TWI761990B - Manufacturing method of rapid mold with reinforced structure - Google Patents

Manufacturing method of rapid mold with reinforced structure Download PDF

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TWI761990B
TWI761990B TW109135616A TW109135616A TWI761990B TW I761990 B TWI761990 B TW I761990B TW 109135616 A TW109135616 A TW 109135616A TW 109135616 A TW109135616 A TW 109135616A TW I761990 B TWI761990 B TW I761990B
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mold
prototype
main
composite material
rapid
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TW202216408A (en
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郭啟全
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明志科技大學
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Abstract

一種具有強化結構的快速模具的製造方法。該製造方法包含步驟A~F。步驟A利用翻製方法以原型工件的原型表面,製作中介模具。步驟B將該中介模具設置於模框內,並使對應於該原型表面的翻印表面朝外開放。步驟C將塗佈於該模框的內表面以及該翻印表面的複合材料加熱使其固化形成表層結構。步驟D將強化結構設置於該模框內,且貼靠於該表層結構的表層貼合面。該強化結構的機械強度優於該複合材料固化後的機械強度。步驟E將該複合材料澆注於該模框內之後,加熱使該複合材料固化形成包覆於該強化結構的主模體。步驟F將該表層結構、該主模體與該中介模具移出該模框,並將該表層結構與該主模體的組合體與該中介模具分離,以完成該快速模具的製作。 A method of manufacturing a rapid mold with a reinforced structure. The manufacturing method includes steps A to F. In step A, an intermediate mold is made from the prototype surface of the prototype workpiece by a reproducing method. In step B, the intermediate mold is placed in the mold frame, and the reprinted surface corresponding to the prototype surface is opened to the outside. In step C, the composite material coated on the inner surface of the mold frame and the reprinted surface is heated and cured to form a surface layer structure. In step D, the reinforcing structure is arranged in the mold frame and abuts against the surface layer adhering surface of the surface layer structure. The mechanical strength of the reinforced structure is better than the mechanical strength of the composite material after curing. Step E: After pouring the composite material into the mold frame, heating to solidify the composite material to form a main mold body covering the reinforcing structure. Step F: Move the surface structure, the main mold body and the intermediate mold out of the mold frame, and separate the combination of the surface structure and the main mold body from the intermediate mold to complete the production of the rapid mold.

Description

具有強化結構的快速模具的製造方法 Manufacturing method of rapid mold with reinforced structure

本發明是有關於一種模具的製造方法,特別是指一種由可固性複合材料製作而成的快速模具的製造方法。 The present invention relates to a method for manufacturing a mold, in particular to a method for manufacturing a rapid mold made of curable composite materials.

隨著市場需求變化快速,使得新開發的產品的生命週期縮短,為了符合市場需求以及提升新產品在市場中的競爭優勢,在產品開發領域中必須縮短新產品的開發週期,因此,在新產品的開發過程中,通常會使用製造成本低廉且容易製造的快速模具來完成新產品的快速試製。現有的快速模具最常使用的是透過環氧樹脂與鋁粉所調配而成的金屬樹脂來製作,然而,利用金屬樹脂所製成的快速模具在試樣產品試製的過程中,容易因為射出成型的壓力過大而導致快速模具變形,使得試樣產品產生溢料的問題。 With the rapid changes in market demand, the life cycle of newly developed products is shortened. In order to meet market demand and enhance the competitive advantage of new products in the market, the development cycle of new products must be shortened in the field of product development. Therefore, in the field of new products In the development process of a new product, the rapid trial production of new products is usually completed by using a rapid mold that is inexpensive and easy to manufacture. Existing rapid molds are most commonly made of metal resin prepared by mixing epoxy resin and aluminum powder. However, rapid molds made of metal resin are prone to injection molding in the process of trial production of sample products. The pressure is too large, which leads to rapid mold deformation, which causes the problem of flashing of the sample product.

因此,本發明的目的,即在提供一種能耐壓且不易變形的具有強化結構的快速模具。 Therefore, the purpose of the present invention is to provide a rapid mold with a reinforced structure that can withstand pressure and is not easily deformed.

於是,本發明具有強化結構的快速模具適用於製作一原型工件的複製品。該原型工件具有一供翻印的原型表面。該快速模具包含一主模體及一強化結構。該主模體包括一主體成型面。該主體成型面適用於互補於該原型表面的形狀。該強化結構設置於該主模體內,且該強化結構的機械強度優於該主模 體的機械強度。 Thus, the rapid die with reinforced structure of the present invention is suitable for making a replica of a prototype workpiece. The prototype workpiece has a prototype surface for reproduction. The rapid mold includes a main mold body and a strengthening structure. The main mold body includes a main body forming surface. The body forming surface is adapted to complement the shape of the prototype surface. The reinforcement structure is arranged in the main mold, and the mechanical strength of the reinforcement structure is superior to that of the main mold the mechanical strength of the body.

在一些實施態樣中,該快速模具還包含一表層結構。該表層結構包覆於該主模體外圍,並包括兩相反的一表層貼合面及一表層成型面。該表層貼合面貼靠且結合於該主體成型面。該表層成型面適用於互補於該原型表面的形狀。 In some embodiments, the rapid mold further includes a skin structure. The surface layer structure covers the periphery of the main mold body, and includes two opposite surfaces, a surface layer adhering surface and a surface layer forming surface. The surface layer adhering surface is abutted against and combined with the main body molding surface. The skin forming surface is adapted to complement the shape of the prototype surface.

在一些實施態樣中,該表層結構的厚度為5公釐至10公釐。 In some embodiments, the thickness of the surface structure is 5 mm to 10 mm.

在一些實施態樣中,該強化結構與該主模體為相似形態。 In some embodiments, the reinforcement structure is similar in shape to the main motif.

在一些實施態樣中,該強化結構包括數個彼此堆疊排列的基體單元。 In some embodiments, the reinforcement structure includes a plurality of base units arranged in a stacked manner.

在一些實施態樣中,每一基體單元的橫截面為六角形,使該強化結構呈現為蜂巢結構。 In some embodiments, the cross-section of each base unit is hexagonal, so that the reinforcing structure exhibits a honeycomb structure.

在一些實施態樣中,每一基體單元的橫截面為X字形,使該強化結構呈現為肋型結構。 In some embodiments, the cross-section of each base unit is X-shaped, so that the reinforcing structure presents a rib-shaped structure.

在一些實施態樣中,每一基體單元的縱截面為三角形,使該強化結構呈現為桁架結構。 In some embodiments, the longitudinal section of each base unit is triangular, so that the reinforcement structure is presented as a truss structure.

本發明之另一目的,即在提供一種前述的該快速模具的製造方法。 Another object of the present invention is to provide a method for manufacturing the aforementioned rapid mold.

於是,本發明具有強化結構的快速模具的製造方法,藉由一原型工件及一模框進行。該原型工件具有一供翻印的原型表面。該製造方法包含以下步驟: Therefore, the manufacturing method of the rapid mold with the reinforced structure of the present invention is carried out by a prototype workpiece and a mold frame. The prototype workpiece has a prototype surface for reproduction. The manufacturing method includes the following steps:

一步驟(A),利用一翻製方法以該原型工件的該原型表面,製作一 中介模具。該中介模具具有一對應於該原型表面的翻印表面。 A step (A), using a reproducing method to make a prototype surface of the prototype workpiece Intermediate mold. The intermediate mold has a reprint surface corresponding to the prototype surface.

一步驟(B),將該中介模具設置於該模框內,並使該翻印表面朝外開放。 In a step (B), the intermediate mold is set in the mold frame, and the reprinted surface is opened to the outside.

一步驟(C),將一可固性的複合材料塗佈於該模框的內表面以及該中介模具的該翻印表面之後,加熱使該複合材料固化形成一表層結構。該表層結構包括兩相反的一表層貼合面及一表層成型面。該表層成型面互補於該翻印表面的形狀。 In step (C), after coating a curable composite material on the inner surface of the mold frame and the reprinted surface of the intermediate mold, heating the composite material to solidify to form a surface layer structure. The surface layer structure includes two opposite surfaces, a surface layer adhering surface and a surface layer forming surface. The skin forming surface is complementary to the shape of the reprint surface.

一步驟(D),將一強化結構設置於該模框內,且貼靠於該表層貼合面。該強化結構的機械強度優於該複合材料固化後的機械強度。 In a step (D), a reinforcing structure is disposed in the mold frame and abutted on the surface layer bonding surface. The mechanical strength of the reinforced structure is better than the mechanical strength of the composite material after curing.

一步驟(E),將該複合材料澆注於該模框內之後,加熱使該複合材料固化形成一包覆於該強化結構的主模體。且該主模體貼合該表層結構的該表層貼合面。 In a step (E), after the composite material is poured into the mold frame, the composite material is cured by heating to form a main mold body covering the reinforcing structure. And the main mold body is attached to the surface layer adhering surface of the surface layer structure.

一步驟(F),將該表層結構、該主模體與該中介模具移出該模框,並將該表層結構與該主模體的組合體與該中介模具分離,以完成該快速模具的製作。 In a step (F), the surface structure, the main mold body and the intermediate mold are removed from the mold frame, and the combination of the surface structure and the main mold body is separated from the intermediate mold to complete the production of the rapid mold .

在一些實施態樣中,該步驟(D)是將數個基體單元以堆疊方式排列,形成該強化結構。 In some embodiments, the step (D) is to arrange a plurality of base units in a stacked manner to form the strengthening structure.

在一些實施態樣中,該步驟(D)是將該等基體單元依據該主模體的相似形態彼此排列堆疊,使該強化結構呈現為該主模體的順型形態。 In some embodiments, the step (D) is to arrange and stack the base units according to the similar shape of the main pattern, so that the reinforcement structure exhibits a cis-shape of the main pattern.

本發明之另一目的,即在提供一種前述的該快速模具的製造方法。 Another object of the present invention is to provide a method for manufacturing the aforementioned rapid mold.

於是,本發明具有強化結構的快速模具的製造方法,藉由一模框及一原型工件,該原型工件具有一供翻印的原型表面,該製造方法包含以下步驟: Thus, the present invention has a method for manufacturing a rapid mold with a reinforced structure, by means of a mold frame and a prototype workpiece having a prototype surface for reprinting, the manufacturing method comprising the following steps:

一步驟(A),利用一翻製方法以該原型工件的該原型表面,製作一中介模具。該中介模具具有一對應於該原型表面的翻印表面。 In a step (A), an intermediate mold is fabricated from the prototype surface of the prototype workpiece by a reproducing method. The intermediate mold has a reprint surface corresponding to the prototype surface.

一步驟(B),將該中介模具設置於該模框內,並使該翻印表面朝外開放。 In a step (B), the intermediate mold is set in the mold frame, and the reprinted surface is opened to the outside.

一步驟(D),將一強化結構設置於該模框內,且貼靠於該翻印表面。 In a step (D), a reinforcing structure is disposed in the mold frame and abutted on the reprinted surface.

一步驟(E),將一可固性的複合材料澆注於該模框內之後,加熱使該複合材料固化形成一包覆於該強化結構的主模體。該主模體具有一互補於該翻印表面的主體成型面。該主體成型面適用於互補於該原型表面的形狀。其中,該強化結構的機械強度優於該複合材料固化後的機械強度。 In a step (E), after pouring a curable composite material into the mold frame, heating to solidify the composite material to form a main mold body covering the reinforcing structure. The main mold body has a main body forming surface complementary to the imprinting surface. The body forming surface is adapted to complement the shape of the prototype surface. Wherein, the mechanical strength of the reinforced structure is better than the mechanical strength of the composite material after curing.

一步驟(F),將該主模體與該中介模具移出該模框,並將該主模體與該中介模具分離,以完成該快速模具的製作。 In a step (F), the main mold body and the intermediate mold are removed from the mold frame, and the main mold body and the intermediate mold are separated to complete the production of the rapid mold.

本發明之功效在於:藉由該主模體包覆於該強化結構,製得可用於仿製該原型工件的快速模具,同時,該強化結構的機械強度優於該主模體的機械強度,如此,可使得該快速模具整體的機械強度提升,因此,能達到該快速模具用於射出成型的過程中耐壓且不易變形的目的。除此之外,藉由與該主模體相同材質的該表層結構包覆於該主模體外圍,可避免該快速模具的該強化結構顯露於模具的表面,使該快速模具的表面為一體成形的結構而無接縫。如此,在該快速模具用於射出成型的製程時,能避免射出成型的高壓塑料由接縫 處溢入的情形,同樣也能達到該快速模具耐壓且不易變形的目的。 The effect of the present invention is that: by covering the reinforcement structure with the main mold body, a rapid mold that can be used to imitate the prototype workpiece is obtained, and at the same time, the mechanical strength of the reinforcement structure is superior to that of the main mold body, so , the overall mechanical strength of the rapid mold can be improved, and therefore, the purpose of pressure resistance and less deformation during the injection molding process of the rapid mold can be achieved. In addition, by covering the periphery of the main mold body with the surface layer structure of the same material as the main mold body, the reinforcing structure of the fast mold can be prevented from being exposed on the surface of the mold, so that the surface of the fast mold can be integrated Formed structure without seams. In this way, when the rapid mold is used in the injection molding process, the injection molding high-pressure plastic can be prevented from being separated from the seam by the seam. In the case of overflow, the purpose of pressure resistance and not easy to deform can also be achieved.

100:快速模具 100: Quick Die

1:主模體 1: Main Motif

11:主體成型面 11: Main body molding surface

2:強化結構 2: Strengthen the structure

21:基體單元 21: Base unit

3:表層結構 3: Surface structure

31:表層貼合面 31: Surface bonding surface

32:表層成型面 32: Surface molding surface

5:原型工件 5: Prototype Artifacts

51:原型表面 51: Prototype Surface

6:簡易模具 6: Simple mold

7:中介模具 7: Intermediate mold

71:翻印表面 71: Reprint Surface

8:模框 8: Mold frame

(A)至(F):步驟 (A) to (F): Steps

本發明的其他的特徵及功效,將於參照圖式的實施方式中清楚地呈現,其中:圖1是一分解示意圖,說明本發明具有強化結構的快速模具之一實施例與一原型工件的對應關係;圖2是一流程示意圖,說明該實施例的製造流程;圖3是一示意圖,說明該實施例的製造流程的一步驟(A);圖4是一示意圖,說明該實施例的製造流程的一步驟(B);圖5是一示意圖,說明該實施例的製造流程的一步驟(C);圖6是一示意圖,說明該實施例的製造流程的一步驟(D);圖7是一示意圖,說明該實施例的製造流程的一步驟(E);圖8是一示意圖,說明該實施例的製造流程的一步驟(F);及圖9是一流程示意圖,說明該實施例的另一實施態樣的製造流程。 Other features and effects of the present invention will be clearly presented in the embodiments with reference to the drawings, wherein: FIG. 1 is an exploded schematic view illustrating the correspondence between an embodiment of a rapid mold having a reinforced structure of the present invention and a prototype workpiece 2 is a schematic diagram illustrating the manufacturing process of this embodiment; FIG. 3 is a schematic diagram illustrating a step (A) of the manufacturing process of this embodiment; FIG. 4 is a schematic diagram illustrating the manufacturing process of this embodiment. Fig. 5 is a schematic diagram illustrating a step (C) of the manufacturing process of this embodiment; Fig. 6 is a schematic diagram illustrating a step (D) of the manufacturing process of this embodiment; Fig. 7 is a A schematic diagram illustrating a step (E) of the manufacturing process of this embodiment; FIG. 8 is a schematic diagram illustrating a step (F) of the manufacturing process of this embodiment; and FIG. Another embodiment of the manufacturing process.

參閱圖1與圖8,為本發明具有強化結構2的快速模具100的一實施例。該快速模具100適用於製作一原型工件5的複製品。該原型工件5可以是任意的物體結構,且具有一供翻印的原型表面51。也就是說,利用該快速模具100,並搭配射出成型的製程,即可生產該原型工件5的複製品。 Referring to FIG. 1 and FIG. 8 , it is an embodiment of the rapid mold 100 having the reinforcing structure 2 of the present invention. The rapid die 100 is suitable for making a replica of a prototype workpiece 5 . The prototype workpiece 5 can be any object structure and has a prototype surface 51 for reproduction. That is, a replica of the prototype workpiece 5 can be produced by using the rapid mold 100 and the injection molding process.

該快速模具100包含一主模體1、一強化結構2及一表層結構3。該主 模體1包括一主體成型面11。該主體成型面11適用於互補於該原型表面51的形狀。在本實施例中,該主模體1的材質為一可固化的複合材料(圖未示),例如:金屬樹脂。詳細的說,金屬樹脂的材料成分包含環氧樹脂與鋁。其中,環氧樹脂的成分比例佔金屬樹脂的20%~30%,鋁的成分比例佔金屬樹脂的70%~80%。在本實施例中,該主模體1是以成分比例為15%的環氧樹脂與成分比例為85%的粉末狀的鋁所構成的金屬樹脂為例說明。 The rapid mold 100 includes a main mold body 1 , a reinforcement structure 2 and a surface layer structure 3 . the master The mold body 1 includes a main body forming surface 11 . The body molding surface 11 is adapted to complement the shape of the prototype surface 51 . In this embodiment, the material of the main mold body 1 is a curable composite material (not shown), such as metal resin. Specifically, the material components of the metal resin include epoxy resin and aluminum. Among them, the composition ratio of epoxy resin accounts for 20%~30% of the metal resin, and the composition ratio of aluminum accounts for 70%~80% of the metal resin. In the present embodiment, the main mold body 1 is illustrated as a metal resin composed of epoxy resin with a composition ratio of 15% and powdered aluminum with a composition ratio of 85%.

該強化結構2設置於該主模體1內,並包括數個彼此堆疊排列的基體單元21。在本實施例中,該強化結構2的材質為麻時效鋼。然而,該強化結構2的材質也可以是不銹鋼、高溫合金鋼、鋁合金鋼、鎂鋁合金鋼或陶瓷材料等高硬度的材料,使該強化結構2的機械強度優於該主模體1的機械強度,不以特定材質為限。 The reinforcement structure 2 is disposed in the main mold body 1 and includes a plurality of base body units 21 stacked on each other. In this embodiment, the material of the reinforcing structure 2 is hemp-aging steel. However, the material of the reinforcement structure 2 can also be high hardness materials such as stainless steel, high temperature alloy steel, aluminum alloy steel, magnesium aluminum alloy steel or ceramic materials, so that the mechanical strength of the reinforcement structure 2 is better than that of the main mold body 1 Mechanical strength is not limited to a specific material.

在本實施例中,該等基體單元21是以3D列印的方式製作,使得該等基體單元21的精細度範圍為10微米至50微米之間,同時也使得該等基體單元21的最小結構尺寸為1立方公釐。此外,該強化結構2的結構類型共有三種。其中一種類型為蜂巢結構,是透過橫截面為六角形的該等基體單元21堆疊排列所構成。第二種類型為肋型結構,是透過橫截面為X字形的該等基體單元21堆疊排列所構成。最後一種類型為桁架結構,是透過縱截面為三角形的該等基體單元21堆疊排列所構成。在本實施例中,該強化結構2是以六角形的該等基體單元21堆疊排列所構成的蜂巢結構示例,透過此特殊設計的力學結構(例如:蜂巢結構),能增加單位面積下所能承受的壓力,使得包覆於該強化結構2的該主模 體1的機械強度優於未包覆該強化結構2的該主模體1的機械強度,而能達到該快速模具100耐壓且不易變形的目的。 In this embodiment, the base units 21 are fabricated by 3D printing, so that the fineness of the base units 21 ranges from 10 μm to 50 μm, and at the same time, the minimum structure of the base units 21 is achieved. The size is 1 cubic millimeter. In addition, there are three types of structure of the reinforcement structure 2 in total. One of the types is the honeycomb structure, which is formed by stacking and arranging the base units 21 with a hexagonal cross section. The second type is a rib structure, which is formed by stacking and arranging the base units 21 with an X-shaped cross section. The last type is the truss structure, which is formed by stacking and arranging the base units 21 with a triangular longitudinal section. In this embodiment, the reinforcing structure 2 is an example of a honeycomb structure formed by stacking and arranging the hexagonal base units 21. Through this specially designed mechanical structure (eg honeycomb structure), the energy per unit area can be increased. Bearing pressure, so that the main mold clad in the reinforcement structure 2 The mechanical strength of the body 1 is superior to that of the main mold body 1 without the reinforcement structure 2 , so that the purpose of the rapid mold 100 being pressure-resistant and not easily deformed can be achieved.

同時,該強化結構2與該主模體1為相似形態。也就是說,該強化結構2可以是形狀近似該主模體1的等比例縮小的相似結構,或是形狀略有差異的縮小化結構。如此,使得該主模體1表面至該強化結構2的厚度均勻,而能將該主體模所承受的應力均勻分散至該強化結構2,進而增加本實施例的耐壓能力。更具體來說,該快速模具100可透過變更該等基體單元21的結構形狀或變更該等基體單元21的排列堆疊方式,調整該強化結構2的型態設計,使得該快速模具100的機械強度是可調控的。也可以透過調整該強化結構2的尺寸大小或是該強化結構2的材質,同樣可以達到調控該快速模具100的機械強度的目的。 At the same time, the reinforcement structure 2 is similar to the main model body 1 . That is to say, the reinforcing structure 2 may be a similar structure whose shape is similar to that of the main mold body 1 which is scaled down, or a miniaturized structure whose shape is slightly different. In this way, the thickness from the surface of the main mold body 1 to the reinforcement structure 2 is uniform, and the stress borne by the main mold body can be uniformly dispersed to the reinforcement structure 2, thereby increasing the pressure resistance of this embodiment. More specifically, the rapid mold 100 can adjust the shape design of the reinforcing structure 2 by changing the structural shape of the base units 21 or changing the arrangement and stacking of the base units 21, so that the mechanical strength of the rapid mold 100 can be adjusted. is controllable. The purpose of adjusting the mechanical strength of the rapid mold 100 can also be achieved by adjusting the size of the reinforcing structure 2 or the material of the reinforcing structure 2 .

該表層結構3包覆於該主模體1外圍,並包括兩相反的一表層貼合面31及一表層成型面32。該表層貼合面31貼靠且結合於該主體成型面11。該表層成型面32對應該主體成型面11的形狀,且適用於互補於該原型表面51的形狀,使該快速模具100用於射出成型製程時,能製造互補於該表層成型面32且對應該原型表面51的成品,以完成該原型工件5的複製品的製作。當該快速模具100的尺寸為50公釐至300公釐時,該表層結構3的厚度為5公釐至10公釐,在此厚度範圍內,該表層結構3可以是透過塗佈方式製作完成,並且該表層結構3的厚度相對於該強化結構2的長度、寬度與高度皆不大於12.5%,如此可在該表層結構3不易破損的前提下調控該快速模具100的機械強度。在本實施例中,該表層結構3的厚度以5公釐示例,而該強化結構2的長度、寬度與高度皆以該表層結 構3的厚度的八倍示例,如此可使該快速模具100具有較佳的機械強度。然而,當該快速模具100的尺寸大於300公釐時,可使該強化結構2的長度、寬度與高度相對於該表層結構3的厚度皆小於八倍,同樣亦可調控該快速模具100的機械強度,使該快速模具100具有較佳的機械強度。 The surface layer structure 3 covers the periphery of the main mold body 1 and includes two opposite surfaces, a surface layer bonding surface 31 and a surface layer molding surface 32 . The surface layer adhering surface 31 is abutted against and combined with the main body molding surface 11 . The surface molding surface 32 corresponds to the shape of the main body molding surface 11 and is adapted to be complementary to the shape of the prototype surface 51 , so that when the rapid mold 100 is used in the injection molding process, the surface molding surface 32 can be manufactured to be complementary to the surface molding surface 32 and corresponding to the shape of the prototype surface 51 . The finished product of the prototype surface 51 to complete the production of a replica of the prototype workpiece 5 . When the size of the rapid mold 100 is 50 mm to 300 mm, the thickness of the surface layer structure 3 is 5 mm to 10 mm. Within this thickness range, the surface layer structure 3 can be fabricated by coating. , and the thickness of the surface layer structure 3 is not more than 12.5% relative to the length, width and height of the reinforcement structure 2, so that the mechanical strength of the rapid mold 100 can be regulated on the premise that the surface layer structure 3 is not easily damaged. In this embodiment, the thickness of the surface layer structure 3 is 5 mm, and the length, width and height of the reinforcement structure 2 are all determined by the surface layer structure. An example of eight times the thickness of the structure 3 can make the rapid die 100 have better mechanical strength. However, when the size of the rapid die 100 is greater than 300 mm, the length, width and height of the reinforcing structure 2 can be made less than eight times the thickness of the surface structure 3, and the mechanical properties of the rapid die 100 can also be adjusted. strength, so that the rapid mold 100 has better mechanical strength.

值得一提的是,在本實施例的另一實施態樣中,該表層結構3是可以省略的。在此實施態樣,該快速模具100包含該主模體1與該強化結構2。該主模體1的該主體成型面11適用於互補於該原型表面51的形狀,使該快速模具100用於射出成型製成時,同樣能製造互補於該表層成型面32且對應該原型表面51的成品,以完成該原型工件5的複製品的製作。 It is worth mentioning that, in another implementation aspect of this embodiment, the surface layer structure 3 can be omitted. In this embodiment, the rapid mold 100 includes the main mold body 1 and the reinforcement structure 2 . The main molding surface 11 of the main mold body 1 is adapted to be complementary to the shape of the prototype surface 51 , so that when the rapid mold 100 is used for injection molding, it can also be made complementary to the surface molding surface 32 and corresponding to the prototype surface 51 to complete the production of a replica of the prototype workpiece 5.

參閱圖2,為本實施例的製造流程。以下配合圖3至圖8詳細說明本實施例的製造方法。 Referring to FIG. 2 , the manufacturing process of this embodiment is shown. The manufacturing method of this embodiment will be described in detail below with reference to FIGS. 3 to 8 .

配合參閱圖3,首先進行一步驟(A):利用一翻製方法以該原型工件5的該原型表面51,製作一中介模具7。該翻製方法是先透過該原型工件5及一模框8翻印製成一簡易模具6,也可以是透過3D列印的方式直接製作輪廓形狀互補於該原型表面51的該簡易模具6。該簡易模具6的材質為硬度較低的塑化材料,例如:ABS樹脂(Acrylonitrile Butadiene Styrene)或聚乳酸(Polylactic Acid)。特別說明的是,該簡易模具6包含一上模具(圖未示)與一下模具(圖未示),該上模具與該下模具互相搭配才能形成互補於該原型工件5的外表面的完整輪廓。因此,以下說明該快速模具100的製造方法僅以製作對應該簡易模具6的該上模具與該下模具的其中一者示例,製作對應另一者的該快速模具100的方式完全 相同,因而不重複贅述。接著,將該簡易模具6設置於該模框8內,並澆注以矽膠與硬化劑之重量比為10:1所調配的可固化材料於該模框8內,加熱使可固化材料硬化後可製成如圖3所示的該中介模具7。該中介模具7具有一互補於該簡易模具6的表面輪廓,且對應於該原型表面51的翻印表面71。在本實施例中,該中介模具7的材質為矽膠,可使得後續該中介模具7在脫模過程中較容易分離。再來,將該中介模具7與該簡易模具6移出該模框8,並將該中介模具7與該簡易模具6分離,以完成該快速模具100的製作。 Referring to FIG. 3 , a step (A) is first performed: an intermediate mold 7 is fabricated from the prototype surface 51 of the prototype workpiece 5 by a reproducing method. In the reproducing method, a simple mold 6 is first reproduced through the prototype workpiece 5 and a mold frame 8 , or the simple mold 6 whose outline and shape complement the prototype surface 51 can be directly produced by 3D printing. The material of the simple mold 6 is a plasticized material with low hardness, such as ABS resin (Acrylonitrile Butadiene Styrene) or polylactic acid (Polylactic Acid). In particular, the simple mold 6 includes an upper mold (not shown) and a lower mold (not shown), and the upper mold and the lower mold can be matched with each other to form a complete contour complementary to the outer surface of the prototype workpiece 5 . Therefore, the following description of the manufacturing method of the quick die 100 is only taken as an example of manufacturing one of the upper die and the lower die corresponding to the simple die 6 , and the method of manufacturing the quick die 100 corresponding to the other is complete. are the same, and thus will not be repeated. Next, the simple mold 6 is placed in the mold frame 8, and a curable material prepared with a weight ratio of silicone glue and a hardener of 10:1 is poured into the mold frame 8, and the curable material is cured by heating. The intermediate mold 7 as shown in FIG. 3 is produced. The intermediate mold 7 has a surface profile complementary to the simple mold 6 and corresponding to the reprint surface 71 of the prototype surface 51 . In this embodiment, the material of the intermediate mold 7 is silicone, which can make the intermediate mold 7 easier to separate during the demolding process. Next, the intermediate mold 7 and the simple mold 6 are removed from the mold frame 8 , and the intermediate mold 7 and the simple mold 6 are separated to complete the fabrication of the rapid mold 100 .

配合參閱圖4,接著進行一步驟(B):將該中介模具7設置於該模框8內,並使該翻印表面71朝外開放。 Referring to FIG. 4 , a step (B) is performed next: the intermediate mold 7 is placed in the mold frame 8 , and the reprinting surface 71 is opened to the outside.

配合參閱圖5,接著進行一步驟(C):將該可固性的複合材料(前述的金屬樹脂)塗佈厚度為5公釐的塗層於該模框8的內表面以及該中介模具7的該翻印表面71,接著以攝氏60~80度加熱1小時使該複合材料固化形成該表層結構3。該表層結構3包括兩相反的該表層貼合面31及該表層成型面32。該表層成型面32互補於該翻印表面71的形狀。本步驟製作該表層結構3,是為了在下一步驟中限位該強化結構2。 Referring to FIG. 5 , a step (C) is then performed: coating the curable composite material (the aforementioned metal resin) with a coating thickness of 5 mm on the inner surface of the mold frame 8 and the intermediate mold 7 The reprinted surface 71 is then heated at 60-80 degrees Celsius for 1 hour to cure the composite material to form the surface layer structure 3 . The surface layer structure 3 includes two opposite surface layer adhering surfaces 31 and the surface layer forming surface 32 . The skin forming surface 32 is complementary to the shape of the reprint surface 71 . In this step, the surface layer structure 3 is fabricated to limit the reinforcement structure 2 in the next step.

配合參閱圖6,接著進行一步驟(D):首先以3D列印方式製作該等基體單元21,並可依據該快速模具100的設計,調整該等基體單元21的結構形狀、堆疊方式與數量。然後,將該等基體單元21以堆疊方式排列,形成該強化結構2。如圖6所示,該等基體單元21在圖6中是以數層間隔交錯排列堆疊且具有剖面線的方格示意,而該強化結構2由六角形的該等基體單元21所構成的結 構中的空隙在圖6中是以空白方格示意。在本實施例的製造方法中,該等基體單元21是以形狀近似於該主模體1的相似結構排列,使該強化結構2呈現為該主模體1的順型(conformal)形態。也就是說,該順型形態是以該表層結構3與該模框8之外型輪廓內縮約70%~80%的外形。再來,將該強化結構2設置於該模框8內,且貼靠於該表層貼合面31,使該強化結構2受到該表層結構3限位,而置於該模框8的中間,可避免該強化結構2顯露於該表層結構3外面。 Referring to FIG. 6 , a step (D) is then performed: firstly, the base units 21 are fabricated by 3D printing, and the structure, shape, stacking method and quantity of the base units 21 can be adjusted according to the design of the rapid mold 100 . . Then, the base units 21 are arranged in a stacked manner to form the reinforcement structure 2 . As shown in FIG. 6 , in FIG. 6 , the base units 21 are shown in a grid with several layers stacked in a staggered arrangement and with hatching lines, and the reinforcement structure 2 is composed of the hexagonal base units 21 . The voids in the structure are shown as blank squares in FIG. 6 . In the manufacturing method of the present embodiment, the base units 21 are arranged in similar structures with shapes similar to the main mold body 1 , so that the reinforcement structure 2 presents a conformal shape of the main mold body 1 . That is to say, the conformal shape is a shape in which the outer contours of the surface structure 3 and the mold frame 8 are shrunk by about 70%-80%. Next, the reinforcing structure 2 is arranged in the mold frame 8 and abuts against the surface layer adhering surface 31, so that the reinforcing structure 2 is limited by the surface layer structure 3 and placed in the middle of the mold frame 8, It can be avoided that the reinforcement structure 2 is exposed outside the surface structure 3 .

配合參閱圖7,接著進行一步驟(E):將以於真空環境(壓力50Pa)中脫泡15~30分鐘且與該主模體1為相同材質的該複合材料澆注於該模框8內,使該複合材料填滿該等基體單元21彼此之間的空隙,以加強該快速模具100的機械強度。如圖7所示,該強化結構2由六角形的該等基體單元21所構成的結構中的空隙在圖7中是利用剖面線填滿空白方格示意該複合材料澆注滿該模框8,並形成該主模體1。之後,將盛裝該複合材料的該模框8置於真空環境中約5~10分鐘,使該複合材料內的氣泡脫離至真空環境,重複此真空脫泡的過程直到氣泡不再冒出,確保後續固化後該快速模具100不會因為氣泡而造成結構強度不足的問題。然後,加熱使該複合材料固化形成一包覆於該強化結構2的主模體1。且該主模體1貼合該表層結構3的該表層貼合面31。在本實施例的製造方法中,該複合材料加熱固化條件是先以攝氏25度加熱24小時至48小時進行初步固化。接著,再以攝氏100度加熱1小時進行第二次固化,然後再以攝氏150度加熱1小時至2小時進行後硬化處理,使該快速模具100更進一步地提升機械強度。 Referring to FIG. 7 , a step (E) is then performed: the composite material, which is degassed in a vacuum environment (pressure 50Pa) for 15 to 30 minutes and is of the same material as the main mold body 1 , is poured into the mold frame 8 , so that the composite material fills the gaps between the base units 21 to strengthen the mechanical strength of the rapid mold 100 . As shown in FIG. 7 , the voids in the structure formed by the hexagonal base units 21 of the reinforcement structure 2 are filled with blank squares by hatching lines in FIG. 7 to indicate that the composite material is filled with the mold frame 8 , And form the main model body 1 . After that, the mold frame 8 containing the composite material is placed in a vacuum environment for about 5 to 10 minutes, so that the air bubbles in the composite material are released from the vacuum environment, and the vacuum defoaming process is repeated until the air bubbles no longer emerge, ensuring that After subsequent curing, the rapid mold 100 will not cause the problem of insufficient structural strength due to air bubbles. Then, the composite material is cured by heating to form a main mold body 1 covering the reinforcing structure 2 . And the main mold body 1 is attached to the surface layer bonding surface 31 of the surface layer structure 3 . In the manufacturing method of the present embodiment, the heating and curing conditions of the composite material are to perform preliminary curing by heating at 25 degrees Celsius for 24 hours to 48 hours. Next, heating at 100 degrees Celsius for 1 hour for secondary curing, and then heating at 150 degrees Celsius for 1 hour to 2 hours for post-hardening treatment, so that the rapid mold 100 further improves the mechanical strength.

配合參閱圖1與圖8,最後進行一步驟(F):將該表層結構3、該主模 體1與該中介模具7移出該模框8,並將該表層結構3與該主模體1的組合體與該中介模具7分離,以完成該快速模具100的製作。重複該步驟(A)至該步驟(F)可分別製成對應該上模具與該下模具的兩個快速模具100,透過該等快速模具100的組合搭配即可藉由射出成型製程製造如圖1所示的該原型工件5的複製品。 Referring to FIG. 1 and FIG. 8, a step (F) is finally performed: the surface layer structure 3, the main mold The body 1 and the intermediate mold 7 are removed from the mold frame 8 , and the combined body of the surface structure 3 and the main mold body 1 is separated from the intermediate mold 7 to complete the fabrication of the rapid mold 100 . Repeating this step (A) to this step (F) can respectively make two rapid molds 100 corresponding to the upper mold and the lower mold, and through the combination of these rapid molds 100 can be manufactured by the injection molding process as shown in the figure. A replica of the prototype workpiece 5 shown at 1.

參閱圖1與圖9,為本實施例的另一實施態樣中的製造流程。此實施態樣的製造流程與前述的圖2之實施態樣的製造流程相近,主要不同的地方在於,在此實施態樣的製造流程中,該步驟(C)是省略的,也就是省略該表層結構3的製作。因此,在此實施態樣中,該步驟(D)在將該強化結構2設置於該模框8內時,是將該強化結構2貼靠於該翻印表面71。而在該步驟(E),該主模體1具有互補於該翻印表面71的該主體成型面11,且該主體成型面11適用於互補於該原型表面51的形狀。最後,在該步驟(F),僅將該主模體1與該中介模具7移出該模框8,並將該主模體1與該中介模具7分離,以完成該快速模具100的製作。如此,使得該快速模具100僅包含該主模體1與該強化結構2,同樣也能達到該快速模具100耐壓且不易變形的目的。 Referring to FIG. 1 and FIG. 9 , the manufacturing process of another implementation of this embodiment is shown. The manufacturing process of this embodiment is similar to the manufacturing process of the aforementioned embodiment of FIG. 2 , and the main difference is that in the manufacturing process of this embodiment, the step (C) is omitted, that is, the step (C) is omitted. Fabrication of Surface Structure 3. Therefore, in this embodiment, when the reinforcement structure 2 is disposed in the mold frame 8 in the step (D), the reinforcement structure 2 is abutted against the printing surface 71 . And in this step (E), the main mold body 1 has the main body molding surface 11 complementary to the reprint surface 71 , and the main body molding surface 11 is adapted to be complementary to the shape of the prototype surface 51 . Finally, in this step (F), only the main mold body 1 and the intermediate mold 7 are moved out of the mold frame 8 , and the main mold body 1 and the intermediate mold 7 are separated to complete the production of the rapid mold 100 . In this way, the quick die 100 only includes the main die body 1 and the reinforcement structure 2 , and the purpose of the quick die 100 being pressure resistant and not easily deformed can also be achieved.

綜上所述,藉由該主模體1包覆於該強化結構2,製得可用於仿製該原型工件5的快速模具100,同時,該強化結構2的機械強度優於該主模體1的機械強度,如此,可使得該快速模具100整體的機械強度提升,因此,能達到該快速模具100用於射出成型的過程中耐壓且不易變形的目的。除此之外,藉由與該主模體1相同材質的該表層結構3包覆於該主模體1外圍,可避免該快速模具100的該強化結構2顯露於模具的表面,使該快速模具100的表面為一體成形 的結構而無接縫。如此,在該快速模具100用於射出成型的製程時,能避免射出成型的高壓塑料由接縫處溢入的情形,同樣也能達到該快速模具100耐壓且不易變形的目的,故確實能達成本發明的目的。 To sum up, by wrapping the main mold body 1 on the reinforcement structure 2 , a rapid mold 100 that can be used to imitate the prototype workpiece 5 is obtained, and at the same time, the mechanical strength of the reinforcement structure 2 is superior to that of the main mold body 1 . In this way, the overall mechanical strength of the rapid mold 100 can be improved, and therefore, the purpose of the rapid mold 100 being pressure-resistant and not easily deformed during injection molding can be achieved. In addition, by covering the periphery of the main mold body 1 with the surface layer structure 3 of the same material as the main mold body 1, the reinforcing structure 2 of the rapid mold 100 can be prevented from being exposed on the surface of the mold, so that the rapid The surface of the mold 100 is integrally formed structure without seams. In this way, when the rapid mold 100 is used in the injection molding process, it can avoid the situation that the injection-molded high-pressure plastic overflows from the seam, and also achieves the purpose of the rapid mold 100 being pressure resistant and not easily deformed, so it can indeed be achieve the purpose of the present invention.

惟以上所述者,僅為本發明的實施例而已,當不能以此限定本發明實施的範圍,凡是依本發明申請專利範圍及專利說明書內容所作的簡單的等效變化與修飾,皆仍屬本發明專利涵蓋的範圍內。 However, the above are only examples of the present invention, and should not limit the scope of implementation of the present invention. Any simple equivalent changes and modifications made according to the scope of the patent application of the present invention and the contents of the patent specification are still included in the scope of the present invention. within the scope of the invention patent.

100:快速模具 100: Quick Die

1:主模體 1: Main Motif

11:主體成型面 11: Main body molding surface

2:強化結構 2: Strengthen the structure

21:基體單元 21: Base unit

3:表層結構 3: Surface structure

31:表層貼合面 31: Surface bonding surface

32:表層成型面 32: Surface molding surface

5:原型工件 5: Prototype Artifacts

51:原型表面 51: Prototype Surface

Claims (4)

一種具有強化結構的快速模具的製造方法,藉由一原型工件及一模框進行,該原型工件具有一供翻印的原型表面,該製造方法包含以下步驟:一步驟(A),利用一翻製方法以該原型工件的該原型表面,製作一中介模具,該中介模具具有一對應於該原型表面的翻印表面;一步驟(B),將該中介模具設置於該模框內,並使該翻印表面朝外開放;一步驟(C),將一可固性的複合材料塗佈於該模框的內表面以及該中介模具的該翻印表面之後,加熱使該複合材料固化形成一表層結構,該表層結構包括兩相反的一表層貼合面及一表層成型面,該表層成型面互補於該翻印表面的形狀;一步驟(D),將一強化結構設置於該模框內,且貼靠於該表層貼合面,該強化結構的機械強度優於該複合材料固化後的機械強度;一步驟(E),將該複合材料澆注於該模框內之後,加熱使該複合材料固化形成一包覆於該強化結構的主模體,且該主模體貼合該表層結構的該表層貼合面;及一步驟(F),將該表層結構、該主模體與該中介模具移出該模框,並將該表層結構與該主模體的組合體與該中介模具分離,以完成該快速模具的製作。 A method of manufacturing a rapid mold with a reinforced structure is carried out by a prototype workpiece and a mold frame, the prototype workpiece having a prototype surface for reprinting, the manufacturing method comprising the following steps: a step (A), using a reproduction The method uses the prototype surface of the prototype workpiece to make an intermediate mold, the intermediate mold has a reprint surface corresponding to the prototype surface; a step (B), the intermediate mold is arranged in the mold frame, and the reprint is made. The surface is open to the outside; a step (C), after coating a curable composite material on the inner surface of the mold frame and the reprinted surface of the intermediate mold, heating to solidify the composite material to form a surface layer structure, the The surface layer structure includes two opposite surface layer adhering surfaces and a surface layer forming surface, the surface layer forming surface is complementary to the shape of the reprinted surface; a step (D), disposing a reinforcing structure in the mold frame, and abutting on the The mechanical strength of the reinforced structure is better than the mechanical strength of the composite material after the surface layer is attached to the surface; in a step (E), after the composite material is poured into the mold frame, the composite material is cured by heating to form a package The main mold body covering the reinforcement structure, and the main mold body is attached to the surface layer adhering surface of the surface layer structure; and a step (F), the surface layer structure, the main mold body and the intermediate mold are moved out of the mold frame , and separate the combination of the surface layer structure and the main mold body from the intermediate mold to complete the production of the rapid mold. 如請求項1所述的具有強化結構的快速模具的製造方法,其中,該步驟(D)是將數個基體單元以堆疊方式排列,形成該強化結構。 The method for manufacturing a rapid mold with a reinforced structure as claimed in claim 1, wherein the step (D) is to arrange a plurality of base units in a stacked manner to form the reinforced structure. 如請求項2所述的具有強化結構的快速模具的製造方法,其中,該 步驟(D)是將該等基體單元依據該主模體的相似形態彼此排列堆疊,使該強化結構呈現為該主模體的順型形態。 The method for manufacturing a rapid mold with a reinforced structure as claimed in claim 2, wherein the In step (D), the base units are arranged and stacked on each other according to the similar shape of the main pattern body, so that the reinforcement structure exhibits a cis-shape shape of the main pattern body. 一種具有強化結構的快速模具的製造方法,藉由一模框及一原型工件,該原型工件具有一供翻印的原型表面,該製造方法包含以下步驟:一步驟(A),利用一翻製方法以該原型工件的該原型表面,製作一中介模具,該中介模具具有一對應於該原型表面的翻印表面;一步驟(B),將該中介模具設置於該模框內,並使該翻印表面朝外開放;一步驟(D),將一強化結構設置於該模框內,且貼靠於該翻印表面;一步驟(E),將一可固性的複合材料澆注於該模框內之後,加熱使該複合材料固化形成一包覆於該強化結構的主模體,該主模體具有一互補於該翻印表面的主體成型面,該主體成型面適用於互補於該原型表面的形狀,其中,該強化結構的機械強度優於該複合材料固化後的機械強度;及一步驟(F),將該主模體與該中介模具移出該模框,並將該主模體與該中介模具分離,以完成該快速模具的製作。 A method for manufacturing a rapid mold with a reinforced structure, using a mold frame and a prototype workpiece, the prototype workpiece having a prototype surface for reprinting, the manufacturing method comprising the following steps: a step (A), using a reproducing method Using the prototype surface of the prototype workpiece to make an intermediate mold, the intermediate mold has a reprint surface corresponding to the prototype surface; a step (B), the intermediate mold is arranged in the mold frame, and the reprint surface is made open to the outside; a step (D), disposing a reinforcing structure in the mold frame, and abutting on the reprinted surface; a step (E), pouring a curable composite material into the mold frame after , heating to solidify the composite material to form a main mold body covering the reinforcing structure, the main mold body having a main molding surface complementary to the reprinted surface, and the main molding surface is suitable for complementing the shape of the prototype surface, wherein, the mechanical strength of the reinforcing structure is better than the mechanical strength of the composite material after curing; and a step (F), removing the main mold body and the intermediate mold from the mold frame, and removing the main mold body and the intermediate mold separation to complete the making of this quick mold.
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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005051627A1 (en) * 2003-11-28 2005-06-09 Moldkar Teknolayer, S.L. Method of producing rapid moulds which are used for plastics processing, and mould thus obtained
TW201438866A (en) * 2013-04-11 2014-10-16 Minchi University Of Technology Rapid tooling manufacturing method
TWI620653B (en) * 2017-02-06 2018-04-11 財團法人塑膠工業技術發展中心 A method for producing a rapid tooling with reinforcement structure
CN111300693A (en) * 2020-04-09 2020-06-19 江苏九铸合金新材料有限公司 Alloy die manufacturing process and die manufactured by same

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005051627A1 (en) * 2003-11-28 2005-06-09 Moldkar Teknolayer, S.L. Method of producing rapid moulds which are used for plastics processing, and mould thus obtained
TW201438866A (en) * 2013-04-11 2014-10-16 Minchi University Of Technology Rapid tooling manufacturing method
TWI620653B (en) * 2017-02-06 2018-04-11 財團法人塑膠工業技術發展中心 A method for producing a rapid tooling with reinforcement structure
CN111300693A (en) * 2020-04-09 2020-06-19 江苏九铸合金新材料有限公司 Alloy die manufacturing process and die manufactured by same

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