CN111793988B - 服装用保温棉透气孔与行线、贴合、镭射综合加工制程技术 - Google Patents

服装用保温棉透气孔与行线、贴合、镭射综合加工制程技术 Download PDF

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CN111793988B
CN111793988B CN202010461120.7A CN202010461120A CN111793988B CN 111793988 B CN111793988 B CN 111793988B CN 202010461120 A CN202010461120 A CN 202010461120A CN 111793988 B CN111793988 B CN 111793988B
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cotton
plate
cloth
tpu
adhesive film
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CN111793988A (zh
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王明田
刘金霞
张昭伟
张家兴
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Yangzhou Baojin Garment Co ltd
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    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M17/00Producing multi-layer textile fabrics
    • D06M17/04Producing multi-layer textile fabrics by applying synthetic resins as adhesives
    • D06M17/10Polyurethanes polyurea
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/26Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • B32B3/266Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B33/00Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/06Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/10Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/12Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
    • B32B37/1284Application of adhesive
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/0004Cutting, tearing or severing, e.g. bursting; Cutter details
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B2038/0052Other operations not otherwise provided for
    • B32B2038/008Sewing, stitching
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/04Punching, slitting or perforating
    • B32B2038/042Punching
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00Layers arrangement
    • B32B2250/20All layers being fibrous or filamentary
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2309/00Parameters for the laminating or treatment process; Apparatus details
    • B32B2309/12Pressure
    • B32B2309/125Pressure vs time profiles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2437/00Clothing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/04Punching, slitting or perforating

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Treatment Of Fiber Materials (AREA)

Abstract

本发明涉及一种服装用保温棉透气孔与行线、贴合、镭射综合加工制程技术,包括以下步骤:(1)布料预缩和裁剪,得到面层布料、底层布料;(2)切割贴合需要的TPU热熔胶膜;用刀模斩切TPU热熔胶膜,防尘恒温存放备用;(3)切割三合一组合模板,割三合一组合模板为行线、贴合、镭射三合一组合模板;(4)棉裁剪与冲孔;(5)平板热压机模具的固定;(6)将TPU热熔胶膜粘于底层布料;(7)固定棉于底层布料;(8)底层布料和面层布料热压结合;(9)贴合点镭射透气孔;(10)行线固定底层布料、棉面层布料四周;通过本发明,优质高效结合呈现棉冲孔、行线、贴合工艺结合制作技术。

Description

服装用保温棉透气孔与行线、贴合、镭射综合加工制程技术
技术领域
本发明涉及一种服装用保温棉透气孔与行线、贴合、镭射综合加工制程技术,涉及棉冲孔、行线、贴合、镭射结合工艺技术,可用于纺织料多工艺结合运用、保暖透气结合化产品生产。
背景技术
传统棉产品工艺单一、外观单调;传统棉冲孔、行线、贴合、镭射结合做法存在操作难、对位不准、偏移、高温压扁棉等问题;同时,传统做法步骤作业报废率大、人工量大、操作步骤繁琐、效率低,且具有成品外观胶片位置偏移、棉孔变形移位、棉被压扁不蓬松、水洗牢度受影响的问题。
发明内容
本发明的目的是针对上述现有技术存在的问题,提供一种服装用保温棉透气孔与行线、贴合、镭射综合加工制程技术,此次发明工艺技术结合呈现多种工艺组合搭配,可运用于设计具有保暖、透气、具有成本竞争力。
本发明的目的是这样实现的,一种服装用保温棉透气孔与行线、贴合、镭射综合加工制程技术,其特征在于,包括以下步骤:
(1)布料预缩和裁剪,得到面层布料、底层布料;
(2)切割贴合需要的TPU热熔胶膜;用刀模斩切TPU热熔胶膜,防尘恒温存放备用;
(3)切割三合一组合模板,割三合一组合模板为行线、贴合、镭射三合一组合模板;
3-1、制备底板、面板;将2mm厚高温黄板按加工部位大小切割成镂空,并刻画上加工部位的轮廓线条,在边缘涂上台板胶,制成底板、面板,得到底板、面板;
3-2、制备松量凸板;将0.2mm厚高温黄板粘上1.5cm高的贴合点形状发泡棉颗粒,然后用牛皮纸覆盖和固定,使其成一个立体的盒状,得到松量凸板;
3-3、制备TPU胶膜对位板:卡纸版按贴合点形状镭射镂空,用于底层布料贴TPU热熔胶膜;
(4)棉裁剪与冲孔;
4-1、将棉从真空袋取出,经过蒸汽预缩机进行对棉的蓬松恢复和定型;
4-2、将蓬松恢复和定型过的棉铺至自动裁床,按照设计需要进行裁剪和冲孔;
4-3、裁剪和冲孔好的棉片,清理镂空孔洞废弃棉,并避免挤压,整齐存放备用;
(5)平板热压机模具的固定;
5-1、制备TPU颗粒模具;依据贴合点形状模切白色高温1.5cm厚TPU颗粒,得到TPU颗粒模具,TPU颗粒模具的直径大于TPU热熔胶膜直径,且小于棉孔四周2mm,并清洗干净;
5-2、将平板热压机清理干净,尤其是平板热压机上的上模发热板、下模发热板用布去除灰尘,并将上模发热板、下模发热板设定为70℃;
5-3、镭射机在卡纸板上镭出TPU颗粒模具的位置,用来粘TPU颗粒模具时对位使用;
5-4、平板热压机的下模发热板安装上TPU胶膜对位板;
5-5、将卡纸版置于平板热压机下模发热板,对位卡入TPU胶膜对位板中;
5-6、用硅橡胶涂于TPU颗粒模具不接触布料的底面;
5-7、将步骤5-6中的TPU颗粒模具正面朝步骤5-5中的卡纸版,对着镭射的位置依序摆放,涂好硅橡胶的底面朝上;
5-8、启动热压机,上模发热板、下模发热板温度70℃,上模发热板、下模发热板压力2.5KG,热压10S,使贴合点形状的白色TPU颗粒模具涂好硅橡胶的底部粘着于平板热压机的上模发热板上;
5-9、在步骤5-8完成后,取出对位卡纸板,再次启动平板热压机,停留在热压机上的上模发热板压下时状态,静置3小时以上,使贴合点形状的白色TPU颗粒模具完全固定到热压机上的上模发热板上;
(6)将TPU热熔胶膜粘于底层布料;
6-1、底层布料平铺固定贴于步骤3-1中三合一模板的底板上;
6-2、将步骤3-3的 TPU胶膜对位板卡入已贴好底层布料的三合一模板的底板;
6-3、将步骤(1)中TPU热熔胶膜对位放置于步骤6-2的TPU胶膜对位板镂空孔洞内,点烫笔加热点状固定后,取出TPU胶膜对位板;
6-4、将已固定好TPU热熔胶膜的底层布料,连同三合一模板底板,卡入步骤5-4的平板热压机的下模发热板;
6-5、启动平板热压机,平板热压机参数为上模发热板220℃、下模发热板110℃,压力为2.5KG, 热压8S,完成后连同三合一模板底板取出;
(7)固定棉于底层布料;
7-1、去除步骤(6)底层布料上TPU热熔胶膜上的离型纸膜;
7-2、将经步骤4-3裁剪和冲孔好的棉,置于步骤(6)的底层布料上,棉孔与TPU热熔胶膜对位,TPU 热熔胶膜居中于棉孔,并将棉的四周固定,使其不会移位;
7-3、固定棉后,连同三合一模板底板,卡入行线机,依照预设轨迹进行行线,使底层布料和棉通过行线结合在一起,完成后从行线机取出;
(8)底层布料和面层布料热压结合;
8-1、将步骤3-2中松量凸板卡入步骤3-1的三合一模板面板;
8-2、将面层布料按轮廓线自然放松覆盖至步骤8-1的模板上,四周固定到三合一模板面板的台板胶上;
8-3、将松量凸板取出,得到已固定面层布料的三合一模板面板,将三合一模板面板与三合一模板底板对位卡在一起;
8-4、将经步骤8-3卡在一起的模板,置于平板热压机下模发热板,面层布料向上,面层布料上覆盖铁氟龙隔热纸,启动平板热压机,平板热压机参数为上模发热板220℃、下模发热板110℃、压力2.5KG,热压 25S,完成底层布料和面层布料的粘合;
8-5、完成后将热压结合后的底层布料和面层布料取出;
(9)贴合点镭射透气孔;
9-1、将经步骤(8)热压结合后的底层布料和面层布料连通模板置于镭射机台面,进行对位;
9-2、启动镭射机,进行对位镭孔;
9-3、完成对位镭孔后取出;
(10)行线固定底层布料、棉面层布料四周;
10-1、将完成镭射孔的模板和布料再次卡入行线机台面;
10-2、启动行线机,行线固定底层布料、棉、面层布料三层结构的四周,使其平整无扭曲;
10-3、完成后,将行线固定底层布料、棉、面层布料后的布料从模板上分离下来,平整置放,后续进行拼装缝制。
步骤(1)中,包括以下步骤:
1-1、使用滚轮式预缩机,将布料进行预缩,以解决后续热压时面料收缩变形,造成对位不准;
1-2、预缩后静置24H,使其冷却定型,收缩到位;
1-3、预缩后裁剪成需要的布料裁片,得到预缩和裁剪好的面层布料、底层布料。
步骤(2)中,TPU热熔胶膜的型号为BEMIS-3829,TPU热熔胶膜介绍网址为:https://www.bemisworldwide.com。
步骤(3)中,将2mm厚高温黄板按加工部位大小切割成镂空,并刻画上加工部位的轮廓线条,在边缘涂上台板胶,制成底板、面板;
步骤4-1中,蒸汽预缩机内的温度为120℃,对棉的蓬松恢复和定型的速度为5m/分钟。
本发明方法先进科学,通过本发明,优质高效结合呈现棉冲孔、行线、贴合工艺结合制作技术。本发明由于采用以上技术方案,具有以下优点:
1、棉冲孔造型、行线、贴合、镭射透气工艺结合,外观层次丰富,设计更多样化;
2、使得棉冲孔、行线、贴合、镭射工艺结合做法对位精准(包括贴合,镭射,热压对位),维持棉的蓬松度柔软度;
3、本发明技术利用三合一组合模板减少人工工时量,运用操作简单,提升成功率与品质良率;
4、本发明技术做法操作步骤简洁、简单,有效提升作业效率;
5、本发明技术做法成品外观胶片位置准确、棉孔形状固定、棉蓬松柔软、牢度更佳。
具体实施方式
一种服装用保温棉透气孔与行线、贴合、镭射综合加工制程技术,其特征在于,包括以下步骤:
(1)布料预缩和裁剪,得到面层布料、底层布料;
1-1、使用滚轮式预缩机,将布料进行预缩,以解决后续热压时面料收缩变形,造成对位不准;
1-2、预缩后静置24H,使其冷却定型,收缩到位;
1-3、预缩后裁剪成需要的布料裁片,得到预缩和裁剪好的面层布料、底层布料。
(2)切割贴合需要的TPU热熔胶膜;用刀模斩切TPU热熔胶膜,防尘恒温存放备用;TPU热熔胶膜的型号为BEMIS-3829,TPU热熔胶膜介绍网址为:https://www.bemisworldwide.com。
(3)切割三合一组合模板,割三合一组合模板为行线、贴合、镭射三合一组合模板;
3-1、制备底板、面板;将2mm厚高温黄板按加工部位大小切割成镂空,并刻画上加工部位的轮廓线条,在边缘涂上台板胶,制成底板、面板,得到底板、面板;
3-2、制备松量凸板;将0.2mm厚高温黄板粘上1.5cm高的贴合点形状发泡棉颗粒,然后用牛皮纸覆盖和固定,使其成一个立体的盒状,得到松量凸板;
3-3、制备TPU胶膜对位板:卡纸版按贴合点形状镭射镂空,用于底层布料贴TPU热熔胶膜;
(4)棉裁剪与冲孔;
4-1、将棉从真空袋取出,经过蒸汽预缩机进行对棉的蓬松恢复和定型,蒸汽预缩机内的温度为120℃,对棉的蓬松恢复和定型的速度为5m/分钟;
4-2、将蓬松恢复和定型过的棉铺至自动裁床,按照设计需要进行裁剪和冲孔;
4-3、裁剪和冲孔好的棉片,清理镂空孔洞废弃棉,并避免挤压,整齐存放备用;
(5)平板热压机模具的固定;
5-1、制备TPU颗粒模具;依据贴合点形状模切白色高温1.5cm厚TPU颗粒,得到TPU颗粒模具,TPU颗粒模具的直径大于TPU热熔胶膜直径,且小于棉孔四周2mm,并清洗干净;
5-2、将平板热压机清理干净,尤其是平板热压机上的上模发热板、下模发热板用布去除灰尘,并将上模发热板、下模发热板设定为70℃;
5-3、镭射机在卡纸板上镭出TPU颗粒模具的位置,用来粘TPU颗粒模具时对位使用;
5-4、平板热压机的下模发热板安装上TPU胶膜对位板;
5-5、将卡纸版置于平板热压机下模发热板,对位卡入TPU胶膜对位板中;
5-6、用硅橡胶涂于TPU颗粒模具不接触布料的底面;
5-7、将步骤5-6中的TPU颗粒模具正面朝步骤5-5中的卡纸版,对着镭射的位置依序摆放,涂好硅橡胶的底面朝上;
5-8、启动热压机,上模发热板、下模发热板温度70℃,上模发热板、下模发热板压力2.5KG,热压10S,使贴合点形状的白色TPU颗粒模具涂好硅橡胶的底部粘着于平板热压机的上模发热板上;
5-9、在步骤5-8完成后,取出对位卡纸板,再次启动平板热压机,停留在热压机上的上模发热板压下时状态,静置3小时以上,使贴合点形状的白色TPU颗粒模具完全固定到热压机上的上模发热板上;
(6)将TPU热熔胶膜粘于底层布料;
6-1、底层布料平铺固定贴于步骤3-1中三合一模板的底板上;
6-2、将步骤3-3的 TPU胶膜对位板卡入已贴好底层布料的三合一模板的底板;
6-3、将步骤(1)中TPU热熔胶膜对位放置于步骤6-2的TPU胶膜对位板镂空孔洞内,点烫笔加热点状固定后,取出TPU胶膜对位板;
6-4、将已固定好TPU热熔胶膜的底层布料,连同三合一模板底板,卡入步骤5-4的平板热压机的下模发热板;
6-5、启动平板热压机,平板热压机参数为上模发热板220℃、下模发热板110℃,压力为2.5KG, 热压8S,完成后连同三合一模板底板取出;
(7)固定棉于底层布料;
7-1、去除步骤(6)底层布料上TPU热熔胶膜上的离型纸膜;
7-2、将经步骤4-3裁剪和冲孔好的棉,置于步骤(6)的底层布料上,棉孔与TPU热熔胶膜对位,TPU 热熔胶膜居中于棉孔,并将棉的四周固定,使其不会移位;
7-3、固定棉后,连同三合一模板底板,卡入行线机,依照预设轨迹进行行线,使底层布料和棉通过行线结合在一起,完成后从行线机取出;
(8)底层布料和面层布料热压结合;
8-1、将步骤3-2中松量凸板卡入步骤3-1的三合一模板面板;
8-2、将面层布料按轮廓线自然放松覆盖至步骤8-1的模板上,四周固定到三合一模板面板的台板胶上;
8-3、将松量凸板取出,得到已固定面层布料的三合一模板面板,将三合一模板面板与三合一模板底板对位卡在一起;
8-4、将经步骤8-3卡在一起的模板,置于平板热压机下模发热板,面层布料向上,面层布料上覆盖铁氟龙隔热纸,启动平板热压机,平板热压机参数为上模发热板220℃、下模发热板110℃、压力2.5KG,热压 25S,完成底层布料和面层布料的粘合;
8-5、完成后将热压结合后的底层布料和面层布料取出;
(9)贴合点镭射透气孔;
9-1、将经步骤(8)热压结合后的底层布料和面层布料连通模板置于镭射机台面,进行对位;
9-2、启动镭射机,进行对位镭孔;
9-3、完成对位镭孔后取出;
(10)行线固定底层布料、棉面层布料四周;
10-1、将完成镭射孔的模板和布料再次卡入行线机台面;
10-2、启动行线机,行线固定底层布料、棉、面层布料三层结构的四周,使其平整无扭曲;
10-3、完成后,将行线固定底层布料、棉、面层布料后的布料从模板上分离下来,平整置放,后续进行拼装缝制。

Claims (5)

1.一种服装用保温棉透气孔与行线、贴合、镭射综合加工制程技术,其特征在于,包括以下步骤:
(1)布料预缩和裁剪,得到面层布料、底层布料;
(2)切割贴合需要的TPU热熔胶膜;用刀模斩切TPU热熔胶膜,防尘恒温存放备用;
(3)切割三合一组合模板,割三合一组合模板为行线、贴合、镭射三合一组合模板;
3-1、制备底板、面板;将2mm厚高温黄板按加工部位大小切割成镂空,并刻画上加工部位的轮廓线条,在边缘涂上台板胶,制成底板、面板,得到底板、面板;
3-2、制备松量凸板;将0.2mm厚高温黄板粘上1.5cm高的贴合点形状发泡棉颗粒,然后用牛皮纸覆盖和固定,使其成一个立体的盒状,得到松量凸板;
3-3、制备TPU胶膜对位板:卡纸板按贴合点形状镭射镂空,用于底层布料贴TPU热熔胶膜;
(4)棉裁剪与冲孔;
4-1、将棉从真空袋取出,经过蒸汽预缩机进行对棉的蓬松恢复和定型;
4-2、将蓬松恢复和定型过的棉铺至自动裁床,按照设计需要进行裁剪和冲孔;
4-3、裁剪和冲孔好的棉片,清理镂空孔洞废弃棉,并避免挤压,整齐存放备用;
(5)平板热压机模具的固定;
5-1、制备TPU颗粒模具;依据贴合点形状模切白色高温1.5cm厚TPU颗粒,得到TPU颗粒模具,TPU颗粒模具的直径大于TPU热熔胶膜直径,且小于棉孔四周2mm,并清洗干净;
5-2、将平板热压机清理干净,尤其是平板热压机上的上模发热板、下模发热板用布去除灰尘,并将上模发热板、下模发热板设定为70℃;
5-3、镭射机在卡纸板上镭出TPU颗粒模具的位置,用来粘TPU颗粒模具时对位使用;
5-4、平板热压机的下模发热板安装上TPU胶膜对位板;
5-5、将卡纸板置于平板热压机下模发热板,对位卡入TPU胶膜对位板中;
5-6、用硅橡胶涂于TPU颗粒模具不接触布料的底面;
5-7、将步骤5-6中的TPU颗粒模具正面朝步骤5-5中的卡纸板,对着镭射的位置依序摆放,涂好硅橡胶的底面朝上;
5-8、启动热压机,上模发热板、下模发热板温度70℃,上模发热板、下模发热板压力2.5KG,热压10S,使贴合点形状的白色TPU颗粒模具涂好硅橡胶的底部粘着于平板热压机的上模发热板上;
5-9、在步骤5-8完成后,取出对位卡纸板,再次启动平板热压机,停留在热压机上的上模发热板压下时状态,静置3小时以上,使贴合点形状的白色TPU颗粒模具完全固定到热压机上的上模发热板上;
(6)将TPU热熔胶膜粘于底层布料;
6-1、底层布料平铺固定贴于步骤3-1中三合一模板的底板上;
6-2、将步骤3-3的 TPU胶膜对位板卡入已贴好底层布料的三合一模板的底板;
6-3、将步骤(2)中TPU热熔胶膜对位放置于步骤6-2的TPU胶膜对位板镂空孔洞内,点烫笔加热点状固定后,取出TPU胶膜对位板;
6-4、将已固定好TPU热熔胶膜的底层布料,连同三合一模板底板,卡入步骤5-4的平板热压机的下模发热板;
6-5、启动平板热压机,平板热压机参数为上模发热板220℃、下模发热板110℃,压力为2.5KG, 热压8S,完成后连同三合一模板底板取出;
(7)固定棉于底层布料;
7-1、去除步骤(6)底层布料上TPU热熔胶膜上的离型纸膜;
7-2、将经步骤4-3裁剪和冲孔好的棉,置于步骤(6)的底层布料上,棉孔与TPU热熔胶膜对位,TPU 热熔胶膜居中于棉孔,并将棉的四周固定,使其不会移位;
7-3、固定棉后,连同三合一模板底板,卡入行线机,依照预设轨迹进行行线,使底层布料和棉通过行线结合在一起,完成后从行线机取出;
(8)底层布料和面层布料热压结合;
8-1、将步骤3-2中松量凸板卡入步骤3-1的三合一模板面板;
8-2、将面层布料按轮廓线自然放松覆盖至步骤8-1的模板上,四周固定到三合一模板面板的台板胶上;
8-3、将松量凸板取出,得到已固定面层布料的三合一模板面板,将三合一模板面板与三合一模板底板对位卡在一起;
8-4、将经步骤8-3卡在一起的模板,置于平板热压机下模发热板,面层布料向上,面层布料上覆盖铁氟龙隔热纸,启动平板热压机,平板热压机参数为上模发热板220℃、下模发热板110℃ 、压力2.5KG,热压 25S,完成底层布料和面层布料的粘合;
8-5、完成后将热压结合后的底层布料和面层布料取出;
(9)贴合点镭射透气孔;
9-1、将经步骤(8)热压结合后的底层布料和面层布料连通模板置于镭射机台面,进行对位;
9-2、启动镭射机,进行对位镭孔;
9-3、完成对位镭孔后取出;
(10)行线固定底层布料、棉面层布料四周;
10-1、将完成镭射孔的模板和布料再次卡入行线机台面;
10-2、启动行线机,行线固定底层布料、棉、面层布料三层结构的四周,使其平整无扭曲;
10-3、完成后,将行线固定底层布料、棉、面层布料后的布料从模板上分离下来,平整置放,后续进行拼装缝制。
2.根据权利要求1所述的服装用保温棉透气孔与行线、贴合、镭射综合加工制程技术,其特征在于,步骤(1)中,包括以下步骤:
1-1、使用滚轮式预缩机,将布料进行预缩,以解决后续热压时面料收缩变形,造成对位不准;
1-2、预缩后静置24H,使其冷却定型,收缩到位;
1-3、预缩后裁剪成需要的布料裁片,得到预缩和裁剪好的面层布料、底层布料。
3.根据权利要求1所述的服装用保温棉透气孔与行线、贴合、镭射综合加工制程技术,其特征在于,步骤(2)中,TPU热熔胶膜的型号为BEMIS-3829。
4.根据权利要求1所述的服装用保温棉透气孔与行线、贴合、镭射综合加工制程技术,其特征在于,步骤(3)中,将2mm厚高温黄板按加工部位大小切割成镂空,并刻画上加工部位的轮廓线条,在边缘涂上台板胶,制成底板、面板。
5.根据权利要求1所述的服装用保温棉透气孔与行线、贴合、镭射综合加工制程技术,其特征在于,步骤4-1中,蒸汽预缩机内的温度为120℃,对棉的蓬松恢复和定型的速度为5m/分钟。
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