WO2022099540A1 - Suitcase formed from composite material and manufacturing method therefor - Google Patents
Suitcase formed from composite material and manufacturing method therefor Download PDFInfo
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- WO2022099540A1 WO2022099540A1 PCT/CN2020/128355 CN2020128355W WO2022099540A1 WO 2022099540 A1 WO2022099540 A1 WO 2022099540A1 CN 2020128355 W CN2020128355 W CN 2020128355W WO 2022099540 A1 WO2022099540 A1 WO 2022099540A1
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- carbon fiber
- fiber plastic
- layer
- thermosetting carbon
- shell
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- A—HUMAN NECESSITIES
- A45—HAND OR TRAVELLING ARTICLES
- A45C—PURSES; LUGGAGE; HAND CARRIED BAGS
- A45C13/00—Details; Accessories
- A45C13/36—Reinforcements for edges, corners, or other parts
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- A—HUMAN NECESSITIES
- A45—HAND OR TRAVELLING ARTICLES
- A45C—PURSES; LUGGAGE; HAND CARRIED BAGS
- A45C5/00—Rigid or semi-rigid luggage
- A45C5/03—Suitcases
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C51/00—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C69/00—Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore
Definitions
- the present invention relates to a carbon fiber product, in particular to a manufacturing method of a composite material-shaped luggage case and a composite material-shaped luggage case produced by the manufacturing method.
- the luggage currently sold on the market is usually made of thermoplastic or aluminum-magnesium alloy.
- the luggage is usually composed of two half shells. Manufacturers usually The fabric will be sewn on the inside of the half shell, the two half shells will be pivoted to each other, and the wheels and handles will be assembled to make the finished luggage. Therefore, some luggage made of thermoplastics (such as ABS resin) may be broken and damaged, which will cause inconvenience to travelers, and even need to buy a new luggage for replacement.
- thermoplastics such as ABS resin
- the applicant proposed a method for manufacturing a luggage case on 2018/06/20 (Taiwan Invention Patent No. 202003202A), which utilizes a vacuum forming process to make a thermoplastic sheet into a case, Then set the shell on the inner die area of the heating mold and make the outer surface of the shell correspond to the inner wall surface of the inner die area, then set the thermosetting plastic layer on the inner surface of the shell, and finally set the airbag on the inner surface of the shell.
- Taiwan's new patent No. M579915 discloses a corner protection structure for a luggage case.
- the plastic shell at the corners of the box is not directly impacted to reduce the problem of cracking at the corners.
- the main purpose of the present invention is to provide a method for manufacturing a suitcase formed by a composite material.
- the suitcase formed by the composite material produced by the method has the advantage of better structural strength, especially for the exterior of the suitcase that requires the composite material to be formed. In the case of uniform structure, it still has the effect of impact resistance and collision resistance at the corners.
- the manufacturing method of the composite material-shaped suitcase of the present invention includes the following steps: A) using a vacuum molding process (vacuum molding method) to make a thermoplastic sheet into a shell, the shell has an outer surface, an inner surface, an accommodating area surrounded by the inner surface, and a corner; B) provide a heating mold, the heating mold has an inner female mold area, and the shell is arranged on the inner female mold C) provide a thermosetting carbon fiber plastic layer, the thermosetting carbon fiber plastic layer has an outer surface and an inner surface, the outer surface of the thermosetting carbon fiber plastic layer is provided on the inner surface of the shell; D) provide a reinforcement layer, the reinforcement layer is arranged on the inner surface of the thermosetting carbon fiber plastic layer and is located at the corner of the shell; and E) an airbag is arranged on the shell of the shell accommodating area, and make the air bag expand to support the inner surface of the thermosetting carbon fiber plastic layer and the reinforcing layer, and at the same time let the heating mold in
- the reinforcing layer is a thermosetting carbon fiber plastic.
- thermosetting carbon fiber plastic layer is cured after being heated by the heating mold and adhered to the inner surface of the casing.
- the reinforcing layer is a metal layer
- the manufacturing method further comprises the step of providing another thermosetting carbon fiber plastic layer, the other thermosetting carbon fiber plastic layer is disposed on the inner surface of the thermosetting carbon fiber plastic layer and the metal layer, the The airbag expands against the other thermosetting carbon fiber plastic layer, and at the same time, the heating mold is heated to the shell, the two thermosetting carbon fiber plastic layers and the metal layer in the inward concave mold area, so that the shell, the two thermosetting carbon fibers are heated.
- the plastic layers are combined with each other, and the metal layer is wrapped in the two thermosetting carbon fiber plastic layers.
- the heating temperature of the inner die zone is between 140 degrees and 150 degrees.
- thermoplastic sheet is a transparent material.
- the manufacturing method further includes the step of providing a pattern, and the pattern is provided on the inner surface of the casing by means of painting, printing or labeling.
- the vacuum forming process is to provide a vacuum molding device with a mold, and put the thermoplastic plastic sheet into the vacuum molding device for heating and softening, and then the vacuum forming
- the apparatus generates negative pressure to attach the thermoplastic sheet to the mold surface to form the housing.
- a step F) is further included after the step E), the airbag is moved out of the accommodating area of the shell, and the luggage case formed from the composite material is cooled.
- the present invention further provides a suitcase made of a composite material formed by the manufacturing method.
- the suitcase formed by the composite material includes a shell, a thermosetting carbon fiber plastic layer and a reinforcing layer, wherein the shell
- the body has an outer surface, an inner surface, an accommodating area surrounded by the inner surface, and a corner
- the thermosetting carbon fiber plastic layer has an outer surface and an inner surface
- the outer surface of the thermosetting carbon fiber plastic layer is provided on the casing.
- the reinforcing layer is arranged on the inner surface of the thermosetting carbon fiber plastic layer and is located at the corner of the shell.
- the composite material-shaped luggage case made by the composite material molding manufacturing method of the present invention can utilize the thermoplastic plastic sheet on the premise that the external structure of the composite material-shaped luggage case is uniform.
- the impact resistance characteristics of the thermosetting carbon fiber plastic layer, as well as the high strength and high bonding characteristics of the thermosetting carbon fiber plastic layer, and the reinforcing layer (thermosetting carbon fiber plastic layer or metal layer) is applied in a specific position according to the needs to achieve better impact resistance and collision resistance effect.
- FIGS. 1 to 3 are schematic diagrams of a method for manufacturing a luggage case formed from a composite material according to a first preferred embodiment of the present invention, which utilizes a vacuum forming process to form a shell from a thermoplastic sheet.
- FIGS. 4 to 5 are schematic diagrams of a method for manufacturing a luggage case formed from a composite material according to the first preferred embodiment of the present invention, in which the casing is set in a heating mold.
- FIG. 6 is a schematic diagram of a method for manufacturing a luggage case formed of a composite material according to the first preferred embodiment of the present invention, in which a thermosetting carbon fiber plastic layer is disposed on the inner surface of the shell.
- thermosetting carbon fiber plastic layer is disposed on the inner surface of the thermosetting carbon fiber plastic layer and is located at a corner of the shell.
- FIGS. 8 to 9 are schematic diagrams of a manufacturing method of a luggage case formed from a composite material according to the first preferred embodiment of the present invention, which utilizes an airbag to support the thermosetting carbon fiber plastic layer and the reinforcing layer.
- FIG. 10 is a cross-sectional view of a luggage case formed by a composite material formed by the manufacturing method according to the first preferred embodiment of the present invention.
- FIGS. 11 to 16 are schematic diagrams of a manufacturing method of a luggage case formed from a composite material according to a second preferred embodiment of the present invention, which is the same as the manufacturing method of FIGS. 1 to 6 .
- FIG. 17 is a schematic diagram of a manufacturing method of a luggage case formed of composite materials according to the second preferred embodiment of the present invention, wherein the reinforcing layer (metal layer) is arranged on the inner surface of the thermosetting carbon fiber plastic layer and is located at the corner of the shell.
- the reinforcing layer metal layer
- FIG. 18 is a schematic diagram of a manufacturing method of a luggage case formed from a composite material according to a second preferred embodiment of the present invention, wherein another thermosetting carbon fiber plastic layer is disposed on the inner surface of the shell and the reinforcing layer.
- 19-20 are schematic diagrams of a manufacturing method of a luggage case formed from a composite material according to a second preferred embodiment of the present invention, which utilizes an airbag to support the thermosetting carbon fiber plastic layer.
- FIG. 21 is a cross-sectional view of a luggage case formed from a composite material produced by a manufacturing method according to a second preferred embodiment of the present invention.
- shell 211 outer surface 213: inner surface
- Thermosetting carbon fiber plastic layer 40 Vacuum forming equipment
- Mould 50 Reinforcing layer (thermosetting carbon fiber plastic layer, metal layer)
- Heating mold 62 Inner die area
- Step S1-2 Step S1-3: Step S1-4: Step
- Step S2-5 Step S2-6: Step S2-7: Step
- FIG. 1 to FIG. 10 are the manufacturing method of the luggage case 10 formed by the composite material according to the first preferred embodiment of the present invention, which includes the following steps:
- Step S1-1 As shown in FIG. 1 to FIG. 3 , a thermoplastic sheet 20 is formed into a shell 21 by a vacuum molding method, and the shell 21 has an outer surface 211 and an inner surface 213 , an accommodating area 215 surrounded by the inner surface 213 and a corner 217, the material of the thermoplastic sheet 20 is selected from PP polypropylene, ABS resin (Acrylonitrile Butadiene Styrene), PC polycarbonate or a combination thereof, of course other Thermoplastics or combinations of thermoplastics are also covered by the present invention; further, the vacuum forming process (also known as the blister process) provided in the first embodiment provides a vacuum with a mold 42 Forming equipment 40, the mold is a male mold, and other auxiliary molds (such as protruding strips) can be set on the male mold to manufacture shells 21 with different shapes, wherein, the thermoplastic sheet 20 needs to be put into the vacuum forming equipment 40 for heating After softening, the vacuum forming apparatus 40 then generates negative pressure to
- Step S1-2 As shown in FIG. 4 to FIG. 5 , a heating mold 60 is provided, the heating mold 60 has an inner concave mold area 62 , the casing 21 is arranged in the inner concave mold area 62 , and the outer part of the casing 21 is formed.
- the surface 211 corresponds to the inner wall surface 64 of the inner die region 62 .
- a thermoplastic sheet 20 of transparent material can be selected in step S1-1, and then the thermoplastic sheet 20 is made into the casing 21, And in step S1-1 or step S1-2, a pattern is set on the inner surface 213 of the housing 21 by painting, printing or labeling.
- thermosetting carbon fiber plastic layer 30 As shown in FIG. 6, a thermosetting carbon fiber plastic layer 30 is provided, the thermosetting carbon fiber plastic layer 30 has an outer surface and an inner surface, and the outer surface of the thermosetting carbon fiber plastic layer 30 is arranged on the inner surface 213 of the housing 21, wherein , the thermosetting plastic of the thermosetting carbon fiber plastic layer 30 is selected from epoxy resin (Epoxy resin) or polyester (Polyester), of course, other thermosetting plastics or combinations of thermosetting plastics are also covered by the present invention.
- epoxy resin epoxy resin
- polyester Polyamide
- Step S1-4 As shown in FIG. 7 , a reinforcing layer 50 is provided.
- the reinforcing layer 50 is a thermosetting carbon fiber plastic, and the reinforcing layer 50 is arranged on the inner surface of the thermosetting carbon fiber plastic layer 30 And it is located at the corners of the casing 21 , thereby reinforcing the most easily damaged corners.
- Step S1-5 As shown in FIG. 8 to FIG. 9 , an airbag 72 is placed in the accommodating area 215 of the housing 21 , and the airbag 72 is inflated and supported against the inner surface of the thermosetting carbon fiber plastic layer 30 and the reinforcing layer 50 , and at the same time Let the heating mold 60 heat the shell 21 , the thermosetting carbon fiber plastic layer 30 and the reinforcement layer 50 in the inner cavity 62 , so that the shell 21 , the thermosetting carbon fiber plastic layer 30 and the reinforcement layer 50 are combined with each other.
- the heating temperature is between 140 degrees Celsius and 150 degrees Celsius, so that the thermosetting carbon fiber plastic layer 30 and the reinforcing layer 50 are cured and bonded to the inner surface 213 of the casing 21, so that the casing 21, the thermosetting carbon fiber plastic layer 30 and the The reinforcing layers 50 are combined with each other to form the composite molded luggage case 10 .
- Step S1-6 As shown in FIG. 9 to FIG. 10 , move the airbag 72 out of the accommodating area 215 of the housing 21, and cool the luggage case 10 formed by the composite material to complete the operation of the luggage case 10 formed by the composite material. manufacturing procedure.
- FIG. 11 to FIG. 21 is a manufacturing method of a luggage case 10 ′ formed by a composite material according to a second preferred embodiment of the present invention, which includes the following steps:
- Steps S2-1 to S2-3 As shown in FIGS. 11 to 16 , steps S2-1 to S2-3 of the second preferred embodiment of the present invention are the same as steps S1-1 to S1-3 of the first preferred embodiment , so it is not repeated here.
- Step S2-4 As shown in FIG. 17 , a reinforcing layer 50 is provided.
- the reinforcing layer 50 is a metal layer, which can also be Kevlar fiber.
- the metal layer 50 is provided On the inner surface of the thermosetting carbon fiber plastic layer 30 and at the corner 217 of the casing 21 .
- Step S2-5 As shown in FIG. 18 , another thermosetting carbon fiber plastic layer 30 is provided, and another thermosetting carbon fiber plastic layer 30 is disposed on the inner surface of the thermosetting carbon fiber plastic layer 30 and the metal layer 50 .
- Step S2-6 As shown in FIGS. 19 to 20 , use the airbag 72 to expand and support the other thermosetting carbon fiber plastic layer 30 , and at the same time let the heating mold 60 face the shell 21 and the two thermosetting carbon fiber plastic layers 30 in the concave mold area 62 And the metal layer 50 is heated, so that the shell 21 and the two thermosetting carbon fiber plastic layers 30 are combined with each other, and the metal layer 50 is wrapped in the two thermosetting carbon fiber plastic layers 30 .
- Step S2-7 As shown in FIGS. 20-21, the airbag 72 is moved out of the accommodating area 215 of the housing 21, and the composite material-shaped luggage case 10' is cooled to complete the composite material-shaped luggage case 10' manufacturing procedure.
- the suitcases 10 and 10' formed by composite materials made by the composite carbon fiber manufacturing method in the present invention can be used under the premise that the external structures of the suitcases 10 and 10' formed by composite materials are uniform.
- the impact resistance properties of the thermoplastic sheet 20, and the high strength and high bonding properties of the thermosetting carbon fiber plastic layer 30, and the reinforcing layer (thermosetting carbon fiber plastic layer or metal layer) 50 is applied at a specific position according to the requirements to achieve higher Excellent impact and collision resistance.
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Abstract
Disclosed are a suitcase formed from a composite material and a manufacturing method therefor. The method comprises the following steps: A) fabricating a housing using a thermoplastic sheet material by means of a vacuum forming process; B) disposing the housing in a recessed mold region of a heating mold, such that an outer surface of the housing corresponds to an inner wall surface of the recessed mold region; C) disposing an outer surface of a thermosetting carbon fiber plastic layer on an inner surface of the housing; D) disposing a reinforcement layer on an inner surface of the thermosetting carbon fiber plastic layer and at corners of the housing; and E) disposing an airbag in an accommodation region of the housing, such that the airbag is expanded and abuts the inner surface of the thermosetting carbon fiber plastic layer and the reinforcement layer, and simultaneously heating, by means of the heating mold, the housing, the thermosetting carbon fiber plastic layer and the reinforcement layer in the recessed mold region, such that the housing, the thermosetting carbon fiber plastic layer and the reinforcement layer are combined with each other.
Description
本发明涉及一种碳纤维制品,特别是一种复合材料成型的行李箱的制造方法及使用该制造方法所制成的复合材料成型的行李箱。The present invention relates to a carbon fiber product, in particular to a manufacturing method of a composite material-shaped luggage case and a composite material-shaped luggage case produced by the manufacturing method.
目前市面上贩卖的行李箱通常为热塑性塑料或是铝镁合金的材质制成,以热塑性塑料制成的行李箱来说,行李箱通常会由两个半壳体所组合而成,制造商通常会在半壳体内侧缝上布料,并将两个半壳体相互枢接,并组装上轮子及手把以制成行李箱成品,其中,当行李箱于机场运输线运送时,可能会面临碰撞以及掉落的状况,因此,某些热塑性塑料(例如ABS树脂)制成的行李箱可能会有破裂损坏的情形发生,进而造成旅者的不便,甚至需要再购买新的行李箱进行替换。The luggage currently sold on the market is usually made of thermoplastic or aluminum-magnesium alloy. For luggage made of thermoplastic, the luggage is usually composed of two half shells. Manufacturers usually The fabric will be sewn on the inside of the half shell, the two half shells will be pivoted to each other, and the wheels and handles will be assembled to make the finished luggage. Therefore, some luggage made of thermoplastics (such as ABS resin) may be broken and damaged, which will cause inconvenience to travelers, and even need to buy a new luggage for replacement.
为克服上述的缺失,申请人于2018/06/20提出一行李箱壳体的制造方法(台湾发明第202003202A号专利案),其利用真空成型工艺将一热塑性塑料片材制成一壳体,再将壳体设置于加热模具的内凹模区并使壳体的外表面对应内凹模区的内壁面,接着将热固性塑料层设置于壳体的内表面,最后利用气囊设置于壳体的容置区,并使气囊膨胀撑抵热固性塑料层,同时使加热模具向内凹模区内的壳体及热固性塑料层进行加热,使得壳体及热固性塑料层相互结合以制成行李箱壳体,由此达到补强结构强度并兼具减低行李箱壳体的整体重量的功效。In order to overcome the above deficiencies, the applicant proposed a method for manufacturing a luggage case on 2018/06/20 (Taiwan Invention Patent No. 202003202A), which utilizes a vacuum forming process to make a thermoplastic sheet into a case, Then set the shell on the inner die area of the heating mold and make the outer surface of the shell correspond to the inner wall surface of the inner die area, then set the thermosetting plastic layer on the inner surface of the shell, and finally set the airbag on the inner surface of the shell. accommodating area, and make the airbag inflate against the thermosetting plastic layer, and at the same time make the heating mold heat the shell and the thermosetting plastic layer in the inner female mold area, so that the shell and the thermosetting plastic layer are combined with each other to make the luggage case shell , thereby achieving the effect of reinforcing the structural strength and reducing the overall weight of the luggage case.
此外,为了补强行李箱角隅处的强度,如台湾新型第M579915号专利案公开一种行李箱的护角结构,于行李箱角隅处的外表面固设护角结构,由此让行李箱角隅处的塑料壳体不会直接受到撞击,以减低角隅处破裂的问题。In addition, in order to strengthen the strength of the corners of the luggage case, for example, Taiwan's new patent No. M579915 discloses a corner protection structure for a luggage case. The plastic shell at the corners of the box is not directly impacted to reduce the problem of cracking at the corners.
发明内容SUMMARY OF THE INVENTION
本发明的主要目的在于提供一种复合材料成型的行李箱的制造方法,该方法制造的复合材料成型的行李箱具有结构强度较佳的优点,尤其是对于要求该复合材料成型的行李箱的外部结构一致化的情况下,仍兼具角隅处具耐冲击、耐碰撞的功效。The main purpose of the present invention is to provide a method for manufacturing a suitcase formed by a composite material. The suitcase formed by the composite material produced by the method has the advantage of better structural strength, especially for the exterior of the suitcase that requires the composite material to be formed. In the case of uniform structure, it still has the effect of impact resistance and collision resistance at the corners.
为了达成上述主要目的,本发明的复合材料成型的行李箱的制造方法包含有下列步骤:A)利用真空成型工艺(vacuum molding method)将一热塑性塑料片材制成一壳体,该壳体具有一外表面、一内表面、一由该内表面围绕出的容置区以及一角落;B)提供一加热模具,该加热模具具一内凹模区,将该壳体设置于该内凹模区,并使该壳体的外表面对应该内凹模区的内壁面;C)提供一热固性碳纤维塑料层,该热固性碳纤维塑料层具有一外面及一内面,将该热固性碳纤维塑料层的外面设于该壳体的内表面;D)提供一补强层,将该补强层设置于该热固性碳纤维塑料层的内面且位于该壳体的角落;以及E)将一气囊设置于该壳体的容置区,并使该气囊膨胀撑抵该热固性碳纤维塑料层的内面及该补强层,同时让该加热模具向内凹模区内的该壳体、该热固性碳纤维塑料层及该补强层进行加热,使得该壳体、该热固性碳纤维塑料层以及该补强层相互结合。In order to achieve the above-mentioned main purpose, the manufacturing method of the composite material-shaped suitcase of the present invention includes the following steps: A) using a vacuum molding process (vacuum molding method) to make a thermoplastic sheet into a shell, the shell has an outer surface, an inner surface, an accommodating area surrounded by the inner surface, and a corner; B) provide a heating mold, the heating mold has an inner female mold area, and the shell is arranged on the inner female mold C) provide a thermosetting carbon fiber plastic layer, the thermosetting carbon fiber plastic layer has an outer surface and an inner surface, the outer surface of the thermosetting carbon fiber plastic layer is provided on the inner surface of the shell; D) provide a reinforcement layer, the reinforcement layer is arranged on the inner surface of the thermosetting carbon fiber plastic layer and is located at the corner of the shell; and E) an airbag is arranged on the shell of the shell accommodating area, and make the air bag expand to support the inner surface of the thermosetting carbon fiber plastic layer and the reinforcing layer, and at the same time let the heating mold inwardly move the shell, the thermosetting carbon fiber plastic layer and the reinforcing layer in the concave mold area Heating is performed so that the shell, the thermosetting carbon fiber plastic layer and the reinforcing layer are bonded to each other.
优选地,于步骤D)中,该补强层为热固性碳纤维塑料。Preferably, in step D), the reinforcing layer is a thermosetting carbon fiber plastic.
优选地,于步骤E)中,该热固性碳纤维塑料层经该加热模具加热后固化并黏接于该壳体的内表面。Preferably, in step E), the thermosetting carbon fiber plastic layer is cured after being heated by the heating mold and adhered to the inner surface of the casing.
优选地,该补强层为金属层,且该制造方法更包含提供另一热固性碳纤维塑料层的步骤,将该另一热固性碳纤维塑料层设置于该热固性碳纤维塑料层的内面及该金属层,该气囊膨胀撑抵该另一热固性碳纤维塑料层,同时让该加热模具向内凹模区内的该壳体、该二热固性碳纤维塑料层及该金属层进行加热,使得该壳体、该二热固性碳纤维塑料层相互结合,并将该金属层包覆于该二热固性碳纤维塑料层之中。Preferably, the reinforcing layer is a metal layer, and the manufacturing method further comprises the step of providing another thermosetting carbon fiber plastic layer, the other thermosetting carbon fiber plastic layer is disposed on the inner surface of the thermosetting carbon fiber plastic layer and the metal layer, the The airbag expands against the other thermosetting carbon fiber plastic layer, and at the same time, the heating mold is heated to the shell, the two thermosetting carbon fiber plastic layers and the metal layer in the inward concave mold area, so that the shell, the two thermosetting carbon fibers are heated. The plastic layers are combined with each other, and the metal layer is wrapped in the two thermosetting carbon fiber plastic layers.
优选地,在步骤E)中,该内凹模区加热的温度介于140度~150度之间。Preferably, in step E), the heating temperature of the inner die zone is between 140 degrees and 150 degrees.
优选地,在步骤A)中,该热塑性塑料片材为透明材质。Preferably, in step A), the thermoplastic sheet is a transparent material.
优选地,该制造方法更包含有提供一图案的步骤,该图案以喷漆、印刷或贴标签的方式设置于该壳体的内表面。Preferably, the manufacturing method further includes the step of providing a pattern, and the pattern is provided on the inner surface of the casing by means of painting, printing or labeling.
优选地,在步骤A)中,该真空成型工艺为提供一具有一模具的真空成型设备(vacuum molding device),并将该热塑性塑料片材放入该真空成型设备进行加热软化,接着该真空成型设备产生负压使该热塑性塑料片材贴附于该模具表面以制成该壳体。Preferably, in step A), the vacuum forming process is to provide a vacuum molding device with a mold, and put the thermoplastic plastic sheet into the vacuum molding device for heating and softening, and then the vacuum forming The apparatus generates negative pressure to attach the thermoplastic sheet to the mold surface to form the housing.
优选地,在步骤E)之后更包含一步骤F),将该气囊移出该壳体的容置区,并将该复合材料成型的行李箱进行冷却。Preferably, a step F) is further included after the step E), the airbag is moved out of the accommodating area of the shell, and the luggage case formed from the composite material is cooled.
优选地,本发明更提供一种使用该制造方法所制成的复合材料成型的行李箱,该复合材料成型的行李箱包含有一壳体、一热固性碳纤维塑料层以及一补强层,其中该壳体具有一外表面、一内表面、一由该内表面围绕出的容置区以及一角落,该热固性碳纤维塑料层具有一外面及一内面,该热固性碳纤维塑料层的外面设于该壳体的内表面,该补强层设置于该热固性碳纤维塑料层的内面且位于该壳体的角落。Preferably, the present invention further provides a suitcase made of a composite material formed by the manufacturing method. The suitcase formed by the composite material includes a shell, a thermosetting carbon fiber plastic layer and a reinforcing layer, wherein the shell The body has an outer surface, an inner surface, an accommodating area surrounded by the inner surface, and a corner, the thermosetting carbon fiber plastic layer has an outer surface and an inner surface, and the outer surface of the thermosetting carbon fiber plastic layer is provided on the casing. On the inner surface, the reinforcing layer is arranged on the inner surface of the thermosetting carbon fiber plastic layer and is located at the corner of the shell.
由上述可知,本发明使用该复合材料成型的制造方法所制成的复合材料成型的行李箱,能在该复合材料成型的行李箱的外部结构为一致化的前提下,利用该热塑性塑料片材的耐冲击特性,以及该热固性碳纤维塑料层的高强度与高结合度特性,并因应需求在特定位置施加该补强层(热固性碳纤维塑料层或金属层),以达到较佳耐冲击及耐碰撞的功效。It can be seen from the above that the composite material-shaped luggage case made by the composite material molding manufacturing method of the present invention can utilize the thermoplastic plastic sheet on the premise that the external structure of the composite material-shaped luggage case is uniform. The impact resistance characteristics of the thermosetting carbon fiber plastic layer, as well as the high strength and high bonding characteristics of the thermosetting carbon fiber plastic layer, and the reinforcing layer (thermosetting carbon fiber plastic layer or metal layer) is applied in a specific position according to the needs to achieve better impact resistance and collision resistance effect.
有关本发明所提供的详细构造、特点,将于后续的实施方式详细说明中予以描述。然而,在本领域中具有通常知识者应能了解,该等详细说明以及实施本发明所列举的特定实施例,仅用于说明本发明,并非用以限制本发明的保护范围。The detailed structure and features provided by the present invention will be described in the detailed description of the following embodiments. However, those skilled in the art should understand that these detailed descriptions and specific embodiments for implementing the present invention are only used to illustrate the present invention, and not to limit the protection scope of the present invention.
图1~3为本发明第一优选实施例的复合材料成型的行李箱的制造方法的示意图,其利用真空成型工艺将热塑性塑料片材制成壳体。1 to 3 are schematic diagrams of a method for manufacturing a luggage case formed from a composite material according to a first preferred embodiment of the present invention, which utilizes a vacuum forming process to form a shell from a thermoplastic sheet.
图4~5为本发明第一优选实施例的复合材料成型的行李箱的制造方法的示意图,其将壳体设置于加热模具。4 to 5 are schematic diagrams of a method for manufacturing a luggage case formed from a composite material according to the first preferred embodiment of the present invention, in which the casing is set in a heating mold.
图6为本发明第一优选实施例的复合材料成型的行李箱的制造方法的示意图,其将热固性碳纤维塑料层设置于壳体内表面。FIG. 6 is a schematic diagram of a method for manufacturing a luggage case formed of a composite material according to the first preferred embodiment of the present invention, in which a thermosetting carbon fiber plastic layer is disposed on the inner surface of the shell.
图7为本发明第一优选实施例的复合材料成型的行李箱的制造方法的示意图,其将补强层(热固性碳纤维塑料层)设置于热固性碳纤维塑料层内面且位于壳体的角落。7 is a schematic diagram of the first preferred embodiment of the method for manufacturing a suitcase made of composite materials, wherein a reinforcing layer (thermosetting carbon fiber plastic layer) is disposed on the inner surface of the thermosetting carbon fiber plastic layer and is located at a corner of the shell.
图8~9为本发明第一优选实施例的复合材料成型的行李箱的制造方法的示意图,其利用气囊撑抵热固性碳纤维塑料层及补强层。8 to 9 are schematic diagrams of a manufacturing method of a luggage case formed from a composite material according to the first preferred embodiment of the present invention, which utilizes an airbag to support the thermosetting carbon fiber plastic layer and the reinforcing layer.
图10为本发明第一优选实施利的制造方法所制成的复合材料成型的行李箱的剖视图。FIG. 10 is a cross-sectional view of a luggage case formed by a composite material formed by the manufacturing method according to the first preferred embodiment of the present invention.
图11~16为本发明第二优选实施例的复合材料成型的行李箱的制造方法的示意图,其与图1~6的制造方法相同。11 to 16 are schematic diagrams of a manufacturing method of a luggage case formed from a composite material according to a second preferred embodiment of the present invention, which is the same as the manufacturing method of FIGS. 1 to 6 .
图17为本发明第二优选实施例的复合材料成型的行李箱的制造方法的示意图,其将补强层(金属层)设置于热固性碳纤维塑料层内面且位于壳体的角落。17 is a schematic diagram of a manufacturing method of a luggage case formed of composite materials according to the second preferred embodiment of the present invention, wherein the reinforcing layer (metal layer) is arranged on the inner surface of the thermosetting carbon fiber plastic layer and is located at the corner of the shell.
图18为本发明第二优选实施例的复合材料成型的行李箱的制造方法的示意图,其将另一热固性碳纤维塑料层设置于壳体的内表面及补强层上。18 is a schematic diagram of a manufacturing method of a luggage case formed from a composite material according to a second preferred embodiment of the present invention, wherein another thermosetting carbon fiber plastic layer is disposed on the inner surface of the shell and the reinforcing layer.
图19~20为本发明第二优选实施例的复合材料成型的行李箱的制造方法的示意图,其利用气囊撑抵热固性碳纤维塑料层。19-20 are schematic diagrams of a manufacturing method of a luggage case formed from a composite material according to a second preferred embodiment of the present invention, which utilizes an airbag to support the thermosetting carbon fiber plastic layer.
图21为本发明第二优选实施利的制造方法所制成的复合材料成型的行李箱的剖视图。FIG. 21 is a cross-sectional view of a luggage case formed from a composite material produced by a manufacturing method according to a second preferred embodiment of the present invention.
10、10':复合材料成型的行李箱 20:热塑性塑料片材10, 10': Composite molded luggage 20: Thermoplastic sheet
21:壳体 211:外表面 213:内表面21: shell 211: outer surface 213: inner surface
215:容置区 217:角落 219:料边215: accommodating area 217: corner 219: material edge
30:热固性碳纤维塑料层 40:真空成型设备30: Thermosetting carbon fiber plastic layer 40: Vacuum forming equipment
42:模具 50:补强层(热固性碳纤维塑料层、金属层)42: Mould 50: Reinforcing layer (thermosetting carbon fiber plastic layer, metal layer)
60:加热模具 62:内凹模区60: Heating mold 62: Inner die area
64:内壁面 72:气囊 S1-1:步骤64: Inner wall surface 72: Airbag S1-1: Step
S1-2:步骤 S1-3:步骤 S1-4:步骤S1-2: Step S1-3: Step S1-4: Step
S1-5:步骤 S1-6:步骤 S2-1:步骤S1-5: Step S1-6: Step S2-1: Step
S2-2:步骤 S2-3:步骤 S2-4:步骤S2-2: Step S2-3: Step S2-4: Step
S2-5:步骤 S2-6:步骤 S2-7:步骤S2-5: Step S2-6: Step S2-7: Step
为使本发明的目的、技术方案和优点更加清楚明白,以下结合具体实施例,并参照附图,对本发明做进一步的详细说明。In order to make the objectives, technical solutions and advantages of the present invention more clearly understood, the present invention will be further described in detail below in conjunction with specific embodiments and with reference to the accompanying drawings.
申请人首先在此说明,于整篇说明书中,包括以下介绍的实施例以及权利要求书的权利要求中,有关方向性的名词皆以附图中的方向为基准。其次,在以下将要介绍的实施例以及附图中,相同的元件标号,代表相同或近似的元件或其结构特征。The applicant first explains that in the entire specification, including the embodiments described below and the claims in the claims, the terms related to the directionality are based on the directions in the drawings. Next, in the embodiments to be introduced below and the accompanying drawings, the same element numbers represent the same or similar elements or their structural features.
请先参阅图1~图10,为本发明第一优选实施例的复合材料成型的行李箱10的制造方法,其包含以下步骤:Please refer to FIG. 1 to FIG. 10 first, which are the manufacturing method of the luggage case 10 formed by the composite material according to the first preferred embodiment of the present invention, which includes the following steps:
步骤S1-1:如图1~图3所示,利用真空成型工艺(vacuum molding method)将一热塑性塑料片材20制成一壳体21,壳体21具有一外表面211、一内表面213、一由内表面213围绕出的容置区215以及一角落217,热塑性塑料片材20的材料选自PP聚丙烯、ABS树脂(Acrylonitrile Butadiene Styrene)、PC聚碳酸酯或是其组合,当然其它的热塑性塑料或是热塑性塑料的组合亦为本发明所涵盖;更进一步来说,在第一实施例中所提供的真空成型工艺(亦称吸塑工艺),提供一种具有一模具42的真空成型设备40,模具为公模,并且公模上可设置其他辅助模具(例如凸条)以制造出不同外形的壳体21,其中,需将热塑性塑料片材20放入真空成型设备40进行加热软化,接着真空成型设备40随即产生负压使热塑性塑料片材20贴附于模具42表面以制成壳体21,其中,真空成型设备40加热软化热塑性塑料片材20以及产生负压使热塑性塑料片材20贴附于模具42表面以制成壳体21的技术内容为现有技术,于此不再赘述。此外,利用真空成型设备 40制作成壳体21时,壳体21的周围会留下料边219,如图2所示,因此通常会进行二度加工以切除料边,以形成如图3所示的壳体21。Step S1-1: As shown in FIG. 1 to FIG. 3 , a thermoplastic sheet 20 is formed into a shell 21 by a vacuum molding method, and the shell 21 has an outer surface 211 and an inner surface 213 , an accommodating area 215 surrounded by the inner surface 213 and a corner 217, the material of the thermoplastic sheet 20 is selected from PP polypropylene, ABS resin (Acrylonitrile Butadiene Styrene), PC polycarbonate or a combination thereof, of course other Thermoplastics or combinations of thermoplastics are also covered by the present invention; further, the vacuum forming process (also known as the blister process) provided in the first embodiment provides a vacuum with a mold 42 Forming equipment 40, the mold is a male mold, and other auxiliary molds (such as protruding strips) can be set on the male mold to manufacture shells 21 with different shapes, wherein, the thermoplastic sheet 20 needs to be put into the vacuum forming equipment 40 for heating After softening, the vacuum forming apparatus 40 then generates negative pressure to make the thermoplastic sheet 20 adhere to the surface of the mold 42 to form the shell 21, wherein the vacuum forming apparatus 40 heats and softens the thermoplastic sheet 20 and generates negative pressure to make the thermoplastic The technical content of attaching the sheet 20 to the surface of the mold 42 to form the casing 21 is in the prior art, and will not be repeated here. In addition, when the shell 21 is formed by using the vacuum forming equipment 40 , a trim 219 will be left around the shell 21 , as shown in FIG. housing 21 shown.
步骤S1-2:如图4~图5所示,提供一加热模具60,加热模具60具一内凹模区62,将壳体21设置于内凹模区62,并使壳体21的外表面211对应内凹模区62的内壁面64。此外,若要在壳体21上显示图案(例如商标或是造型图案),可在步骤S1-1中选择透明材质的热塑性塑料片材20,再将热塑性塑料片材20制成壳体21,并在步骤S1-1或步骤S1-2中,将一图案以喷漆、印刷或贴标签地方式设置于壳体21的内表面213。Step S1-2: As shown in FIG. 4 to FIG. 5 , a heating mold 60 is provided, the heating mold 60 has an inner concave mold area 62 , the casing 21 is arranged in the inner concave mold area 62 , and the outer part of the casing 21 is formed. The surface 211 corresponds to the inner wall surface 64 of the inner die region 62 . In addition, if a pattern (such as a trademark or a modeling pattern) is to be displayed on the casing 21, a thermoplastic sheet 20 of transparent material can be selected in step S1-1, and then the thermoplastic sheet 20 is made into the casing 21, And in step S1-1 or step S1-2, a pattern is set on the inner surface 213 of the housing 21 by painting, printing or labeling.
步骤S1-3:如图6所示,提供一热固性碳纤维塑料层30,热固性碳纤维塑料层30具有一外面及一内面,将热固性碳纤维塑料层30的外面设于壳体21的内表面213,其中,热固性碳纤维塑料层30的热固性塑料选自环氧树脂(Epoxy resin)或聚酯(Polyester),当然其它的热固性塑料或是热固性塑料的组合亦为本发明所涵盖。Step S1-3: As shown in FIG. 6, a thermosetting carbon fiber plastic layer 30 is provided, the thermosetting carbon fiber plastic layer 30 has an outer surface and an inner surface, and the outer surface of the thermosetting carbon fiber plastic layer 30 is arranged on the inner surface 213 of the housing 21, wherein , the thermosetting plastic of the thermosetting carbon fiber plastic layer 30 is selected from epoxy resin (Epoxy resin) or polyester (Polyester), of course, other thermosetting plastics or combinations of thermosetting plastics are also covered by the present invention.
步骤S1-4:如图7所示,提供一补强层50,在第一实施例中的补强层50是一种热固性碳纤维塑料,将补强层50设置于热固性碳纤维塑料层30的内面且位于壳体21的角落,由此补强最容易破损的角落地方。Step S1-4: As shown in FIG. 7 , a reinforcing layer 50 is provided. In the first embodiment, the reinforcing layer 50 is a thermosetting carbon fiber plastic, and the reinforcing layer 50 is arranged on the inner surface of the thermosetting carbon fiber plastic layer 30 And it is located at the corners of the casing 21 , thereby reinforcing the most easily damaged corners.
步骤S1-5:如图8~图9所示,将一气囊72设置于壳体21的容置区215,并使气囊72膨胀撑抵热固性碳纤维塑料层30的内面及补强层50,同时让加热模具60向内凹模区62内的壳体21、热固性碳纤维塑料层30及补强层50进行加热,使得壳体21、热固性碳纤维塑料层30以及补强层50相互结合,其中较佳的加热温度介于摄氏140度~150度之间,使得热固性碳纤维塑料层30与补强层50固化并黏接于壳体21的内表面213,进而使壳体21、热固性碳纤维塑料层30与补强层50相互结合以制成复合材料成型的行李箱10。Step S1-5: As shown in FIG. 8 to FIG. 9 , an airbag 72 is placed in the accommodating area 215 of the housing 21 , and the airbag 72 is inflated and supported against the inner surface of the thermosetting carbon fiber plastic layer 30 and the reinforcing layer 50 , and at the same time Let the heating mold 60 heat the shell 21 , the thermosetting carbon fiber plastic layer 30 and the reinforcement layer 50 in the inner cavity 62 , so that the shell 21 , the thermosetting carbon fiber plastic layer 30 and the reinforcement layer 50 are combined with each other. The heating temperature is between 140 degrees Celsius and 150 degrees Celsius, so that the thermosetting carbon fiber plastic layer 30 and the reinforcing layer 50 are cured and bonded to the inner surface 213 of the casing 21, so that the casing 21, the thermosetting carbon fiber plastic layer 30 and the The reinforcing layers 50 are combined with each other to form the composite molded luggage case 10 .
步骤S1-6:如图9~图10所示,将气囊72移出壳体21的容置区215,并将复合材料成型的行李箱10进行冷却,即可完成复合材料成型的行李箱10的制造程序。Step S1-6: As shown in FIG. 9 to FIG. 10 , move the airbag 72 out of the accommodating area 215 of the housing 21, and cool the luggage case 10 formed by the composite material to complete the operation of the luggage case 10 formed by the composite material. manufacturing procedure.
请再参阅图11~图21,为本发明第二优选实施例的复合材料成型的行李箱10'的制造方法,其包含以下步骤:Please refer to FIG. 11 to FIG. 21 again, which is a manufacturing method of a luggage case 10 ′ formed by a composite material according to a second preferred embodiment of the present invention, which includes the following steps:
步骤S2-1~S2-3:如图11~图16所示,本发明第二优选实施例的步骤S2-1~S2-3相同于第一优选实施例的步骤S1-1~S1-3,故不再赘述。Steps S2-1 to S2-3: As shown in FIGS. 11 to 16 , steps S2-1 to S2-3 of the second preferred embodiment of the present invention are the same as steps S1-1 to S1-3 of the first preferred embodiment , so it is not repeated here.
步骤S2-4:如图17所示,提供一补强层50,在第二实施例中的补强层50为金属层,也可为克维拉纤维(Kevlar fiber),将金属层50设置于热固性碳纤维塑料层30的内面且位于壳体21的角落217。Step S2-4: As shown in FIG. 17 , a reinforcing layer 50 is provided. In the second embodiment, the reinforcing layer 50 is a metal layer, which can also be Kevlar fiber. The metal layer 50 is provided On the inner surface of the thermosetting carbon fiber plastic layer 30 and at the corner 217 of the casing 21 .
步骤S2-5:如图18所示,提供另一热固性碳纤维塑料层30,将另一热固性碳纤维塑料层30设置于热固性碳纤维塑料层30的内面及金属层50。Step S2-5: As shown in FIG. 18 , another thermosetting carbon fiber plastic layer 30 is provided, and another thermosetting carbon fiber plastic layer 30 is disposed on the inner surface of the thermosetting carbon fiber plastic layer 30 and the metal layer 50 .
步骤S2-6:如图19~20所示,利用气囊72膨胀撑抵另一热固性碳纤维塑料层30,同时让加热模具60向内凹模区62内的壳体21、二热固性碳纤维塑料层30及金属层50进行加热,使得壳体21、二热固性碳纤维塑料层30相互结合,并将金属层50包覆于二热固性碳纤维塑料层30之中。Step S2-6: As shown in FIGS. 19 to 20 , use the airbag 72 to expand and support the other thermosetting carbon fiber plastic layer 30 , and at the same time let the heating mold 60 face the shell 21 and the two thermosetting carbon fiber plastic layers 30 in the concave mold area 62 And the metal layer 50 is heated, so that the shell 21 and the two thermosetting carbon fiber plastic layers 30 are combined with each other, and the metal layer 50 is wrapped in the two thermosetting carbon fiber plastic layers 30 .
步骤S2-7:如图20~21所示,将气囊72移出壳体21的容置区215,并将复合材料成型的行李箱10'进行冷却,即可完成复合材料成型的行李箱10'的制造程序。Step S2-7: As shown in FIGS. 20-21, the airbag 72 is moved out of the accommodating area 215 of the housing 21, and the composite material-shaped luggage case 10' is cooled to complete the composite material-shaped luggage case 10' manufacturing procedure.
综上所陈,本发明使用复合碳纤维制造方法所制成的复合材料成型的行李箱10、10',能在复合材料成型的行李箱10、10'的外部结构为一致化的前提下,利用热塑性塑料片材20的耐冲击特性,以及热固性碳纤维塑料层30的高强度与高结合度特性,并因应需求在特定位置施加该补强层(热固性碳纤维塑料层或金属层)50,以达到较佳耐冲击及耐碰撞的功效。To sum up, the suitcases 10 and 10' formed by composite materials made by the composite carbon fiber manufacturing method in the present invention can be used under the premise that the external structures of the suitcases 10 and 10' formed by composite materials are uniform. The impact resistance properties of the thermoplastic sheet 20, and the high strength and high bonding properties of the thermosetting carbon fiber plastic layer 30, and the reinforcing layer (thermosetting carbon fiber plastic layer or metal layer) 50 is applied at a specific position according to the requirements to achieve higher Excellent impact and collision resistance.
以上所述的具体实施例,对本发明的目的、技术方案和有益效果进行了进一步详细说明,应理解的是,以上所述仅为本发明的具体实施例而已,并不用于限制本发明,凡在本发明的精神和原则之内,所做的任何修改、等同替换、改进等,均应包括在本发明的保护范围之内。The specific embodiments described above further describe the purpose, technical solutions and beneficial effects of the present invention in detail. It should be understood that the above-mentioned specific embodiments are only specific embodiments of the present invention, and are not intended to limit the present invention. Within the spirit and principle of the present invention, any modifications, equivalent replacements, improvements, etc. made should be included within the protection scope of the present invention.
Claims (13)
- 一种复合材料成型的行李箱的制造方法,包含以下步骤:A manufacturing method of a suitcase formed by composite materials, comprising the following steps:A)利用真空成型工艺(vacuum molding method)将一热塑性塑料片材制成一壳体,该壳体具有一外表面、一内表面、一由该内表面围绕出的容置区以及一角落;A) using a vacuum molding process (vacuum molding method) to form a thermoplastic sheet into a shell, the shell has an outer surface, an inner surface, a receiving area surrounded by the inner surface and a corner;B)提供一加热模具,该加热模具具一内凹模区,将该壳体设置于该内凹模区,并使该壳体的外表面对应该内凹模区的内壁面;B) providing a heating mold, the heating mold has an inner female mold area, the shell is arranged in the inner female mold area, and the outer surface of the shell should correspond to the inner wall surface of the inner female mold area;C)提供一热固性碳纤维塑料层,该热固性碳纤维塑料层具有一外面及一内面,将该热固性碳纤维塑料层的外面设于该壳体的内表面;C) providing a thermosetting carbon fiber plastic layer, the thermosetting carbon fiber plastic layer has an outer surface and an inner surface, and the outer surface of the thermosetting carbon fiber plastic layer is provided on the inner surface of the housing;D)提供一补强层,将该补强层设置于该热固性碳纤维塑料层的内面且位于该壳体的角落;以及D) providing a reinforcement layer, the reinforcement layer is disposed on the inner surface of the thermosetting carbon fiber plastic layer and at the corner of the shell; andE)将一气囊设置于该壳体的容置区,并使该气囊膨胀撑抵该热固性碳纤维塑料层的内面及该补强层,同时让该加热模具向内凹模区内的该壳体、该热固性碳纤维塑料层及该补强层进行加热,使得该壳体、该热固性碳纤维塑料层以及该补强层相互结合。E) Disposing an airbag in the accommodating area of the housing, and inflating the airbag against the inner surface of the thermosetting carbon fiber plastic layer and the reinforcing layer, and at the same time allowing the heating mold to face the housing in the concave mold area , The thermosetting carbon fiber plastic layer and the reinforcing layer are heated, so that the shell, the thermosetting carbon fiber plastic layer and the reinforcing layer are combined with each other.
- 如权利要求1所述的行李箱的制造方法,其中,该补强层为热固性碳纤维塑料。The manufacturing method of a luggage case according to claim 1, wherein the reinforcing layer is a thermosetting carbon fiber plastic.
- 如权利要求1所述的行李箱的制造方法,其中,于步骤E)中,该热固性碳纤维塑料层经该加热模具加热后固化并黏接于该壳体的内表面。The method for manufacturing a luggage case as claimed in claim 1 , wherein, in step E), the thermosetting carbon fiber plastic layer is heated by the heating mold and then cured and adhered to the inner surface of the shell.
- 如权利要求1所述的行李箱的制造方法,其中,该补强层为金属层,且该制造方法更包含提供另一热固性碳纤维塑料层的步骤,将该另一热固性碳纤维塑料层设置于该热固性碳纤维塑料层的内面及该金属层,该气囊膨胀撑抵该另一热固性碳纤维塑料层,同时让该加热模具向内凹模区内的该壳体、该二热固性碳纤维塑料层及该金属层进行加热,使得该壳体、该二热固性碳纤维塑料层相互结合,并将该金属层包覆于该二热固性碳纤维塑料层之中。The manufacturing method of a luggage case according to claim 1, wherein the reinforcing layer is a metal layer, and the manufacturing method further comprises the step of providing another thermosetting carbon fiber plastic layer, and disposing the other thermosetting carbon fiber plastic layer on the The inner surface of the thermosetting carbon fiber plastic layer and the metal layer, the airbag expands and supports the other thermosetting carbon fiber plastic layer, and at the same time, the heating mold is moved inward to the shell, the two thermosetting carbon fiber plastic layers and the metal layer in the female mold area Heating is performed so that the shell and the two thermosetting carbon fiber plastic layers are combined with each other, and the metal layer is wrapped in the two thermosetting carbon fiber plastic layers.
- 如权利要求1所述的行李箱的制造方法,其中,在步骤E)中,该内凹模区加热的温度介于140度~150度之间。The method for manufacturing a luggage case according to claim 1, wherein, in step E), the heating temperature of the inner die area is between 140 degrees and 150 degrees.
- 如权利要求1所述的行李箱的制造方法,其中,在步骤A)中,该热塑性塑料片材为透明材质。The method for manufacturing a luggage case according to claim 1, wherein, in step A), the thermoplastic plastic sheet is made of transparent material.
- 所述复合材料成型的行李箱的制造方法,其中,该制造方法更包含有提供一图案的步骤,该图案以喷漆、印刷或贴标签的方式设置于该壳体的内表面。The manufacturing method of the composite material-shaped suitcase, wherein the manufacturing method further includes the step of providing a pattern, and the pattern is provided on the inner surface of the shell by means of painting, printing or labeling.
- 如权利要求1所述的行李箱的制造方法,其中,在步骤A)中,该真空成型工艺为提供一具有一模具的真空成型设备(vacuum molding device),并将该热塑性塑料片材放入该真空成型设备进行加热软化,接着该真空成型设备产生负压使该热塑性塑料片材贴附于该模具表面以制成该壳体。The manufacturing method of a luggage case as claimed in claim 1, wherein, in step A), the vacuum forming process is to provide a vacuum molding device with a mold, and put the thermoplastic plastic sheet into The vacuum forming equipment is heated and softened, and then the vacuum forming equipment generates negative pressure to make the thermoplastic plastic sheet adhere to the surface of the mold to form the shell.
- 如权利要求1所述的行李箱的制造方法,其中,在步骤E之后更包含一步骤F),将该气囊移出该壳体的容置区,并将该复合材料成型的行李箱进行冷却。The manufacturing method of a luggage case as claimed in claim 1, further comprising a step F) after step E, removing the airbag from the accommodating area of the shell, and cooling the luggage case formed from the composite material.
- 一种由权利要求1至权利要求9中任一项所述的制造方法所制成的复合材料成型的行李箱,包含有:A suitcase made of composite material formed by the manufacturing method according to any one of claims 1 to 9, comprising:一壳体,具有一外表面、一内表面、一由该内表面围绕出的容置区以及一角落;a casing, having an outer surface, an inner surface, an accommodating area surrounded by the inner surface, and a corner;一热固性碳纤维塑料层,具有一外面及一内面,该热固性碳纤维塑料层的外面设于该壳体的内表面;以及a thermosetting carbon fiber plastic layer having an outer surface and an inner surface, the outer surface of the thermosetting carbon fiber plastic layer is disposed on the inner surface of the casing; and一补强层,设置于该热固性碳纤维塑料层的内面且位于该壳体的角落。A reinforcing layer is arranged on the inner surface of the thermosetting carbon fiber plastic layer and is located at a corner of the shell.
- 如权利要求10所述的行李箱,其中,该补强层为热固性碳纤维塑料层。The luggage case of claim 10, wherein the reinforcing layer is a thermosetting carbon fiber plastic layer.
- 如权利要求10所述的行李箱,其中,该补强层为金属层,且该复合材料成型的行李箱更包含提供另一热固性碳纤维塑料层,该另一热固性碳纤维塑料层设置于该热固性碳纤维塑料层的内面及该金属层,该壳体、该二热固性碳纤维塑料层相互结合,且该金属层包覆于该二热固性碳纤维塑料层之中。The luggage case as claimed in claim 10, wherein the reinforcing layer is a metal layer, and the luggage case formed by the composite material further comprises providing another thermosetting carbon fiber plastic layer, and the another thermosetting carbon fiber plastic layer is disposed on the thermosetting carbon fiber The inner surface of the plastic layer and the metal layer, the shell and the two thermosetting carbon fiber plastic layers are combined with each other, and the metal layer is wrapped in the two thermosetting carbon fiber plastic layers.
- 如权利要求10所述的行李箱,其中,该复合材料成型的行李箱更包含一图案,该图案设置于该壳体的内表面。The luggage case of claim 10 , wherein the composite material-molded luggage case further comprises a pattern, and the pattern is disposed on the inner surface of the shell.
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