JPH11320029A - Core for precision casting - Google Patents

Core for precision casting

Info

Publication number
JPH11320029A
JPH11320029A JP13151198A JP13151198A JPH11320029A JP H11320029 A JPH11320029 A JP H11320029A JP 13151198 A JP13151198 A JP 13151198A JP 13151198 A JP13151198 A JP 13151198A JP H11320029 A JPH11320029 A JP H11320029A
Authority
JP
Japan
Prior art keywords
oxide
core
sio
precision casting
ceramic
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.)
Withdrawn
Application number
JP13151198A
Other languages
Japanese (ja)
Inventor
Hisayuki Takesue
久幸 竹末
Yoshikazu Kutaragi
義和 久多良木
Akira Mihashi
章 三橋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Materials Corp
Original Assignee
Mitsubishi Materials Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mitsubishi Materials Corp filed Critical Mitsubishi Materials Corp
Priority to JP13151198A priority Critical patent/JPH11320029A/en
Publication of JPH11320029A publication Critical patent/JPH11320029A/en
Withdrawn legal-status Critical Current

Links

Landscapes

  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Abstract

PROBLEM TO BE SOLVED: To provide a core for precision casting, having a slight reaction to molten heat resistant alloy. SOLUTION: This core for precision casting is manufactured, the surface of which of a ceramic core body 2 consisting essentially of silica with oxide coating layer 3 composed of single layer of one kind and plural layers of two or more kinds among zirconium oxide, barium oxide, cerium oxide, hafnium oxide, beryllium oxide, yttrium oxide, calcium oxide and therium oxide, is formed so as to be in the range of total layer thickness 3-8 μm.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】この発明は、Ni基超合金な
どの耐熱合金溶湯を精密鋳造して複雑形状中空部分を有
する各種耐熱機械部品を製造する際に使用する精密鋳造
用中子に関するものであり、特に耐熱合金溶湯に対して
反応しにくい酸化物被覆層をシリカを主成分とするセラ
ミックス中子本体に被覆してなる精密鋳造用中子に関す
るものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a precision casting core used for precision casting of a heat-resistant alloy such as a Ni-base superalloy to produce various heat-resistant mechanical parts having a hollow portion having a complicated shape. More particularly, the present invention relates to a precision casting core in which an oxide coating layer that is hardly reactive to a heat-resistant alloy melt is coated on a ceramic core body containing silica as a main component.

【0002】[0002]

【従来の技術】一般に、Ni基超合金などの耐熱合金製
タービンブレードやベーンには、使用中に過度の高温に
ならないように中心部に空気、蒸気または水などの流体
を流して冷却するための中空部分が設けられており、こ
の中空部分は、中空部分と同一形状を有する中子を鋳型
にセットし、鋳型と中子で構成されるキャビティに耐熱
合金溶湯を鋳込み、ついで中子を水酸化カリウム溶液な
どの苛性液体で浸出除去することにより形成される。前
記耐熱合金溶湯を精密鋳造するための中子として、従
来、シリカを主成分とするセラミックス中子が使用され
ており、このシリカを主成分とするセラミックス中子
は、SiO2 系セラミックス、SiO2 −ZrSiO4
系セラミックスまたはSiO2 −Al2 3 系セラミッ
クスで構成されている。前記SiO2 系セラミックスは
SiO2 からなる組成を有し、前記SiO2 −ZrSi
4 系セラミックスはZrSiO4 :20〜40%を含
有し、残部:SiO2 からなる組成を有し、さらに前記
SiO2 −Al2 3 系セラミックスはAl2 3 :3
〜10%を含有し、残部:SiO2 からなる組成を有る
ことも知られている。
2. Description of the Related Art Generally, a turbine blade or a vane made of a heat-resistant alloy such as a Ni-base superalloy is cooled by flowing a fluid such as air, steam or water to a central portion thereof so that an excessively high temperature does not occur during use. The hollow portion is provided, and in this hollow portion, a core having the same shape as the hollow portion is set in a mold, a heat-resistant alloy melt is cast into a cavity formed by the mold and the core, and then the core is cooled with water. It is formed by leaching out with a caustic liquid such as a potassium oxide solution. Wherein the heat-resistant alloy melt as core for precision casting, conventionally, silica has been used a ceramic core consisting mainly of a ceramic core mainly composed of silica is, SiO 2 based ceramics, SiO 2 -ZrSiO 4
It is made of a ceramic or SiO 2 —Al 2 O 3 ceramic. The SiO 2 based ceramics having a composition consisting of SiO 2, the SiO 2 -ZrSi
The O 4 -based ceramic has a composition of ZrSiO 4 : 20 to 40% and the balance: SiO 2 , and the SiO 2 -Al 2 O 3 -based ceramic has an Al 2 O 3 : 3.
It is also known to have a composition containing 10% to 10%, with the balance being SiO 2 .

【0003】[0003]

【発明が解決しようとする課題】しかし、タービンブレ
ードやベーンを製造するためのNi基超合金などの耐熱
合金は融点が高く、したがって、この耐熱合金の溶湯は
シリカを主成分とするセラミックス中子に対して反応し
やすい。耐熱合金の溶湯が上記シリカを主成分とするセ
ラミックス中子と反応すると、鋳造終了後、中子を水酸
化カリウム溶液などの苛性液体で浸出除去しようとして
も、タービンブレードやベーンの中空部分の内面に中子
の残査が張り付いて離れず、これを機械的に剥離するこ
とは困難である。また耐熱合金の溶湯が上記シリカを主
成分とするセラミックス中子と反応すると、耐熱合金の
成分組成がずれると共に中空部分の内面の鋳肌が荒れて
表面性状が悪化し、さらに中空部分の内面に欠陥が発生
することがある。中空部分の内面の鋳肌が荒れて表面性
状が悪いと中空部分を流れる流体の流れが悪くなって冷
却効率が低下し、さらに中空部分の内面に欠陥が生じる
と不良鋳物となって廃棄処分にしなければならなくな
る。
However, heat-resistant alloys such as Ni-base superalloys for producing turbine blades and vanes have a high melting point. Therefore, the molten metal of this heat-resistant alloy is a ceramic core mainly composed of silica. Easy to react to. When the molten metal of the heat-resistant alloy reacts with the above-mentioned ceramic core containing silica as a main component, after casting is completed, even if the core is leached and removed with a caustic liquid such as a potassium hydroxide solution, the inner surface of the hollow portion of the turbine blade or vane is removed. However, it is difficult to mechanically peel off the core residue. In addition, when the molten metal of the heat-resistant alloy reacts with the ceramic core containing silica as a main component, the component composition of the heat-resistant alloy is deviated, and the casting surface on the inner surface of the hollow portion is roughened to deteriorate the surface properties. Defects may occur. If the casting surface on the inner surface of the hollow part is rough and the surface properties are poor, the flow of the fluid flowing through the hollow part will be worse and the cooling efficiency will be reduced. I have to.

【0004】[0004]

【課題を解決するための手段】そこで、本発明者等は、
これらの課題を解決すべく研究を行った結果、従来のシ
リカを主成分とする従来のセラミックス中子を本体と
し、その表面に酸化ジルコニウム、酸化バリウム、酸化
セリウム、酸化ハフニウム、酸化ベリリウム、酸化イッ
トリウム、酸化カルシウム、酸化トリウムの内の1種の
単層または2種以上の複層からなる酸化物被覆層を形成
すると、中子表面に対する耐熱合金溶湯の反応性が低下
し、中子に接触する鋳物の鋳肌の荒れが無くなり、表面
欠陥もなくなって中子の残査が鋳肌に残ることがないと
云う知見を得たのである。
Means for Solving the Problems Accordingly, the present inventors have
As a result of conducting research to solve these problems, the main body was a conventional ceramic core containing conventional silica as the main component, and zirconium oxide, barium oxide, cerium oxide, hafnium oxide, beryllium oxide, yttrium oxide on the surface. When an oxide coating layer composed of a single layer or two or more layers of calcium oxide and thorium oxide is formed, the reactivity of the heat-resistant alloy melt on the core surface is reduced and the core comes into contact with the core. It has been found that there is no roughening of the casting surface of the casting, no surface defects, and no residue of the core remains on the casting surface.

【0005】この発明は、かかる知見にもとづいてなさ
れたものであって、シリカを主成分とするセラミックス
中子本体の表面に酸化ジルコニウム、酸化バリウム、酸
化セリウム、酸化ハフニウム、酸化ベリリウム、酸化イ
ットリウム、酸化カルシウム、酸化トリウムの内の1種
の単層または2種以上の複層からなる酸化物被覆層を形
成してなる精密鋳造用中子に特徴を有するものである。
The present invention has been made on the basis of the above findings. Zirconium oxide, barium oxide, cerium oxide, hafnium oxide, beryllium oxide, yttrium oxide, The present invention has a feature in a core for precision casting in which an oxide coating layer composed of a single layer of calcium oxide or thorium oxide or a multilayer of two or more layers is formed.

【0006】この発明の精密鋳造用中子を図面にもとづ
いてさらに具体的に説明する。図1は、この発明の精密
鋳造用中子の断面図であり、図1において、1はこの発
明の精密鋳造用中子、2はシリカを主成分とするセラミ
ックス中子本体、3は酸化物被覆層である。この発明の
精密鋳造用中子1の酸化物被覆層3は、吹き付け塗装、
塗布などいろいろな方法で形成することができるが、酸
化物被覆層3は総層厚が3〜8μmの範囲内にあること
が好ましく、かかる厚さの酸化物被覆層を表面滑らかに
形成するには物理蒸着法または化学蒸着法により形成す
ることが最も好ましい。
The precision casting core of the present invention will be described more specifically with reference to the drawings. FIG. 1 is a cross-sectional view of a precision casting core of the present invention. In FIG. 1, 1 is a precision casting core of the present invention, 2 is a ceramic core body mainly composed of silica, and 3 is an oxide. It is a coating layer. The oxide coating layer 3 of the core 1 for precision casting of the present invention is formed by spray coating,
Although the oxide coating layer 3 can be formed by various methods such as coating, the total thickness of the oxide coating layer 3 is preferably in the range of 3 to 8 μm. Is most preferably formed by a physical vapor deposition method or a chemical vapor deposition method.

【0007】上記酸化物被覆層の総層厚を3〜8μmに
定めたのは、酸化物被覆層の総層厚が3μm未満では薄
すぎて耐熱合金溶湯が中子本体と反応するのを阻止する
ことができず、一方、酸化物被覆層の総層厚を8μmを
越えて厚くしても物理蒸着または化学蒸着のためのコス
トがかかるだけでそれ以上の効果がないことによるもの
である。
The reason why the total thickness of the oxide coating layer is set to 3 to 8 μm is that if the total thickness of the oxide coating layer is less than 3 μm, it is too thin to prevent the molten heat-resistant alloy from reacting with the core body. On the other hand, if the total thickness of the oxide coating layer exceeds 8 μm, the cost for physical vapor deposition or chemical vapor deposition is increased and there is no further effect.

【0008】[0008]

【発明の実施の形態】平均粒径:2μmのSiO2
末、平均粒径:2μmのZrSiO4 粉末、平均粒径:
2μmのAl2 3 粉末およびワックス系の有機バイン
ダーを用意し、これら粉末と有機バインダーを配合し、
混練したのち射出成形し、得られた射出成形体を脱脂、
焼成することにより、長さ:120mm、幅:12m
m、厚さ:6mmの寸法を有する表1〜表6に示される
成分組成のセラミックス中子本体を作製した。
BEST MODE FOR CARRYING OUT THE INVENTION Average particle size: 2 μm SiO 2 powder, average particle size: 2 μm ZrSiO 4 powder, average particle size:
A 2 μm Al 2 O 3 powder and a wax-based organic binder were prepared, and these powders and an organic binder were blended.
After kneading, injection molding, the obtained injection molded body is degreased,
By firing, length: 120mm, width: 12m
m, thickness: A ceramic core body having a component composition shown in Tables 1 to 6 having a dimension of 6 mm was produced.

【0009】このシリカを主成分とするセラミックス中
子本体の全表面に、真空蒸着により表1〜表6に示され
る酸化物被覆層を表1〜表6に示される厚さとなるよう
に形成し、本発明精密鋳造用中子1〜45を作製した。
一方、上記シリカを主成分とするセラミックス中子本体
をそのまま従来精密鋳造用中子1〜3とした。上記本発
明精密鋳造用中子1〜45および従来精密鋳造用中子1
〜3をそれぞれ図2の断面図に示されるようにロストワ
ックス鋳型4にセットした。
An oxide coating layer shown in Tables 1 to 6 is formed on the entire surface of the ceramic core body containing silica as a main component so as to have a thickness shown in Tables 1 to 6 by vacuum deposition. The cores 1 to 45 for precision casting of the present invention were produced.
On the other hand, the above-mentioned ceramic core bodies containing silica as a main component were used as conventional cores 1 to 3 for precision casting. The above-mentioned cores for precision casting 1 to 45 of the present invention and the conventional core for precision casting 1
3 were set in the lost wax mold 4 as shown in the sectional view of FIG.

【0010】一方、Cr:10%、Co:4.5%、
W:6.0%、Al:5.5%、Ti:2.1%、T
a:5.6%、Tl:2.1%、Mo:0.7%、R
e:0.2%を含有し、残りがNiからなる成分組成を
有するNi基超合金を真空溶解し、得られた溶湯を温
度;1450℃に保持し、鋳型4の湯口から鋳型4のキ
ャビティ5を十分満たすように鋳込むと共に冷却板6に
より鋳型底部から冷却することにより単結晶Ni基超合
金鋳物を鋳造した。
On the other hand, Cr: 10%, Co: 4.5%,
W: 6.0%, Al: 5.5%, Ti: 2.1%, T
a: 5.6%, Tl: 2.1%, Mo: 0.7%, R
e: A Ni-based superalloy containing 0.2% and having a component composition consisting of Ni is vacuum-melted, and the obtained molten metal is kept at a temperature of 1450 ° C. 5 and sufficiently cooled from the bottom of the mold by a cooling plate 6 to cast a single crystal Ni-based superalloy casting.

【0011】得られた単結晶Ni基超合金鋳物を鋳型か
らはずし、さらに上記中子を含む鋳物を水酸化カリウム
水溶液中に浸漬し、中子を浸出除去することにより中空
部分を有する単結晶Ni基超合金鋳物を作製した。得ら
れた単結晶Ni基超合金鋳物を切断し、中子と接した中
空部分の鋳肌表面を光学顕微鏡で観察し、表面粗さRm
axを求め、その結果を表1〜表6に示した。
The obtained single-crystal Ni-base superalloy casting is removed from the mold, and the casting containing the core is immersed in an aqueous potassium hydroxide solution, and the core is leached out to remove single-crystal Ni having a hollow portion. A base superalloy casting was prepared. The obtained single crystal Ni-base superalloy casting is cut, and the casting surface of the hollow portion in contact with the core is observed with an optical microscope, and the surface roughness Rm
ax was determined, and the results are shown in Tables 1 to 6.

【0012】さらに得られた単結晶Ni基超合金鋳物の
中空部分を蛍光浸透探査検査することにより中空部分の
鋳肌表面に発生した欠陥数を測定し、その結果を表1〜
表6に示した。
Further, the number of defects generated on the casting surface of the hollow portion was measured by subjecting the hollow portion of the obtained single-crystal Ni-base superalloy casting to a fluorescent penetration inspection test.
The results are shown in Table 6.

【0013】[0013]

【表1】 [Table 1]

【0014】[0014]

【表2】 [Table 2]

【0015】[0015]

【表3】 [Table 3]

【0016】[0016]

【表4】 [Table 4]

【0017】[0017]

【表5】 [Table 5]

【0018】[0018]

【表6】 [Table 6]

【0019】表1〜表6に示される結果から、セラミッ
クス中子本体の表面に酸化物被覆層を形成した本発明精
密鋳造用中子1〜45を使用すると、表面に酸化物被覆
層の無いセラミックス中子本体からなる従来精密鋳造用
中子1〜3を使用するよりも得られた単結晶Ni基超合
金鋳物の中空部分の表面粗さRmaxが小さく、さらに
単結晶Ni基超合金鋳物の中空部分の表面に発生する欠
陥数が少ないことが分かる。なお、この実施例ではセラ
ミックス中子本体の表面に形成する酸化物被覆層は代表
的な化学蒸着法である真空蒸着法により形成したが、代
表的な物理蒸着法であるスパッタリング法で形成しても
同じ結果が得られた。
From the results shown in Tables 1 to 6, it can be seen that when the cores for precision casting of the present invention 1 to 45, each having an oxide coating layer formed on the surface of the ceramic core body, were used, there was no oxide coating layer on the surface. The surface roughness Rmax of the hollow portion of the obtained single crystal Ni-based superalloy casting is smaller than that obtained by using the conventional precision casting cores 1 to 3 composed of a ceramic core body, and the single crystal Ni-based superalloy casting is obtained. It can be seen that the number of defects generated on the surface of the hollow portion is small. In this example, the oxide coating layer formed on the surface of the ceramic core body was formed by a vacuum deposition method which is a typical chemical vapor deposition method, but was formed by a sputtering method which was a typical physical vapor deposition method. The same result was obtained.

【0020】[0020]

【発明の効果】上述のように、この発明の精密鋳造用中
子を使用すると耐熱合金鋳物の複雑な形状を有する中空
部分の鋳肌を平滑にかつ欠陥が発生することなく製造す
ることができ、産業上すぐれた効果を奏するものであ
る。
As described above, when the core for precision casting of the present invention is used, the casting surface of a hollow portion having a complicated shape of a heat-resistant alloy casting can be manufactured smoothly and without defects. It has excellent industrial effects.

【図面の簡単な説明】[Brief description of the drawings]

【図1】この発明の精密鋳造用中子の断面図である。FIG. 1 is a sectional view of a core for precision casting of the present invention.

【図2】この発明の精密鋳造用中子をロストワックス鋳
型にセットした状態を示す断面図である。
FIG. 2 is a sectional view showing a state in which the core for precision casting of the present invention is set in a lost wax mold.

【符号の説明】[Explanation of symbols]

1 この発明の精密鋳造用中子 2 セラミックス中子本体 3 酸化物被覆層 4 ロストワックス鋳型 5 キャビティ 6 冷却板 DESCRIPTION OF SYMBOLS 1 Core for precision casting of this invention 2 Ceramic core body 3 Oxide coating layer 4 Lost wax mold 5 Cavity 6 Cooling plate

Claims (5)

【特許請求の範囲】[Claims] 【請求項1】 シリカを主成分とするセラミックス中子
本体の表面に酸化ジルコニウム、酸化バリウム、酸化セ
リウム、酸化ハフニウム、酸化ベリリウム、酸化イット
リウム、酸化カルシウム、酸化トリウムの内の1種の単
層または2種以上の複層からなる酸化物被覆層を形成し
てなることを特徴とする精密鋳造用中子。
1. A monolayer of one of zirconium oxide, barium oxide, cerium oxide, hafnium oxide, beryllium oxide, yttrium oxide, calcium oxide, and thorium oxide on a surface of a ceramic core body containing silica as a main component. A precision casting core comprising an oxide coating layer comprising at least two types of multiple layers.
【請求項2】 シリカを主成分とするセラミックス中子
本体の表面に酸化ジルコニウム、酸化バリウム、酸化セ
リウム、酸化ハフニウム、酸化ベリリウム、酸化イット
リウム、酸化カルシウム、酸化トリウムの内の1種の単
層または2種以上の複層からなる酸化物被覆層を、総層
厚が3〜8μmの範囲内にあるように形成してなること
を特徴とする精密鋳造用中子。
2. A monolayer of one of zirconium oxide, barium oxide, cerium oxide, hafnium oxide, beryllium oxide, yttrium oxide, calcium oxide, and thorium oxide on the surface of a ceramic core body containing silica as a main component. A core for precision casting, wherein an oxide coating layer comprising two or more types of multiple layers is formed so that the total layer thickness is in the range of 3 to 8 μm.
【請求項3】 前記酸化物被覆層は、物理蒸着法または
化学蒸着法により形成された被覆層であることを特徴と
する請求項1または2記載の精密鋳造用中子。
3. The core for precision casting according to claim 1, wherein the oxide coating layer is a coating layer formed by a physical vapor deposition method or a chemical vapor deposition method.
【請求項4】 前記シリカを主成分とするセラミックス
中子本体は、SiO 2 系セラミックス、SiO2 −Zr
SiO4 系セラミックスまたはSiO2 −Al2 3
セラミックスからなることを特徴とする請求項1または
2記載の精密鋳造用中子。
4. A ceramic containing silica as a main component.
The core body is SiO TwoCeramics, SiOTwo-Zr
SiOFourCeramics or SiOTwo-AlTwoOThreesystem
2. The method according to claim 1, wherein the material is made of ceramics.
2. The core for precision casting according to 2.
【請求項5】 前記SiO2 系セラミックスはSiO2
からなるセラミックスであり、前記SiO2 −ZrSi
4 系セラミックスはZrSiO4 :20〜40%を含
有し、残部:SiO2 からなるセラミックスであり、前
記SiO2 −Al2 3 系セラミックスはAl2 3
3〜10%を含有し、残部:SiO2からなるセラミッ
クスであることを特徴とする請求項4記載の精密鋳造用
中子。
5. The method according to claim 1, wherein the SiO 2 ceramic is SiO 2.
A ceramic comprising the SiO 2 —ZrSi
The O 4 -based ceramics are ceramics containing ZrSiO 4 : 20 to 40% and the balance: SiO 2 , and the SiO 2 -Al 2 O 3 -based ceramics is Al 2 O 3 :
Containing 3-10%, balance: 4. precision casting core according which is a ceramic made of SiO 2.
JP13151198A 1998-05-14 1998-05-14 Core for precision casting Withdrawn JPH11320029A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13151198A JPH11320029A (en) 1998-05-14 1998-05-14 Core for precision casting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13151198A JPH11320029A (en) 1998-05-14 1998-05-14 Core for precision casting

Publications (1)

Publication Number Publication Date
JPH11320029A true JPH11320029A (en) 1999-11-24

Family

ID=15059755

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13151198A Withdrawn JPH11320029A (en) 1998-05-14 1998-05-14 Core for precision casting

Country Status (1)

Country Link
JP (1) JPH11320029A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112317695A (en) * 2020-11-05 2021-02-05 山东瑞泰新材料科技有限公司 Casting method of marine reversible turbine blade
CN112321287A (en) * 2020-11-05 2021-02-05 山东瑞泰新材料科技有限公司 Silicon oxide ceramic core with corrosion resistance on surface and manufacturing method thereof
CN116375492A (en) * 2023-01-18 2023-07-04 华中科技大学 Coating for improving surface precision of layered extrusion molding ceramic, preparation and treatment method

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112317695A (en) * 2020-11-05 2021-02-05 山东瑞泰新材料科技有限公司 Casting method of marine reversible turbine blade
CN112321287A (en) * 2020-11-05 2021-02-05 山东瑞泰新材料科技有限公司 Silicon oxide ceramic core with corrosion resistance on surface and manufacturing method thereof
CN116375492A (en) * 2023-01-18 2023-07-04 华中科技大学 Coating for improving surface precision of layered extrusion molding ceramic, preparation and treatment method

Similar Documents

Publication Publication Date Title
US20220088674A1 (en) Castings and Manufacture Methods
KR100611278B1 (en) Refractory metal core coatings
EP1652602B1 (en) Non-oxidizable coating
US6676381B2 (en) Method and apparatus for casting near-net shape articles
JP4137593B2 (en) Core for precision investment casting
US8210240B2 (en) Casting processes, casting apparatuses therefor, and castings produced thereby
TWI404901B (en) Crucibles for melting titanium alloys
US11014151B2 (en) Method of making airfoils
CN1935411A (en) Manufacture of casting cores
JP6660573B2 (en) Manufacturing method of hot forgings
JPH06583A (en) Core for casting of titanium and its alloy
JP5925411B2 (en) Casting process and yttria-containing facecoat material therefor
JPH11320029A (en) Core for precision casting
US11014152B1 (en) Method of making complex internal passages in turbine airfoils
JPH11320028A (en) Core for precision casting excellent in high temperature strength and heat shock resistance
JPH05330957A (en) Core for precision casting
JP3524684B2 (en) Casting mold parts and casting equipment
JPH11342449A (en) Core for precesion casting having low reactivity against heat resistant alloy molten metal
JP2005008454A (en) Refractory for molten glass and method for producing the same
US20230304409A1 (en) Protection against oxidation or corrosion of a hollow part made of a superalloy
JPH09227243A (en) Molybdenum boride-containing composite thermal spraying material and thermally sprayed coating film
JP2002241920A (en) Thermal spray coating and composite thermal spraying material
JP2024057982A (en) Manufacturing method of turbine airfoil part and turbine airfoil part using the same
JPH0297431A (en) Mold for molding optical element
JP2014083587A (en) Surface treatment method of metallic material and metal mold for die cast

Legal Events

Date Code Title Description
A300 Withdrawal of application because of no request for examination

Free format text: JAPANESE INTERMEDIATE CODE: A300

Effective date: 20050802