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JPS5921692B2 - How to make a propeller wing model - Google Patents
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JPS5921692B2 - How to make a propeller wing model - Google Patents

How to make a propeller wing model

Info

Publication number
JPS5921692B2
JPS5921692B2 JP53005298A JP529878A JPS5921692B2 JP S5921692 B2 JPS5921692 B2 JP S5921692B2 JP 53005298 A JP53005298 A JP 53005298A JP 529878 A JP529878 A JP 529878A JP S5921692 B2 JPS5921692 B2 JP S5921692B2
Authority
JP
Japan
Prior art keywords
model
wing
propeller
casting
foamed resin
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
JP53005298A
Other languages
Japanese (ja)
Other versions
JPS5499171A (en
Inventor
倉松 渡辺
和明 河波
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 Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP53005298A priority Critical patent/JPS5921692B2/en
Publication of JPS5499171A publication Critical patent/JPS5499171A/en
Publication of JPS5921692B2 publication Critical patent/JPS5921692B2/en
Expired legal-status Critical Current

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  • Moulds For Moulding Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Description

【発明の詳細な説明】 本発明は、推進器、特に舶用推進器の翼模型の製作方法
の改良に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an improvement in a method for manufacturing a wing model of a propulsion device, particularly a marine propulsion device.

舶用推進器の鋳造品を得るための翼模型として使用され
る材料は、そのほとんどが木材であり、舶用推進器の鋳
造に当つては、その鋳造用鋳型を作る方法として、(i
フ廻し型による方法、G目現型による方法、面)その他
の方法などの種々の方法があるが、いずれの方法の場合
でも模型は必ず必要である。
Most of the materials used as wing models to obtain cast products for marine propulsors are wood, and when casting marine propulsors, the method of making the casting mold is (i).
There are various methods such as the cylindrical mold method, the G-eye mold method, and other methods, but a model is always required for each method.

本発明方法は、上記(ii)による方法に用ぃる翼模型
の製作方法の改良に関するものである。
The method of the present invention relates to an improvement in the method for manufacturing a wing model used in the method (ii) above.

第1図〜第3図により、従来の舶用推進器の鋳造用具模
型の製作方法の一例を説明すると、この例は累積法とも
云われる方法で、檜や杉などの多数の長方形状の板材1
を第1図図示の如く基端を重ね合せ、先端に行くにつれ
て相隣る板材1の重ね合せ目が適当にずれるように貼り
合せて一体化したのち、第2図に示す如く翼縁2を設計
図面と照合しながら手作業で曲面を削り出して模型が形
成される。第3図は模型の翼面の断面における板材1の
積み重ね状態と捨型を示す図であるが、3は捨型、4は
模型の翼の断面を示している線である。通常、推進器は
、中心からの角度、翼の面積、曲線のなだらかさ、翼の
肉厚などの因子み推進性能に大きく影響を及ぼすので、
従来その鋳造用模型の製作に当つては、特に細心な注意
を払わなければならず、使用する材料の木材の乾燥度や
変形の少ない材料の選定などに高度の熟練を必要とする
ばかりでなく、多くの手間を要し、かつ完成した模型は
非常に重いため運搬等の取扱(・が困難であり、また完
成後時間の経過とともに変形しやすく長期間の保存に耐
えられないという欠点があつた。
An example of a method for manufacturing a conventional casting tool model for a marine propulsion device will be explained with reference to FIGS.
The base ends are overlapped as shown in Fig. 1, and the adjacent plates 1 are bonded together so that the overlapping lines are shifted appropriately toward the tip, and then the blade edges 2 are assembled as shown in Fig. The model is created by manually carving out the curved surface while checking against the design drawings. FIG. 3 is a diagram showing the piled-up state of the plate materials 1 in a cross section of the wing surface of the model, and the discarded shape, and 3 is the discarded shape, and 4 is a line showing the cross section of the model's wing. Normally, the propulsion performance of a propeller is greatly influenced by factors such as the angle from the center, the area of the blade, the smoothness of the curve, and the thickness of the blade.
Traditionally, when making casting models, special care must be taken, and not only does it require a high degree of skill to select the dryness of the wood used and the selection of materials that are less likely to deform. However, it requires a lot of work, and the completed model is very heavy, making it difficult to transport and handle.It also has the drawbacks of being easily deformed over time after completion and not being able to withstand long-term storage. Ta.

本発明は、上記従来方法の欠点を解消し、簡易。The present invention solves the drawbacks of the above conventional methods and is simple.

迅促に製作でき、かつ軽量で変形が少なく長期間の保存
に耐える正確な推進器の鋳造用具模型の製作方法を提供
することを目的として提案されたもので、推進器の鋳造
用模型を製作するに当り、定盤上に、上面に推進器の翼
曲面に相当する形状をもつ多数枚のゲージ板を配夕Iル
たのち、それら各ゲージ板間に発泡樹脂を、上記各翼曲
面と面一となるように埋め込んで推進器鋳造用模型の翼
曲面を形成する捨型を作り、ついで、該捨型の各ゲージ
板の翼曲面上に、推進器鋳造用模型の翼肉厚を形成する
基準型板を、補強材を介して配列固定したのち,それぞ
れ基準型板間に発泡樹脂を埋め込むとともに6その表面
を基準型板の翼曲面に沿つて仕上げ.かつその全表面に
強化ブラスチツクを被覆硬化せしめることを特徴とする
推進器用翼模型の製作方法に係るものである。以下第4
図〜第7図を参照しながら本発明方法につき具体的に説
明する。
This was proposed for the purpose of providing a method for manufacturing an accurate propulsion device casting tool model that can be manufactured quickly, is lightweight, has minimal deformation, and can be stored for a long period of time. To do this, a large number of gauge plates with shapes corresponding to the curved surfaces of the blades of the thruster are placed on the top surface of the surface plate, and then foamed resin is placed between each of the gauge plates and in contact with the curved surfaces of each of the blades. Create a waste mold that is flush-embedded to form the blade curved surface of the propeller casting model, and then form the blade wall thickness of the propeller casting model on the blade curved surface of each gauge plate of the waste mold. After arranging and fixing the standard templates using reinforcing materials, foamed resin is embedded between each standard template, and the surface is finished along the curved surface of the standard template. The present invention also relates to a method for manufacturing a propeller wing model, characterized in that the entire surface of the model is coated with reinforced plastic and hardened. 4th below
The method of the present invention will be specifically explained with reference to FIGS.

第4図において、5は基準となるべき定盤で、同定盤5
上には推進器の鋳造用模型の翼の裏面各断面毎の曲線を
もつ複数枚(本例では6枚)のゲージ板6が図示の如く
等間隔毎に互いに平行に配設されている。
In Figure 4, 5 is the surface plate that should be the reference, and the identification plate 5
As shown in the figure, a plurality of gauge plates 6 (six in this example) having curves for each cross-section of the back surface of the wing of the casting model of the thruster are arranged parallel to each other at equal intervals.

7はそれらゲージ板の上端面に形成された推進器の鋳造
用模型の翼面(裏面)となるべき曲面で、該曲面7は予
かじめ設定された形状、寸法に従つて加工されてぃる。
Reference numeral 7 denotes a curved surface formed on the upper end surface of these gauge plates, which is to become the wing surface (back surface) of the casting model of the thruster, and the curved surface 7 is processed according to a preset shape and dimensions. Ru.

8は推進器の模型の翼縁となる想定線を示す。8 shows the assumed line that will be the blade edge of the model of the thruster.

上述の如く定盤5上に多数枚のゲージ板6の配列が所定
の如く終つたのちは、各相隣るゲージ板6の間に発泡樹
脂9を埋め込み、その表面を上記曲面7に合せて仕上げ
加工を行なうと推進器の鋳造用模型の翼の裏面となる捨
型ができる。この場合の発泡樹脂としては,硬質ウレタ
ン樹脂を用ぃる。この発泡樹脂9を相隣るゲージ板6間
および後述する基準型板10間に埋め込む方法としては
.発泡ずみの樹脂を現場で切断成形しながら隙間を埋め
る方法あるぃは樹脂原液を現場に持ち込み、上記隙間に
注入して発泡させ,余分のところを刃物で切除する方法
のぃづれでもよい。以上のようにしてでき上つた捨型の
各ゲージ板6の翼曲面7の上に、第5図に示すように、
推進器の鋳造用模型の翼の肉厚となる基準型板10を置
く。
After a large number of gauge plates 6 are arranged in a predetermined manner on the surface plate 5 as described above, foamed resin 9 is embedded between each adjacent gauge plate 6, and its surface is aligned with the curved surface 7. After finishing, a mold is created that will become the back side of the blade for the casting model of the thruster. In this case, hard urethane resin is used as the foamed resin. A method of embedding this foamed resin 9 between adjacent gauge plates 6 and between reference templates 10 described later is as follows. A method of filling the gap while cutting and molding the foamed resin on-site may be to bring resin stock solution to the site, inject it into the gap, foam it, and cut off the excess with a knife. As shown in FIG.
A reference template 10 having the wall thickness of a wing of a casting model of a propulsion device is placed.

この基準型板10は推進器の鋳造用模型の翼の各断面の
面積を正確に写し出し6かつ仕上げ代などを自めて予か
じめ加工形成されている。以上のようにして基準板10
の各ゲージ板6の曲面7上への配列が終つたら.鉄棒ま
たは木材棒の補強材11を第5図に示す如く各基準型板
10間に通し6それら基準型板10を固定する。ついで
第4図に示したと同じ方法で、相隣る基準型板10間に
発泡樹脂9を埋め込み,基準型板10の曲面12に沿つ
て仕上げ切削加工を行なう。かくして鋳造用模型の翼の
表面が完成したならば、その表面に強化プラスチツクの
被覆を行なう。この強化ブラスチツクによる表面被覆は
、エポキシ樹脂あるいはポリエステル樹脂の原液に、硬
化剤を混入したものを模型表面に刷毛により塗布し6そ
の上にガラス繊維などをかぶせ、さらにその上から原液
を塗り、これを2〜3回繰り返えして2〜3朋の厚さに
被覆したのち6放置すれば硬化し、強固な被覆面が得ら
れる。このようにして完成した模型の状況を第6図およ
び第7図によつて説明すれば、第6図は推進器の翼の中
心線の断面図で613は翼縁、14は表面の強化プラス
チツク層を示し615リ発泡樹脂、16は補強材となる
鉄棒または木材棒である。
This reference template 10 is pre-processed to accurately represent the area of each cross-section of the wing of the casting model of the propulsion device 6 and to have finishing allowances. As described above, the reference plate 10
After each gauge plate 6 has been arranged on the curved surface 7. A reinforcing material 11 such as an iron rod or a wood rod is passed between each reference template 10 as shown in FIG. 5, and the reference templates 10 are fixed. Then, in the same manner as shown in FIG. 4, foamed resin 9 is embedded between adjacent reference templates 10, and finish cutting is performed along the curved surface 12 of the reference templates 10. Once the surface of the wing of the casting model has been completed, the surface is coated with reinforcing plastic. Surface coating with this reinforced plastic is done by applying a mixture of undiluted epoxy resin or polyester resin mixed with a curing agent to the surface of the model with a brush6, covering it with glass fiber, etc., and then applying the undiluted solution over it. Repeat this process 2 to 3 times to form a coating with a thickness of 2 to 3 mm, and then leave it for 6 hours to cure and obtain a strong coated surface. The state of the model completed in this way will be explained with reference to Figs. 6 and 7. Fig. 6 is a sectional view taken along the center line of the blade of the thruster, 613 is the blade edge, and 14 is the reinforced plastic surface. The layers are shown at 615, a re-foamed resin, and 16, an iron rod or wood rod serving as a reinforcing material.

第7図は第6図の直角方向に見た模型翼の断面図で61
4は強化ブラスチツク層、15は発泡樹脂.16は補強
材を示している。以上6要するに本発明は.推進器の鋳
造用模型を製作するに当り,定盤上に、上面に推進器の
翼曲面に相当する形状をもつ多数枚のゲージ板を配列し
たのち,それら各ゲージ板間に発泡樹脂を6上記各翼曲
面と面一となるように埋め込んで推進器鋳造用模型の翼
重面を形成する捨型を作り、ついで6該捨型の各ゲージ
板の翼曲面上に、推進器鋳造用模型の翼肉厚を形成する
基準型板を.補強材を介して配列固定したのち、それで
基準型板間に発泡樹脂を埋め込むとともに6その表面を
基準型板の翼曲面に沿つて仕士げ、かつその全表面に強
化ブラスチツクを被覆硬化せしめることを特徴とする推
進器用翼模型の製作方法を要旨とするものであるから、
本発明によれば6(1)従来方法に比し、推進器の鋳造
用翼模型の製作工数が少なく,簡易迅速に製作でき6多
くの手間を要しなぃ。
Figure 7 is a cross-sectional view of the model wing seen in the direction perpendicular to Figure 6.
4 is a reinforced plastic layer, 15 is a foamed resin layer. 16 indicates a reinforcing material. 6 In short, the present invention is as follows. To manufacture a casting model of the thruster, a large number of gauge plates with shapes corresponding to the curved surfaces of the blades of the propeller were arranged on the surface plate, and then 6 pieces of foamed resin were placed between each gauge plate. 6. Make a waste mold that is embedded flush with each of the blade curved surfaces to form a blade weight surface of a model for casting a propeller, and then place a mold for casting a propeller on the blade curved surface of each gauge plate of the waste mold. A reference template for forming the wing thickness. After arranging and fixing through the reinforcing material, foamed resin is embedded between the standard templates, its surface is finished along the curved surface of the standard template, and reinforced plastic is coated and hardened on the entire surface. Since the gist of this article is a method for manufacturing a propeller wing model featuring the following,
According to the present invention, 6(1) Compared to the conventional method, the number of man-hours required for manufacturing a blade model for casting of a propulsion device is small, and it can be manufactured simply and quickly without requiring much labor.

(2)鋳型の大部を軽量な発泡樹脂で形成しているため
.模型重量を従来に比し著しく軽減でき.取扱いが容易
であり、また材料費を大幅に低減できる。
(2) Most of the mold is made of lightweight foamed resin. The weight of the model can be significantly reduced compared to conventional models. It is easy to handle and can significantly reduce material costs.

(3)強化ブラスチツクにより模型表面には強固な被覆
面が形成されることと、主要部が発泡樹脂で形成される
ため6時間経過による変形が従来に比し著しく少なくな
り、長期保存に耐える。
(3) Since a strong covering surface is formed on the surface of the model by reinforced plastic, and the main part is formed of foamed resin, deformation after 6 hours is significantly less than before, and it can be stored for a long time.

(4)従来のように材料の乾燥度合や選定等に余り配慮
する要がなぃので製作に高度な熟練を必要としない。な
どの実用的効果を挙げることができる。
(4) Unlike conventional methods, there is no need to pay much attention to the degree of dryness or selection of materials, so manufacturing does not require a high degree of skill. The following practical effects can be mentioned.

【図面の簡単な説明】 第1図、第2図および第3図は、従来の製作方去の一例
の略示的説明図6第4図および第5図は本発明方法の一
実施態様の慨略説明図で、第4図はゲージ板の配列状態
説明図、第5図は基準型板の配列状態説明図、第6図6
第7図は本発明により完成した模型の概略説明図で6第
6図は推進器の翼の中心線の断面図、第7図は第6図の
A−A線断面図である。 第4図乃至第7図において6 5・・・定盤,6・・・ケージ板、7・・・翼曲面68
・・・翼縁想定線.9・・・発泡樹脂610・・・基準
型板、11・・・補強材、12・・・基準型板の曲面、
13・・・翼縁、14・・・強化プラスチツク層、15
・・・発泡樹脂,16・・・補強材。
[BRIEF DESCRIPTION OF THE DRAWINGS] FIGS. 1, 2 and 3 are schematic illustrations of an example of a conventional manufacturing method. FIGS. 4 and 5 are schematic illustrations of an embodiment of the method of the present invention. These are schematic explanatory diagrams: FIG. 4 is an explanatory diagram of the arrangement of gauge plates, FIG. 5 is an explanatory diagram of the arrangement of reference templates, and FIG.
7 is a schematic explanatory diagram of a model completed according to the present invention, 6. FIG. 6 is a sectional view taken along the center line of the propeller blade, and FIG. 7 is a sectional view taken along the line A--A in FIG. 6. In Figures 4 to 7, 6 5... surface plate, 6... cage plate, 7... wing curved surface 68
...Estimated wing edge line. 9... Foamed resin 610... Reference template, 11... Reinforcement material, 12... Curved surface of reference template,
13... Wing edge, 14... Reinforced plastic layer, 15
... Foamed resin, 16... Reinforcement material.

Claims (1)

【特許請求の範囲】[Claims] 1 推進器の鋳造用模型を製作するに当り、定盤上に、
上面に推進器の翼曲面に相当する形状をもつ多数枚のゲ
ージ板を配列したのち、それら各ゲージ板間に発泡樹脂
を、上記各翼曲面と面一となるように埋込んで推進器鋳
造用模型の翼曲面を形成する捨型を作り、ついで、該捨
型の各ゲージ板の翼曲面上に、推進器鋳造用模型の翼肉
厚を形成する基準型板を、補強材を介して配列固定した
のち、それぞれ基準型板間に発泡樹脂を埋め込むととも
に、その表面を基準型板の翼曲面に沿つて仕上げ、かつ
その全表面に強化プラスチックを被覆硬化せしめること
を特徴とする推進器用翼模型の製作方法。
1. When manufacturing the casting model of the thruster, on the surface plate,
After arranging a large number of gauge plates with shapes corresponding to the curved surfaces of the propeller's blades on the top surface, foamed resin is embedded between each gauge plate so that it is flush with the curved surfaces of each of the blades, and the propeller is cast. A waste mold for forming the wing curved surface of the model for use is made, and then a reference template for forming the wing thickness of the model for propulsion casting is placed on the blade curved surface of each gauge plate of the waste mold via a reinforcing material. A propeller blade characterized in that after the arrangement and fixation, foamed resin is embedded between each reference template, the surface is finished along the wing curved surface of the reference template, and the entire surface is coated and hardened with reinforced plastic. How to make a model.
JP53005298A 1978-01-23 1978-01-23 How to make a propeller wing model Expired JPS5921692B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP53005298A JPS5921692B2 (en) 1978-01-23 1978-01-23 How to make a propeller wing model

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP53005298A JPS5921692B2 (en) 1978-01-23 1978-01-23 How to make a propeller wing model

Publications (2)

Publication Number Publication Date
JPS5499171A JPS5499171A (en) 1979-08-04
JPS5921692B2 true JPS5921692B2 (en) 1984-05-22

Family

ID=11607331

Family Applications (1)

Application Number Title Priority Date Filing Date
JP53005298A Expired JPS5921692B2 (en) 1978-01-23 1978-01-23 How to make a propeller wing model

Country Status (1)

Country Link
JP (1) JPS5921692B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61215746A (en) * 1985-03-19 1986-09-25 旭化成株式会社 Weaving method of water jet loom

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60255233A (en) * 1984-05-29 1985-12-16 Enshu Cloth Kk Pseudo casting pattern
JPS60255234A (en) * 1984-05-31 1985-12-16 Toyota Motor Corp Working method of full mold pattern material for casting
CA2667006A1 (en) * 2006-10-23 2008-05-02 Constructions Industrielles De La Mediterranee - Cnim Composite tool for moulding cylindrical parts
JP5079768B2 (en) * 2009-10-21 2012-11-21 かもめプロペラ株式会社 Mold, mold manufacturing method, casting production method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61215746A (en) * 1985-03-19 1986-09-25 旭化成株式会社 Weaving method of water jet loom

Also Published As

Publication number Publication date
JPS5499171A (en) 1979-08-04

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