JPH01210165A - Cast-in method - Google Patents

Cast-in method

Info

Publication number
JPH01210165A
JPH01210165A JP3705588A JP3705588A JPH01210165A JP H01210165 A JPH01210165 A JP H01210165A JP 3705588 A JP3705588 A JP 3705588A JP 3705588 A JP3705588 A JP 3705588A JP H01210165 A JPH01210165 A JP H01210165A
Authority
JP
Japan
Prior art keywords
cast
hub
casting
blades
model
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
Application number
JP3705588A
Other languages
Japanese (ja)
Inventor
Atsushi Magata
曲田 淳
Toshio Tanaka
俊夫 田中
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.)
Komatsu Ltd
Original Assignee
Komatsu Ltd
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 Komatsu Ltd filed Critical Komatsu Ltd
Priority to JP3705588A priority Critical patent/JPH01210165A/en
Publication of JPH01210165A publication Critical patent/JPH01210165A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To improve strength and castability of a product by coat-forming a fitted assembling body with a material to be cast in and a pattern by a molding material and pouring molten metal into formed space part after removing the pattern from the molding material. CONSTITUTION:The material to be cast in having complicate shape of blade 10, etc., is manufactured with independent to a main body of hub 12, etc., to attach excess thickness for casting 10A. The blades 10 are fitted into slits 14A in the pattern 14 of rubber-made, etc., having the same shape as the hub 12, to form the assembling body. Successively, by coat-forming and molding the assembling body with gypsum, etc., the gypsum mold 16 is formed and also cavity 18 remaining the blades 10 is formed. Further, molten metal for forming material of the hub 12 is poured into the cavity 18 to obtain the product 20, in which the blades 10 is cast in. As the material to be cast in is preformed with the high strength material, the strength of the product 20 is improved and as the part having complicate shape and insufficient flowing is cast in, the castability is improved.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明はエンジンの過給機やタービン型機関の:177
”L/ツサ用プロアインペラのように高強度が必要な複
雑形状部品を低コストで製造できる鋳ぐるみ方法に関す
る。
[Detailed Description of the Invention] [Industrial Application Field] The present invention is applicable to engine superchargers and turbine type engines.
``This article relates to a casting method that allows complex-shaped parts that require high strength, such as pro-ain impellers for L/tubers, to be manufactured at low cost.

〔従来の技術〕[Conventional technology]

従来、プロアインペラのように高強度が必要で、しかも
複雑形状の部品を製作する場合は、一体鋳造法が採用さ
れており、例えば日本鋳物協会編「鋳物便覧(改訂4版
)」の1031〜1069真に記載されているように、
ロウ型、石膏型、セラミック型等の鋳型を利用して製造
していた。
Traditionally, when manufacturing parts that require high strength and have complex shapes, such as pro-ain impellers, the monolithic casting method has been adopted. As stated in 1069,
They were manufactured using molds such as wax molds, plaster molds, and ceramic molds.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

ところが、上記従来の一体鋳造方法では、その性質とし
て製品の材質が一様となって機械強度が一様となるもの
の、プロアインペラのような複雑形状部品では鋳造性が
良好なアルミ合金で製造されるので、通常、引っ張り強
度が35kgf/c−程度までの製品しか製造できなか
った。このため疲労強度上から高温、高回転に充分耐え
られるものと言い難かった。特に、プロアインペラはそ
の機関効率、出力、特性を決める重要な部品であるため
苛酷な条件下で使用されるようになっており、より高回
転化、軽量化、吸気温度の高温化が要望され、高強度材
によるプロアインペラの製造法を確立する必要があった
However, with the conventional monolithic casting method described above, although the material of the product is uniform and the mechanical strength is uniform, parts with complex shapes such as pro-air impellers cannot be manufactured from aluminum alloy, which has good castability. Therefore, normally only products with a tensile strength of up to about 35 kgf/c- could be manufactured. For this reason, it was difficult to say that it could sufficiently withstand high temperatures and high rotations from the viewpoint of fatigue strength. In particular, the pro-air impeller is an important component that determines engine efficiency, output, and characteristics, so it is used under harsh conditions, and there is a demand for higher rotation speeds, lighter weight, and higher intake air temperatures. , it was necessary to establish a manufacturing method for pro-ain impellers using high-strength materials.

本発明は上記従来の問題点に着目し、強度が高く複雑な
インペラ形状でも簡単に製作することのできる鋳ぐるみ
方法を提供することを目的とする。
The present invention has focused on the above-mentioned conventional problems, and an object of the present invention is to provide a casting method that has high strength and can easily manufacture even a complex impeller shape.

〔課題を解決するための手段〕[Means to solve the problem]

上記目的を達成するために、本発明に係る鋳ぐるみ方法
は、鋳ぐるみ材と同形の模型に形成された嵌合部に被鋳
ぐるみ材を嵌合装着し、前記模型と被鋳ぐるみ材との組
立体を型材にて被覆成形して固化し、この型材から前記
模型を除去することによって生じた空間部に鋳ぐるみ材
を注湯して鋳造するように構成した。
In order to achieve the above object, the casting method according to the present invention involves fitting a material to be cast into a fitting part formed on a model having the same shape as the material to be cast, and connecting the model and the material to be cast. The assembly was covered with molding material and solidified, and cast material was poured into the space created by removing the model from the molding material for casting.

〔作用〕[Effect]

上記構成によれば、複雑形状部品を一体鋳造するのでは
なく、この複雑形状部品を分割し易い箇所で複数個の部
分に分割し、当該分割部分のうち鋳ぐるみ材をこれと同
形の模型に置換しておく。
According to the above configuration, instead of integrally casting a complex-shaped part, the complex-shaped part is divided into a plurality of parts at easy-to-divide points, and the cast material of the divided parts is made into a model of the same shape. Replace it.

そしてこれと別に製造された被鋳ぐるみ材を前記模型に
設けた嵌合部に嵌合して一体化して組立体を構成し、こ
の組立体の外表面を液体の型材にて固めて鋳型を形成す
る。このとき、型材は被鋳ぐるみ材を一体的に固化する
。次いで、型材内に固定されている鋳ぐるみ材をこの型
材内に残し、模型のみを型材から除去すると、鋳ぐるみ
材と同形状の空間部が生じるので、これを型として鋳ぐ
るみ材を注湯することにより、空間部に露出した被鋳ぐ
るみ材を鋳ぐるんだ鋳造品が製造される。
Then, a separately manufactured cast material is fitted into a fitting part provided on the model and integrated to form an assembly, and the outer surface of this assembly is hardened with liquid molding material to form a mold. Form. At this time, the mold material solidifies the cast material integrally. Next, when only the model is removed from the mold, leaving the casting material fixed in the mold material inside, a space with the same shape as the casting material will be created, and this will be used as a mold to pour the casting material into. By doing so, a cast product is manufactured in which the cast material exposed in the space is cast.

〔実施例〕〔Example〕

以下に本発明に係る鋳ぐるみ方法の実施例を図面を参照
して詳細に説明する。
Embodiments of the casting method according to the present invention will be described in detail below with reference to the drawings.

第1図は実施例に係るプロアインペラの製造工程の説明
図である。プロアインペラを製作するにあたり、本実施
例ではまずプロアインペラの構成部材である羽根10を
ハブ12と独立して製作するようにしている。この羽根
10はアルミニウム合金の板材をプレスで打ち抜き成形
するものとしており(第1図(1))、このとき羽根1
0にはハブ12への鋳込み代10Aを設けるようにして
いる。
FIG. 1 is an explanatory diagram of the manufacturing process of a pro-air impeller according to an embodiment. In manufacturing the pro-ain impeller, in this embodiment, the blades 10, which are the constituent members of the pro-ain impeller, are first manufactured independently of the hub 12. This blade 10 is formed by stamping an aluminum alloy plate using a press (Fig. 1 (1)).
0 is provided with a casting allowance 10A for the hub 12.

一方、ハブ12と同形状のゴム形模型14を作製するよ
うにしている(第1図(2))、このゴム形模型14に
は羽根10の鋳込み代10Aを差し込むためのスリット
14Aが形成され、ハブ12の成形に際して最初ゴム形
模型14に羽根lOを差し込んでプロアインペラの組立
体を形成するものとしている(第1図(3))。そして
、次にはハブ12の型取りをなす。この型取りは前記模
型を反対向きにして、石膏により組立体と同形状の型を
取り(第1図(3))、羽根10を残してハブ12のゴ
ム形模型14のみを除去することによって行われる(第
1図(4))。このような石膏型16には前記したよう
に羽根10が残存し、ゴム形模型14を除去した空洞部
にはハブ12のキャビティ18が形成されると同時にこ
のキャビティ18には羽根10の鋳込み代10Aが臨ん
だものとなっている。
On the other hand, a rubber model 14 having the same shape as the hub 12 is manufactured (FIG. 1 (2)). A slit 14A is formed in this rubber model 14 for inserting the casting allowance 10A of the blade 10. When molding the hub 12, the blades 1O are first inserted into the rubber model 14 to form a pro-impeller assembly (FIG. 1 (3)). Next, a mold of the hub 12 is made. This molding is done by turning the model in the opposite direction, making a mold of the same shape as the assembly using plaster (Fig. 1 (3)), and removing only the rubber-shaped model 14 of the hub 12, leaving the blades 10. (Fig. 1 (4)). As described above, the blade 10 remains in such a plaster mold 16, and the cavity 18 of the hub 12 is formed in the hollow part from which the rubber model 14 has been removed. 10A has come.

このように羽根10を残した石膏型16に対し、ハブ1
2の成形材料であるアルミニウムの溶湯をキャビティ1
8内に重力鋳造、あるいは加圧鋳造にて注湯し、羽根1
0を鋳ぐるんだ状態でハブ12相当部を固化し、第1図
(5)に示されるような最終製品としてのプロアインペ
ラ20を得るのである。この場合、羽!110の材質を
アルミ材としたが、ハブ12の材質との関係で鋳ぐるみ
が可能でアレば、繊維強化アルミニウムや鉄鋼材等を用
いることはもちろん可能である。
In this way, the hub 1 is placed against the plaster mold 16 in which the blades 10 are left.
The molten aluminum, which is the molding material in step 2, is poured into cavity 1.
8 by gravity casting or pressure casting, and form the blade 1.
The part corresponding to the hub 12 is solidified in the state in which the 0 is cast, thereby obtaining a pro-air impeller 20 as a final product as shown in FIG. 1 (5). In this case, feathers! Although aluminum is used as the material of the hub 110, it is of course possible to use fiber-reinforced aluminum, steel, or the like if casting is possible in relation to the material of the hub 12.

このように、本実施例では、羽110を一枚一枚ハプ1
2とは別に予め製作しておくので、羽根IOの素材とし
て各種の材料を選択することができる。そしてこの羽根
10を含むハブ12のゴム形模型14を作成し、このゴ
ム形模型14を用いて石膏型16を取ることによりハブ
12のキャビティ18を形成し、羽根10を同時に鋳ぐ
るんで鋳造するようにしているので、ハブ12も任意の
材料で製造することができる。しかも、羽根10が独立
製作であるのでプロアインペラの形状が複雑であっても
一体鋳造の場合に問題となる羽根IOへの湯回りを考慮
する必要がないので簡単に製作することができる。
In this way, in this embodiment, the feathers 110 are attached to the hap 1 one by one.
Since it is manufactured in advance separately from 2, various materials can be selected as the material for the blade IO. Then, a rubber model 14 of the hub 12 including the blade 10 is created, and a plaster mold 16 is taken using this rubber model 14 to form the cavity 18 of the hub 12, and the blade 10 is cast at the same time. Therefore, the hub 12 can also be made of any material. Moreover, since the blades 10 are manufactured independently, even if the shape of the pro-ain impeller is complicated, there is no need to consider the hot water supply to the blade IO, which is a problem in the case of integral casting, so it can be manufactured easily.

なお、上記実施例では、ゴム形模型14を用いたが、羽
根10が平板等の単純な形状であれば、石膏型16に直
接羽根10を差し込むスリットを形成することによりゴ
ム形模型14を用いなくてもよくなる。
In the above embodiment, the rubber-shaped model 14 was used, but if the blade 10 has a simple shape such as a flat plate, the rubber-shaped model 14 can be used by forming a slit in which the blade 10 is inserted directly into the plaster mold 16. You'll be better off without it.

次に、第2図には第二実施例に係る鋳ぐるみ方法を示す
。この場合は、まずアルミ材を所定形状にプレス打ち抜
きした羽f110を所定個数製作しく同図(1))、当
該羽根10をインペラのハブ12と同じ形状に形成した
ロー型模型22(同図(2))のスリット24に羽[1
0の鋳込み代10A部分を差し込んで組立体を形成する
。次に前記ロー型模型22と羽根10の組立体に耐火物
をコーティングした後(同図(3))、上下を反転して
熱することにより脱ローすると(同図(4))、耐火物
中には羽根10が耐火物鋳型に固定された状態で保持さ
れ、羽根10のロー型模型22との鋳込み代10Aが突
き出されたキャビティ28が形成される(同図(3))
。そして、このキャビティ内にアルミの溶湯を流し込め
ば、羽根10を鋳ぐるんだハブ12が鋳造される。
Next, FIG. 2 shows a casting method according to a second embodiment. In this case, first, a predetermined number of blades f110 are made by press-punching an aluminum material into a predetermined shape ((1) in the same figure), and a low-type model 22 ((1) in the same figure) is made by forming the blades 10 into the same shape as the hub 12 of the impeller. 2)) Feather [1
Insert the casting allowance 10A portion of 0 to form an assembly. Next, after coating the assembly of the wax model 22 and the blade 10 with a refractory material ((3) in the same figure), the refractory material is removed by turning it upside down and heating it ((4) in the same figure). Inside, the blade 10 is held fixed to the refractory mold, and a cavity 28 is formed in which the casting allowance 10A of the blade 10 and the low model 22 is protruded ((3) in the same figure).
. Then, by pouring molten aluminum into this cavity, the hub 12 with the blades 10 cast therein is cast.

かかる実施例においても第一実施例と同様、羽根IOの
材質はハブ12の材質との関係で鋳ぐるみが可能であれ
ば、繊維強化アルミや鋳鋼材、あるいはプラスチック材
とすることができる。
In this embodiment, as in the first embodiment, the material of the vane IO may be fiber-reinforced aluminum, cast steel, or plastic, as long as it can be cast in relation to the material of the hub 12.

なお、上記いずれの実施例においても、ハブ12の鋳造
を加圧鋳造すれば重力鋳造に比べてより良質な製品が製
作できるのはいうまでもない。
In any of the embodiments described above, it goes without saying that if the hub 12 is cast by pressure casting, a product of higher quality can be manufactured than by gravity casting.

〔発明の効果〕〔Effect of the invention〕

以上説明したように、本発明によれば、鋳ぐるみ材と被
鋳ぐるみ材が別の材質であるため、複雑形状部品であっ
て寸法的に制約を受けるような部分があっても、その部
分を高強度材とすることができ、耐畜温性に優れた高強
度の製品を鋳造することができる。また、複雑形状部品
であっても、湯液れの悪い部分は別に蛎造しておき、そ
の復信の部分を鋳ぐるむことによって鋳造性の向上を図
ることができるので、従来のように鋳造性の良いアルミ
合金に限定されていた制限がなくなり、鉄系の材料を使
用することができ、かかる面によっても耐高温性で高強
度の製品を製作することができる効果が得られる。
As explained above, according to the present invention, the cast material and the cast material are made of different materials, so even if there is a part with a complex shape that is subject to dimensional restrictions, the part can be made into a high-strength material, and high-strength products with excellent storage temperature resistance can be cast. In addition, even for parts with complex shapes, it is possible to improve castability by separately molding the parts that have poor liquid flow and then casting the parts that need to be replaced. This eliminates the limitation of using aluminum alloys, which have good properties, and allows the use of iron-based materials, which also makes it possible to manufacture high-strength products with high temperature resistance.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は第一実施例に係る鋳ぐるみ方法の工程を示す説
明図、第2図は第二実施例に係る鋳ぐるみ方法の工程を
示す説明図である。 10・・・・・・羽根、12・・・・・・ハブ、14・
旧・・ゴム形模型、16・・・・・・石膏型、18・・
・・・・キャビティ、20・・・・・・プロアインペラ
。 代理人 弁理士 岡 1)和 喜
FIG. 1 is an explanatory diagram showing the steps of the casting method according to the first embodiment, and FIG. 2 is an explanatory diagram showing the steps of the casting method according to the second embodiment. 10...Blade, 12...Hub, 14.
Old... Rubber model, 16... Plaster mold, 18...
...Cavity, 20... Pro-ain impeller. Agent Patent Attorney Oka 1) Kazuki

Claims (1)

【特許請求の範囲】[Claims] (1)、鋳ぐるみ材と同形の模型に形成された嵌合部に
被鋳ぐるみ材を嵌合装着し、前記模型と被鋳ぐるみ材と
の組立体を型材にて被覆成形して固化し、この型材から
前記模型を除去することによって生じた空間部に鋳ぐる
み材を注湯して鋳造することを特徴とする鋳ぐるみ方法
(1) A material to be cast is fitted into a fitting part formed on a model having the same shape as the material to be cast, and the assembly of the model and material to be cast is covered with molding material and solidified. A casting method characterized in that casting is performed by pouring casting material into a space created by removing the model from the mold material.
JP3705588A 1988-02-19 1988-02-19 Cast-in method Pending JPH01210165A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3705588A JPH01210165A (en) 1988-02-19 1988-02-19 Cast-in method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3705588A JPH01210165A (en) 1988-02-19 1988-02-19 Cast-in method

Publications (1)

Publication Number Publication Date
JPH01210165A true JPH01210165A (en) 1989-08-23

Family

ID=12486887

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3705588A Pending JPH01210165A (en) 1988-02-19 1988-02-19 Cast-in method

Country Status (1)

Country Link
JP (1) JPH01210165A (en)

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