱間ダイス鋼、高速度鋼および超硬合金が使用できる。これについては、JIS等による規格金属種(鋼種)を含め、従来金型への使用が可能な鋼種として提案のされてきた改良金属種も適用できる。   The metal material of the base material is not particularly defined, and for example, hot die steel, high speed steel and cemented carbide as described above can be used. In this regard, improved metal types that have been proposed as steel types that can be used in conventional molds, including standard metal types (steel types) according to JIS and the like, can also be applied.

本発明の鋳造用部材の作業面においては、その形成した被覆層の最表層であるa層ならびに母材直上のc層は、b層との硬さならびに層厚の関係を満足していれば良い。しかしながら、a層ならびにc層は、鋳造用部材の用途に応じて、その金属元素部分がTiもしくはCrを主体とする窒化物、炭化物、炭窒化物のいずれかであることが望ましい。なお、その主体とすることについては、窒素・炭素を除いた、金属(半金属を含む)組成部のみの割合で、TiもしくはCrが70(原子%)以上、更には90(原子%)以上とすることが良い(実質100(原子%)を含む)。 In the working surface of the casting member of the present invention, the a layer which is the outermost layer of the formed coating layer and the c layer immediately above the base material satisfy the relationship between the hardness and the layer thickness with the b layer. good. However, it is desirable that the a layer and the c layer are any of nitride, carbide, and carbonitride whose metal element portion is mainly Ti or Cr depending on the use of the casting member. In addition, regarding the main component, Ti or Cr is 70 (atomic%) or more, and further 90 (atomic%) or more in the ratio of only the metal (including semimetal) composition part excluding nitrogen and carbon. (Essentially 100 (atomic%) included).

また、本発明の鋳造用部材の作業面において、a層とc層の間に被覆される、b層は、その金属元素部分がTi、Cr、Alから選んだ1種もしくは2種以上、より限定的には、Ti、Crから選んだ1種もしくは2種を主体とする窒化物、炭化物、炭窒化物のいずれかであることが望ましい。なお、その主体とすることについては、上記のa,c層に同様であり、70(原子%)以上、更には90(原子%)以上とすることが良い(実質100(原子%)を含む)。そして、このとき、a層ならびにc層との硬さの関係を満足するために、例えばa層およびc層がTiNである場合は、TiNに比べ硬質であるTiAlN系の硬質材料をb層に選択し、各層の硬さの関係を満足するTiとAlの成分比もしくは成膜条件を用いて被覆するか、TiCやTiCNといったTiNに比べ硬質の炭化物もしくは炭窒化物を同じく各層の硬さの関係を満足する成膜条件で被覆する必要がある。 Further, in the working plane of the casting member of the present invention is coated between a layer and the layer c, b layer, the metal element portion Ti, Cr, 1 kind or 2 or more species selected from Al, more In a limited manner, it is desirable to use any one of nitride, carbide, and carbonitride mainly composed of one or two selected from Ti and Cr . In addition, about making it the main body, it is the same as that of said a and c layer, It is good to set it as 70 (atomic%) or more, Furthermore, it is good to set it as 90 (atomic%) or more (substantially 100 (atomic%) is included. ). At this time, in order to satisfy the hardness relationship with the a layer and the c layer, for example, when the a layer and the c layer are TiN, a TiAlN-based hard material that is harder than TiN is used as the b layer. Select and coat using the component ratio of Ti and Al that satisfies the hardness relationship of each layer or film forming conditions, or hard carbide or carbonitride compared to TiN such as TiC and TiCN of the hardness of each layer It is necessary to coat under film forming conditions that satisfy the relationship.

なお、本発明のa層、b層、c層は、それぞれの層が同金属系化合物であることが、各層間の密着性の面で、更に望ましく、これに限定する。例えばCr系窒化物の場合は、a層がCrN、b層がCrAlN、c層がCrNのような構成が望ましい。すなわち、a層ならびにc層は、金属元素部分がCrを主体とする窒化物、炭化物、炭窒化物のいずれかからなり、b層は、金属元素部分がCrおよびAlを主体とする窒化物、炭化物、炭窒化物のいずれかであることが望ましい。 In the present invention, the a layer, the b layer, and the c layer are more preferably, in terms of adhesion between the respective layers, and are limited to this. For example, in the case of Cr-based nitride, it is desirable that the a layer is CrN, the b layer is CrAlN, and the c layer is CrN. That is, the a layer and the c layer are composed of any one of a nitride, carbide, and carbonitride whose metal element portion is mainly Cr, and the b layer is a nitride whose metal element portion is mainly Cr and Al. It is desirable to be either carbide or carbonitride.

上記は一例として挙げたが、a層およびc層のそれぞれは、その金属元素部分がTiもしくはCrを主体とするも、必要に応じてIVa、Va、VIa属ならびにAl,Si、B等の、他の金属(半金属)元素を、b層においても、その金属元素部分がTi、Cr、Alから選んだ1種もしくは2種以上を主体とするも、必要に応じてIVa、Va、VIa属ならびにSi、B等の、他の金属(半金属)元素を、各層において10原子%以下微量添加してもよい。   Although the above is given as an example, each of the a layer and the c layer is mainly composed of Ti or Cr in the metal element portion, but if necessary, such as IVa, Va, VIa group and Al, Si, B, Other metal (semi-metal) elements, even in the b layer, the metal element part is mainly composed of one or more selected from Ti, Cr, Al, but if necessary, IVa, Va, VIa group Further, other metal (metalloid) elements such as Si and B may be added in a small amount of 10 atomic% or less in each layer.

次に、本発明の被覆層を構成する、それぞれの層の厚さについて述べる。本発明の最表層であるa層は、その層厚が1〜5μmであることが望ましい。層厚が1μm未満であると、耐溶損性が十分でなく早期に滅失してしまい、a層の役割の1つである初期の突発的なカジリを抑制する効果が得られない場合がある。逆に5μmを越えて被覆すると、使用条件によっては、早期に剥離してしまう場合がある。よって、本発明の作業面にある被覆層のうちの、最表層であるa層の層厚は、1〜5μmであることが望ましい。   Next, the thickness of each layer constituting the coating layer of the present invention will be described. The layer a which is the outermost layer of the present invention preferably has a layer thickness of 1 to 5 μm. When the layer thickness is less than 1 μm, the melt resistance is not sufficient and the layer is lost at an early stage, and the effect of suppressing the initial sudden galling, which is one of the roles of the a layer, may not be obtained. On the contrary, if the coating exceeds 5 μm, it may be peeled off early depending on the use conditions. Therefore, the layer thickness of the a layer that is the outermost layer among the coating layers on the work surface of the present invention is preferably 1 to 5 μm.

また、最表層であるa層と母材直上層c層の間に被覆されるb層は、層厚が1〜5μmであることが望ましい。層厚が1μm未満であると、b層の被覆の目的である耐摩耗性が十分でないことがあり、逆に5μmを越えて被覆すると密着性が乏しくなり、早期に剥離する場合がある。よって、本発明のb層は、層厚が1〜5μmであることが望ましい。   Moreover, it is desirable that the b layer coated between the outermost layer a and the layer c immediately above the base material has a layer thickness of 1 to 5 μm. If the layer thickness is less than 1 μm, the abrasion resistance, which is the purpose of coating the b layer, may not be sufficient. Conversely, if the layer thickness exceeds 5 μm, the adhesion may be poor and peeling may occur early. Therefore, the layer b of the present invention desirably has a layer thickness of 1 to 5 μm.

そして、本発明の母材直上層であるc層は、その層厚が2〜7μmであることが望ましい。使用条件によっては、層厚が2μm未満であると、薄すぎるため母材との密着性が十分に得られ難い。逆に、7μmを越えて被覆すると、その密着性を向上させる効果は変わらないばかりか、使用条件によっては、早期に剥離してしまう場合がある。よって、本発明の母材直上層であるc層の層厚は、2〜7μmであることが望ましい。   And as for c layer which is the base material layer of this invention, it is desirable that the layer thickness is 2-7 micrometers. Depending on the use conditions, if the layer thickness is less than 2 μm, it is difficult to obtain sufficient adhesion with the base material because it is too thin. On the other hand, when the coating exceeds 7 μm, the effect of improving the adhesion is not changed, and depending on the use conditions, it may be peeled off early. Therefore, the layer thickness of the c layer, which is the layer immediately above the base material of the present invention, is desirably 2 to 7 μm.

更に本発明の鋳造用部材は、より耐溶損性、耐摩耗性の向上を目的にして、被覆層が形成された母材は、その最表面から25μmの深さにおける硬さが、該最表面から500μmの深さにおける硬さに比べ、JIS−Z−2244に定義されるビッカース硬さで100HV0.2以上高いことが望ましい。硬さ記号HV0.2とは、ビッカース硬さ試験方法においての、試験荷重1.961Nによる硬さ値である。具体例としては、窒化処理、浸炭処理等と言った拡散を利用した表面硬化処理を予め適用することが望ましい。この時、窒化処理で形成される白層と呼ばれる窒化物層や、浸炭で認められる炭化物層と言った化合物層は、母材直上のc層の密着性を低下させる原因となるため、処理条件の制御により形成させないようにするか、あるいは研磨等により除去することが望ましい。   Further, the casting member of the present invention has a hardness at a depth of 25 μm from the outermost surface of the base material on which the coating layer is formed for the purpose of further improving the resistance to melting and abrasion. It is desirable that the Vickers hardness defined by JIS-Z-2244 is 100HV0.2 or more higher than the hardness at a depth of 500 μm to 500 μm. The hardness symbol HV0.2 is a hardness value with a test load of 1.961N in the Vickers hardness test method. As a specific example, it is desirable to apply in advance a surface hardening process using diffusion such as nitriding or carburizing. At this time, a nitride layer called a white layer formed by nitriding treatment and a compound layer called a carbide layer recognized by carburizing cause a decrease in the adhesion of the c layer directly above the base material. It is desirable not to form the film by controlling the thickness or to remove it by polishing or the like.

次に実施例に基づき詳細に説明するが、本発明は下記実施例によって限定を受けるものではなく、本発明の要旨を逸脱しない範囲で任意に変更が可能であり、それらはいずれも本発明の技術的範囲に含まれる。   Next, the present invention will be described in detail based on examples. However, the present invention is not limited by the following examples, and can be arbitrarily changed without departing from the gist of the present invention. Included in the technical scope.

(実施例1)
JISに規定される熱間ダイス鋼SKD61を用意し、1030℃より油焼入れ後、550〜630℃での焼戻しにより47HRCに調質した。その後、耐溶損性評価用に直径10mm、長さ100mmの円柱状テストピース、密着性の評価用に厚み3mm、一辺が30mmの板状テストピースの加工を行った。そして、これらのテストピースを母材として、被覆処理を行った。なお被覆処理の前には、全テストピースに対し、表面硬化処理として次に示す条件にてイオン窒化処理を施した。
Example 1
Hot die steel SKD61 prescribed by JIS was prepared, oil-quenched from 1030 ° C, and tempered to 47HRC by tempering at 550-630 ° C. Thereafter, a cylindrical test piece having a diameter of 10 mm and a length of 100 mm was evaluated for the evaluation of the melt resistance, and a plate-shaped test piece having a thickness of 3 mm and a side of 30 mm was evaluated for the evaluation of adhesion. Then, a coating treatment was performed using these test pieces as a base material. Before the coating treatment, ion nitriding treatment was performed on all test pieces under the following conditions as surface hardening treatment.

被覆処理前の、表面硬化処理は、流量比5%N(残H)雰囲気中で、500℃、10時間保持の条件でイオン窒化処理を施した後、それぞれの試験面を研磨によって仕上げた。なお、仕上げ後の表面より25μmの深さにおける硬さは、この窒化処理を施した全テストピースにて680HV0.2であったことから、その500μmの深さにおける硬さ47HRC(=471HV0.2)より100HV0.2以上に硬化されていることを確認済みである。そして、仕上げ後の母材表面に対し、下記の条件の被覆処理を行った。 The surface hardening treatment before the coating treatment is performed by ion nitriding treatment at 500 ° C. for 10 hours in an atmosphere with a flow rate ratio of 5% N 2 (remaining H 2 ), and then finishing each test surface by polishing. It was. Since the hardness at a depth of 25 μm from the finished surface was 680 HV0.2 in all the test pieces subjected to this nitriding treatment, the hardness at a depth of 500 μm was 47 HRC (= 471 HV0.2 ) Has been confirmed to be cured to 100HV0.2 or higher. And the coating process of the following conditions was performed with respect to the base material surface after finishing.

被覆方法は、アークイオンプレーティング装置を用い、まずは圧力0.5PaのAr雰囲気中で、母材に−400VのBias電圧を印可し、60分の熱フィラメントによるプラズマクリーニングを行った。そして、この後、金属成分の蒸発源である各種金属製ターゲットならびに反応ガスとしてNガスをベースに、必要に応じCHガスを用い、母材温度500℃、反応ガス圧力3.0Pa、−50VのBias電圧にて成膜を行った。 As a coating method, an arc ion plating apparatus was used. First, a bias voltage of −400 V was applied to the base material in an Ar atmosphere at a pressure of 0.5 Pa, and plasma cleaning with a hot filament for 60 minutes was performed. After that, various metal targets that are evaporation sources of the metal components and N 2 gas as a reaction gas, using CH 4 gas as necessary, a base material temperature of 500 ° C., a reaction gas pressure of 3.0 Pa, − Film formation was performed at a Bias voltage of 50V.

得られたテストピースについて、その被覆面の各層に関する層厚の測定ならびに硬さ試験、ロックウェル硬さ試験を応用した密着性評価試験、耐溶損性評価を実施した。各評価試験方法を以下に示す。   The obtained test piece was subjected to the measurement of the layer thickness for each layer of the coated surface, the hardness test, the adhesion evaluation test applying the Rockwell hardness test, and the melt resistance evaluation. Each evaluation test method is shown below.

(1)層厚の測定
被覆層の断面が出る様、厚み方向にテストピースを切断後、樹脂に埋め込み組織観察用に研磨を実施し、光学顕微鏡(倍率1000倍)にて各層の層厚を測定した。
(1) Measurement of layer thickness After cutting the test piece in the thickness direction so that the cross section of the coating layer appears, the sample is embedded in a resin and polished for structure observation, and the thickness of each layer is measured with an optical microscope (1000 times magnification). It was measured.

(2)硬さ試験
層厚を測定したテストピースと同じものを使用し、マイクロビッカース試験機(ミツトヨ製HM−115)にて各層断面の硬さを測定した。
(2) Hardness test The same test piece as the layer thickness was used, and the hardness of each layer cross section was measured with a micro Vickers tester (HM-115 manufactured by Mitutoyo Corporation).

(3)密着性評価試験
ロックウェル硬さ試験機(ミツトヨ製AR−10)にて被覆面(30mm×30mm)にCスケールで圧痕をつけ、その部分を光学顕微鏡にて観察し、図1に示す基準で圧痕の周囲に発生する剥離を評価した。
(3) Adhesion evaluation test Indentation was made on the coated surface (30 mm × 30 mm) with a C scale with a Rockwell hardness tester (Mitutoyo AR-10), and the portion was observed with an optical microscope. The peeling that occurs around the indentation was evaluated according to the criteria shown.

(4)耐溶融金属溶損試験
アルミニウム合金AC4Cの750℃の溶湯中に試験片を、毎分90回のサイクルで、振幅30mmの上下運動にて3時間の試験を実施し、試験片の試験前後の質量比でその耐溶損性を比較した。
(4) Melt resistance test for molten metal The test piece was tested in a molten metal of 750 ° C. of aluminum alloy AC4C for 90 hours per minute with a vertical motion of 30 mm amplitude for 3 hours. The melt resistance was compared with the mass ratio before and after.

表1に本発明例および比較例に関する被覆層の詳細(金属(半金属)組成部に付されている下付き係数は原子比)と、各種評価の結果を示す。なお、従来例においては、本発明の被覆層の構成を満たさないことから、その成膜された最表層、母材直上層、中間層の定義がし難いため表2に示す。
Table 1 shows the details of the coating layers relating to the inventive examples and comparative examples (subscript coefficients attached to the metal (semi-metal) composition part are atomic ratios) and the results of various evaluations. In the conventional example, since the configuration of the coating layer of the present invention is not satisfied, it is difficult to define the formed outermost layer, the layer immediately above the base material, and the intermediate layer.

表1に示す通り、本発明例は被覆層の構成が本発明の規定範囲を満足しているため、層厚が厚いにも係わらず、いずれも密着性が著しく優れていることがわかる。図2,3はそれぞれ、本発明例No.3およびNo.4の密着性評価試験結果(ロックウェル圧痕周辺の状態)を示した顕微鏡写真である。他の本発明例に比べて、その有する被覆層が厚い本発明例No.4であっても、十分に優れた密着性を達成している。また、密着性が良好であるため、耐溶損性についても、いずれも優れていることがわかる。   As shown in Table 1, the examples of the present invention satisfy the prescribed range of the present invention, so that the adhesion is remarkably excellent regardless of the thickness of the layer. 2 and 3 are examples of the present invention. 3 and no. 4 is a photomicrograph showing the adhesion evaluation test result of 4 (state around the Rockwell indentation). Compared to other examples of the present invention, the present invention example No. Even if it is 4, sufficiently excellent adhesion is achieved. Moreover, since adhesiveness is favorable, it turns out that all are excellent also about melt-resistance.

一方、比較例ならびに従来例の評価結果については、比較例No.11は、各層の硬さに関しては本発明を満足するが、b層ならびにc層が厚すぎるため、密着性、耐溶損性が著しく劣る。比較例No.12、15については、各層の硬さの関係が本発明を満足しておらず、母材直上および最表層に比較的硬質な層を被覆したことで、硬さのバランスが崩れてしまい密着性、耐溶損性に劣る結果となった。比較例No.13、14は、他の比較例に比べると密着性は良好であるが、c層の層厚がb層よりも薄いため、密着性は本発明例より劣る結果となった。図4に、比較例No.13の密着性評価試験結果(ロックウェル圧痕周辺の状態)の顕微鏡写真を示しておく。   On the other hand, for the evaluation results of the comparative example and the conventional example, comparative example No. No. 11 satisfies the present invention with respect to the hardness of each layer, but the b layer and the c layer are too thick, so that the adhesion and the erosion resistance are extremely poor. Comparative Example No. For Nos. 12 and 15, the hardness relationship of each layer does not satisfy the present invention, and the hardness balance is lost due to the coating of a relatively hard layer directly on the base material and the outermost layer. As a result, the melt resistance was poor. Comparative Example No. Although the adhesiveness of 13 and 14 was favorable compared with the other comparative examples, since the layer thickness of c layer was thinner than b layer, the adhesiveness was inferior to the example of this invention. In FIG. 13 shows a micrograph of the adhesion evaluation test result 13 (state around the Rockwell indentation).

また、基本的な被覆構造からして異なる従来例No.21、23は、本発明のような層厚が比較的厚い領域では密着性が著しく劣る。図5は、従来例No.23の密着性評価試験結果(ロックウェル圧痕周辺の状態)を示した顕微鏡写真である。比較的軟質なCrNを被覆した従来例No.22は層厚が厚くとも密着性に優れるが、硬さが著しく低いため、金型へ適用した場合は、早期の摩耗が予想される。   Further, the conventional example No. different from the basic covering structure. Nos. 21 and 23 are remarkably inferior in adhesion in a region where the layer thickness is relatively thick as in the present invention. FIG. It is the microscope picture which showed the adhesive evaluation test result of 23 (state around Rockwell impression). Conventional example No. coated with relatively soft CrN No. 22 is excellent in adhesion even when the layer thickness is thick, but since the hardness is extremely low, early wear is expected when applied to a mold.

(実施例2)
次に、表1中の本発明例No.4、No.5、表2中の従来例No.22と同等の表面被覆層構成であるダイカスト鋳抜きピンを作製して、実金型における寿命で評価を行った。
(Example 2)
Next, the invention example No. 1 in Table 1 was used. 4, no. 5, conventional example No. 2 in Table 2. A die-cast core pin having a surface coating layer configuration equivalent to that of No. 22 was produced and evaluated based on the life of the actual mold.

まず、表3に示す化学組成の高速度鋼ベースの靭性改良材を、焼鈍状態にて鋳抜きピン近似形状に粗加工し、1080℃の油焼入れを行い、600℃の焼戻しにより55HRCに調質した。その後、仕上げ加工を行い、それぞれ(実施例1)と同様の条件で被覆処理を行なった。なお、被覆処理の前には、表面硬化処理を行なわなかった、これらの鋳抜きピンは、その母材最表面から25μmの深さおよび500μmの深さにおける硬さは、被覆処理の前後に亘り、共に上記の調質硬さ55HRC(=595HV0.2)を維持していた。   First, a high-speed steel-based toughness improving material having the chemical composition shown in Table 3 is roughly processed into an approximate shape of a cast pin in an annealed state, subjected to oil quenching at 1080 ° C., and tempered to 55 HRC by tempering at 600 ° C. did. Thereafter, finishing was performed, and coating treatment was performed under the same conditions as in (Example 1). In addition, these cast pins that were not subjected to surface hardening treatment before the coating treatment had a hardness at a depth of 25 μm and a depth of 500 μm from the outermost surface of the base material before and after the coating treatment. Both maintained the above-mentioned tempered hardness 55HRC (= 595HV0.2).

上記にて作製された鋳抜きピンは、図6に示す形状である。そして、300tのダイカストマシンにて、溶湯温度700℃のアルミニウム合金AC4Cを用い鋳造を行った。表4に各鋳抜きピンの寿命を示す。   The core pin produced above has the shape shown in FIG. Then, casting was performed using a 300-ton die casting machine using an aluminum alloy AC4C having a molten metal temperature of 700 ° C. Table 4 shows the life of each core pin.

本発明を適用した鋳抜きピンは、従来例適用のピンに比べ、金型寿命は2倍以上に向上した。最終的に本発明適用のピンは、焼付きが発生し寿命となったが、従来例適用のピンは、先端部で摩耗が発生した後、最終的には折損によって寿命となった。以上のように、本発明をダイカスト用鋳抜きピンに適用することで、ピンの寿命は飛躍的に向上することが確認された。   The cast pin to which the present invention is applied has improved the mold life by more than twice as compared with the conventional pin. Finally, the pin applied to the present invention had a lifetime due to seizure, but the pin applied to the conventional example eventually had a lifetime due to breakage after wear at the tip. As described above, it has been confirmed that the life of the pin is dramatically improved by applying the present invention to a die-cast core pin.

本発明は、ダイカストおよび鋳造に使用される金型もしくは鋳抜きピンや、ダイカストの射出機に使用されるピストンリング等の、溶融金属に接して使用される鋳造用部材について述べたものであるが、その溶融金属(鋳造材料)は、アルミニウムならびにアルミニウム合金に限らず、マグネシウム合金の鋳造にも適用が可能である。また、本発明の鋳造用部材は、冷間ならびに温熱間における鍛造およびプレス加工といった金属の塑性加工に使用され、耐摩耗性が必要とされる硬質材料被覆塑性加工用金型としても、転用が可能である。   The present invention describes a casting member used in contact with molten metal, such as a die or a die pin used for die casting and casting, or a piston ring used for an injection machine for die casting. The molten metal (casting material) is not limited to aluminum and aluminum alloys, but can be applied to casting of magnesium alloys. Further, the casting member of the present invention is used for metal plastic processing such as forging and pressing in cold and warm conditions, and can be diverted as a hard material-covered plastic processing die that requires wear resistance. Is possible.

実施例で用いた、ロックウェル硬さ試験機を応用した密着性評価試験の、剥離発生状況の評価基準を示す図である。It is a figure which shows the evaluation criteria of the peeling generation | occurrence | production situation of the adhesiveness evaluation test which applied the Rockwell hardness tester used in the Example. 本発明例No.3の密着性評価試験結果(ロックウェル圧痕周辺の状態)を示した顕微鏡写真である。Invention Example No. 3 is a photomicrograph showing the result of 3 adhesion evaluation test (state around the Rockwell indentation). 本発明例No.4の密着性評価試験結果(ロックウェル圧痕周辺の状態)を示した顕微鏡写真である。Invention Example No. 4 is a photomicrograph showing the adhesion evaluation test result of 4 (state around the Rockwell indentation). 比較例No.13の密着性評価試験結果(ロックウェル圧痕周辺の状態)を示した顕微鏡写真である。Comparative Example No. It is the microscope picture which showed the adhesive evaluation test result of 13 (state around Rockwell impression). 従来例No.23の密着性評価試験結果(ロックウェル圧痕周辺の状態)を示した顕微鏡写真である。Conventional Example No. It is the microscope picture which showed the adhesive evaluation test result of 23 (state around Rockwell impression). (実施例2)で使用した鋳抜きピンの形状を示す図である。It is a figure which shows the shape of the core pin used in (Example 2).

Claims (5)

金属を母材とする鋳造用部材の、その少なくとも作業面に物理蒸着法による被覆層を有した鋳造用部材であって、該被覆層は、最表層にa層、母材直上にc層、a層とc層の間にb層の少なくとも3層が被覆されており、a層、b層、c層は同金属系化合物であり、硬さ記号HV0.025による各層の硬さが、
2500>(a層の硬さ)>1000、
3500>(b層の硬さ)>2300、
2500>(c層の硬さ)>1000かつ、
(500+a層の硬さ)<(b層の硬さ)、
(500+c層の硬さ)<(b層の硬さ)であり、
層厚にてb層<c層であり、被覆層の層厚の合計が5〜15μmであることを特徴とする鋳造用部材。
A casting member having a metal as a base material, a casting member having a coating layer formed by physical vapor deposition on at least a work surface, the coating layer having an a layer as an outermost layer, a c layer directly above the base material, At least 3 layers of b layer are coat | covered between a layer and c layer, a layer, b layer, and c layer are the same metal type compounds, and the hardness of each layer by hardness symbol HV0.025,
2500> (hardness of layer a)> 1000,
3500> (b layer hardness)> 2300,
2500> (hardness of c layer)> 1000 and
(500 + a layer hardness) <(b layer hardness),
(500 + c layer hardness) <(b layer hardness),
A casting member, wherein the layer thickness is b layer <c layer, and the total thickness of the coating layers is 5 to 15 μm.
該a層ならびに該c層は、金属元素部分がTiもしくはCrを主体とする窒化物、炭化物、炭窒化物のいずれかとし、該b層は、金属元素部分がTi、Crから選んだ1種もしくは2種を主体とする窒化物、炭化物、炭窒化物のいずれかであることを特徴とする請求項1に記載の鋳造用部材。 The a layer and the c layer, nitride metal element portion is composed mainly of Ti or Cr, carbides, either as carbonitride, the b layer is selected metallic element portion Ti, C r or al 2. The casting member according to claim 1, wherein the casting member is any one of nitride, carbide, and carbonitride mainly composed of one or two kinds . 該a層ならびに該c層は、金属元素部分がCrを主体とする窒化物、炭化物、炭窒化物のいずれかとし、該b層は、金属元素部分がCrおよびAlを主体とする窒化物、炭化物、炭窒化物のいずれかであることを特徴とする請求項1に記載の鋳造用部材。The a layer and the c layer are any one of a nitride, carbide, and carbonitride in which the metal element portion is mainly Cr, and the b layer is a nitride in which the metal element portion is mainly Cr and Al, The casting member according to claim 1, wherein the casting member is one of carbide and carbonitride. 該a層の層厚が1〜5μm、該b層の層厚が1〜5μm、該c層の層厚が2〜7μmであることを特徴とする請求項1ないし3のいずれかに記載の鋳造用部材。 Thickness of the layer a is 1 to 5 [mu] m, the layer thickness of the b layer is 1 to 5 [mu] m, the layer thickness of the c layer according to any one of claims 1 to 3, characterized in that a 2~7μm Casting member. 被覆層が形成された母材は、その最表面から25μmの深さにおける硬さが、該最表面から500μmの深さにおける硬さに比べ、硬さ記号HV0.2にて100以上高いことを特徴とする請求項1ないしのいずれかに記載の鋳造用部材。 The base material on which the coating layer is formed has a hardness at a depth of 25 μm from the outermost surface being 100 or more higher at a hardness symbol HV0.2 than a hardness at a depth of 500 μm from the outermost surface. The casting member according to any one of claims 1 to 4 , characterized in that:
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