CN108065460B - Underwear structure - Google Patents
Underwear structure Download PDFInfo
- Publication number
- CN108065460B CN108065460B CN201611051153.4A CN201611051153A CN108065460B CN 108065460 B CN108065460 B CN 108065460B CN 201611051153 A CN201611051153 A CN 201611051153A CN 108065460 B CN108065460 B CN 108065460B
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- China
- Prior art keywords
- fabric
- cup
- cups
- wing
- undergarment
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- 239000004744 fabric Substances 0.000 claims abstract description 140
- 239000000463 material Substances 0.000 claims abstract description 26
- 230000002093 peripheral effect Effects 0.000 claims abstract description 26
- 229920000742 Cotton Polymers 0.000 claims abstract description 10
- 239000000758 substrate Substances 0.000 claims description 33
- 238000000748 compression moulding Methods 0.000 claims description 7
- 239000004677 Nylon Substances 0.000 claims description 6
- 229920000297 Rayon Polymers 0.000 claims description 6
- 229920001778 nylon Polymers 0.000 claims description 6
- 239000002964 rayon Substances 0.000 claims description 6
- 239000000835 fiber Substances 0.000 claims description 5
- 229920000728 polyester Polymers 0.000 claims description 5
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- 230000036461 convulsion Effects 0.000 claims description 3
- 210000004177 elastic tissue Anatomy 0.000 claims description 3
- 239000010959 steel Substances 0.000 claims description 3
- 210000002268 wool Anatomy 0.000 claims description 3
- 239000002759 woven fabric Substances 0.000 claims description 3
- 238000004049 embossing Methods 0.000 claims description 2
- 238000005096 rolling process Methods 0.000 claims 1
- 125000006850 spacer group Chemical group 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 abstract description 13
- 230000035699 permeability Effects 0.000 abstract 1
- 239000010410 layer Substances 0.000 description 37
- 238000009958 sewing Methods 0.000 description 4
- 238000003825 pressing Methods 0.000 description 3
- 238000009423 ventilation Methods 0.000 description 3
- 239000011247 coating layer Substances 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- NOQGZXFMHARMLW-UHFFFAOYSA-N Daminozide Chemical group CN(C)NC(=O)CCC(O)=O NOQGZXFMHARMLW-UHFFFAOYSA-N 0.000 description 1
- 230000003796 beauty Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 239000000806 elastomer Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000008093 supporting effect Effects 0.000 description 1
- 238000009941 weaving Methods 0.000 description 1
Images
Classifications
-
- A—HUMAN NECESSITIES
- A41—WEARING APPAREL
- A41C—CORSETS; BRASSIERES
- A41C3/00—Brassieres
-
- A—HUMAN NECESSITIES
- A41—WEARING APPAREL
- A41C—CORSETS; BRASSIERES
- A41C3/00—Brassieres
- A41C3/0014—Brassieres made from one piece with one or several layers
-
- A—HUMAN NECESSITIES
- A41—WEARING APPAREL
- A41C—CORSETS; BRASSIERES
- A41C5/00—Machines, appliances, or methods for manufacturing corsets or brassieres
- A41C5/005—Machines, appliances, or methods for manufacturing corsets or brassieres by moulding
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04B—KNITTING
- D04B1/00—Weft knitting processes for the production of fabrics or articles not dependent on the use of particular machines; Fabrics or articles defined by such processes
- D04B1/22—Weft knitting processes for the production of fabrics or articles not dependent on the use of particular machines; Fabrics or articles defined by such processes specially adapted for knitting goods of particular configuration
- D04B1/24—Weft knitting processes for the production of fabrics or articles not dependent on the use of particular machines; Fabrics or articles defined by such processes specially adapted for knitting goods of particular configuration wearing apparel
- D04B1/246—Upper torso garments, e.g. sweaters, shirts, leotards
-
- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2401/00—Physical properties
- D10B2401/04—Heat-responsive characteristics
- D10B2401/041—Heat-responsive characteristics thermoplastic; thermosetting
-
- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2403/00—Details of fabric structure established in the fabric forming process
- D10B2403/02—Cross-sectional features
- D10B2403/022—Lofty fabric with variably spaced front and back plies, e.g. spacer fabrics
-
- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2501/00—Wearing apparel
- D10B2501/02—Underwear
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Corsets Or Brassieres (AREA)
Abstract
The present invention provides an undergarment structure comprising: two cups connected with each other, each cup having a peak area and a peripheral area, the outer edges of the peripheral areas of the two cups extending a wing respectively, and the ends of the two wings far away from the cups respectively being connected together; wherein, two cups connected and two extending wings are molded by one piece of seamless 3D three-dimensional fabric base material (which can be sandwich fabric or space cotton cloth) at the same time, and the thickness of the molded 3D three-dimensional fabric base material in the cup peak area is larger than the thickness of the peripheral area and the wings. The underwear has the advantages of seamless structure, air permeability, lightness, thinness, no burden and comfortable feeling, and the manufacturing time is short, so that the manufacturing cost can be reduced.
Description
Technical Field
The invention mainly relates to an underwear structure, in particular to an air-permeable, light and thin underwear structure.
Background
The bra is the most close-fitting clothes for women, and the requirements of consumers on the quality and the use comfort of the bra are relatively increased under the environment that the living quality of the Chinese people is generally improved nowadays. As shown in fig. 1, a typical brassiere 10 mainly comprises left and right cups 12, left and right side wings 14, left and right shoulder straps 16, and a back buckle 18, wherein the left and right cups 12 and the left and right side wings 14 are mostly made of multiple pieces of same or different fabric by stitching and sewing, and a plurality of seams 20 are formed, which affects the beauty and comfort. On the other hand, the fabric used in the conventional bra cup 12 includes at least two fabrics, i.e., an outer fabric and two bottom surfaces, and an elastomer or a cotton layer is sandwiched between the outer fabric and the two bottom surfaces, so that the bra cup 12 needs to be made of two or more fabrics, and has the disadvantages of complicated processing, long making time and high production cost.
Disclosure of Invention
In order to solve the above problems, an objective of the present invention is to provide an underwear structure, wherein a single seamless 3D three-dimensional fabric substrate (such as a sandwich fabric or a space cotton fabric) is integrally molded, so as to reduce the complexity of the traditional underwear that needs to be formed by splicing and sewing multiple Fabrics, and improve the defect of insufficient appearance of the traditional underwear due to multiple seams.
The invention aims to provide an underwear structure, which is integrally molded by using a single seamless 3D three-dimensional fabric base material, has the ventilation, light and thin comfort of the 3D three-dimensional fabric base material and no burden, can be attached to the chest of a human body due to no splicing and no seam, and has better covering property.
One of the purposes of the invention is to provide an underwear structure which has the suitability of being worn or exposed and has a fashion effect.
One of the objectives of the present invention is to provide an underwear structure having the advantages of saving manufacturing time and reducing manufacturing cost.
In order to achieve the above object, an undergarment structure according to an embodiment of the present invention includes: two cups connected with each other, each cup having a peak area and a peripheral area, the outer edges of the peripheral areas of the two cups extending a wing respectively, and two ends of the two wings respectively far away from the cups being connected together; wherein, two cups that link and two wings parts that extend are moulded by the integrative compression molding of monolithic seamless 3D three-dimensional fabric substrate simultaneously, and the thickness of the three-dimensional fabric substrate of 3D after the mould pressing is greater than the thickness of peripheral zone and alar part in the cupular peak district.
In one embodiment, the thickness of the molded 3D three-dimensional fabric substrate is gradually thinner from the cup peak region to the outer edge of the peripheral region; in another embodiment, the thickness of the molded 3D three-dimensional fabric substrate in the peripheral region is less than or equal to the thickness of the wing portion; in another embodiment, the thickness of the molded 3D solid fabric substrate at the wing portion is gradually thinner from the end of the wing portion adjacent to the cup to the end away from the cup.
In one embodiment, the peak area is located approximately at the center of the cup and accounts for 30% to 50% of the area of the cup; the thickness of the 3D three-dimensional fabric base material in the cup peak area is between 2 mm and 10 mm, and the thickness of the peripheral area and the wing part is between 0.1 mm and 5 mm.
In one embodiment, the two cups are connected by a central part, and the two cups, the central part and the extending two wing parts are simultaneously integrally molded by a single piece of seamless 3D three-dimensional fabric base material; in another embodiment, the ends of the two wing parts respectively far away from the cups are connected with each other by a buckling structure, a felt structure or an elastic band.
In one embodiment, the three-dimensional fabric comprises an outer covering layer attached to an outer surface of the 3D three-dimensional fabric base material, two cups and two extending wing parts, wherein the two cups are connected with the 3D three-dimensional fabric base material and the outer covering layer in an integrated compression molding manner; wherein the outer cover layer can be a knitted fabric, a plain woven fabric, a wool fabric, a nylon fabric, a rayon fabric, a polyester fabric or a cotton fabric. In another embodiment, at least one surface of the 3D three-dimensional fabric substrate is further formed with one or a combination of twitch, embossing and printing.
In one embodiment, the 3D three-dimensional fabric substrate comprises an upper fabric layer, a lower fabric layer, and a middle fabric layer disposed between the upper fabric layer and the lower fabric layer, wherein the middle fabric layer is formed by a plurality of corrugated yarns, wherein peaks of the corrugated yarns are connected to the upper fabric layer, valleys of the corrugated yarns are connected to the lower fabric layer, and the corrugated yarns of the middle fabric layer are formed by monofilament fibers.
In an embodiment, the upper fabric layer and/or the lower fabric layer of the 3D three-dimensional fabric substrate are woven by using the shrinkable covering yarn, and the upper fabric layer and/or the lower fabric layer are woven by using one or a combination of polyester fiber yarn, elastic fiber yarn, nylon yarn, cotton yarn, and rayon yarn.
Drawings
Fig. 1 is a schematic view showing a structure of a conventional multi-seamed undergarment.
Fig. 2 is a schematic view showing the structure of an undergarment according to an embodiment of the present invention.
Fig. 3 is a cross-sectional view of the undergarment according to an embodiment of the invention.
Fig. 4 is a schematic view showing the application of the underwear structure according to one embodiment of the present invention.
Fig. 5 is a schematic view of a 3D three-dimensional fabric substrate used in the construction of an undergarment according to another embodiment of the present invention.
Fig. 6 is a schematic view of the mold used to manufacture the undergarment structure of the present invention.
Description of the symbols
10 bra
12 cup
14 side wing
16 shoulder strap
18 back button
20 seam
30 underwear structure
32. 32' cup
321. 321' peak area of cup
322. 322' peripheral region
34. 34' wing part
363D three-dimensional fabric base material
361 Upper fabric layer
362 middle fabric layer
363 lower fabric layer
38 central portion
40 positioning groove
42 binding part
44. 44' steel ring
46. 46' shoulder strap
48 outer cover
50 male die
52 master model
54 gap
Detailed Description
FIG. 2 is a schematic view of an undergarment structure according to an embodiment of the present invention, as shown, an undergarment structure 30 includes two cups 32, 32 ' connected to each other, and a wing portion 34, 34 ' extending from the outer edge of the two cups 32, 32 ', wherein the two cups 32, 32 ' connected to each other and the two wing portions 34, 34 ' extending from the two cups are integrally molded by a single piece of seamless 3D three-dimensional fabric base material 36; referring to fig. 3, each cup 32, 32 'has a peak area 321, 321' and a peripheral area 322, 322 ', two wing portions 34, 34' respectively extend from one side of the peripheral area 322, 322 ', and as shown in fig. 3, the thickness of the molded 3D three-dimensional fabric substrate 36 in the peak area 321, 321' is greater than the thickness of the peripheral area 322, 322 'and the wing portions 34, 34'.
Continuing with the above description, in one embodiment, the cup peak areas 321, 321 ' are located at the central portion of the cups 32, 32 ' and occupy about 30% to 50% of the areas of the cups 32, 32 ', and the peripheral areas 322, 322 ' surround the cup peak areas 321, 321 '; the two cups 32, 32 ' can be connected by a central portion 38, the central portion 38 can be in a shape of a strip, a belt or a triangle, and the central portion 38, the two cups 32, 32 ' and the two wing portions 34, 34 ' are integrally molded by a single piece of seamless 3D three-dimensional fabric base material 36. In one embodiment, the positioning groove 40 for disposing a retaining ring can be formed on the end surface of one of the wings 34 ' away from the cup 32 ' by pressing, which is advantageous for disposing a retaining ring to correspond to the hook disposed on the other wing 34, so that the two wings 34, 34 ' are connected to each other by the engagement of the retaining ring and the hook. In another embodiment, the ends of the two wing parts 34, 34 'respectively far from the cups 32, 32' can be connected to each other by a felt structure or an elastic band.
In one embodiment, as shown in fig. 3, the thickness of the cups 32, 32 'formed by the molded 3D three-dimensional fabric substrate 36 is gradually reduced from the peak areas 321, 321' to the outer edges of the peripheral areas 322, 322 ', the thickness of the peripheral areas 322, 322' may be less than or equal to the thickness of the wing portions 34, 34 ', and the thickness of the wing portions 34, 34' may be integrally uniform or regionally have different thicknesses, in one embodiment, the thickness of the molded 3D three-dimensional fabric substrate 36 at the wing portions 34, 34 'is gradually reduced from the ends of the wing portions 34, 34' adjacent to the cups 32, 32 'to the ends far away from the cups 32, 32'. The thickness of the 3D three-dimensional fabric substrate 36 in the cup peak areas 321 and 321 ' is between 2 mm and 10 mm, and the thickness of the peripheral areas 322 and 322 ' and the wing portions 34 and 34 ' is between 0.1 mm and 5 mm.
The 3D three-dimensional fabric substrate 36 is a sandwich fabric (also called "spacecotton cloth") formed by a 3D three-dimensional weaving method among an upper fabric layer 361, a middle fabric layer 362 and a lower fabric layer 363, the middle fabric layer 362 is formed by a plurality of corrugated yarns, wherein the wave crests of the corrugated yarns are connected with the upper fabric layer 361, and the wave troughs of the corrugated yarns are connected with the lower fabric layer 363, and the 3D three-dimensional fabric substrate 36 has the advantage of ventilation by the design of the corrugated yarns of the middle fabric layer 362; in one embodiment, the corrugated yarns of the middle fabric layer 362 are formed from monofilament fibers.
When the underwear structure 30 of the present invention is manufactured by using a male mold and a female mold of the mold to be pressed and molded, in an embodiment, a male mold 50 and a female mold 52 of the mold are as shown in fig. 6, wherein the thickness of the molded 3D three-dimensional fabric substrate 36 (shown in fig. 2 and 3) in the areas of the cups 32, 32 'and the wings 34, 34' is determined by the gap 54 reserved between the male mold 50 and the female mold 52 when the male mold 50 and the female mold are pressed and molded, if the reserved gap 54 is larger, the thickness of the molded 3D three-dimensional fabric substrate 36 is thicker, and if the reserved gap 54 is smaller, the thickness of the molded 3D three-dimensional fabric substrate 36 is smaller; in one embodiment, the gap 54 remaining between the male mold 50 and the female mold 52 for forming the cup peak areas 321, 321' corresponds to the thickness of the 3D solid fabric substrate 36 before being molded. The underwear structure 30 of the invention uses a single piece of seamless 3D three-dimensional fabric base material to integrally form cups and wing parts by compression molding, and the design that the whole underwear structure 30 is a single piece of cloth has the advantages of saving material cost and manufacturing time to reduce manufacturing cost.
In the present invention, the upper fabric layer 361 and/or the lower fabric layer 363 of the 3D three-dimensional fabric substrate 36 are woven by using a shrinkable covering yarn, and the upper fabric layer 361 and/or the lower fabric layer 363 are woven by using one or a combination of polyester fiber yarn, elastic fiber yarn, nylon yarn, cotton yarn, and rayon yarn. In one embodiment, upper fabric layer 361 and/or lower fabric layer 363 may be patterned with one or a combination of twitch, print, or emboss.
In the present invention, the underwear structure 30 formed by compression molding a single piece of fabric (3D three-dimensional fabric substrate) may be further processed to meet different functional requirements of the underwear, fig. 4 is an application diagram of the underwear structure according to an embodiment of the present invention, as shown in the figure, the peripheral edges of the cups 32, 32 ' and the wing portions 34, 34 ' may be sewn with the hem portion 42, in the present invention, the thickness of the molded 3D three-dimensional fabric substrate 36 is gradually thinner from the peak areas 321, 321 ' (shown in fig. 2) to the outer edges of the peripheral areas 322, 322 ' (shown in fig. 2), and the design of the thinner outer edge of the cups 32, 32 ' may facilitate the selvage sewing of the hem portion 42. As shown in fig. 4, steel rings 44, 44 'may be further disposed on the inner lower edges of the cups 32, 32' to increase the supporting effect; in one embodiment, the undergarment 30 also includes two shoulder straps 46, 46 ', one end of each shoulder strap 46, 46' being connected to the apex or a point slightly proximal to the apex of the upper edge of one of the cups 32, 32 ', and the other end of the shoulder strap 46, 46' being connected to the upper edge of the wing 34, 34 'from which the cup 32, 32' extends.
Fig. 5 is a schematic view of a 3D three-dimensional fabric substrate used in an underwear structure according to another embodiment of the present invention, wherein before being molded, an outer cover layer 48 can be further attached to at least one outer surface of the 3D three-dimensional fabric substrate 36, the outer cover layer 48 can be different from the 3D three-dimensional fabric substrate 36 and has a knitted fabric structure or a flat fabric structure, and the outer cover layer 48 can be made of wool cloth, nylon cloth, rayon cloth, polyester cloth, or cotton cloth; when the underwear structure 30 is manufactured, the 3D three-dimensional fabric substrate 36 and the attached outer cover 48 are placed between the male mold and the female mold of the mold, and are relatively pressed and molded by the male mold and the female mold. The design of the undergarment structure 30 with the outer cover 48 can provide different visual effects by selecting the material or design of the outer cover 48, so that the undergarment structure 30 has the suitability for wearing or exposing.
In the invention, the underwear structure manufactured by using a single piece of cloth (3D three-dimensional fabric base material) only uses a single piece of cloth, so that the manufacturing process is not complicated, the production and material cost is low, the complexity of the traditional underwear formed by splicing and sewing multiple pieces of cloth is further reduced by the design of integral compression molding, and the defect of insufficient attractiveness of the traditional underwear caused by multiple seams is improved. Meanwhile, the single piece of cloth is integrally molded and has the advantage of saving the manufacturing time and reducing the manufacturing cost. On the other hand, the underwear structure is integrally molded by using a single seamless 3D three-dimensional fabric base material, has the ventilation, light and thin and burden-free comfort of the 3D three-dimensional fabric base material, can be attached to the chest of a human body due to no splicing and no seam, and has better covering property. Besides the manufacturing process is not complex, the underwear structure formed by integrally pressing and molding the outer coating layer is attached to the 3D three-dimensional fabric base material, and different visual effects can be presented on the underwear through the selection of the material or the pattern of the outer coating layer, so that the underwear structure has the suitability of being worn or exposed externally and has a popular effect.
The above-mentioned embodiments are merely illustrative of the technical spirit and features of the present invention, and the object of the present invention is to enable those skilled in the art to understand the content of the present invention and to implement the same, and the scope of the present invention should not be limited by the above-mentioned embodiments, i.e. all equivalent changes and modifications made in the spirit of the present invention should be covered in the scope of the present invention.
Claims (18)
1. An undergarment structure characterized by comprising:
two cups, each cup is connected with each other and is provided with a cupular peak area and a peripheral area, the cupular peak area is positioned at the central part of the cup and the peripheral area surrounds the cupular peak area; and
two wing parts respectively extending from the outer edges of the peripheral areas of the two cups, wherein one ends of the two wing parts respectively far away from the cups can be connected together, and the two cups and the two wing parts are simultaneously molded by a single piece of seamless 3D three-dimensional fabric base material in an integral compression molding mode;
the thickness of the molded 3D three-dimensional fabric substrate in the cup peak area is larger than the thickness of the peripheral area and the wing area.
2. The undergarment structure of claim 1, wherein: wherein the thickness of the molded 3D three-dimensional fabric substrate is gradually thinner from the cup peak area to the outer edge of the peripheral area.
3. The undergarment structure of claim 1, wherein: wherein the thickness of the molded 3D three-dimensional fabric substrate in the peripheral area is less than or equal to that of the wing part.
4. The undergarment structure of claim 1, wherein: wherein the thickness of the molded 3D three-dimensional fabric substrate on the wing part is gradually thinner from one end of the wing part close to the bra cup to one end far away from the bra cup.
5. The undergarment structure of claim 1, wherein: wherein the peak area is located at the center of the cup and accounts for 30-50% of the area of the cup.
6. The undergarment structure of claim 1, wherein: wherein the thickness of the 3D three-dimensional fabric substrate in the cup peak area is between 2 mm and 10 mm, and the thickness of the peripheral area and the wing area is between 0.1 mm and 5 mm.
7. The undergarment structure of claim 1, wherein: wherein the two cups are connected by a central part, and the two cups, the central part and the extended two wing parts are simultaneously molded integrally by a single piece of seamless 3D three-dimensional fabric base material.
8. The undergarment structure of claim 1, wherein: wherein the 3D three-dimensional fabric base material is sandwich cloth (Spacer Fabrics or woven Fabrics) or space cotton cloth.
9. The undergarment structure of claim 1, wherein: the 3D three-dimensional fabric base material comprises an upper fabric layer, a lower fabric layer and a middle fabric layer, wherein the middle fabric layer is arranged between the upper fabric layer and the lower fabric layer and is composed of a plurality of corrugated yarns, the wave crests of the corrugated yarns are connected with the upper fabric layer, and the wave troughs of the corrugated yarns are connected with the lower fabric layer.
10. The undergarment structure of claim 9, wherein: wherein the corrugated yarns of the middle fabric layer are formed of monofilament fibers.
11. The undergarment structure of claim 9, wherein: wherein the upper fabric layer and/or the lower fabric layer are woven by using the shrinkable covering yarn.
12. The undergarment structure of claim 9, wherein: wherein the upper fabric layer and/or the lower fabric layer is woven by one or the combination of elastic fiber yarn, nylon yarn, cotton yarn and rayon yarn.
13. The undergarment structure of claim 1, wherein: further comprises an outer covering layer which is attached to an outer surface of the 3D three-dimensional fabric base material, so that the two cups which are connected with the 3D three-dimensional fabric base material and the outer covering layer in an integrated compression molding mode and the two extending wing parts are formed.
14. The undergarment structure of claim 13 wherein: wherein the outer cover layer is a knitted fabric, a plain woven fabric, a wool fabric, a nylon fabric, a rayon fabric, a polyester fabric or a cotton fabric.
15. The undergarment structure of claim 1, wherein: wherein at least one surface of the 3D three-dimensional fabric substrate is formed with one or a combination of twitch, embossing and printing.
16. The undergarment structure of claim 1, wherein: wherein the peripheries of part of the cups and the wing parts are sewed with edge rolling parts, and the lower edge of the inner side of the cup is provided with a steel ring.
17. The undergarment structure of claim 1, wherein: further comprises two shoulder straps, one end of each shoulder strap is connected with the upper edge of one cup, and the other end of each shoulder strap is connected with the upper edge of the wing part extended by the cup.
18. The undergarment structure of claim 1, wherein: wherein, one end of each wing part far away from the bra cup is connected with each other by a buckling structure, a felt structure or an elastic band.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW105137132A TWI623276B (en) | 2016-11-14 | 2016-11-14 | Brassiere |
| TW105137132 | 2016-11-14 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108065460A CN108065460A (en) | 2018-05-25 |
| CN108065460B true CN108065460B (en) | 2020-07-28 |
Family
ID=62106257
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611051153.4A Active CN108065460B (en) | 2016-11-14 | 2016-11-25 | Underwear structure |
Country Status (3)
| Country | Link |
|---|---|
| US (2) | US20180132540A1 (en) |
| CN (1) | CN108065460B (en) |
| TW (1) | TWI623276B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TW202001021A (en) * | 2018-06-29 | 2020-01-01 | 黛莉股份有限公司 | Integral spacer fabrics provided with adaptive thickness and method of fabricating the same |
| US20230346050A1 (en) * | 2022-04-28 | 2023-11-02 | Tamika MAYES | Support garments |
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| US20090233523A1 (en) * | 2008-03-17 | 2009-09-17 | Maria Pardo | Dimensional foam brassiere |
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| US9565877B2 (en) * | 2013-10-18 | 2017-02-14 | Mast Industries (Far East) Limited | Garment that clings to a wearer's skin and method of manufacture thereof |
| CN105815827A (en) * | 2015-01-06 | 2016-08-03 | 维珍妮国际(集团)有限公司 | Supporting parts used for bra |
| CN105433452A (en) * | 2016-01-12 | 2016-03-30 | 邓一博 | Bra cup |
-
2016
- 2016-11-14 TW TW105137132A patent/TWI623276B/en active
- 2016-11-25 CN CN201611051153.4A patent/CN108065460B/en active Active
- 2016-11-25 US US15/361,230 patent/US20180132540A1/en not_active Abandoned
-
2020
- 2020-04-13 US US16/846,712 patent/US20200237025A1/en not_active Abandoned
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI316848B (en) * | 2005-10-07 | 2009-11-11 | ||
| CN101156715A (en) * | 2007-11-21 | 2008-04-09 | 刘亚明 | Single piece type seamless bra and its preparation method |
| CN201403504Y (en) * | 2009-02-24 | 2010-02-17 | 康孝钲 | Sandwich cup structure |
| CN205044252U (en) * | 2015-09-06 | 2016-02-24 | 孙卫民 | Construction improvement's 3D fabric |
| CN206324237U (en) * | 2016-11-14 | 2017-07-14 | 黛莉股份有限公司 | Underwear structure |
Also Published As
| Publication number | Publication date |
|---|---|
| US20180132540A1 (en) | 2018-05-17 |
| TW201817327A (en) | 2018-05-16 |
| TWI623276B (en) | 2018-05-11 |
| US20200237025A1 (en) | 2020-07-30 |
| CN108065460A (en) | 2018-05-25 |
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