Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JPS6114907B2 - - Google Patents
[go: Go Back, main page]

JPS6114907B2 - - Google Patents

Info

Publication number
JPS6114907B2
JPS6114907B2 JP7829577A JP7829577A JPS6114907B2 JP S6114907 B2 JPS6114907 B2 JP S6114907B2 JP 7829577 A JP7829577 A JP 7829577A JP 7829577 A JP7829577 A JP 7829577A JP S6114907 B2 JPS6114907 B2 JP S6114907B2
Authority
JP
Japan
Prior art keywords
model
propeller
blade
boss
split
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.)
Expired
Application number
JP7829577A
Other languages
Japanese (ja)
Other versions
JPS5413194A (en
Inventor
Takeshi Ugata
Yasuji Morita
Masayuki Horiki
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.)
Kubota Corp
Original Assignee
Kubota 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 Kubota Corp filed Critical Kubota Corp
Priority to JP7829577A priority Critical patent/JPS5413194A/en
Publication of JPS5413194A publication Critical patent/JPS5413194A/en
Publication of JPS6114907B2 publication Critical patent/JPS6114907B2/ja
Granted legal-status Critical Current

Links

Landscapes

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

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、船舶用プロペラの精密鋳造用模型を
得るための消失性模型の製作に当り、プロペラの
大きさの限界を克服したプロペラ用模型の製作法
に関する。
Detailed Description of the Invention (Industrial Application Field) The present invention is directed to a propeller model that overcomes the limitations of propeller size in producing a fugitive model for precision casting of a marine propeller. Regarding the production method.

(従来の技術とその問題点) 船舶用プロペラの精密鋳造用模型を製作するた
めに、消失性材料でプロペラ模型を得るに当り、
従来は中心ボスより3翼なり4翼なりの各翼が、
所定ピツチ、所定間隔の下に突出された全体を一
体模型として製作するため、その得られるプロペ
ラ大きさには制限があり、一般にはその直径1000
mm程度が大きさの限界である。
(Prior art and its problems) In order to produce a precision casting model of a marine propeller, when obtaining a propeller model using fugitive material,
Conventionally, each of the three or four wings from the central boss,
Since the entire projecting part is manufactured as an integral model with a specified pitch and a specified interval, there is a limit to the size of the propeller that can be obtained, and generally the diameter is 1000 mm.
The size limit is about mm.

本発明は、かかるプロペラ用模型の製作上の限
界に鑑みなされたもので、プロペラの大きさに拘
らず、容易に高精度の精密鋳造用消失性模型が得
られる方法を提供することを目的とする。
The present invention was made in view of the limitations in manufacturing propeller models, and an object of the present invention is to provide a method for easily obtaining a high-precision fugitive model for precision casting, regardless of the size of the propeller. do.

(問題点を解決するための手段) 上記目的を達成するために講じられた本発明の
特徴とするところは、精密鋳造用の消失性プロペ
ラ模型の製作に当り、翼本体とボス一部とからな
る各翼単位の分割模型を夫々に成形し、これら分
割模型を定盤上に集合させ、翼本体に予め形成さ
れたピツチ出し用支持棒及びボス一部の底面によ
りプロペラピツチを設定すると共に翼本体に予め
形成された翼間割出し用ピンの相互の間隔を一定
にすることによりプロペラ翼間隔を設定して、分
割模型の集合体を形成し、該集合体のボス上面に
押湯部成形雌型を載置し、該雌型内に模型材料を
流し込んで前記集合体を一体化する点にある。
(Means for Solving the Problems) A feature of the present invention taken to achieve the above object is that when manufacturing a fugitive propeller model for precision casting, the blade body and a part of the boss are separated from each other. Separate models of each wing unit are molded, and these split models are assembled on a surface plate, and the propeller pitch is set using the support rod for pitch adjustment formed in advance on the blade body and the bottom surface of a part of the boss, and the blade is assembled. The propeller blade spacing is set by making the mutual spacing of the indexing pins between the blades pre-formed on the main body constant, forming an assembly of split models, and forming a feeder part on the upper surface of the boss of the assembly. The method consists of placing a female mold and pouring a model material into the female mold to integrate the assembly.

(実施例) 以下図示の実施例について本発明を詳述する
と、第1図,は本発明方法による1翼の分割
模型を示し、第2図は定盤上における分割模型の
集合状態を示している。本発明では従来法と相違
して、第1図に示すように、目的プロペラにお
ける翼数に応じて、各1箇の翼本体1aと翼本体
1aに続くボス一部1bとによる分割模型1を、
夫々成形雌型によつて成形するのである。このさ
い図示の実施例では、4翼プロペラの一例を示し
ており、従つて4箇の分割模型1を成形するので
あり、従つて各模型1における翼本体1aに続く
ボス一部1bは1/4円周に止まるセグメント形状
のものとされる。
(Example) The present invention will be described in detail below with reference to the illustrated embodiments. Fig. 1 shows a split model of one wing made by the method of the present invention, and Fig. 2 shows the assembled state of the split models on a surface plate. There is. In the present invention, unlike the conventional method, as shown in FIG. 1, a divided model 1 is created, each consisting of one blade body 1a and a boss portion 1b following the blade body 1a, depending on the number of blades in the target propeller. ,
Each is molded using a female mold. In the illustrated embodiment, an example of a four-blade propeller is shown, and accordingly, four divided models 1 are molded. Therefore, the boss portion 1b following the blade main body 1a in each model 1 is 1/1/2. It is said to have a segment shape that stops at four circumferences.

このさい各分割模型1において、翼本体1aに
はその翼正面側にピツチ出し用支持棒2が図示の
ように一体に予め突出形成され、又翼背面側には
翼間割出し用ピン3が同じく一体に予め突出形成
しておくのである。
At this time, in each split model 1, a support rod 2 for pitch adjustment is integrally formed in advance on the front side of the blade to protrude from the blade main body 1a as shown in the figure, and a pin 3 for indexing between the blades is formed on the back side of the blade. Similarly, it is formed in advance so as to protrude integrally.

第1図において4はボス一部1bに挿設される
芯金を示しており、5は後にボス部上に形成され
る押湯模型であり、分割模型1と割じく消失性材
料によるもので、7は押湯模型5の成形用雌型で
あり、6は定盤を示している。本発明ではこのよ
うに分割して夫々翼単位でボス一部と共に形成し
た分割模型1の図例では4個を、第2図に例示す
るように定盤6上に集合させるのである。
In Fig. 1, numeral 4 indicates a core bar inserted into the boss part 1b, and numeral 5 indicates a feeder model to be formed later on the boss part, which is made of a fugitive material that is separated from the split model 1. 7 is a female die for molding the feeder model 5, and 6 is a surface plate. In the present invention, four pieces of the divided model 1, each of which is divided into blades and formed with a portion of the boss in the illustrated example, are assembled on a surface plate 6 as illustrated in FIG.

このさい、各翼におけるピツチ及びレーキは、
各分割模型におけるボス一部1bの各合せ面、即
ち第2図示の0A,0B,0C,0Dと、ボス一
部1bの各底面、更に翼本体1aの正面側に予め
突出形成されたピツチ出し用支持棒2によつて容
易に確保できる。
At this time, the pitch and rake on each wing are
Each mating surface of the boss part 1b in each split model, that is, 0A, 0B, 0C, 0D shown in the second figure, each bottom face of the boss part 1b, and pitch projections formed in advance on the front side of the wing body 1a. This can be easily secured using the support rod 2.

また、各翼間の割り出しは、各翼本体1aの背
面側に予め突出形成された翼間割出し用ピン3の
相互の間隔を一定にすることによつて容易にかつ
正確に設定される。具体的な設定方法としては、
所定の翼間隔を定めるための位置決め孔が開設さ
れた型板を用いて、この位置決め孔に前記翼間割
出し用ピン3の各々を係合させるように各分割模
型を微動調整すればよい。また、所定角度ごとに
回動可能な割出し定盤を用いて、割出し時に前記
翼間割出し用ピン3を定盤外に固定された位置決
め基準に順次合せるように各分割模型を微動調整
してもよい。
Furthermore, the indexing between the blades can be easily and accurately set by making the mutual spacing between the blade indexing pins 3, which are formed in advance and protruding from the back side of each blade main body 1a, constant. The specific setting method is as follows.
Using a template with positioning holes for determining a predetermined blade spacing, each divided model may be finely adjusted so that each of the blade indexing pins 3 is engaged with the positioning hole. In addition, by using an indexing surface plate that can be rotated at predetermined angles, each divided model is finely adjusted so that the inter-blade indexing pin 3 is sequentially aligned with the positioning reference fixed outside the surface plate during indexing. You may.

こうして4個の分割模型1群を調整セツトした
後、集合したボス部によるボス部上肩部分に、第
1図示のように押湯部成形雌型7をセツトして、
模型材料と同様材料を流し込んで、これら分割模
型1群の集合体を押湯部5を介して一体化し、し
かる後各模型1の翼面に形成したピツチ出し用支
持棒2及び翼間割出し用ピン3を除去することに
よつて目的の消失性プロペラ模型を得ることがで
きる。このように分割模型1群の単独形成と、集
合セツトによつて、得ようとするプロペラ模型の
大きさは理論的には制限なく大きなものが得られ
る。
After adjusting and setting the first group of four divided models in this way, the female die 7 for molding the riser part is set on the upper shoulder part of the boss part formed by the gathered boss parts as shown in the first figure.
The same material as the model material is poured, and the assembly of these divided models 1 group is integrated via the feeder part 5, and then the support rod 2 for pitching and the indexing between the blades are formed on the wing surface of each model 1. By removing the pin 3, the desired evanescent propeller model can be obtained. In this way, the size of the propeller model to be obtained can theoretically be large without any limit, by forming one group of divided models individually and by assembling them.

尚、プロペラが3翼の場合は、分割模型1は3
個であり、そのボス一部1bは1/3円周のものに
なるように、翼の数に応じて分割模型の数は増減
される。
In addition, if the propeller has 3 blades, split model 1 will have 3 blades.
The number of divided models is increased or decreased depending on the number of wings so that the boss part 1b has a circumference of 1/3.

(発明の効果) 本発明は以上の通りであり、この種プロペラ模
型を、その翼単位に分割した分割模型1とし、こ
の分割模型1に予めピツチ出し用支持棒及び翼間
割出し用ピンを設けたから、分割模型群を所期の
プロペラ模型の外形に合致させるように精密かつ
容易に位置決めすることができる。また、定盤上
に位置決めされた分割模型の集合体のボス上面に
押湯部成形雌型を載置し、該雌型内に模型材料を
流し込むから、所定のピツチ、翼間隔に精密に位
置決めされた状態を保持して前記集合体を容易に
一体化させることができ、高精度の精密鋳造用の
消失性プロペラ模型を極めて容易に製作すること
ができる。従つて、従来のようにそのプロペラ直
径が1000mm程度に制限されることなく、より大き
な直径サイズのプロペラの鋳造製作がきわめて容
易に可能となり、しかもこの模型製作用の成形雌
型費用も1/3程度に低減できるのであり、少量生
産の場合でもプロペラ1箇当りの型費用は少なく
て済むことになり、本発明方法によれば、従来の
プロペラ直径1000mm程度が、1000〜2000mm程度ま
で大型化できるのであり、又重量的には7〜8倍
のものが得られるのであり、更には同様の舶用サ
イドスラスターや撹拌機用インペラのようなプロ
ペラ類にも適用可能であり、優れた利点と効果と
を持つものである。
(Effects of the Invention) The present invention is as described above, and this type of propeller model is made into a divided model 1 which is divided into blade units, and a support rod for pitch adjustment and a pin for indexing between the blades are attached to this divided model 1 in advance. Because of this provision, the divided model group can be precisely and easily positioned so as to match the external shape of the desired propeller model. In addition, the feeder molding female mold is placed on the top surface of the boss of the assembly of split models positioned on the surface plate, and the model material is poured into the female mold, allowing precise positioning at a predetermined pitch and blade spacing. The assembly can be easily integrated while maintaining the same state, and a fugitive propeller model for high precision precision casting can be manufactured extremely easily. Therefore, unlike in the past, the propeller diameter is not limited to about 1000 mm, and it is extremely easy to cast propellers with larger diameters, and the cost of molding female molds for model production can be reduced to 1/3. The mold cost per propeller can be reduced even in small-volume production, and according to the method of the present invention, the conventional propeller diameter of about 1000 mm can be increased to about 1000 to 2000 mm. Moreover, it is 7 to 8 times heavier in weight, and can also be applied to propellers such as similar marine side thrusters and agitator impellers, with excellent advantages and effects. It is something that has.

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

第1図は本発明による1翼単位の分割模型の平
面及び側面図、第2図は同分割模型の集合状態の
平面図である。 1…翼単位分割模型、1a…翼本体、1b…ボ
ス一部、2…ピツチ出し用支持棒、3…翼間割出
し用ピン、4…芯金、5…押湯部、6…定盤、7
…押湯部成形雌型。
FIG. 1 is a plan and side view of a divided model of one wing unit according to the present invention, and FIG. 2 is a plan view of the divided model in an assembled state. DESCRIPTION OF SYMBOLS 1...Blade unit division model, 1a...Blade main body, 1b...Boss part, 2...Support rod for pitch adjustment, 3...Blade indexing pin, 4...Core metal, 5...Riser part, 6...Surface plate ,7
...Female die for molding the riser part.

Claims (1)

【特許請求の範囲】[Claims] 1 精密鋳造用の消失性プロペラ模型の製作に当
り、翼本体とボス一部とからなる各翼単位の分割
模型を夫々に成形し、これら分割模型を定盤上に
集合させ、翼本体に予め形成されたピツチ出し用
支持棒及びボス一部の底面によりプロペラピツチ
を設定すると共に翼本体に予め形成された翼間割
出し用ピンの相互の間隔を一定にすることにより
プロペラ翼間隔を設定して、分割模型の集合体を
形成し、該集合体のボス上面に押湯部成形雌型を
載置し、該雌型内に模型材料を流し込んで前記集
合体を一体化することを特徴とするプロペラ用模
型の製作法。
1. When producing a fugitive propeller model for precision casting, a split model of each wing unit consisting of a wing body and a part of the boss is molded separately, these split models are assembled on a surface plate, and the blade body is pre-assembled. The propeller pitch is set by the formed pitching support rod and the bottom surface of a part of the boss, and the propeller blade spacing is set by making the mutual spacing of the blade indexing pins formed in advance on the blade body constant. The method is characterized by forming an assembly of split models, placing a feeder molding female mold on the upper surface of the boss of the assembly, and pouring model material into the female mold to integrate the assembly. How to make a propeller model.
JP7829577A 1977-06-28 1977-06-28 Method of fabricating propeller model Granted JPS5413194A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7829577A JPS5413194A (en) 1977-06-28 1977-06-28 Method of fabricating propeller model

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7829577A JPS5413194A (en) 1977-06-28 1977-06-28 Method of fabricating propeller model

Publications (2)

Publication Number Publication Date
JPS5413194A JPS5413194A (en) 1979-01-31
JPS6114907B2 true JPS6114907B2 (en) 1986-04-21

Family

ID=13657930

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7829577A Granted JPS5413194A (en) 1977-06-28 1977-06-28 Method of fabricating propeller model

Country Status (1)

Country Link
JP (1) JPS5413194A (en)

Also Published As

Publication number Publication date
JPS5413194A (en) 1979-01-31

Similar Documents

Publication Publication Date Title
DE60032824T2 (en) MULTI-WALL CORE AND PROCEDURE
CN108971698B (en) A method for additive manufacturing of propeller arc fuse
US3981344A (en) Investment casting mold and process
DE102005021666B4 (en) Method and apparatus for determining the position of equipment features generated in the center core in a lost wax casting
EP2992982B1 (en) Investment casting of engine parts
DE2937452C2 (en) Method of making a shell shape with lost pattern for making single crystal castings
CN108941511A (en) A kind of moulding process based on 3D printing cast aluminium alloy gold cylinder cap
US4044815A (en) Precision investment casting mold, pattern assembly and method
CN107745087B (en) Sand core and its cold-box core shooting universal mold and manufacturing method
CN107008863A (en) The superposing type casting method of large scale annular steel-casting
GB2346340A (en) A ceramic core, a disposable pattern, a method of making a disposable pattern, a method of making a ceramic shell mould and a method of casting
CN106392004A (en) Wall thickness control method for hollow blade provided with blind hole cavity
JPS6114907B2 (en)
JPH0235879B2 (en)
EP0537417B1 (en) Lost pattern and process for making the same
CN105798230A (en) Wax mould module for casting gas turbine blades and assembling method thereof
DE2659224C2 (en) Carrying device for a model for precision casting processes
DE2453090A1 (en) METHOD AND CASTING FORM FOR CASTING HIGH TEMPERATURE RESISTANT ALLOYS
US3387645A (en) Shaping method including fixing the position of predetermined points in particulate mold material
CN207154688U (en) A kind of mechanical arm mould
WO2006007787A1 (en) Pattern-cutting device, manufacture method and mould thereof
DE1604739B1 (en) PROCESS FOR MANUFACTURING PLASTIC MODELS OF BARREL AND VANE WHEELS AND DEVICE FOR CARRYING OUT THIS PROCESS
CN104057024B (en) A kind of combined shaping manufacture method of metalwork
CN209110100U (en) A kind of engine turbine blade mold size adjustment mechanism
CN209110099U (en) 3D Hard Gold Bracelet Wax Mould Forming Mould