TWM580551U - Bulk bag with hot-melting fusion part - Google Patents
Bulk bag with hot-melting fusion part Download PDFInfo
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- TWM580551U TWM580551U TW108201800U TW108201800U TWM580551U TW M580551 U TWM580551 U TW M580551U TW 108201800 U TW108201800 U TW 108201800U TW 108201800 U TW108201800 U TW 108201800U TW M580551 U TWM580551 U TW M580551U
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- 238000002844 melting Methods 0.000 title claims abstract description 5
- 230000004927 fusion Effects 0.000 title description 2
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 38
- 239000004033 plastic Substances 0.000 claims abstract description 31
- 239000012943 hotmelt Substances 0.000 claims abstract description 28
- 239000004744 fabric Substances 0.000 claims abstract description 22
- 239000002985 plastic film Substances 0.000 claims abstract description 19
- 229920006255 plastic film Polymers 0.000 claims abstract description 18
- 230000002093 peripheral effect Effects 0.000 claims abstract description 14
- 230000004308 accommodation Effects 0.000 claims description 3
- 239000002131 composite material Substances 0.000 abstract description 4
- 238000009958 sewing Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 239000000463 material Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 230000008719 thickening Effects 0.000 description 1
- 238000009941 weaving Methods 0.000 description 1
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Abstract
本創作係包括一外袋單元、一內袋單元、複數加強單元及複數熱融結合部。內袋單元設於外袋單元內,內袋單元係由兩層第一塑膠膜夾設一第一編織塑膠布層構成複合結構;且內袋單元具有一內表面部及四個周邊角部。每一加強單元係由兩層第二塑膠膜夾設一第二編織塑膠布層構成複合結構;每一加強單元係連結於內表面部,且面對相對應之周邊角部,構成強化內袋單元之結構。每一熱融結合部分別位於每一加強單元與內表面部之連結位置,其係為每一加強單元與內表面部經熱融黏合後固化之結構。故,本案兼具內袋單元與複數個加強單元之整體結構強度較佳,內袋單元具有熱融結合部革除車縫孔洩漏問題等問題。 The creation system includes an outer bag unit, an inner bag unit, a plurality of reinforcing units and a plurality of hot melt joints. The inner bag unit is disposed in the outer bag unit, and the inner bag unit is formed by sandwiching a first woven plastic cloth layer with two first plastic films to form a composite structure; and the inner bag unit has an inner surface portion and four peripheral corner portions. Each reinforcing unit is composed of two second plastic films sandwiching a second woven plastic cloth layer to form a composite structure; each reinforcing unit is coupled to the inner surface portion and faces the corresponding peripheral corner portion to form a reinforced inner bag The structure of the unit. Each of the heat-melting joints is respectively located at a joint position of each of the reinforcing unit and the inner surface portion, and is a structure in which each of the reinforcing unit and the inner surface portion is cured by heat-melting and curing. Therefore, in this case, the overall structural strength of the inner bag unit and the plurality of reinforcing units is better, and the inner bag unit has problems such as the problem of leakage of the seam hole in the hot-melt joint portion.
Description
本創作係有關一種具有熱融結合部的太空袋,尤指一種兼具內袋單元與複數個加強單元之整體結構強度較佳,內袋單元具有熱融結合部革除車縫孔洩漏問題之具有熱融結合部的太空袋。 The present invention relates to a space bag having a hot-melt joint, in particular, an overall structural strength of an inner bag unit and a plurality of reinforcing units, and the inner bag unit has a hot-melt joint to remove the seam hole leakage problem. The space bag of the hot melt joint.
參閱第7、第8及第9圖,公知太空袋係包括:一外袋單元91,係具有複數個外牆片體911,該複數外牆片體11係用以包圍出一容納空間912。 Referring to Figures 7, 8, and 9, the known space bag includes an outer bag unit 91 having a plurality of outer wall sheets 911 for enclosing an accommodation space 912.
一內袋單元92,係設於該容納空間912內,該內袋單元92係具有一內表面部92A及四個周邊角部92B。 An inner bag unit 92 is disposed in the accommodating space 912. The inner bag unit 92 has an inner surface portion 92A and four peripheral corner portions 92B.
複數個加強單元93,該每一加強單元93係以車縫線931車縫於該內表面部92A,且面對相對應之該周邊角部92B。 A plurality of reinforcing units 93 are sewn to the inner surface portion 92A by a sewing thread 931 and face the corresponding peripheral corner portion 92B.
由於該加強單元93係以該車縫線931車縫固定於該內袋單元92上,車縫過程複數車縫線31產生相對應之複數車縫孔932。當太空袋裝滿之物體為粉末時,粉末易透過這些車縫孔932由該內袋單元92洩漏出,特別時承載之物體較重時,內裝之粉末極易向外撐大該內袋單元92,使太空袋上之該複數車縫孔932再擴大,外漏之問題更惡化。 Since the reinforcing unit 93 is sewn to the inner bag unit 92 by the sewing thread 931, the plurality of sewing threads 31 of the sewing process generate corresponding plurality of sewing holes 932. When the object filled in the space bag is a powder, the powder is easily leaked from the inner bag unit 92 through the sewing holes 932. When the object to be loaded is heavy, the powder inside is easily extended to the inner bag. The unit 92 expands the plurality of sewn holes 932 on the space bag, and the problem of external leakage is further deteriorated.
其次,若要增加該內袋單元92與該加強單元93之強度,當然可以採用加厚之作法,但是,一旦該內袋單元92與該加強單元93太厚,會產生不易車縫與車縫時易斷針之新問題。 Secondly, if the strength of the inner bag unit 92 and the reinforcing unit 93 is to be increased, it is of course possible to use a thickening method. However, once the inner bag unit 92 and the reinforcing unit 93 are too thick, it is difficult to sewn and sewn. A new problem with easy breaks.
有鑑於此,必須研發出可解決上述習用缺點之技術。 In view of this, it is necessary to develop a technique that can solve the above disadvantages.
本創作之目的,在於提供一種具有熱融結合部的太空袋,其兼具內袋單元與複數個加強單元之整體結構強度較佳,內袋單元具有熱融結合部革除車縫孔洩漏問題等優點。特別是,本創作所欲解決之問題係在於公知太空袋之車縫孔易造成滲漏之問題。 The purpose of the present invention is to provide a space bag having a hot-melt joint, which has the overall structural strength of the inner bag unit and the plurality of reinforcing units, and the inner bag unit has a hot-melt joint to remove the seam hole leakage problem. advantage. In particular, the problem to be solved by this creation is that the seam of the known space bag is prone to leakage.
解決上述問題之技術手段係提供一種具有熱融結合部的太空袋,其包括:一外袋單元,係具有複數個外牆片體,該複數外牆片體係用以包圍出一容納空間;一內袋單元,係設於該容納空間內,該內袋單元係具有兩層第一塑膠膜及一第一編織塑膠布層,該第一編織塑膠布層係為經緯交錯之編織結構,該第一編織塑膠布層係介於該兩層第一塑膠膜之間;且該內袋單元係具有一內表面部及四個周邊角部;複數加強單元,該每一加強單元係具有兩層第二塑膠膜及一第二編織塑膠布層,該第二編織塑膠布層係為經緯交錯之編織結構,該第二編織塑膠布層係介於該兩層第二塑膠膜之間;該每一加強單元係用以連結於該內表面部,且面對相對應之該周邊角部,構成強化該內袋單元之結構;複數個熱融結合部,係分別位於該每一加強單元與該內表面部之連結位置,該每一熱融結合部係為該每一加強單元與該內表面部經熱融黏合後固化之結構。 The technical means for solving the above problems is to provide a space bag having a hot-melt joint, comprising: an outer bag unit having a plurality of outer wall sheets, wherein the plurality of outer wall systems are used to surround a receiving space; The inner bag unit is disposed in the accommodating space, the inner bag unit has two layers of a first plastic film and a first woven plastic cloth layer, and the first woven plastic cloth layer is a warp and weft interlaced woven structure, the first a woven plastic cloth layer is interposed between the two first plastic films; and the inner bag unit has an inner surface portion and four peripheral corner portions; a plurality of reinforcing units each having two layers a second plastic film layer and a second woven plastic cloth layer, wherein the second woven plastic cloth layer is a warp and weft interlaced structure, and the second woven plastic cloth layer is interposed between the two second plastic films; The reinforcing unit is configured to be coupled to the inner surface portion and face the corresponding peripheral corner portion to constitute a structure for reinforcing the inner bag unit; a plurality of hot-melt joint portions are respectively located in the reinforcing unit and the inner reinforcing portion The joint position of the surface portion, Each curing hot melt binding portion after fusion bonding unit and the inner surface of that portion of each structural thermally strengthened.
本創作之上述目的與優點,不難從下述所選用實施例之詳細說明與附圖中,獲得深入瞭解。 The above objects and advantages of the present invention will be readily understood from the following detailed description of the embodiments and the accompanying drawings.
茲以下列實施例並配合圖式詳細說明本創作於後: The following examples are used in conjunction with the drawings to illustrate the creation in detail:
10、91‧‧‧外袋單元 10, 91‧‧‧ outer bag unit
11、911‧‧‧外牆片體 11, 911 ‧ ‧ façade
12、912‧‧‧容納空間 12, 912‧‧‧ accommodation space
20、92‧‧‧內袋單元 20, 92‧‧‧ inner bag unit
20A、92A‧‧‧內表面部 20A, 92A‧‧‧ inside surface
20B、92B‧‧‧周邊角部 20B, 92B‧‧‧ peripheral corners
21‧‧‧第一塑膠膜 21‧‧‧First plastic film
22‧‧‧第一編織塑膠布層 22‧‧‧First woven plastic layer
30、93‧‧‧加強單元 30, 93‧‧‧ Strengthening unit
30A‧‧‧主片部 30A‧‧‧Main Film Department
30B‧‧‧側邊部 30B‧‧‧ Side
301‧‧‧開口 301‧‧‧ openings
31‧‧‧第二塑膠膜 31‧‧‧Second plastic film
32‧‧‧第二編織塑膠布層 32‧‧‧Second woven plastic fabric
931‧‧‧車縫線 931‧‧‧Sewing line
932‧‧‧車縫孔 932‧‧‧Sewed holes
M‧‧‧熱融結合部 M‧‧‧Hot and Fuse Department
第1圖係本創作之外袋單元與內袋單元之對應關係之示意圖 Figure 1 is a schematic diagram of the correspondence between the outer bag unit and the inner bag unit of the present invention.
第2圖係本創作之內袋單元之示意圖 Figure 2 is a schematic diagram of the inner bag unit of the present creation
第3圖係本創作之第一(第二)編織塑膠布層之局部放大之示意圖 Figure 3 is a partial enlarged view of the first (second) woven plastic fabric layer of the present creation
第4A圖係本創作之內袋單元之局部放大剖視圖 Figure 4A is a partial enlarged cross-sectional view of the inner bag unit of the present creation
第4B圖係本創作之加強單元之局部放大剖視圖 Figure 4B is a partial enlarged cross-sectional view of the reinforcing unit of the present creation
第5圖係本創作之內袋單元與加強單元結合前之放大剖視圖 Figure 5 is an enlarged cross-sectional view of the inner bag unit and the reinforcing unit of the present invention.
第6圖係第5圖之內袋單元與加強單元結合後產生熱融結合部之放大剖視圖 Figure 6 is an enlarged cross-sectional view showing the combination of the inner and outer bag units and the reinforcing unit in Fig. 5
第7圖係公知太空袋之外袋單元與內袋單元之對應關係之示意圖 Figure 7 is a schematic diagram showing the correspondence between the outer bag unit and the inner bag unit of the known space bag.
第8圖係第7圖之內袋單元之示意圖 Figure 8 is a schematic view of the inner bag unit of Figure 7
第9圖係第8圖之其他角度之示意圖 Figure 9 is a schematic diagram of other angles of Figure 8.
參閱第1、第2、第3、第4A、第4B、第5及第6圖,本創作係為一具有熱融結合部的太空袋,其包括:一外袋單元10,係具有複數個外牆片體11,該複數外牆片體11係用以包圍出一容納空間12。 Referring to Figures 1, 2, 3, 4A, 4B, 5 and 6, the present invention is a space bag having a hot-melt joint, comprising: an outer bag unit 10 having a plurality of The outer wall sheet 11 is used to surround a receiving space 12.
一內袋單元20,係設於該容納空間12內,該內袋單元20係具有兩層第一塑膠膜21及一第一編織塑膠布層22,該第一編織塑膠布層22係為經緯交錯之編織結構,該第一編織塑膠布層22係介於該兩層第一塑膠膜21之間;且該內袋單元20係具有一內表面部20A及四個周邊角部20B。 An inner bag unit 20 is disposed in the accommodating space 12, and the inner bag unit 20 has two layers of a first plastic film 21 and a first woven plastic cloth layer 22, and the first woven plastic cloth layer 22 is a warp and weft. The interwoven woven structure, the first woven plastic layer 22 is interposed between the two first plastic films 21; and the inner bag unit 20 has an inner surface portion 20A and four peripheral corner portions 20B.
複數加強單元30,該每一加強單元30係具有兩層第二塑膠膜31及一第二編織塑膠布層32,該第二編織塑膠布層32係為經緯交錯之編織結構,該第二編織塑膠布層32係介於該兩層第二塑膠膜31之間。該每一加強單元30係用以連結於該內表面部20A,且面對相對應之該周邊角部20B,構成強化該內袋單元20之結構。 A plurality of reinforcing units 30 each having two layers of a second plastic film 31 and a second woven plastic layer 32, wherein the second woven plastic layer 32 is a warp and weft interlaced structure, the second weaving The plastic cloth layer 32 is interposed between the two second plastic films 31. Each of the reinforcing units 30 is coupled to the inner surface portion 20A and faces the corresponding peripheral corner portion 20B to constitute a structure for reinforcing the inner bag unit 20.
複數個熱融結合部M,係分別位於該每一加強單元30與該內表面部20A之連結位置,該每一熱融結合部M係為該每一加強單元30與該內表面部20A經熱融黏合後固化之結構。 A plurality of hot-melt joints M are respectively located at a joint position of each of the reinforcing units 30 and the inner surface portion 20A, and each of the heat-melting joints M is the reinforcing unit 30 and the inner surface portion 20A. The structure after curing by hot melt bonding.
實務上,該第一編織塑膠布層22係由複數條塑膠材質之條片,呈經緯交錯之編織結構。 In practice, the first woven plastic cloth layer 22 is composed of a plurality of strips of plastic material, and has a warp and weft interlaced structure.
該每一加強單元30係具有一主片部30A及兩側邊部30B。該兩側邊部30B係用以連結於該內表面部20A,而將該主片部30A固定於相對應之該周邊角部20B。 Each of the reinforcing units 30 has a main piece portion 30A and two side edges 30B. The side edge portions 30B are connected to the inner surface portion 20A, and the main piece portion 30A is fixed to the corresponding peripheral corner portion 20B.
該主片部30A具有至少一個開口301,其係連通該周邊角部20B與該內袋單元20之內部。 The main piece portion 30A has at least one opening 301 that communicates with the peripheral corner portion 20B and the inside of the inner bag unit 20.
該第二編織塑膠布層32係由複數條塑膠材質之條片,呈經緯交錯之編織結構。 The second woven plastic cloth layer 32 is composed of a plurality of strips of plastic material, and has a warp and weft interlaced structure.
該複數個熱融結合部M係分別位於該每一側邊部30B與該內表面部20A之連結位置,該每一熱融結合部M係為該每一側邊部30B與該內表面部20A經熱融黏合後固化之結構。 The plurality of hot-melt joints M are respectively located at a joint position of each of the side edges 30B and the inner surface portion 20A, and each of the hot-melt joints M is the side edge portion 30B and the inner surface portion. 20A is a structure that is cured by hot melt bonding.
本創作之重點在於,該內袋單元20係由該兩層第一塑膠膜22夾設該第一編織塑膠布層21構成之複合結構。且該第一編織塑膠布層22係為經緯交錯之編織 結構,結構強度佳。又,該加強單元30係由該兩層第二塑膠膜32夾設該第二編織塑膠布層31構成之複合結構。且,該第二編織塑膠布層32亦為經緯交錯之編織結構,結構強度佳。再加上該內袋單元20經熱融黏合該每一加強單元30時,均相對應產生該熱融結合部M,如此,熱融黏合過程除無車縫之針孔(可能造成洩漏)問題外,結合強度亦大大輔助提昇太空袋整體之結構強度。 The focus of the present invention is that the inner bag unit 20 is a composite structure in which the first woven plastic cloth layer 21 is sandwiched between the two first plastic films 22. And the first woven plastic cloth layer 22 is woven by warp and weft Structure, structural strength. Further, the reinforcing unit 30 is a composite structure in which the second woven plastic sheet layer 31 is interposed between the two second plastic films 32. Moreover, the second woven plastic cloth layer 32 is also a warp and weft interlaced structure, and has good structural strength. In addition, when the inner bag unit 20 is thermally melt-bonded to each of the reinforcing units 30, the hot-melt joint portion M is correspondingly generated, so that the hot-melt bonding process is free of pinholes (may cause leakage). In addition, the bonding strength also greatly enhances the structural strength of the overall space bag.
本創作之優點及功效係如下所述: The advantages and functions of this creation are as follows:
[1]內袋單元與複數個加強單元之整體結構強度較佳。本案之內袋單元與複數個加強單元均具有編織塑膠布層,由於經緯交錯之編織結構強度佳,再加上每一加強單元之側邊部與該內袋單元之內表面部為熱融結合部,黏固力強,故,內袋單元與複數個加強單元之整體結構強度較佳。 [1] The overall structural strength of the inner bag unit and the plurality of reinforcing units is better. In the present case, the inner bag unit and the plurality of reinforcing units each have a woven plastic cloth layer, and the woven structure of the warp and weft is excellent in strength, and the side portions of each reinforcing unit are thermally combined with the inner surface portion of the inner bag unit. In addition, the adhesive strength is strong, so the overall structural strength of the inner bag unit and the plurality of reinforcing units is better.
[2]內袋單元具有熱融結合部革除車縫孔洩漏問題。本案之內袋單元與加強單元固定後產生熱融結合部,完全解決公知車縫產生車縫孔易造成洩漏的缺點。故,內袋單元具有熱融結合部革除車縫孔洩漏問題。 [2] The inner bag unit has a hot-melt joint to remove the leakage problem of the seam hole. In the present case, the inner bag unit and the reinforcing unit are fixed to generate a hot-melt joint, which completely solves the shortcoming that the known sewn seam is easy to cause leakage. Therefore, the inner bag unit has a hot-melt joint to remove the leakage problem of the seam hole.
以上僅是藉由較佳實施例詳細說明本創作,對於該實施例所做的任何簡單修改與變化,皆不脫離本創作之精神與範圍。 The above is only a detailed description of the present invention by way of a preferred embodiment, and any modifications and variations of the embodiments are possible without departing from the spirit and scope of the present invention.
Claims (4)
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| Application Number | Priority Date | Filing Date | Title |
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| TW108201800U TWM580551U (en) | 2019-02-08 | 2019-02-08 | Bulk bag with hot-melting fusion part |
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| TW108201800U TWM580551U (en) | 2019-02-08 | 2019-02-08 | Bulk bag with hot-melting fusion part |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI844301B (en) * | 2023-03-15 | 2024-06-01 | 金樹塑膠工業股份有限公司 | Bulk bag |
-
2019
- 2019-02-08 TW TW108201800U patent/TWM580551U/en not_active IP Right Cessation
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI844301B (en) * | 2023-03-15 | 2024-06-01 | 金樹塑膠工業股份有限公司 | Bulk bag |
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Legal Events
| Date | Code | Title | Description |
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| MM4K | Annulment or lapse of a utility model due to non-payment of fees |