JPS63140740A - Mold for casting active metal of high melting point - Google Patents
Mold for casting active metal of high melting pointInfo
- Publication number
- JPS63140740A JPS63140740A JP28638186A JP28638186A JPS63140740A JP S63140740 A JPS63140740 A JP S63140740A JP 28638186 A JP28638186 A JP 28638186A JP 28638186 A JP28638186 A JP 28638186A JP S63140740 A JPS63140740 A JP S63140740A
- Authority
- JP
- Japan
- Prior art keywords
- mold
- sand
- casting
- melting point
- active metal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 229910052751 metal Inorganic materials 0.000 title claims abstract description 24
- 239000002184 metal Substances 0.000 title claims abstract description 24
- 238000005266 casting Methods 0.000 title claims abstract description 19
- 238000002844 melting Methods 0.000 title claims abstract description 12
- 230000008018 melting Effects 0.000 title claims abstract description 12
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 37
- 239000004576 sand Substances 0.000 claims abstract description 27
- 239000000843 powder Substances 0.000 claims abstract description 9
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 5
- 239000000377 silicon dioxide Substances 0.000 claims abstract description 5
- 229910052721 tungsten Inorganic materials 0.000 claims abstract description 5
- 229910052845 zircon Inorganic materials 0.000 claims abstract description 5
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 claims abstract description 5
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 claims abstract description 4
- 229910052863 mullite Inorganic materials 0.000 claims abstract description 4
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 4
- 229910052715 tantalum Inorganic materials 0.000 claims abstract description 4
- 150000002739 metals Chemical class 0.000 claims description 4
- 238000000034 method Methods 0.000 abstract description 16
- 229910052719 titanium Inorganic materials 0.000 abstract description 12
- 229910001069 Ti alloy Inorganic materials 0.000 abstract description 9
- 238000006243 chemical reaction Methods 0.000 abstract description 8
- 238000001035 drying Methods 0.000 abstract description 4
- 239000011248 coating agent Substances 0.000 abstract description 3
- 238000000576 coating method Methods 0.000 abstract description 3
- 230000007547 defect Effects 0.000 abstract description 3
- 235000019353 potassium silicate Nutrition 0.000 abstract description 3
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 abstract description 3
- 239000002904 solvent Substances 0.000 abstract description 3
- 238000002156 mixing Methods 0.000 abstract description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 11
- 239000010936 titanium Substances 0.000 description 11
- 239000000463 material Substances 0.000 description 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 6
- 229910002804 graphite Inorganic materials 0.000 description 6
- 239000010439 graphite Substances 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 6
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 4
- 239000011230 binding agent Substances 0.000 description 4
- 238000000465 moulding Methods 0.000 description 4
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000005495 investment casting Methods 0.000 description 3
- 239000010410 layer Substances 0.000 description 3
- 239000002002 slurry Substances 0.000 description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- YLQBMQCUIZJEEH-UHFFFAOYSA-N Furan Chemical compound C=1C=COC=1 YLQBMQCUIZJEEH-UHFFFAOYSA-N 0.000 description 2
- 239000002253 acid Substances 0.000 description 2
- 229910052786 argon Inorganic materials 0.000 description 2
- 239000011247 coating layer Substances 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000011049 filling Methods 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- RMAQACBXLXPBSY-UHFFFAOYSA-N silicic acid Chemical compound O[Si](O)(O)O RMAQACBXLXPBSY-UHFFFAOYSA-N 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- -1 their oxides Inorganic materials 0.000 description 2
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 description 2
- 229920001875 Ebonite Polymers 0.000 description 1
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N Phenol Chemical compound OC1=CC=CC=C1 ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000009750 centrifugal casting Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000004927 clay Substances 0.000 description 1
- 238000000855 fermentation Methods 0.000 description 1
- 230000004151 fermentation Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000008187 granular material Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000006263 metalation reaction Methods 0.000 description 1
- 239000003110 molding sand Substances 0.000 description 1
- 239000005416 organic matter Substances 0.000 description 1
- 239000003960 organic solvent Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 229920003002 synthetic resin Polymers 0.000 description 1
- 239000000057 synthetic resin Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、高融点活性金属、例えばチタンまたはチタン
合金の鋳造において、M型との反応を抑制し、健全なる
鋳造品を製造するための鋳型に関するものである。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention provides a method for suppressing the reaction with the M-type and producing sound cast products in the casting of high melting point active metals, such as titanium or titanium alloys. It is related to molds.
チタンまたはチタン合金等の高融点活性金属の鋳造にお
いては、溶融状態の金属と#8型材とが反応し、反応層
が硬化して機械加工困難となるばかりか、鋳造品内部に
欠陥を生ずる。これは鋳型材が黒鉛の場合にはチタンの
炭化物を作るためであり、鋳型材が酸化物の場合にはこ
の酸化物が還元されて酸素がチタンまたはチタン合金中
に溶解することが原因である。When casting active metals with high melting points such as titanium or titanium alloys, the metal in the molten state reacts with the #8 mold material, and the reaction layer hardens, making machining difficult and causing defects inside the cast product. This is because when the mold material is graphite, titanium carbide is created, and when the mold material is an oxide, this oxide is reduced and oxygen is dissolved into the titanium or titanium alloy. .
チタンまたはチタン合金の鋳造法には大別してラムドグ
ラファイト法とインへストメント精密鋳造法とがある。Casting methods for titanium or titanium alloys are broadly divided into the lambda graphite method and the investment precision casting method.
前者は粘結剤と混練したグラファイト粒を模型上に充填
し、つき固めた後、模型を脱型して鋳型とするものであ
り、中ないし大物で寸法精度をそれほど必要としない鋳
造品の製造に用いられるものである。The former involves filling a model with graphite grains mixed with a binder, compacting them, and then removing the model to form a mold, and is used to manufacture medium to large castings that do not require high dimensional accuracy. It is used for.
後者は鋳造品と相似のワックスパターンを製造し、これ
を耐火物スラリー中に浸漬した後、耐火物粒をふりかけ
て層となし、これを数回繰り返して厚さ6〜10mmと
なったところでワックスパターンを消失させR型とする
方法であって、寸法精度が高く複雑な形状の鋳造、9の
製造に用いられる。For the latter, a wax pattern similar to that of the cast product is manufactured, which is immersed in a refractory slurry and then sprinkled with refractory granules to form a layer.This process is repeated several times, and when the thickness reaches 6 to 10 mm, wax is applied. This method eliminates the pattern and creates an R shape, and is used for casting and manufacturing 9 of complex shapes with high dimensional accuracy.
その他にクロマイト砂を用いて、通常の鋳型製造法と同
様にして鋳型を作る方法が開発されている。In addition, a method of making a mold using chromite sand in the same manner as a normal mold manufacturing method has been developed.
上記の従来方法では下記の問題点があった。 The above conventional method has the following problems.
ラムドグラファイト法においては、グラファイトとチタ
ンまたはチタン合金溶湯との反応によって生ずる炭化チ
タンの反応層が厚く、これを除去するのに多大の手数を
必要とする。In the lambda graphite method, the reaction layer of titanium carbide produced by the reaction between graphite and titanium or titanium alloy molten metal is thick and requires a great deal of effort to remove.
インベストメント精密鋳造法においては、鋳型を製作す
るのに特別な設備と技術とを必要とする。Investment precision casting requires special equipment and technology to produce molds.
本発明は上記の問題点を同時に解決した鋳型を提供しよ
うとするものである。The present invention aims to provide a mold that solves the above problems at the same time.
本発明は、珪砂、ジルコン砂、ムライト酸、モロカイト
砂あるいはシャモット砂からなる鋳型の高融点活性金属
溶湯と接するキャビティ部に。The present invention applies to a cavity portion of a mold made of silica sand, zircon sand, mullite acid, molochite sand, or chamotte sand, which is in contact with a molten metal having a high melting point.
W 、 M o 、 N b 、 T aおよびこれら
の酸化物ならびにY2O3から選択された何れか1種類
の粉末を塗布して構成した高融点活性金属鋳造用鋳型を
問題解決の技術手段とするものである。A technical means for solving the problem is a mold for casting active metals with a high melting point, which is constructed by applying powder of any one selected from W, Mo, Nb, Ta, their oxides, and Y2O3. be.
本発明の鋳型は塗布層が高融点活性金属溶湯と接するの
で、溶湯と鋳型との反応が抑制され、表面硬化を生ずる
ことなく、また鋳造品の内部欠陥の発生を防止する。Since the coating layer of the mold of the present invention comes into contact with the molten metal having a high melting point, the reaction between the molten metal and the mold is suppressed, preventing surface hardening and preventing internal defects in the cast product.
また本発明の鋳型は製作方法が簡単である。すなわち一
般の砂型鋳型の造型方法と同様に、模型を定盤上に固定
し、その周囲を囲んで鋳枠をおき、この中に鋳物砂を充
填して突き固めた後、鋳枠を天地反転させ、模型を抜い
て鋳型とする。次いで溶湯と接する鋳型キャビティ部に
、溶湯と反応を生じないか、あるいは反応を生じてもそ
の度合いの小さな物質を塗布する。このような物質とし
ては、W、Mo、Nb、Taおよびこれらの酸化物なら
びにY2O3のうちから選択した1種を用いる。Furthermore, the mold of the present invention is easy to manufacture. In other words, in the same way as the general sand mold making method, the model is fixed on a surface plate, a casting flask is placed around it, and after filling the molding sand and compacting it, the flask is turned upside down. Then remove the model and use it as a mold. Next, a substance that does not react with the molten metal or reacts only to a small degree is applied to the mold cavity that comes into contact with the molten metal. As such a substance, one selected from W, Mo, Nb, Ta, oxides thereof, and Y2O3 is used.
この鋳型は、チタンまたはチタン合金溶湯を注湯した際
に、鋳型材と溶湯との接触面で容易に反応が生ずるのを
防止することができる。This mold can prevent reactions from easily occurring at the contact surfaces between the mold material and the molten metal when titanium or titanium alloy molten metal is poured into the mold.
第1図は本発明の型枠を模式的に示したもので、鋳型2
のキャビティ内部に塗布層lを形成したものである。Figure 1 schematically shows the mold of the present invention.
A coating layer l is formed inside the cavity.
次に本発明の鋳型の造型方法を第2図に示したフローチ
ャートに従って説明する。Next, the molding method of the present invention will be explained according to the flowchart shown in FIG.
チタンあるいはチタン合金の凝固収縮率ならびに熱膨張
率と鋳型の熱膨張率を考慮して製作した木製、合成樹脂
製あるいは硬質ゴム製の模型を定盤に固定し、その周囲
に鋳枠をたてる。骨材として珪砂、ジルコン砂、ムライ
ト酸、モロカイト砂またはシャモット砂のうち1種類を
用い、粘結剤として水ガラス、シリカゾル、アルミナゾ
ルまたはジルコニアゾルのうち1種類を用い、必要に応
じてフラン、フェノール等の有機粘結剤を用い、これら
を混合、攪拌して上記鋳枠中に充填する。A wooden, synthetic resin, or hard rubber model made considering the solidification shrinkage rate and thermal expansion coefficient of titanium or titanium alloy and the thermal expansion coefficient of the mold is fixed to a surface plate, and a casting flask is erected around it. . One type of silica sand, zircon sand, mullite acid, molochite sand, or chamotte sand is used as the aggregate, and one type of water glass, silica sol, alumina sol, or zirconia sol is used as the binder, and furan and phenol are used as necessary. These organic binders are mixed, stirred, and filled into the flask.
この際、必要ならば硬化剤を使用する。鋳型材が硬化し
た後、模型を脱型する。また必要ならば鋳枠を取り外す
。At this time, use a hardening agent if necessary. After the mold material has hardened, the model is demolded. Also, remove the flask if necessary.
上記方法によって得られた鋳型のキャビティ部に、W
、 M o 、 N b 、 T aおよびこれらの酸
化物ならびにY2O3粉末から選択した何れか1種類の
粉末を水、アルコールまたはアセトン等の有機溶媒、シ
リカゾル、アルミナゾルあるいはジルコニアゾルのうち
1種類を溶媒として塗布し、溶媒が乾燥した後、鋳型キ
ャビティ部がこれら高融点金属ないしは醸化物粉によっ
て被覆された状態になるようにする。In the cavity of the mold obtained by the above method, W
, M o , N b , Ta and their oxides, and any one type of powder selected from Y2O3 powder is mixed with water, an organic solvent such as alcohol or acetone, and one type of silica sol, alumina sol, or zirconia sol as a solvent. After coating and drying of the solvent, the mold cavity is coated with the high melting point metal or fermentation powder.
上記方法によって鋳型の上型、下型あるいは必要に応じ
て中子を作製し、これらを組合わせて1組の鋳型とする
。An upper mold, a lower mold or, if necessary, a core are prepared by the above method, and these are combined to form a set of molds.
上記鋳型は800〜12O0℃の大気炉あるいは還元雰
囲気炉中で十分に焼成し、水分あるいは有機物を除去し
、あるいは砂粒子間を焼結せしめて鋳型の強度を増加さ
せた後に、チタンまたはチタン合金溶湯の注湯に供する
。The above-mentioned mold is sufficiently fired in an atmospheric furnace or reducing atmosphere furnace at 800 to 1200°C to remove moisture or organic matter, or to increase the strength of the mold by sintering between sand particles. Used for pouring molten metal.
チタンまたはチタン合金の注湯に際して、鋳型の温度は
常温でもこれより高くても構わない。When pouring titanium or titanium alloy, the temperature of the mold may be at room temperature or higher.
また鋳造方法は、重力PI造、加圧鋳造あるいは遠心鋳
造の何れでも構わない。Further, the casting method may be gravity casting, pressure casting, or centrifugal casting.
実施例1
鋳型材の骨材として、5f02:53重量%、AJlj
2Oa : 42重量%の焼結粘土砂(シャモット砂)
(粒径0.3〜1.0mm)を用い、これに粘結剤とし
て、シャモット砂lOO重量部に対して水ガラス8重量
部を加えて調合し、CO2ガス法によって外径80mm
、高さ60mm、内径40mmで深さ40mmの鋳型を
成形した。Example 1 As aggregate for mold material, 5f02:53% by weight, AJlj
2Oa: 42% by weight sintered clay sand (chamotte sand)
(particle size: 0.3 to 1.0 mm), and as a binder, 8 parts by weight of water glass was added to 10 parts by weight of chamotte sand, and the outer diameter was 80 mm using the CO2 gas method.
A mold with a height of 60 mm, an inner diameter of 40 mm, and a depth of 40 mm was molded.
この鋳型キャビティ部に、Y2O3粉末2重量部とアル
ミナゾル1重量部の割合で調合したスラリーを均一の厚
みに塗布した。A slurry prepared at a ratio of 2 parts by weight of Y2O3 powder and 1 part by weight of alumina sol was applied to the mold cavity to a uniform thickness.
乾燥後、電気炉を用いて大気雰囲気中で12O0℃で焼
成し、さらに常温に降下させた鋳型に、アルゴンアーク
溶解加圧鋳造機を用いて純チタンを鋳造した。After drying, it was fired at 1200° C. in an air atmosphere using an electric furnace, and pure titanium was cast into a mold that was lowered to room temperature using an argon arc melting pressure casting machine.
鋳造後のチタン鋳造材の鋳肌状態、引張強度、伸び、硬
度を測定し、第1表の結果を得た。第1表中の判定で×
は使用不可の状態、Oは使用可部の状態、Δは問題は少
しあるが使用可源の状態を示す。The cast surface condition, tensile strength, elongation, and hardness of the titanium cast material after casting were measured, and the results shown in Table 1 were obtained. × according to the judgment in Table 1
indicates an unusable state, O indicates a usable state, and Δ indicates a usable state with some problems.
実施例2
実施例1と同様の方法で鋳型を成形し、この鋳型内面に
W粉末をジルコニアゾル1重量部に対してW粉末4重量
部の割合で調合したスラリーを各種の厚みに均一に塗布
した。Example 2 A mold was formed in the same manner as in Example 1, and a slurry prepared by mixing W powder at a ratio of 4 parts by weight to 1 part by weight of zirconia sol was uniformly applied to the inner surface of the mold to various thicknesses. did.
乾燥後、水素雰囲気炉を用いて還元雰囲気中で12O0
℃で焼成し、さらに常温に降下させた鋳型に、アルゴン
アーク溶解加圧鋳造機を用いて純チタンを鋳造し、実施
例1と同様に第2表の結果を得た。After drying, 12O0 was added in a reducing atmosphere using a hydrogen atmosphere furnace.
Pure titanium was cast into a mold fired at .degree. C. and then cooled to room temperature using an argon arc melting pressure casting machine, and the results shown in Table 2 were obtained in the same manner as in Example 1.
従来の黒鉛鋳型あるいは精密鋳造鋳型に比較して、造型
法が一般の砂型造型法と同一であるために、造型技術が
容易であり、低コストである。Compared to conventional graphite molds or precision casting molds, the molding method is the same as the general sand molding method, so the molding technology is easier and the cost is lower.
塗型材として酸化物を使用する場合には、従来の方法の
ように真空炉あるいは還元雰囲気炉を使用する必要がな
く、通常の大気雰囲気炉が使用できる。When an oxide is used as the coating material, there is no need to use a vacuum furnace or a reducing atmosphere furnace as in conventional methods, and a normal atmospheric furnace can be used.
第1図は本発明の鋳型の模式断面図、第2図はその製造
工程のフローチャートである。FIG. 1 is a schematic sectional view of the mold of the present invention, and FIG. 2 is a flowchart of its manufacturing process.
Claims (1)
はシャモット砂からなる鋳型の高融点活性金属溶湯と接
するキャビティ部に、 W、Mo、Nb、Taおよびこれらの酸化物ならびにY
_2O_3から選ばれた1種の粉末を塗布してなる高融
点活性金属鋳造用鋳型。[Scope of Claims] 1. W, Mo, Nb, Ta and their oxides, and Y are added to the cavity portion of a mold made of silica sand, zircon sand, mullite sand, molochite sand, or chamotte sand that comes into contact with the high melting point active metal molten metal.
A mold for casting high melting point active metals coated with one type of powder selected from _2O_3.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP28638186A JPS63140740A (en) | 1986-12-01 | 1986-12-01 | Mold for casting active metal of high melting point |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP28638186A JPS63140740A (en) | 1986-12-01 | 1986-12-01 | Mold for casting active metal of high melting point |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS63140740A true JPS63140740A (en) | 1988-06-13 |
Family
ID=17703656
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP28638186A Pending JPS63140740A (en) | 1986-12-01 | 1986-12-01 | Mold for casting active metal of high melting point |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS63140740A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH06583A (en) * | 1992-06-19 | 1994-01-11 | Agency Of Ind Science & Technol | Core for casting of titanium and its alloy |
KR100616412B1 (en) | 2004-09-01 | 2006-08-29 | 김영직 | Molds manufacturing for high quality titanium cast alloys |
WO2014192819A1 (en) * | 2013-05-29 | 2014-12-04 | 三菱重工業株式会社 | Core for precision casting, production method therefor, and mold for precision casting |
JP2014231076A (en) * | 2013-05-29 | 2014-12-11 | 三菱重工業株式会社 | Core for precision casting, production method therefor, and mold for precision casting |
JP2016140876A (en) * | 2015-01-30 | 2016-08-08 | 三菱重工航空エンジン株式会社 | Method for manufacturing mold for precision casting |
-
1986
- 1986-12-01 JP JP28638186A patent/JPS63140740A/en active Pending
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH06583A (en) * | 1992-06-19 | 1994-01-11 | Agency Of Ind Science & Technol | Core for casting of titanium and its alloy |
US5394933A (en) * | 1992-06-19 | 1995-03-07 | Agency Of Industrial Science & Technology | Core for casting titanium and titanium alloy |
KR100616412B1 (en) | 2004-09-01 | 2006-08-29 | 김영직 | Molds manufacturing for high quality titanium cast alloys |
WO2014192819A1 (en) * | 2013-05-29 | 2014-12-04 | 三菱重工業株式会社 | Core for precision casting, production method therefor, and mold for precision casting |
JP2014231076A (en) * | 2013-05-29 | 2014-12-11 | 三菱重工業株式会社 | Core for precision casting, production method therefor, and mold for precision casting |
US10166598B2 (en) | 2013-05-29 | 2019-01-01 | Mitsubish Heavy Industries, Ltd. | Precision-casting core, precision-casting core manufacturing method, and precision-casting mold |
JP2016140876A (en) * | 2015-01-30 | 2016-08-08 | 三菱重工航空エンジン株式会社 | Method for manufacturing mold for precision casting |
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