TW202325180A - Luggage case shell and manufacturing method thereof - Google Patents

Luggage case shell and manufacturing method thereof Download PDF

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TW202325180A
TW202325180A TW110147889A TW110147889A TW202325180A TW 202325180 A TW202325180 A TW 202325180A TW 110147889 A TW110147889 A TW 110147889A TW 110147889 A TW110147889 A TW 110147889A TW 202325180 A TW202325180 A TW 202325180A
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manufacturing
polyester sheet
luggage case
shell
luggage
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TW110147889A
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Chinese (zh)
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TWI818388B (en
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廖德超
曹俊哲
鄭文瑞
劉岳欣
王傳鈞
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南亞塑膠工業股份有限公司
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Priority to TW110147889A priority Critical patent/TWI818388B/en
Priority to CN202210098891.3A priority patent/CN116277891A/en
Publication of TW202325180A publication Critical patent/TW202325180A/en
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Publication of TWI818388B publication Critical patent/TWI818388B/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C51/00Shaping 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
    • B29C51/10Forming by pressure difference, e.g. vacuum
    • AHUMAN NECESSITIES
    • A45HAND OR TRAVELLING ARTICLES
    • A45CPURSES; LUGGAGE; HAND CARRIED BAGS
    • A45C13/00Details; Accessories
    • AHUMAN NECESSITIES
    • A45HAND OR TRAVELLING ARTICLES
    • A45CPURSES; LUGGAGE; HAND CARRIED BAGS
    • A45C5/00Rigid or semi-rigid luggage
    • A45C5/02Materials therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/42Moulds or cores; Details thereof or accessories therefor characterised by the shape of the moulding surface, e.g. ribs or grooves
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C51/00Shaping 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
    • B29C51/002Shaping 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 characterised by the choice of material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C51/00Shaping 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
    • B29C51/26Component parts, details or accessories; Auxiliary operations
    • B29C51/30Moulds
    • B29C51/36Moulds specially adapted for vacuum forming, Manufacture thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2067/00Use of polyesters or derivatives thereof, as moulding material
    • B29K2067/003PET, i.e. poylethylene terephthalate

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
  • Making Paper Articles (AREA)

Abstract

The present invention provides a luggage case shell and a manufacturing method thereof. The manufacturing method includes the following steps. A heated and softened polyester sheet is subjected to a vacuum blister molding process, so that a surface of the polyester sheet is adsorbed on a surface of a master mold to perform a surface texture processing process of the polyester sheet, and a surface texture of the master mold is transferred to the polyester sheet to form the luggage case shell.

Description

行李箱殼及其製造方法Luggage case and manufacturing method thereof

本發明是有關於一種行李箱殼及其製造方法,且特別是有關於一種聚酯材質行李箱殼及其製造方法。The present invention relates to a luggage case and its manufacturing method, and in particular to a polyester luggage case and its manufacturing method.

塑料行李箱習於在表面壓紋,使箱殼具有紋路,以達到抗刮、觸感、視覺美觀效果。現有製法常以PC、ABS、PP等材料經押出機製板,在製板押出成型過程中,直接以壓紋輪進行壓紋,再經裁切板材為適當尺寸,之後經加熱使塑料板材軟化,使用殼體公模模具真空吸速成型,以製成行李箱殼體。Plastic suitcases are used to embossing on the surface to make the case shell have textures, so as to achieve scratch resistance, tactile feeling and visual beauty. Existing methods often use PC, ABS, PP and other materials to extrude machine-made boards. During the board extrusion molding process, embossing is directly carried out with an embossing wheel, and then the board is cut to an appropriate size, and then the plastic board is softened by heating. Use the shell male mold mold vacuum suction speed molding to make the luggage shell.

然而,現有製法因板材先壓紋再經真空成型,基於殼體各部位成型倍率不同,可能會導致原先壓紋紋路受延伸而平坦化,使得壓紋紋路外觀不均,甚至平坦,影響行李箱外觀美感。However, in the existing manufacturing method, because the board is first embossed and then vacuum formed, the original embossed lines may be stretched and flattened due to the different molding ratios of each part of the shell, making the appearance of the embossed lines uneven or even flat, which will affect the suitcase. Aesthetic appearance.

基於上述,發展出一種行李箱殼的製造方法,使殼體紋路均勻,以提升行李箱的美觀及質感,為目前所需研究的重要課題。Based on the above, developing a manufacturing method of a luggage case to make the texture of the case uniform so as to improve the aesthetics and texture of the luggage case is an important subject of current research.

本發明提供一種行李箱殼及其製造方法,不受到成型延伸倍率影響,能夠使殼體紋路均勻,以提升行李箱的美觀及質感。The invention provides a suitcase shell and a manufacturing method thereof, which can make the texture of the shell uniform without being affected by the molding elongation ratio, so as to improve the appearance and texture of the suitcase.

本發明之行李箱殼的製造方法包括以下步驟。將經加熱軟化的聚酯板材進行真空吸塑成型製程,使聚酯板材的表面與母模模具的表面吸附,以進行聚酯板材的表面紋路加工製程,將母模模具的表面紋路轉寫於聚酯板材,以形成行李箱殼。The manufacturing method of the luggage case of the present invention includes the following steps. The heated and softened polyester sheet is subjected to a vacuum suction molding process, so that the surface of the polyester sheet and the surface of the master mold are adsorbed to process the surface texture of the polyester sheet, and the surface texture of the master mold is transferred to the Polyester sheet to form the trunk shell.

在本發明的一實施例中,行李箱殼的製造方法更包括在真空吸塑成型製程中,同時進行氣體加壓製程。In an embodiment of the present invention, the manufacturing method of the luggage case further includes performing a gas pressurization process during the vacuum blister forming process.

在本發明的一實施例中,氣體加壓製程包括使用高壓氣體,壓力為15 kg/cm 2至45 kg/cm 2In one embodiment of the present invention, the gas pressurization process includes the use of high-pressure gas with a pressure of 15 kg/cm 2 to 45 kg/cm 2 .

在本發明的一實施例中,聚酯板材的加熱軟化溫度為85℃至140℃。In an embodiment of the present invention, the heating softening temperature of the polyester sheet is 85°C to 140°C.

在本發明的一實施例中,母模模具的溫度為110℃至160℃,以使聚酯板材產生結晶。In an embodiment of the present invention, the temperature of the master mold is 110° C. to 160° C. to crystallize the polyester sheet.

在本發明的一實施例中,產生結晶的聚酯板材的結晶度為8.5%至25%。In an embodiment of the present invention, the crystallinity of the crystallized polyester sheet is 8.5% to 25%.

在本發明的一實施例中,母模模具的表面紋路深度小於或等於聚酯板材的1/2厚度。In an embodiment of the present invention, the surface texture depth of the master mold is less than or equal to 1/2 thickness of the polyester sheet.

在本發明的一實施例中,聚酯板材的厚度為0.8 mm至4.5 mm。In an embodiment of the present invention, the thickness of the polyester sheet is 0.8 mm to 4.5 mm.

在本發明的一實施例中,聚酯板材包括PET樹脂, PET樹脂包括原生粒或環保回收粒,PET樹脂的相對黏度為0.60至1.1。In an embodiment of the present invention, the polyester sheet includes PET resin, the PET resin includes primary pellets or environmentally friendly recycled pellets, and the relative viscosity of the PET resin is 0.60 to 1.1.

本發明的行李箱殼藉由上述行李箱殼的製造方法製成,行李箱殼的耐衝擊強度大於30 kg-cm/cm。The luggage shell of the present invention is made by the above-mentioned manufacturing method of the luggage shell, and the impact strength of the luggage shell is greater than 30 kg-cm/cm.

基於上述,本發明提供一種行李箱殼及其製造方法,不受到成型延伸倍率影響,能夠使殼體紋路均勻,以提升行李箱的美觀及質感。此外,押出製板不需壓紋輪,可節省壓紋輪具費用。另一方面,更可靈活設計母模模具紋路,生產個性化圖案。所使用的PET材料具有高衝擊強度、高剛性、低密度以及易加工等特性,除了PET原生粒之外,更可使用環保回收PET,其機械性能與原生粒相當,因此,可實現回收材料導入之需求。Based on the above, the present invention provides a luggage case and a manufacturing method thereof, which can make the texture of the case uniform without being affected by the molding elongation ratio, so as to improve the appearance and texture of the luggage case. In addition, there is no need for embossing wheels for extrusion, which can save the cost of embossing wheels. On the other hand, it is more flexible to design the pattern of the master mold and produce personalized patterns. The PET material used has the characteristics of high impact strength, high rigidity, low density and easy processing. In addition to PET primary grains, environmentally friendly recycled PET can be used, and its mechanical properties are equivalent to those of primary grains. Therefore, recycled materials can be imported needs.

以下,將詳細描述本發明的實施例。然而,這些實施例為例示性,且本發明揭露不限於此。Hereinafter, embodiments of the present invention will be described in detail. However, these embodiments are illustrative, and the present disclosure is not limited thereto.

在本文中,由「一數值至另一數值」表示的範圍,是一種避免在說明書中一一列舉該範圍中的所有數值的概要性表示方式。因此,某一特定數值範圍的記載,涵蓋該數值範圍內的任意數值以及由該數值範圍內的任意數值界定出的較小數值範圍,如同在說明書中說明文寫出該任意數值和該較小數值範圍一樣。Herein, a range indicated by "one value to another value" is a general representation which avoids enumerating all values in the range in the specification. Therefore, the description of a specific numerical range covers any numerical value within the numerical range and the smaller numerical range bounded by any numerical value within the numerical range, as if the arbitrary numerical value and the smaller numerical range are written in the specification. The value range is the same.

本發明提出一種行李箱殼的製造方法,主要是在真空吸塑成型製程中,使用母模模具對聚酯板材進行表面紋路加工。更詳細而言,本發明行李箱殼的製造方法包括以下步驟。將經加熱軟化的聚酯板材進行真空吸塑成型製程,使聚酯板材的表面與母模模具的表面吸附,以進行聚酯板材的表面紋路加工製程,將母模模具的表面紋路轉寫於聚酯板材,以形成行李箱殼。The invention proposes a method for manufacturing a luggage case, which mainly uses a master mold to process surface textures of polyester sheets in a vacuum suction molding process. More specifically, the manufacturing method of the luggage shell of the present invention includes the following steps. The heated and softened polyester sheet is subjected to a vacuum suction molding process, so that the surface of the polyester sheet and the surface of the master mold are adsorbed to process the surface texture of the polyester sheet, and the surface texture of the master mold is transferred to the Polyester sheet to form the trunk shell.

本發明行李箱殼的製造方法可更包括在真空吸塑成型製程中,同時進行氣體加壓製程,以加速成型速度。在本實施例中,氣體加壓製程包括使用高壓氣體,壓力為15 kg/cm 2至45 kg/cm 2The manufacturing method of the luggage shell of the present invention may further include performing a gas pressurization process during the vacuum blister forming process to speed up the forming process. In this embodiment, the gas pressurization process includes the use of high-pressure gas at a pressure of 15 kg/cm 2 to 45 kg/cm 2 .

在本實施例中,聚酯板材的加熱軟化溫度例如是85℃至145℃。母模模具的溫度例如是以110℃至160℃進行溫度控制,以使聚酯板材產生結晶,產生結晶的聚酯板材的結晶度例如是8.5%至25%,以使行李箱殼體耐熱性呈現70℃14天,箱體無型變。相較於習知公膜成型技術,大多不管制溫度,因此,不會產生結晶,故導致紋路變化及耐熱性不佳的缺點。更詳細而言,母模模具的表面紋路深度例如是小於或等於所述聚酯板材的1/2厚度,而聚酯板材的厚度例如是0.8 mm至4.5 mm,較佳例如如是1 mm至4 mm,最佳例如如是1.2 mm至3.5 mm。如此一來,可使殼體紋路成型良好,具有優異的耐衝擊特性,耐衝擊強度大於30 kg-cm/cm。In this embodiment, the heating softening temperature of the polyester sheet is, for example, 85°C to 145°C. The temperature of the master mold is, for example, controlled at 110°C to 160°C to crystallize the polyester sheet, and the crystallinity of the crystallized polyester sheet is, for example, 8.5% to 25% to improve the heat resistance of the luggage case shell. After 14 days at 70°C, the cabinet has no shape change. Compared with the conventional film forming technology, most of them do not control the temperature. Therefore, crystallization will not occur, which leads to the disadvantages of texture change and poor heat resistance. In more detail, the surface texture depth of the master mold is, for example, less than or equal to 1/2 the thickness of the polyester sheet, and the thickness of the polyester sheet is, for example, 0.8 mm to 4.5 mm, preferably, for example, 1 mm to 4 mm. mm, optimally such as 1.2 mm to 3.5 mm. In this way, the texture of the shell can be formed well, and it has excellent impact resistance properties, and the impact resistance strength is greater than 30 kg-cm/cm.

在本實施例中,聚酯板材是由耐衝擊聚酯組成物加工而成。耐衝擊聚酯組成物可包括PET樹脂、耐衝擊改質劑、相容劑、抗氧化劑及滑劑。以耐衝擊聚酯組成物的總重量計,PET樹脂的含量例如是70 wt%至92 wt%,耐衝擊改質劑的含量例如是5 wt%至15 wt%,相容劑的含量例如是2 wt%至15 wt%,抗氧化劑的含量例如是0.1 wt%至1 wt%,滑劑的含量例如是0.1 wt%至1 wt%。將上述成分混練改質而成的耐衝擊聚酯組成物具有高耐衝擊強度、高剛性、低密度以及易加工等特性,適合應用於耐衝擊押出以及真空成型加工產品,例如:行李箱殼。In this embodiment, the polyester sheet is processed from an impact-resistant polyester composition. The impact-resistant polyester composition may include PET resin, impact modifier, compatibilizer, antioxidant and slip agent. Based on the total weight of the impact-resistant polyester composition, the content of the PET resin is, for example, 70 wt% to 92 wt%, the content of the impact modifier is, for example, 5 wt% to 15 wt%, and the content of the compatibilizer is, for example, 2 wt% to 15 wt%, the content of antioxidant is, for example, 0.1 wt% to 1 wt%, and the content of slip agent is, for example, 0.1 wt% to 1 wt%. The impact-resistant polyester composition obtained by kneading and modifying the above components has the characteristics of high impact strength, high rigidity, low density and easy processing, and is suitable for impact-resistant extrusion and vacuum forming products, such as luggage shells.

在本實施例中,PET樹脂可包括原生粒或環保回收粒,其中環保回收粒的來源可包括瓶用回收粒、膜材回收粒、織物回收粒或工業回收環保再生聚酯粒(離型膜等),以實現回收材料導入之需求,但本發明並不以此為限。PET樹脂的相對黏度例如是0.60至1.1。In this embodiment, the PET resin may include raw pellets or environmentally friendly recycled pellets, wherein the sources of environmentally friendly recycled pellets may include recycled pellets for bottles, recycled film materials, recycled fabric pellets, or industrially recycled environmentally friendly recycled polyester pellets (release film etc.), in order to realize the requirement of importing recycled materials, but the present invention is not limited thereto. The relative viscosity of PET resin is, for example, 0.60 to 1.1.

在本實施例中,耐衝擊改質劑例如是聚烯烴彈性體(POE)。相容劑分散於耐衝擊聚酯組成物中,相容劑例如是聚烯烴彈性體接枝甲基丙烯酸縮水甘油酯(POE-g-GMA)及聚烯烴彈性體接枝馬來酸酐(POE-g-MAH)的至少其中之一。抗氧化劑是選自由酚類抗氧化劑、亞磷酸類抗氧化劑、受阻酚類抗氧劑所組成的材料群組的至少其中之一。滑劑是選自由二氧化矽、硬脂酸、聚乙烯蠟、硬脂酸鹽類、脂肪酸酯類、及複合型滑劑所組成的材料群組的至少其中之一,但本發明並不以此為限。In this embodiment, the impact modifier is, for example, polyolefin elastomer (POE). The compatibilizer is dispersed in the impact-resistant polyester composition, such as polyolefin elastomer grafted glycidyl methacrylate (POE-g-GMA) and polyolefin elastomer grafted maleic anhydride (POE-g-GMA) g-MAH) at least one of them. The antioxidant is at least one selected from the material group consisting of phenolic antioxidants, phosphorous acid antioxidants, and hindered phenolic antioxidants. The slip agent is at least one selected from the material group consisting of silicon dioxide, stearic acid, polyethylene wax, stearates, fatty acid esters, and composite slip agents, but the present invention does not rely on This is the limit.

本發明也公開一種行李箱殼,藉由上述行李箱殼的製造方法製成,行李箱殼的耐衝擊強度大於30 kg-cm/cm。The present invention also discloses a suitcase shell, which is made by the above-mentioned manufacturing method of the suitcase shell, and the impact resistance strength of the suitcase shell is greater than 30 kg-cm/cm.

以下,藉由實驗例來詳細說明上述本發明的行李箱殼及其製造方法。然而,下述實驗例並非用以限制本發明。 實驗例 Hereinafter, the above-mentioned luggage case of the present invention and its manufacturing method will be described in detail by using experimental examples. However, the following experimental examples are not intended to limit the present invention. Experimental example

為了證明本發明所提出的製造方法可製造出具有良好耐衝擊強度及耐熱性的行李箱殼,以下特別作此實驗例。In order to prove that the manufacturing method proposed by the present invention can manufacture a suitcase shell with good impact strength and heat resistance, the following experiment example is specially made.

以下表1列出實例1至實例5以及比較例中各成分用量比例、加工條件以及物性結果。 表1   配方別 實例1 實例2 實例3 實例4 實例5 比較例 用量比例   PET樹脂 88 90 76 86 78 87 耐衝擊改質劑 7 6 14 8 14 8 相容劑 4.2 3.2 9.2 5.2 7.2 4.2 抗氧化劑 0.5 0.5 0.5 0.5 0.5 0.5 滑劑 0.3 0.3 0.3 0.3 0.3 0.3 加工條件 板材厚度mm 2.1 2.1 2.5 2.3 1.8 2.1 模具紋路深度mm 0.3 0.3 0.2 0.1 0.15 0.1 氣體加壓成型壓力 kg / cm 2 20 20 25 20 15 板材成型溫度℃ 100 110 130 100 120 110 成型模具溫度℃ 110 130 150 130 130 50 物性 成型品結晶度 8.5% 9.2% 18.8% 14.6% 13.8% 2.8% 耐衝擊強度 kg-cm/cm 42.8 40.1 32.5 38.2 35.1 51 紋路完整性 良好 良好 良好 良好 良好 耐熱性: 70℃*14天 OK 無型變 OK 無型變 OK 無型變 OK 無型變 OK 無型變 NG 殼體有型變 用量比例單位:重量份 實例 1 Table 1 below lists the dosage ratios, processing conditions and physical property results of each component in Examples 1 to 5 and Comparative Examples. Table 1 Recipe Example 1 Example 2 Example 3 Example 4 Example 5 comparative example Dosage ratio PET resin 88 90 76 86 78 87 impact modifier 7 6 14 8 14 8 Compatibilizer 4.2 3.2 9.2 5.2 7.2 4.2 Antioxidants 0.5 0.5 0.5 0.5 0.5 0.5 lubricant 0.3 0.3 0.3 0.3 0.3 0.3 Processing conditions Plate thickness mm 2.1 2.1 2.5 2.3 1.8 2.1 Mold texture depth mm 0.3 0.3 0.2 0.1 0.15 0.1 Gas pressurized molding pressure kg/cm 2 20 20 25 20 15 none Plate forming temperature ℃ 100 110 130 100 120 110 Forming mold temperature ℃ 110 130 150 130 130 50 physical properties Crystallinity of molded product 8.5% 9.2% 18.8% 14.6% 13.8% 2.8% Impact strength kg-cm/cm 42.8 40.1 32.5 38.2 35.1 51 texture integrity good good good good good Difference Heat resistance: 70℃*14 days OK no change OK no change OK no change OK no change OK no change NG shell has deformation Consumption ratio unit: parts by weight Example 1

PET樹脂重量份88%、耐衝擊改質劑聚烯烴彈性體(POE)重量份7%、相容劑聚烯烴彈性體接枝甲基丙烯酸縮水甘油酯(POE-g-GMA)重量份4.2%。抗氧化劑亞磷酸類抗氧化劑重量份0.5%、滑劑二氧化矽0.3%。以上述配方組成,可先經混練造粒得到混合均勻高耐衝母粒,再經押出機製得板材,供為行李箱用板;亦可以上述配方混合均勻直接於押出機製板,供為行李箱用板,本工法為業界所習知。PET resin 88% by weight, impact modifier polyolefin elastomer (POE) 7% by weight, compatibilizer polyolefin elastomer grafted glycidyl methacrylate (POE-g-GMA) 4.2% by weight . Antioxidant Phosphite antioxidant 0.5% by weight, slip agent silicon dioxide 0.3%. Composed of the above formula, it can be mixed and granulated first to obtain a uniformly mixed high-impact masterbatch, and then through an extrusion machine to obtain a board for a suitcase board; the above formula can also be mixed evenly and directly on the extrusion machine board for a suitcase Using boards, this construction method is well known in the industry.

板材厚度2.1mm,成型模具開立紋路深度0.3mm、溫度110℃加工。先將板材置入成型機烘箱加熱,使板材表面膜溫100℃後,再進入成型區真空吸塑成型,並同時以20kg/cm 2氣體加壓輔助成型,定型時間5秒,再釋放氣體壓力為常壓取出行李箱殼體。 分析本行李箱殼體,結晶度8.5%、耐衝擊強度42.8kg-cm/cm、壓紋紋路完整良好,殼體經70℃*14天耐熱性試驗,殼體無型變。 實例 2 The thickness of the plate is 2.1mm, the depth of the forming mold is 0.3mm, and the temperature is 110°C. Put the plate into the oven of the molding machine to heat it, so that the surface film temperature of the plate is 100°C, then enter the forming area for vacuum forming, and at the same time use 20kg/cm2 gas pressurization to assist the forming, the setting time is 5 seconds, and then release the gas pressure Remove the trunk shell for normal pressure. Analysis of the suitcase shell shows that the crystallinity is 8.5%, the impact strength is 42.8kg-cm/cm, and the embossed lines are complete and good. The shell has passed the heat resistance test at 70°C for 14 days, and the shell has no deformation. Example 2

PET樹脂重量份90%、耐衝擊改質劑聚烯烴彈性體(POE)重量份6%、相容劑聚烯烴彈性體接枝甲基丙烯酸縮水甘油酯(POE-g-GMA)重量份3.2%。抗氧化劑亞磷酸類抗氧化劑重量份0.5%、滑劑二氧化矽0.3%。以上述配方組成,可先經混練造粒得到混合均勻高耐衝母粒,再經押出機製得板材,供為行李箱用板;亦可以上述配方混合均勻直接於押出機製板,供為行李箱用板,本工法為業界所習知。PET resin 90% by weight, impact modifier polyolefin elastomer (POE) 6% by weight, compatibilizer polyolefin elastomer grafted glycidyl methacrylate (POE-g-GMA) 3.2% by weight . Antioxidant Phosphite antioxidant 0.5% by weight, slip agent silicon dioxide 0.3%. Composed of the above formula, it can be mixed and granulated first to obtain a uniformly mixed high-impact masterbatch, and then through an extrusion machine to obtain a board for a suitcase board; the above formula can also be mixed evenly and directly on the extrusion machine board for a suitcase Using boards, this construction method is well known in the industry.

板材厚度2.1mm,成型模具開立紋路深度0.3mm、溫度130℃加工。先將板材置入成型機烘箱加熱,使板材表面膜溫110℃後,再進入成型區真空吸塑成型,並同時以20kg/cm 2氣體加壓輔助成型,定型時間5秒,再釋放氣體壓力為常壓取出行李箱殼體。分析本行李箱殼體,結晶度9.2%、耐衝擊強度40.1kg-cm/cm、壓紋紋路完整良好,殼體經70℃*14天耐熱性試驗,殼體無型變。 實例 3 The thickness of the plate is 2.1mm, the depth of the forming mold is 0.3mm, and the temperature is 130°C. Put the plate into the oven of the molding machine to heat it, so that the surface film temperature of the plate is 110°C, then enter the forming area for vacuum suction molding, and at the same time use 20kg/cm2 gas pressurization to assist the forming, the setting time is 5 seconds, and then release the gas pressure Remove the trunk shell for normal pressure. Analysis of the suitcase shell shows that the crystallinity is 9.2%, the impact strength is 40.1kg-cm/cm, and the embossed lines are complete and good. The shell has passed the heat resistance test at 70°C for 14 days, and the shell has no deformation. Example 3

PET樹脂重量份76%、耐衝擊改質劑聚烯烴彈性體(POE)重量份14%、相容劑聚烯烴彈性體接枝甲基丙烯酸縮水甘油酯(POE-g-GMA)重量份9.2%。抗氧化劑亞磷酸類抗氧化劑重量份0.5%、滑劑二氧化矽0.3%。以上述配方組成,可先經混練造粒得到混合均勻高耐衝母粒,再經押出機製得板材,供為行李箱用板;亦可以上述配方混合均勻直接於押出機製板,供為行李箱用板,本工法為業界所習知。PET resin 76% by weight, impact modifier polyolefin elastomer (POE) 14% by weight, compatibilizer polyolefin elastomer grafted glycidyl methacrylate (POE-g-GMA) 9.2% by weight . Antioxidant Phosphite antioxidant 0.5% by weight, slip agent silicon dioxide 0.3%. Composed of the above formula, it can be mixed and granulated first to obtain a uniformly mixed high-impact masterbatch, and then through an extrusion machine to obtain a board for a suitcase board; the above formula can also be mixed evenly and directly on the extrusion machine board for a suitcase Using boards, this construction method is well known in the industry.

板材厚度2.5mm,成型模具開立紋路深度0.2mm、溫度150℃加工。先將板材置入成型機烘箱加熱,使板材表面膜溫130℃後,再進入成型區真空吸塑成型,並同時以25kg/cm 2氣體加壓輔助成型,定型時間5秒,再釋放氣體壓力為常壓取出行李箱殼體。分析本行李箱殼體,結晶度18.8%、耐衝擊強度32.5kg-cm/cm、壓紋紋路完整良好,殼體經70℃*14天耐熱性試驗,殼體無型變。 實例 4 The thickness of the plate is 2.5mm, the depth of the forming mold is 0.2mm, and the temperature is 150°C. Put the plate into the oven of the molding machine to heat it, so that the surface film temperature of the plate is 130°C, then enter the forming area for vacuum forming, and at the same time use 25kg/cm 2 gas pressurization to assist the forming, the setting time is 5 seconds, and then release the gas pressure Remove the trunk shell for normal pressure. Analysis of the suitcase shell shows that the crystallinity is 18.8%, the impact strength is 32.5kg-cm/cm, and the embossed lines are complete and good. The shell has passed the heat resistance test at 70°C for 14 days, and the shell has no shape change. Example 4

PET樹脂重量份86%、耐衝擊改質劑聚烯烴彈性體(POE)重量份8%、相容劑聚烯烴彈性體接枝甲基丙烯酸縮水甘油酯(POE-g-GMA)重量份5.2%。抗氧化劑亞磷酸類抗氧化劑重量份0.5%、滑劑二氧化矽0.3%。以上述配方組成,可先經混練造粒得到混合均勻高耐衝母粒,再經押出機製得板材,供為行李箱用板;亦可以上述配方混合均勻直接於押出機製板,供為行李箱用板,本工法為業界所習知。PET resin 86% by weight, impact modifier polyolefin elastomer (POE) 8% by weight, compatibilizer polyolefin elastomer grafted glycidyl methacrylate (POE-g-GMA) 5.2% by weight . Antioxidant Phosphite antioxidant 0.5% by weight, slip agent silicon dioxide 0.3%. Composed of the above formula, it can be mixed and granulated first to obtain a uniformly mixed high-impact masterbatch, and then through an extrusion machine to obtain a board for a suitcase board; the above formula can also be mixed evenly and directly on the extrusion machine board for a suitcase Using boards, this construction method is well known in the industry.

板材厚度2.3mm,成型模具開立紋路深度0.1mm、溫度130℃加工。先將板材置入成型機烘箱加熱,使板材表面膜溫100℃後,再進入成型區真空吸塑成型,並同時以20kg/cm 2氣體加壓輔助成型,定型時間5秒,再釋放氣體壓力為常壓取出行李箱殼體。分析本行李箱殼體,結晶度14.6%、耐衝擊強度38.2kg-cm/cm、壓紋紋路完整良好,殼體經70℃*14天耐熱性試驗,殼體無型變。 實例 5 The thickness of the plate is 2.3mm, the depth of the forming mold is 0.1mm, and the temperature is 130°C. Put the plate into the oven of the molding machine to heat it, so that the surface film temperature of the plate is 100°C, then enter the forming area for vacuum forming, and at the same time use 20kg/cm2 gas pressurization to assist the forming, the setting time is 5 seconds, and then release the gas pressure Remove the trunk shell for normal pressure. Analyzing the suitcase shell, the crystallinity is 14.6%, the impact strength is 38.2kg-cm/cm, and the embossed lines are complete and good. The shell has passed the heat resistance test at 70°C for 14 days, and the shell has no shape change. Example 5

PET樹脂重量份78%、耐衝擊改質劑聚烯烴彈性體(POE)重量份14%、相容劑聚烯烴彈性體接枝甲基丙烯酸縮水甘油酯(POE-g-GMA)重量份7.2%。抗氧化劑亞磷酸類抗氧化劑重量份0.5%、滑劑二氧化矽0.3%。以上述配方組成,可先經混練造粒得到混合均勻高耐衝母粒,再經押出機製得板材,供為行李箱用板;亦可以上述配方混合均勻直接於押出機製板,供為行李箱用板,本工法為業界所習知。PET resin 78% by weight, impact modifier polyolefin elastomer (POE) 14% by weight, compatibilizer polyolefin elastomer grafted glycidyl methacrylate (POE-g-GMA) 7.2% by weight . Antioxidant Phosphite antioxidant 0.5% by weight, slip agent silicon dioxide 0.3%. Composed of the above formula, it can be mixed and granulated first to obtain a uniformly mixed high-impact masterbatch, and then through an extrusion machine to obtain a board for a suitcase board; the above formula can also be mixed evenly and directly on the extrusion machine board for a suitcase Using boards, this construction method is well known in the industry.

板材厚度1.8mm,成型模具開立紋路深度0.15mm、溫度130℃加工。先將板材置入成型機烘箱加熱,使板材表面膜溫120℃後,再進入成型區真空吸塑成型,並同時以15kg/cm 2氣體加壓輔助成型,定型時間5秒,再釋放氣體壓力為常壓取出行李箱殼體。分析本行李箱殼體,結晶度13.8%、耐衝擊強度35.1kg-cm/cm、壓紋紋路完整良好,殼體經70℃*14天耐熱性試驗,殼體無型變。 比較例 The thickness of the plate is 1.8mm, the depth of the forming mold is 0.15mm, and the temperature is 130°C. First put the plate into the oven of the forming machine to heat it so that the film temperature on the surface of the plate is 120°C, then enter the forming area for vacuum suction molding, and at the same time use 15kg/cm 2 gas pressurization to assist the forming, the setting time is 5 seconds, and then release the gas pressure Remove the trunk shell for normal pressure. Analyzing the suitcase shell, the crystallinity is 13.8%, the impact strength is 35.1kg-cm/cm, and the embossed lines are complete and good. The shell has passed the heat resistance test at 70°C for 14 days, and the shell has no shape change. comparative example

PET樹脂重量份87%、耐衝擊改質劑聚烯烴彈性體(POE)重量份8%、相容劑聚烯烴彈性體接枝甲基丙烯酸縮水甘油酯(POE-g-GMA)重量份4.2%。抗氧化劑亞磷酸類抗氧化劑重量份0.5%、滑劑二氧化矽0.3%。板材厚度2.1mm,成型模具開立紋路深度0.1mm、溫度50℃加工。先將板材置入成型機烘箱加熱,使板材表面模溫110℃後,再進入成型區真空吸塑成型,定型時間5秒,再釋放氣體壓力為常壓取出行李箱殼體。分析本行李箱殼體,結晶度2.8%、耐衝擊強度51kg-cm/cm、壓紋紋路不良,部分紋路不明顯、且殼體經70℃*14天耐熱性試驗,殼體會型變。PET resin 87% by weight, impact modifier polyolefin elastomer (POE) 8% by weight, compatibilizer polyolefin elastomer grafted glycidyl methacrylate (POE-g-GMA) 4.2% by weight . Antioxidant Phosphite antioxidant 0.5% by weight, slip agent silicon dioxide 0.3%. The thickness of the plate is 2.1mm, the depth of the forming mold is 0.1mm, and the temperature is 50°C. Put the board into the oven of the molding machine to heat it up, so that the mold temperature on the surface of the board is 110°C, and then enter the molding area for vacuum suction molding. The setting time is 5 seconds, and then release the gas pressure to normal pressure to take out the suitcase shell. Analysis of the suitcase shell shows that the crystallinity is 2.8%, the impact strength is 51kg-cm/cm, the embossed lines are poor, and some lines are not obvious, and the shell has undergone a heat resistance test at 70°C for 14 days, and the shell will change shape.

實例1至實例5中,真空成型過程,板材表面膜溫85-140℃、模具溫度110℃至160℃、並同時以10 kg/cm 2至45kg/cm 2氣體加壓輔助成型,可使PET板材表面紋路均勻美觀。並因溫度達可結晶溫度,使結晶度達8.5%至25%、使製得的行李箱殼體於70℃高溫環境下無型變。 In example 1 to example 5, vacuum forming process, sheet surface film temperature 85-140 ℃, mold temperature 110 ℃ to 160 ℃, and at the same time with 10 kg/cm 2 to 45 kg/cm 2 gas pressure-assisted forming, can make PET The surface texture of the board is uniform and beautiful. And because the temperature reaches the crystallization temperature, the crystallinity can reach 8.5% to 25%, so that the suitcase shell made will not change shape under the high temperature environment of 70°C.

至於比較例是採用真空成型模具溫度50℃加工,不足以使PET材料誘發結晶,造成製品耐熱性不足,經70℃*14天耐熱性試驗,殼體明顯型變,不符合行李箱製品要求。壓紋紋路不良,紋路不均勻,部分紋路不明顯。 測試方法 As for the comparative example, the vacuum forming mold was processed at a temperature of 50°C, which was not enough to induce crystallization of the PET material, resulting in insufficient heat resistance of the product. After a heat resistance test at 70°C for 14 days, the shell was obviously deformed and did not meet the requirements for luggage products. The embossed texture is poor, the texture is uneven, and some textures are not obvious. Test Methods

結晶度測試方法: 以DSC圖譜分析,由下式計算: 結晶度=[熔融峰面積-重結晶峰面積)/100%結晶的理論熱焓]X100%,其中100%結晶的理論熱焓為140J/g計算 Crystallinity test method: Analyzed by DSC spectrum, calculated by the following formula: Crystallinity = [melting peak area - recrystallization peak area) / theoretical enthalpy of 100% crystallization] X100%, where the theoretical enthalpy of 100% crystallization is calculated as 140J/g

耐衝擊強度測試方法:ASTM256Impact strength test method: ASTM256

綜上所述,本發明提供一種行李箱殼及其製造方法,不受到成型延伸倍率影響,能夠使殼體紋路均勻,以提升行李箱的質感。此外,押出製板不需壓紋輪,可節省壓紋輪具費用。另一方面,更可靈活設計母模模具紋路,生產個性化圖案。所使用的PET材料具有高衝擊強度、高剛性、低密度以及易加工等特性,除了PET原生粒之外,更可使用環保回收PET,其機械性能與原生粒相當,因此,可實現回收材料導入之需求。所製造而成的行李箱殼不僅殼體紋路成型良好,更具有優異的耐衝擊特性及耐熱性,兼具美觀與實用性。To sum up, the present invention provides a suitcase shell and a manufacturing method thereof, which can make the texture of the shell uniform without being affected by the molding elongation ratio, so as to improve the texture of the suitcase. In addition, there is no need for embossing wheels for extrusion, which can save the cost of embossing wheels. On the other hand, it is more flexible to design the pattern of the master mold and produce personalized patterns. The PET material used has the characteristics of high impact strength, high rigidity, low density and easy processing. In addition to PET primary grains, environmentally friendly recycled PET can be used, and its mechanical properties are equivalent to those of primary grains. Therefore, recycled materials can be imported needs. The manufactured luggage shell not only has a well-formed shell pattern, but also has excellent impact resistance and heat resistance, and is both beautiful and practical.

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Claims (10)

一種行李箱殼的製造方法,包括: 將經加熱軟化的聚酯板材進行真空吸塑成型製程,使所述聚酯板材的表面與母模模具的表面吸附,以進行所述聚酯板材的表面紋路加工製程,將所述母模模具的表面紋路轉寫於所述聚酯板材,以形成行李箱殼。 A method of manufacturing a luggage case, comprising: The heated and softened polyester sheet is subjected to a vacuum suction molding process, so that the surface of the polyester sheet and the surface of the master mold are adsorbed, so as to process the surface texture of the polyester sheet, and the master mold The surface texture is transferred to the polyester sheet to form the luggage shell. 如請求項1所述之行李箱殼的製造方法,更包括在所述真空吸塑成型製程中,同時進行氣體加壓製程。The method for manufacturing a luggage shell as claimed in Claim 1 further includes performing a gas pressurization process during the vacuum blister forming process. 如請求項2所述之行李箱殼的製造方法,其中所述氣體加壓製程包括使用高壓氣體,壓力為15 kg/cm 2至45 kg/cm 2The method for manufacturing a luggage case according to claim 2, wherein the gas pressurization process includes using high-pressure gas with a pressure of 15 kg/cm 2 to 45 kg/cm 2 . 如請求項1所述之行李箱殼的製造方法,其中所述聚酯板材的加熱軟化溫度為85℃至140℃。The method for manufacturing a luggage case according to claim 1, wherein the softening temperature of the polyester sheet is 85°C to 140°C. 如請求項1所述之行李箱殼的製造方法,其中所述母模模具的溫度為110℃至160℃,以使所述聚酯板材產生結晶。The method for manufacturing a luggage shell according to claim 1, wherein the temperature of the master mold is 110°C to 160°C to crystallize the polyester sheet. 如請求項5所述之行李箱殼的製造方法,其中產生結晶的所述聚酯板材的結晶度為8.5%至25%。The manufacturing method of the luggage shell according to claim 5, wherein the crystallinity of the crystallized polyester sheet is 8.5% to 25%. 如請求項1所述之行李箱殼的製造方法,其中所述母模模具的表面紋路深度小於或等於所述聚酯板材的1/2厚度。The method for manufacturing a luggage case according to claim 1, wherein the surface texture depth of the master mold is less than or equal to 1/2 of the thickness of the polyester sheet. 如請求項1所述之行李箱殼的製造方法,其中所述聚酯板材的厚度為0.8 mm至4.5 mm。The method for manufacturing a luggage case according to claim 1, wherein the thickness of the polyester sheet is 0.8 mm to 4.5 mm. 如請求項1所述之行李箱殼的製造方法,其中所述聚酯板材包括PET樹脂,所述PET樹脂包括原生粒或環保回收粒,所述PET樹脂的相對黏度為0.60至1.1。The method for manufacturing a luggage case according to claim 1, wherein the polyester sheet includes PET resin, the PET resin includes primary grains or environmentally friendly recycled grains, and the relative viscosity of the PET resin is 0.60 to 1.1. 一種行李箱殼,藉由請求項1至請求項9中任一項所述之行李箱殼的製造方法製成,所述行李箱殼的耐衝擊強度大於30 kg-cm/cm。A luggage case made by the method for manufacturing a luggage case described in any one of claim 1 to claim 9, the impact resistance of the luggage case is greater than 30 kg-cm/cm.
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