JPH06182493A - Mold for casting blade - Google Patents

Mold for casting blade

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Publication number
JPH06182493A
JPH06182493A JP4336068A JP33606892A JPH06182493A JP H06182493 A JPH06182493 A JP H06182493A JP 4336068 A JP4336068 A JP 4336068A JP 33606892 A JP33606892 A JP 33606892A JP H06182493 A JPH06182493 A JP H06182493A
Authority
JP
Japan
Prior art keywords
mold
blade
core
cores
forming surface
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.)
Granted
Application number
JP4336068A
Other languages
Japanese (ja)
Other versions
JP2633162B2 (en
Inventor
Katsuo Ueno
勝夫 上野
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.)
Ebara Corp
Original Assignee
Ebara 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 Ebara Corp filed Critical Ebara Corp
Priority to JP4336068A priority Critical patent/JP2633162B2/en
Publication of JPH06182493A publication Critical patent/JPH06182493A/en
Application granted granted Critical
Publication of JP2633162B2 publication Critical patent/JP2633162B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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

Abstract

PURPOSE:To provide a mold for casting blades which is low pattern manufacturing cost and can easily mold with high molding precision without needing the skillfulness. CONSTITUTION:A mold member for forming a space (cavity) Sb for blade matching to blade shape to be cast is constituted with dividable cores 20, 21 and an insert core 10 on the surface faced to the space Sb. At the time of molding, after inserting the insert core 10 around mold center axis X to constitute the lower mold, the cores 20, 21 are piled on the insert core 10 while following to the assembling order to the peripheral direction. A second blade forming surface 203 in each core 20, 21 is continued to the blade forming surface 105 in the insert core 10 to form the space Sb for blade in between these blade forming surfaces 203, 105 and a first blade forming surface 202 in the adjacent cores 20, 21.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、ポンプ用インペラなど
の羽根部品を鋳造するための鋳型に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a mold for casting vane parts such as impellers for pumps.

【0002】[0002]

【従来の技術】ポンプ用インペラなどの羽根部品を鋳造
するための鋳型を造型する場合、通常は、羽根形状に等
しい模型の隙間に砂等の鋳型材料を充填して模型を引き
抜くいわゆる引き抜き造型法が用いられる。羽根形状が
3次元的にひねられていて造型後の模型の引き抜きが不
可能な場合は、ロストワックス法のような消失模型法
か、模型をゴム等の弾性体で成形して模型を変形させつ
つ鋳型から引き抜く弾性模型法が一般に用いられる。し
かし、消失模型法は鋳造数と同数の模型を必要とするの
で模型費が高く付き、弾性模型法は造型時の鋳型材料の
重量で模型が変形するので鋳造精度が損われる。そこ
で、上述した各造型法に代え、複数の中子を組合せて鋳
造すべき羽根部品の羽根形状に応じた空隙を形成する寄
せ型法が用いられることがある。
2. Description of the Related Art When molding a mold for casting impeller parts for pumps or the like, usually, a so-called pultrusion molding method in which a mold material such as sand is filled in a gap of a model having the same blade shape and the model is extracted. Is used. If the blade shape is three-dimensionally twisted and it is impossible to pull out the model after molding, use the vanishing model method like the lost wax method or deform the model by molding it with an elastic body such as rubber. The elastic model method of pulling out from the mold is generally used. However, the disappearance model method requires the same number of models as the number of castings, so that the model cost is high, and the elastic model method deteriorates the casting accuracy because the model is deformed by the weight of the mold material at the time of molding. Therefore, instead of each of the above-described molding methods, there is a case where an approach molding method is used in which a plurality of cores are combined to form a void according to the blade shape of the blade component to be cast.

【0003】図16および図17は上述した寄せ型法に
よる鋳型の一例を示すものである。この鋳型は、一対の
下型Lおよび上型Uの間に複数の中子Nが周方向に並べ
て介装されたもので、不図示の湯口から注湯される溶湯
が各中子Nの間の羽根用空隙Sbに回り込むことによ
り、図18に示すように、回転軸の回りに螺旋状に延び
る複数枚(図では5枚)の羽根Bを備えたインペラIが
鋳造される。中子Nは、鋳造すべきインペラIの羽根間
の隙間Cに対応した形状の本体Mと、本体Mの両端に設
けられた幅木Hi,Ho(図16の斜線部分)とを有す
るもので、幅木Hi,Hoが下型Lないしは上型Uと嵌
合して各中子Nが所定の位置に保持される。このような
寄せ型法では、同一の中子取りから多数の中子Nを造型
できるので、模型の製作費用が大幅に低減される。
16 and 17 show an example of a mold by the above-mentioned gathering type method. In this mold, a plurality of cores N are arranged side by side in the circumferential direction between a pair of lower mold L and upper mold U, and molten metal poured from a spout (not shown) is present between the cores N. As shown in FIG. 18, the impeller I including a plurality of (five in the figure) blades B spirally extending around the rotation axis is cast by wrapping around the blade void Sb. The core N has a main body M having a shape corresponding to the gap C between the blades of the impeller I to be cast, and baseboards Hi and Ho (hatched portions in FIG. 16) provided at both ends of the main body M. , The skirting boards Hi, Ho are fitted to the lower mold L or the upper mold U to hold each core N at a predetermined position. In such a grouping method, a large number of cores N can be molded from the same core taker, so that the cost of manufacturing a model is significantly reduced.

【0004】[0004]

【発明が解決しようとする課題】ところが、上述した寄
せ型法では、鋳造すべき羽根BがインペラIの回転軸の
回りに3次元的にひねられているので、図17に示すよ
うに中子Nを周方向へずらしつつ順にセットしてゆく
と、最後の中子N5を収納すべき隙間C5の上部に最初
にセットした中子N1が突き出てしまい、最後の中子N
5を回転軸方向に下ろして下型Lに収めることが不可能
となる。この場合、最後の中子N5を羽根の捩れ方向に
沿ってひねりつつセットすることも考えられるが、中心
側の幅木Hiが邪魔して入らない。
However, in the above-mentioned approach-type method, since the blade B to be cast is three-dimensionally twisted around the rotation axis of the impeller I, as shown in FIG. When N is shifted in the circumferential direction and set in order, the first set core N1 protrudes above the gap C5 in which the last core N5 should be stored, and the last core N
It becomes impossible to lower 5 in the direction of the rotation axis and fit it in the lower mold L. In this case, it is conceivable to set the last core N5 while twisting it along the direction of twist of the blades, but the skirting board Hi on the center side does not get in the way.

【0005】そこで、上記の中子Nをセットするには、
すべての中子Nを実際の組み付け径よりも大きな円を描
くように組合せ(このときは中子N同士の間に大きな隙
間が空く)、しかる後、各中子Nを同時に径方向中心側
へ寄せ集める必要があり、要領良く作業を進めるには相
当の熟練を要する。しかも、この寄せ集め手順では、中
子Nの相互のバランスが取り難いので中子Nの位置決め
精度が悪く、鋳造精度が劣化するおそれが大きい。仮に
幅木Hiがなかったとしても、羽根Bの回転軸方向に対
するひねり度合いや回転軸回りの巻き付き長さが増加す
れば、やはり中子Nの中心側が邪魔となって中子Nを寄
せ合わせることが困難となる。
Therefore, to set the above core N,
Combine all cores N so as to draw a circle larger than the actual assembly diameter (in this case, a large gap will be created between the cores N), and then each core N will be moved to the radial center side at the same time. It is necessary to gather them together, and considerable skill is required to carry out the work well. Moreover, in this gathering procedure, since it is difficult to balance the cores N with each other, the positioning accuracy of the cores N is poor, and the casting accuracy is likely to deteriorate. Even if there is no skirting board Hi, if the degree of twist of the blade B with respect to the rotation axis direction and the winding length around the rotation axis increase, the center side of the core N still interferes and the cores N are brought together. Will be difficult.

【0006】本発明の目的は、模型製作費が安価で、熟
練を要することなく容易に造型でき、鋳造精度も高くで
きる羽根鋳造用鋳型を提供することにある。
An object of the present invention is to provide a blade casting mold which is inexpensive in model production, can be easily molded without requiring skill, and has high casting precision.

【0007】[0007]

【課題を解決するための手段】一実施例を示す図1に対
応付けて説明すると、本発明は、複数の型部材10,2
0,21を組合せてこれら型部材10,20,21の間
に鋳造すべき羽根部品の羽根形状に応じた空隙Sbを形
成する羽根鋳造用鋳型1に適用される。そして、上述し
た目的は、空隙Sbを形成する複数の型部材10,2
0,21のうち少なくとも一の型部材(10,20)
を、各型部材10,20,21が羽根部品の回転軸方向
の一方の側から順に組合せ可能となるように空隙Sbに
臨む面203の途中で分割することにより達成される。
DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring to FIG. 1 showing an embodiment, the present invention will be described with reference to a plurality of mold members 10, 2.
It is applied to the blade casting mold 1 which forms a space Sb corresponding to the blade shape of the blade component to be cast between these mold members 10, 20, 21 by combining 0 and 21. And the above-mentioned purpose has a plurality of mold members 10 and 2 forming the void Sb.
At least one mold member (10, 20) of 0, 21
Is achieved by dividing each of the mold members 10, 20, 21 in the middle of the surface 203 facing the space Sb so that the mold members can be combined sequentially from one side in the rotation axis direction of the blade component.

【0008】[0008]

【作用】空隙Sbに臨む面203の途中で分割された型
部材(10,20)のうち、空隙Sbの中心側を形成す
る部分10を先に組み付けておけば、空隙Sbの外周側
を形成する部分20は、中心側の部分10に邪魔される
ことなく、後から型部材10,20,21同士の隙間に
挿入できる。
If the part 10 forming the center side of the space Sb among the mold members (10, 20) divided in the middle of the surface 203 facing the space Sb is assembled first, the outer side of the space Sb is formed. The part 20 to be inserted can be inserted into the gap between the mold members 10, 20, 21 later without being disturbed by the part 10 on the center side.

【0009】なお、本発明の構成を説明する上記課題を
解決するための手段と作用の項では、本発明を分かり易
くするために実施例の図を用いたが、これにより本発明
が実施例に限定されるものではない。
Incidentally, in the section of means and action for solving the above-mentioned problems for explaining the constitution of the present invention, the drawings of the embodiments are used to make the present invention easy to understand. It is not limited to.

【0010】[0010]

【実施例】以下、図1〜図12を参照して、本発明の一
実施例を説明する。なお、本実施例の鋳型は上述した図
18に示す5枚羽根のインペラIを鋳造するためのもの
であり、インペラIに関する構成は図18を参照するも
のとする。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of the present invention will be described below with reference to FIGS. The mold of this embodiment is for casting the above-mentioned five-blade impeller I shown in FIG. 18, and the configuration relating to the impeller I is to refer to FIG.

【0011】図1および図2に示すように、本実施例の
鋳型1では、鋳物砂などの鋳型材料によって成形された
5つの寄せ型10が鋳型中心軸Xの回りに放射状に配置
されるとともに、寄せ型10と同一材料で成形された4
つの中子20および単一の組中子21が寄せ型10上に
設置されて、鋳型1の中心軸Xの回りにインペラIの羽
根Bの形状に応じた5つの羽根用空隙Sbが形成され
る。また、中子20,21の上部に上型30が被せられ
て、上型30と寄せ型10および中子20,21との間
にインペラIのボス部(図18では省略)に応じた円錐
形状のボス用空隙Scが形成される。
As shown in FIG. 1 and FIG. 2, in the mold 1 of this embodiment, five shifting molds 10 formed of a molding material such as foundry sand are arranged radially around the central axis X of the mold. , Molded from the same material as the grouping die 10 4
One core 20 and a single set core 21 are installed on the shifting mold 10 to form five blade voids Sb around the center axis X of the mold 1 according to the shape of the blade B of the impeller I. It Further, the upper mold 30 is put on the upper parts of the cores 20 and 21, and a cone corresponding to the boss portion (not shown in FIG. 18) of the impeller I is provided between the upper mold 30 and the shifting mold 10 and the cores 20 and 21. A shaped boss space Sc is formed.

【0012】図1〜図4に示すように、寄せ型10は鋳
型中心軸Xと直交する下面100と、鋳型中心軸Xと平
行な一対の側面101と、鋳型中心軸Xを中心として円
筒面状に延びる外周面102とを備えた略扇形状をな
す。側面101の挟み角は360゜を羽根Bの枚数で除
した値(実施例の場合は72゜)に設定されている。寄
せ型10の上面側にはボス用空隙Scを形成する段付き
面103およびボス形成面104と、羽根用空隙Sbを
形成する羽根形成面105が形成されている。羽根形成
面105は鋳造すべき羽根Bの反作用面(図29の凹面
側)の中心側に合わせて湾曲し、その外周側には、寄せ
型10の外周へ向って上り勾配となるテーパ面106を
介して下面100と平行な中子支持面107が連設され
ている。
As shown in FIGS. 1 to 4, the shift mold 10 includes a lower surface 100 orthogonal to the mold center axis X, a pair of side surfaces 101 parallel to the mold center axis X, and a cylindrical surface centered on the mold center axis X. And a substantially fan-shaped outer peripheral surface 102. The sandwiching angle of the side surface 101 is set to a value obtained by dividing 360 ° by the number of blades B (72 ° in the case of the embodiment). A stepped surface 103 and a boss forming surface 104 that form a boss space Sc, and a blade forming surface 105 that forms a blade space Sb are formed on the upper surface side of the gathering die 10. The blade forming surface 105 is curved in accordance with the center side of the reaction surface (concave surface side in FIG. 29) of the blade B to be cast, and on the outer peripheral side thereof, a tapered surface 106 having an upward slope toward the outer periphery of the shifting die 10. A core support surface 107 parallel to the lower surface 100 is continuously provided via the.

【0013】図1、図2、図5〜図7に示すように、中
子20は、中子本体200と、中子本体200の外周に
配置される幅木210,220とを備える。中子本体2
00は、ボス用空隙Scを形成する湾曲面201と、羽
根Bの作用面(図29の凸面側)に合わせて湾曲する第
1の羽根形成面202と、羽根Bの反作用面の外周側に
合わせて湾曲する第2の羽根形成面203とを備える。
羽根形成面202,203の間の肉厚は、羽根Bの隙間
Cがその中心部へ向うほど狭まるのに対応して、中子本
体200の外周から内周側の先端面204へ向うほど薄
くなる。
As shown in FIGS. 1, 2, and 5 to 7, the core 20 includes a core body 200 and skirting boards 210 and 220 arranged on the outer periphery of the core body 200. Core body 2
00 is on the outer peripheral side of the reaction surface of the blade B, and the curved surface 201 forming the boss space Sc, the first blade formation surface 202 which is curved to match the operation surface of the blade B (the convex surface side of FIG. 29). And a second blade forming surface 203 that is curved together.
The wall thickness between the blade forming surfaces 202 and 203 is thinner as the gap C of the blade B is narrower toward the center thereof, and is thinner from the outer periphery of the core body 200 toward the inner peripheral end face 204. Become.

【0014】中子本体200の先端面204は寄せ型1
0の側面101と当接可能とされる(図1、図2参
照)。これらが当接したとき寄せ型10の羽根形成面1
05と中子20の第2の羽根形成面203とが連続して
羽根Bの反作用面に対応した一の湾曲面が形成される。
なお、205は寄せ型10の側面101に形成した凹部
108と嵌合して中子20の内周側を位置決めする凸
部、206はテーパ面であって、このテーパ面206の
幅木220よりも下方へ突出する部分は寄せ型10のテ
ーパ面106と当接し、残る部分は隣接する中子20の
テーパ面207と当接する(図2の右側参照)。
The front end surface 204 of the core body 200 is a shift type 1
It can be brought into contact with the side surface 101 of 0 (see FIGS. 1 and 2). When these abut, the blade forming surface 1 of the pulling die 10
05 and the second blade forming surface 203 of the core 20 continuously form one curved surface corresponding to the reaction surface of the blade B.
Numeral 205 is a convex portion that fits with the concave portion 108 formed on the side surface 101 of the closing die 10 to position the inner peripheral side of the core 20, and 206 is a tapered surface. Also, the portion that protrudes downward contacts the tapered surface 106 of the shifting mold 10, and the remaining portion contacts the tapered surface 207 of the adjacent core 20 (see the right side of FIG. 2).

【0015】幅木210,220は鋳型中心軸Xを中心
として弧状に湾曲し、鋳型中心軸Xの方向に段違いに配
置されるとともに、上段の幅木210が中子本体200
の湾曲面201の外周に沿って延び、下段の幅木220
が第2の羽根形成面203の外周に沿って延びるように
周方向へずらして設けられる。幅木210,220の鋳
型中心軸Xに対する中心角は、いずれも360゜を羽根
Bの枚数で除した値(実施例の場合は72゜)に設定さ
れる。
The skirting boards 210 and 220 are curved in an arc shape around the center axis X of the mold and are arranged in different steps in the direction of the center axis X of the mold.
Extending along the outer periphery of the curved surface 201 of the
Are provided so as to be shifted in the circumferential direction so as to extend along the outer circumference of the second blade forming surface 203. The center angles of the skirting boards 210 and 220 with respect to the center axis X of the mold are both set to a value obtained by dividing 360 ° by the number of blades B (72 ° in the case of the embodiment).

【0016】幅木210,220の上面211,221
および下面212,222は鋳型中心軸Xと直交する平
面に形成され、上段の幅木210の下面212と下段の
幅木220の上面221とは同一高さに形成される。こ
れにより、一の中子20の幅木210の下面212と、
他の中子20の幅木220の上面221とを当接させた
とき、幅木210の上面211同士が面一となり、幅木
220の下面222同士が面一となる。中子20の外周
面230は鋳型中心軸Xを中心とする円筒面状に形成さ
れ、その曲率半径は寄せ型10の外周面102と等しく
される。
Upper surfaces 211 and 221 of the skirting boards 210 and 220
The lower surfaces 212 and 222 are formed on a plane orthogonal to the center axis X of the mold, and the lower surface 212 of the upper skirting board 210 and the upper surface 221 of the lower skirting board 220 are formed at the same height. Thereby, the lower surface 212 of the skirting board 210 of the one core 20,
When the upper surfaces 221 of the skirting boards 220 of the other cores 20 are brought into contact with each other, the upper surfaces 211 of the skirting boards 210 are flush with each other and the lower surfaces 222 of the skirting boards 220 are flush with each other. The outer peripheral surface 230 of the core 20 is formed into a cylindrical surface centered on the center axis X of the mold, and its radius of curvature is made equal to that of the outer peripheral surface 102 of the shifting mold 10.

【0017】組中子21は、寄せ型10の合わせ面の延
長上に設けた分割面22a,23a上で分割可能な一対
の分割片22,23によって構成され、その組合せ状態
での形状は中子20と全く同一である。すなわち、組中
子21は、中子20を図5および図6の2点鎖線Lc上
で分割したものである。したがって、本明細書では組中
子21の各構成要素について中子20の対応部分と同一
符号を付し、説明を省略する。
The set core 21 is composed of a pair of split pieces 22 and 23 that can be split on split surfaces 22a and 23a provided on the extension of the mating surface of the gathering die 10, and the shape in the combined state is medium. It is exactly the same as the child 20. That is, the set core 21 is obtained by dividing the core 20 on the alternate long and two short dashes line Lc in FIGS. 5 and 6. Therefore, in the present specification, each component of the set core 21 is designated by the same reference numeral as that of the corresponding part of the core 20, and description thereof is omitted.

【0018】次に鋳型1の造型手順を図8〜図11を参
照して説明する。鋳型1を造型するには、まず図8およ
び図11に示すように5つの寄せ型10を鋳型中心軸X
の回りに寄せ合わせて下型を造型する。ついで、図9お
よび図11に示すように組中子21の分割片22をその
第2の羽根形成面203がいずれか一の寄せ型10の羽
根形成面105と連なるように位置決めしつつ寄せ型1
0上に載置する。このとき、分割片22の下段の幅木2
20の下面222が寄せ型10の中子支持面107に当
接して分割片22が支持される(図2の左側参照)。
Next, the procedure for molding the mold 1 will be described with reference to FIGS. In order to mold the mold 1, first, as shown in FIG. 8 and FIG.
The lower mold is made by gathering around. Next, as shown in FIGS. 9 and 11, the divided pieces 22 of the core assembly 21 are positioned so that the second blade forming surface 203 thereof is continuous with the blade forming surface 105 of any one of the forming molds 10. 1
Place on top of 0. At this time, the skirting board 2 in the lower stage of the split piece 22
The lower surface 222 of 20 comes into contact with the core support surface 107 of the shifting die 10 to support the split piece 22 (see the left side of FIG. 2).

【0019】ついで、図10および図11に示すよう
に、分割片22の第2の羽根形成面203および幅木2
20の側方に中子20を下ろしてその第2の羽根形成面
203が対応する寄せ型10の羽根形成面105に連な
るように位置決めする。このとき、分割片22の幅木2
20の上面221と新たな中子20の上段の幅木210
の下面212が当接して中子20が保持される。これに
より、中子20の第1の羽根形成面202と、分割片2
2の第2の羽根形成面203と、これに連なる寄せ型1
0の羽根形成面105とによって一の羽根用空隙Sbが
形成される。
Next, as shown in FIGS. 10 and 11, the second blade forming surface 203 of the divided piece 22 and the skirting board 2 are formed.
The core 20 is lowered to the side of 20 and positioned so that the second blade forming surface 203 is continuous with the corresponding blade forming surface 105 of the closing die 10. At this time, the skirting board 2 of the divided piece 22
20 upper surface 221 and new core 20 upper skirting board 210
The lower surface 212 of the core contacts the core 20, and the core 20 is held. As a result, the first blade forming surface 202 of the core 20 and the divided piece 2
2nd blade formation surface 203 of 2 and gathering type 1 continuing to this
The blade forming surface 105 of 0 forms one blade space Sb.

【0020】以下同様に中子20の側方に新たな中子2
0をセットして、各中子20の第1の羽根形成面202
と、隣接する中子20の第2の羽根形成面203と、寄
せ型10の羽根形成面105によって羽根用空隙Sbを
順次形成する。4つの中子20をすべてセットして図1
0に示す状態となった後は、分割片22と中子20との
隙間Cに露出する第2の羽根形成面203と幅木220
の上面221を覆うように組中子21の分割片23をセ
ットする。この後、図2に2点鎖線で示すように中子2
0の上部に上型30を被せて、上型30の表面と各中子
20,21の湾曲面201から寄せ型10のボス形成面
104,段付き面103との間にかけてボス用空隙Sc
を形成する。そして、不図示の湯口やガス穴を形成して
鋳型1の造型を完了する。
Similarly, a new core 2 is provided on the side of the core 20.
0 is set, and the first blade forming surface 202 of each core 20 is set.
Then, the second blade forming surface 203 of the core 20 and the blade forming surface 105 of the pulling die 10 which are adjacent to each other sequentially form the blade space Sb. Fig. 1 with all four cores 20 set
After the state shown in 0 is reached, the second blade forming surface 203 and the skirting board 220 exposed in the gap C between the split piece 22 and the core 20.
The divided pieces 23 of the core assembly 21 are set so as to cover the upper surface 221 of the. After this, as shown by the two-dot chain line in FIG.
0 is covered with the upper mold 30, and the boss space Sc is formed between the surface of the upper mold 30 and the curved surface 201 of each core 20, 21 to the boss forming surface 104 of the shift mold 10 and the stepped surface 103.
To form. Then, a sprue and gas holes (not shown) are formed to complete the molding of the mold 1.

【0021】鋳型1を羽根用空隙Sb上で直線的に展開
した断面を図12に示す。この図から明らかなように、
本実施例では従来一体であった寄せ型10と中子20,
21が分割可能とされているので、各寄せ型10を寄せ
合わせた上で組中子21の分割片22から順に中子2
0,21をセットして最後に分割片23をセットすれ
ば、寄せ型10および中子20,21をすべて鋳型中心
軸Xの一方の側から組合せることができ、中子20をひ
ねったり複数の中子20を同時に寄せ合わせたりする必
要がなくなる。したがって、熟練を要しなくとも容易に
鋳型1を造型でき、寄せ型10や中子20,21の位置
決め精度を高めて鋳造精度の向上を図り得る。寄せ型1
0や中子20,21の模型を一旦用意すれば後は模型を
製造する必要がないので、従来の寄せ型法と同様に模型
費が安価で済む。中子20,21と寄せ型10が別体な
ので軽量化され、自重による変形や変位が防止されて鋳
造精度が一層高まる。
FIG. 12 shows a cross section of the mold 1 linearly developed on the blade space Sb. As you can see from this figure,
In this embodiment, the grouping mold 10 and the core 20, which are conventionally integrated,
Since 21 is separable, the cores 2 are arranged in order from the divided pieces 22 of the set core 21 after the molds 10 are brought together.
By setting 0 and 21, and finally setting the divided piece 23, the gathering mold 10 and the cores 20 and 21 can all be combined from one side of the mold central axis X, and the core 20 can be twisted or plural. There is no need to bring the inner cores 20 together. Therefore, the mold 1 can be easily molded without requiring skill, and the positioning accuracy of the shifting mold 10 and the cores 20 and 21 can be improved to improve the casting accuracy. Type 1
Once the models of 0 and cores 20 and 21 are prepared, it is not necessary to manufacture the models thereafter, so that the model cost is low as in the conventional grouping method. Since the cores 20 and 21 and the shifting mold 10 are separate bodies, the weight is reduced, deformation and displacement due to their own weight are prevented, and casting precision is further enhanced.

【0022】本実施例では特に中子20,21の幅木2
10,220を鋳型中心軸Xの方向に2段に設け、隣接
する中子20,21の幅木210,220同士を鋳型中
心軸Xの方向に重ね合わせたので、中子20,21の位
置決め精度および安定性が一層高まる。幅木210,2
20のいずれか一方のみとした場合は、幅木の中心角が
羽根Bの枚数すなわち中子20,21の周方向の分割数
で決まってしまうため、幅木の周方向長さが羽根形成面
202,203の周方向長さに比して不足し、中子2
0,21の安定性が損われて鋳造精度が劣化するおそれ
がある。また、寄せ型10で下型を構成したため、鋳型
1を構成する部品数が減少し、造型コストが削減され
る。
In this embodiment, especially the skirting board 2 of the cores 20 and 21
Positioning of the cores 20 and 21 is made possible by providing 10 and 220 in two stages in the direction of the mold center axis X and overlapping the skirting boards 210 and 220 of the adjacent cores 20 and 21 in the direction of the mold center axis X. Accuracy and stability are further enhanced. Baseboard 210,2
When only one of the 20 is selected, the central angle of the skirting board is determined by the number of blades B, that is, the number of circumferentially divided cores 20 and 21, so that the circumferential length of the skirting board is the blade forming surface. Compared with the circumferential length of 202, 203, it is insufficient and the core 2
There is a risk that the stability of 0, 21 will be impaired and the casting accuracy will deteriorate. Further, since the lower mold is constituted by the gathering mold 10, the number of parts constituting the mold 1 is reduced and the molding cost is reduced.

【0023】なお、本実施例では、すべての中子20,
21を寄せ型10に対して分割可能に設けたが、図13
に示すように一の中子20と寄せ型10とを分割可能と
し、残りの中子を寄せ型と一体の中子20A,21Aと
しても、すべての中子を鋳型中心軸Xの一方の側から順
に組合せできる。図14に示すように、組中子を寄せ型
10とのみ分割可能な中子20Bに変更しても、羽根用
空隙Sbに沿って中子20Bをスライドさせれば最後の
中子20Bもセットできるので、すべての中子を同時に
セットする従来よりも造型が容易である。図14の例で
は、中子20Bを羽根用空隙Sbの方向にスライドさせ
るときの障害とならないように、幅木240の両端24
1,242を羽根用空隙Sbに沿って傾斜させる必要が
ある。実施例では寄せ型10を組合せて鋳型1の下型と
したが、図15に示すように下型40を別途設けてもよ
い。寄せ型10を分割することなく一体に形成して下型
としてもよい。
In this embodiment, all the cores 20,
Although 21 is provided so as to be separable from the grouping mold 10, FIG.
As shown in Fig. 1, one core 20 and the centering die 10 can be divided, and the remaining cores are cores 20A and 21A integrated with the centering die, but all the cores are on one side of the mold central axis X. Can be combined in order. As shown in FIG. 14, even if the set core is changed to the core 20B that can be divided only with the grouping die 10, if the core 20B is slid along the blade gap Sb, the last core 20B is also set. Since it is possible, molding is easier than the conventional method in which all cores are set at the same time. In the example of FIG. 14, both ends 24 of the skirting board 240 are provided so as not to obstruct the sliding of the core 20B in the direction of the blade gap Sb.
It is necessary to incline 1 and 242 along the blade gap Sb. Although the lower mold 40 is combined with the lower mold 40 in the embodiment, a lower mold 40 may be separately provided as shown in FIG. The lower mold may be formed by integrally forming the grouping mold 10 without dividing it.

【0024】以上の実施例では、一の中子20,21と
一の寄せ型10との組合せが一の型部材を構成する。ま
た、鋳型中心軸Xが羽根部材の回転軸に相当する。
In the above embodiment, the combination of the one core 20 or 21 and the one gathering die 10 constitutes one die member. The mold center axis X corresponds to the rotation axis of the blade member.

【0025】[0025]

【発明の効果】以上説明したように、本発明によれば、
鋳造すべき羽根形状に対応した空隙を形成する型部材
を、羽根部品の回転軸方向の一方の側から順に組合せる
ことができるので、熟練を要することなく容易に造型で
き、鋳造精度を高め得る。模型製作費が安価という寄せ
型法の長所も何等損われない。
As described above, according to the present invention,
Mold members that form voids corresponding to the shape of the blade to be cast can be combined in order from one side in the direction of the rotation axis of the blade component, so molding can be easily performed without skill, and casting accuracy can be improved. . The advantage of the group-type method that the model production cost is low is not damaged at all.

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

【図1】本発明の実施例の鋳型の平面図。FIG. 1 is a plan view of a mold according to an embodiment of the present invention.

【図2】図1のII−II線における断面図。FIG. 2 is a sectional view taken along line II-II of FIG.

【図3】実施例の寄せ型の平面図。FIG. 3 is a plan view of a grouping type according to the embodiment.

【図4】図3のIV方向からの側面図。FIG. 4 is a side view from the IV direction in FIG.

【図5】実施例の中子の平面図。FIG. 5 is a plan view of the core of the embodiment.

【図6】図5のVI方向からの側面図。FIG. 6 is a side view from the VI direction in FIG.

【図7】図6のVII−VII線における断面図。7 is a sectional view taken along line VII-VII of FIG.

【図8】実施例で寄せ型を寄せ合わせたときの平面図。FIG. 8 is a plan view of a case where the molds are brought together in the embodiment.

【図9】実施例で最初の中子をセットした状態を示す平
面図。
FIG. 9 is a plan view showing a state in which the first core is set in the embodiment.

【図10】実施例で寄せ型上に最後の中子をセットする
前の状態を示す平面図。
FIG. 10 is a plan view showing a state before the last core is set on the closing mold in the embodiment.

【図11】実施例の中子の組み付け手順を示す斜視図。FIG. 11 is a perspective view showing a procedure for assembling the core of the embodiment.

【図12】図1の鋳型を羽根用空隙上で直線的に展開し
た断面図。
FIG. 12 is a cross-sectional view of the mold of FIG. 1 linearly developed on a blade gap.

【図13】中子の分割状態を変更した変形例を示す図。FIG. 13 is a diagram showing a modified example in which the split state of the core is changed.

【図14】中子の分割状態を変更した他の変形例を示す
図。
FIG. 14 is a diagram showing another modification in which the split state of the core is changed.

【図15】寄せ型と別に下型を設けた変形例を示す図。FIG. 15 is a view showing a modified example in which a lower die is provided separately from the shifting die.

【図16】従来の鋳型構造を示す断面図。FIG. 16 is a cross-sectional view showing a conventional mold structure.

【図17】従来の鋳型を図16の1点鎖線Y上で展開し
た断面図。
FIG. 17 is a cross-sectional view of the conventional mold developed on the alternate long and short dash line Y in FIG.

【図18】鋳造すべき羽根の一例を示す平面図。FIG. 18 is a plan view showing an example of a blade to be cast.

【符号の説明】[Explanation of symbols]

1 鋳型 10 寄せ型 20,21 中子 105 寄せ型の羽根形成面 202 中子の第1の羽根形成面 203 中子の第2の羽根形成面 B インペラの羽根 I インペラ Sb 羽根用空隙 X 鋳型中心軸 DESCRIPTION OF SYMBOLS 1 mold 10 closing type 20,21 core 105 closing type blade forming surface 202 1st blade forming surface of core 203 2nd blade forming surface of core B impeller blade I impeller Sb blade gap X mold center axis

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 複数の型部材を組合せてこれら型部材の
間に鋳造すべき羽根部品の羽根形状に応じた空隙を形成
する羽根鋳造用鋳型において、 前記空隙を形成する複数の型部材のうち少なくとも一の
型部材を、各型部材が前記羽根部品の回転軸方向の一方
の側から順に組合せ可能となるように前記空隙に臨む面
の途中で分割したことを特徴とする羽根鋳造用鋳型。
1. A blade casting mold that combines a plurality of mold members to form a gap between the mold members according to the shape of a blade component to be cast, wherein among the plurality of mold members that form the gap. A blade casting mold characterized in that at least one mold member is divided in the middle of a surface facing the gap so that each mold member can be sequentially combined from one side in the rotation axis direction of the blade component.
JP4336068A 1992-12-16 1992-12-16 Blade casting mold Expired - Fee Related JP2633162B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4336068A JP2633162B2 (en) 1992-12-16 1992-12-16 Blade casting mold

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4336068A JP2633162B2 (en) 1992-12-16 1992-12-16 Blade casting mold

Publications (2)

Publication Number Publication Date
JPH06182493A true JPH06182493A (en) 1994-07-05
JP2633162B2 JP2633162B2 (en) 1997-07-23

Family

ID=18295366

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4336068A Expired - Fee Related JP2633162B2 (en) 1992-12-16 1992-12-16 Blade casting mold

Country Status (1)

Country Link
JP (1) JP2633162B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06328192A (en) * 1993-05-21 1994-11-29 Ebara Corp Manufacture of casting mold for pump impeller

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5668549A (en) * 1979-11-06 1981-06-09 Kubota Ltd Casting method of casing for axial-flow and oblique-flow pump

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5668549A (en) * 1979-11-06 1981-06-09 Kubota Ltd Casting method of casing for axial-flow and oblique-flow pump

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06328192A (en) * 1993-05-21 1994-11-29 Ebara Corp Manufacture of casting mold for pump impeller

Also Published As

Publication number Publication date
JP2633162B2 (en) 1997-07-23

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