CN106213597A - High recovery bra flank and application thereof - Google Patents
High recovery bra flank and application thereof Download PDFInfo
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- CN106213597A CN106213597A CN201610749631.2A CN201610749631A CN106213597A CN 106213597 A CN106213597 A CN 106213597A CN 201610749631 A CN201610749631 A CN 201610749631A CN 106213597 A CN106213597 A CN 106213597A
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- Prior art keywords
- flank
- bra
- high recovery
- layer
- laminating
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- 238000011084 recovery Methods 0.000 title claims abstract description 48
- 239000010410 layer Substances 0.000 claims abstract description 37
- 239000002344 surface layer Substances 0.000 claims abstract description 31
- 239000004744 fabric Substances 0.000 claims abstract description 24
- 239000000835 fiber Substances 0.000 claims abstract description 9
- 229920002334 Spandex Polymers 0.000 claims abstract description 8
- 239000004759 spandex Substances 0.000 claims abstract description 8
- 238000009941 weaving Methods 0.000 claims abstract description 6
- 238000010030 laminating Methods 0.000 claims description 44
- 239000012790 adhesive layer Substances 0.000 claims description 28
- 239000000463 material Substances 0.000 claims description 19
- 239000004433 Thermoplastic polyurethane Substances 0.000 claims description 15
- 229920002803 thermoplastic polyurethane Polymers 0.000 claims description 15
- 239000012528 membrane Substances 0.000 claims description 9
- 239000000693 micelle Substances 0.000 claims description 9
- 239000011230 binding agent Substances 0.000 claims description 3
- 239000003292 glue Substances 0.000 claims description 3
- 238000005507 spraying Methods 0.000 claims description 3
- 229920002635 polyurethane Polymers 0.000 claims description 2
- 239000004814 polyurethane Substances 0.000 claims description 2
- 238000004080 punching Methods 0.000 claims description 2
- 229920001169 thermoplastic Polymers 0.000 claims description 2
- 239000004416 thermosoftening plastic Substances 0.000 claims description 2
- 238000009958 sewing Methods 0.000 description 11
- 238000010586 diagram Methods 0.000 description 8
- 238000000034 method Methods 0.000 description 6
- 230000000052 comparative effect Effects 0.000 description 4
- 238000012360 testing method Methods 0.000 description 4
- 210000003141 lower extremity Anatomy 0.000 description 3
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 2
- 238000009833 condensation Methods 0.000 description 2
- 230000005494 condensation Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000009940 knitting Methods 0.000 description 2
- YIWGJFPJRAEKMK-UHFFFAOYSA-N 1-(2H-benzotriazol-5-yl)-3-methyl-8-[2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidine-5-carbonyl]-1,3,8-triazaspiro[4.5]decane-2,4-dione Chemical compound CN1C(=O)N(c2ccc3n[nH]nc3c2)C2(CCN(CC2)C(=O)c2cnc(NCc3cccc(OC(F)(F)F)c3)nc2)C1=O YIWGJFPJRAEKMK-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 210000000481 breast Anatomy 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000011229 interlayer Substances 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000002040 relaxant effect Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229920002994 synthetic fiber Polymers 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
Classifications
-
- A—HUMAN NECESSITIES
- A41—WEARING APPAREL
- A41C—CORSETS; BRASSIERES
- A41C3/00—Brassieres
- A41C3/12—Component parts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered 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
- B32B3/26—Layered 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
- B32B3/266—Layered 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/06—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/10—Methods 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/12—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered 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
- B32B5/02—Layered 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered 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
- B32B5/02—Layered 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
- B32B5/028—Net structure, e.g. spaced apart filaments bonded at the crossing points
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0292—Polyurethane fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2437/00—Clothing
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Details Of Garments (AREA)
Abstract
The invention discloses a kind of high recovery bra flank, it comprises flank surface layer and flank nexine, also comprises flank intermediate layer, and described flank intermediate layer is selected by the Fabric of 100% spandex fibre weaving.Height recovery bra flank smooth in appearance of the present invention is attractive in appearance, and after dress, its elastic recovery rate is high.The invention also discloses the bra comprising this high recovery bra flank.
Description
Technical field
The present invention relates to a kind of bra flank.More particularly, to a kind of high recovery bra flank and application thereof.
Background technology
Existing bra flank is made up of flank surface layer and flank nexine, mostly is by sewing flank and bonding flank, this
Two kinds of bra flanks suffer from the drawback that
Sewing flank: as shown in figs. 1 a to 1 c, sewing side flap elastic stress is mainly by flank surface layer 1` and flank nexine 2`
Marginal portion elastic 3` provide, easily there is the situation that human body stress is uneven during sewing, thus the bra flank obtained
Have impression to produce；It addition, there is a plurality of sewing thread trace 4` in the bra flank surfaces that obtains of sewing, attractive in appearance to a certain extent
Can be affected, it is impossible to fully meet consumer's demand for bra flank smooth and beautiful appearance.
Tradition laminating flank: as seen in figs. 2a-2c, by flank surface layer 1`` and flank nexine 2`` by adhesive layer 4`` heat
Plastotype elastic polyurethane glued membrane is fitted, but usually high-elastic, the flank surface layer 1`` of bra flank and flank nexine face 2`` material
Material, adhesive layer 4`` thermoplastic polyurethane elastic glued membrane elasticity is the highest, but after hot-working laminating, due to its elastic construction phase
Mutually impact is destroyed, and side flap elastic recovery rate is relatively low, and after wear a few hours, flank can become slack, impact dress and relaxing
After flank be difficult to recover to raw footage.For solving this problem, the bra flank that existing laminating obtains is worn in normal at bra
Must be the shortest and relatively tight during size, solve the elongated and problem that fluffs with this, the method sacrifices part and wears characteristic, not
Tackle the problem at its root.
The bra product of tradition attaching process is when moment stretching (tensile force 50N) wears length, and after dress, response rate is only
Below 70%.After Chang Shijian, its moment, stretching was when wearing length, tensile force can quickly decrease up to product and not possess elasticity be
Only, period, its elastic recovery rate is the most quickly reducing, most can be below 50%, this kind of situation can reduce product service life.
Experience dress test display through the personnel of trying on, if bra flank response rate is below 85%, wear experience sense poor and obvious
Feel uncomfortable.
Spandex fibre material has high resiliency, can bear bigger power, and have deep drawing quality and recovery, but ammonia
The skin-friendly of synthetic fibre fiber is poor, and patch skin sense of touch is bad, thus existing dress ornament class be all by the spandex fibre of certain content and its
Its pro-skin fabric carries out blending and forms fabric, thus improves the problem that fabric is elastic and skin-friendly is compatible to a certain extent.
But the method can only be improved to a certain extent, it is not appropriate for aeroelastic requirements and skin-friendly are being required in higher product.
Accordingly, it is desirable to provide the bra that a kind of smooth in appearance is seamless attractive in appearance and after dress, elastic recovery rate is high and skin-friendly is good
Flank.
Summary of the invention
First purpose of the present invention is to provide a kind of high recovery bra flank, this bra flank smooth in appearance without
After trace, attractive in appearance, ventilative and dress, its elastic recovery rate is high, and skin-friendly is good.
Second object of the present invention is to provide a kind of bra comprising above-mentioned high recovery bra flank.
For reaching above-mentioned first purpose, the present invention uses following technical proposals:
High recovery bra flank, comprises flank surface layer and flank nexine, also comprises flank intermediate layer, in the middle of described flank
Layer is selected by the Fabric of 100% spandex fibre weaving.
Further, described flank surface layer, flank intermediate layer and flank nexine are fitted the most successively.
Further, described bra flank also comprises adhesive layer；Preferably, described flank surface layer passes through with flank intermediate layer
Adhesive layer is comprehensively or fits in local；Preferably, described flank nexine is fitted by adhesive layer with flank intermediate layer comprehensively or locally.
Further, the shape of described adhesive layer can select according to concrete bonding mode, can be by flank surface layer, flank
Laminating shape that intermediate layer and flank nexine fit tightly and laminating position.Such as, the bond area of adhesive layer can be with side
Aerofoil layer size is identical, it is achieved fit comprehensively；Described adhesive layer is alternatively the bar similar to flank surface layer upper and lower part shape
Shape, only makes top edge combine closely with lower limb, it is achieved local laminating, etc..
Further, described laminating uses thermal bonding technology laminating, and bonding temperature is 80 DEG C～200 DEG C.
Further, the mode of described laminating for select concora crush make-up machine, roll make-up machine, thermoplasticity micelle make-up machine or
Glue spraying bonder is fitted.
Preferably, depending on the selection of the material of the selection gist adhesive layer of described laminating type.Heretofore described bonding
The material of layer is in thermoplastic polyurethane elastic glued membrane, thermoplastic polyurethane elastic micelle, thermoplastic polyurethane binding agent
A kind of.
When the material of described adhesive layer is selected from thermoplastic polyurethane elasticity glued membrane, the mode of described laminating is for selecting concora crush
Make-up machine or roll make-up machine laminating, wherein, the laminating parameter of concora crush make-up machine is: temperature 150～190 DEG C, pressure: 2～
4kg, the time: 50～90s；Preferably, in some embodiments, the can parameter of concora crush make-up machine is: temperature: 160
～180 DEG C, pressure: 2～4kg, the time: 60～80s.
The laminating parameter of described roll make-up machine is: temperature: 155～195 DEG C, pressure: 2.5～4.5kg, rotating speed: 200～
500RPM；Preferably, in some embodiments, the laminating parameter of roll make-up machine is: temperature: 165～185 DEG C, pressure
Power: 3～4.5kg, rotating speed: 250～450RPM.
When the material of described adhesive layer is selected from thermoplastic polyurethane elastic micelle, the mode of described laminating is for selecting thermoplastic
Property micelle make-up machine laminating.Laminating parameter is: temperature: 100～160 DEG C, pressure: 2～8kg, time: 20～100s；Preferably,
In some embodiments, the laminating parameter of thermoplasticity micelle make-up machine is: temperature: 120～150 DEG C, pressure: 4～
8kg, the time: 40～90s.
When the material of described adhesive layer is thermoplastic polyurethane binding agent, glue spraying bonder or concora crush make-up machine is used to enter
Row bonding.Wherein, the laminate pressure of concora crush make-up machine is 2～8kg.
Further, the mesh fabric that outward appearance is screen cloth or punching of the Fabric in described flank intermediate layer, it is preferable that
When the most non-stretched, the area of mesh is 0.000001～0.01cm2。
Further, one or more during the shape of described mesh comprises circle, rhombus, rectangle.
Further, described flank nexine is patch skin layers.
In the present invention, described flank surface layer, flank intermediate layer are corresponding with the shape of flank nexine, by attaching process,
Thus obtain bra flank.
Wherein, the bra flank surface layer in the present invention and the cloth being chosen as patch skin of flank interior layer material, such as, flank
Surface material can be the conventional knitting fabric of underskirt, lace etc.；Flank interior layer material can be conventional underskirt silk sense underwear
Fabric, the anti-skidding fabric of sanding, preserving moisture and protecting skin fabric etc..
The shape invention technician of the bra flank of the present invention can be designed according to the actual requirements, such as, comprises
Conventional bra flank shape.
The present invention also protects the bra including above-mentioned high recovery bra flank.
Such as, described bra can be, the high recovery bra flank obtained is used existing technique and bra cup, the back of the body
Button, steel ring position etc. are spliced, thus form the bra containing high recovery bra flank.
If no special instructions, the raw material used in the present invention all can be commercially available or by this area routine hands by commercially available
Section obtains.
If no special instructions, any scope described in the present invention include any numerical value between end value and end value and
The anyon scope that any number between end value or end value is constituted.
Beneficial effects of the present invention is as follows:
The high recovery bra flank of the present invention comprise flank surface layer, flank nexine and by 100% spandex fibre weaving and
The Fabric flank intermediate layer become, creative adding between flank surface layer and nexine is formed by 100% spandex fibre weaving
Fabric as intermediate layer, efficiently solve that bra side flap elastic response rate is limited and skin-friendly experiences the problems such as difference,
Meet demand attractive in appearance and comfortable and easy to wear.
The height recovery each interlayer of bra flank of the present invention uses the mode of laminating to form bra flank, overcomes sewing and obtains
Bra flank have sewing stitching, rough, affect problem attractive in appearance.
Accompanying drawing explanation
Below in conjunction with the accompanying drawings the detailed description of the invention of the present invention is described in further detail.
Figure 1A illustrates the flank surface layer tiling schematic diagram of existing sewing bra flank.
Figure 1B illustrates the flank nexine tiling schematic diagram of existing sewing bra flank.
Fig. 1 C illustrates the generalized section of existing sewing bra flank.
Fig. 2 A illustrates the flank surface layer tiling schematic diagram of existing laminating bra flank.
Fig. 2 B illustrates the flank nexine tiling schematic diagram of existing laminating bra flank.
Fig. 2 C illustrates the generalized section of existing laminating bra flank.
Fig. 3 illustrates the flank surface layer tiling schematic diagram of height recovery bra flank of the present invention.
Fig. 4 illustrates the flank nexine tiling schematic diagram of height recovery bra flank of the present invention.
Fig. 5 illustrates the schematic shapes of the adhesive layer of the embodiment of the present invention 1 high recovery bra flank.
Fig. 6 illustrates the flank intermediate layer close-up schematic view of height recovery bra flank of the present invention.
Fig. 7 illustrates the generalized section of height recovery bra flank of the present invention.
Fig. 8 illustrates the schematic shapes of the adhesive layer of the local laminating of the embodiment of the present invention 3 high recovery bra flank.
Detailed description of the invention
In order to be illustrated more clearly that the present invention, below in conjunction with preferred embodiments and drawings, the present invention is done further
Bright.Parts similar in accompanying drawing are indicated with identical reference.It will be appreciated by those skilled in the art that institute is concrete below
The content described is illustrative and be not restrictive, and should not limit the scope of the invention with this.
Embodiment 1
A kind of high recovery bra flank, including: flank surface layer 1；Flank nexine 2；And flank intermediate layer 3, described side
Wing intermediate layer 3 is selected by the high-elastic screen cloth of 100% spandex fibre weaving.
Described flank surface layer 1, flank intermediate layer 3 and flank nexine 2 are fitted the most successively.
Described bra flank also comprises adhesive layer 4；Wherein, described flank surface layer 1 and flank intermediate layer 3 are by adhesive layer 4
Laminating comprehensively；Described flank nexine 2 is fitted by adhesive layer 4 with flank intermediate layer 3 comprehensively.
The tiling schematic diagram of described flank surface layer 1 and flank nexine 2 is the most as shown in Figure 3 and Figure 4.Both sizes are identical right
Should, the shape in flank intermediate layer 3 is also identical with surface layer and nexine simultaneously.
The knitting fabric of underskirt that the fabric of described flank surface layer 1 is conventional；The fabric of described flank nexine 2 is conventional
Underskirt silk sense underwear fabric.
Wherein, the method for described laminating is: on concora crush make-up machine, and tile flank nexine 2, the biggest on its surface
Little paving jointing material thermoplastic polyurethane elastic glued membrane is as adhesive layer, and adhesive layer form schematic diagram is as it is shown in figure 5, again on surface
Paving flank intermediate layer 3, wherein, as shown in Figure 6, containing diamond-shaped meshes, mesh area is the close-up schematic view in flank intermediate layer 3
0.000004m2, then carrying out concora crush laminating, laminating parameter is: temperature: 150 DEG C, pressure: 4kg, time: 85s.Complete flank
Nexine 2 and the laminating in flank intermediate layer 3.
The most as stated above, the another side in flank intermediate layer 3 is fitted with flank surface layer 1, obtain high recovery bra side
The wing.The generalized section of gained height recovery bra flank is as shown in Figure 7.
Embodiment 2
Repeating embodiment 1, difference is, laminating parameter changes into: temperature: 180 DEG C, pressure: 2kg, time: 65s.Remaining
Part is constant, obtains high recovery bra flank.
Embodiment 3
Repeating embodiment 1, difference is, described flank nexine 2 and flank intermediate layer 3 are by the laminating of adhesive layer 4 local.Viscous
Condensation material thermoplastic polyurethane elastic glued membrane only exists and nexine top edge and lower limb position, wherein, top edge adhesive layer, under
Edge adhesive layer form is respectively as shown in Fig. 85,6.Remaining condition is constant, obtains high recovery bra flank.
Embodiment 4
Repeating embodiment 1, difference is, described flank surface layer 1 and flank intermediate layer 3 are by the laminating of adhesive layer 4 local.Viscous
Condensation material thermoplastic polyurethane elastic glued membrane only exists and nexine top edge and lower limb position.Remaining condition is constant, obtains height
Recovery bra flank.
Embodiment 5
Repeating embodiment 1, difference is, described mesh is circular, and area is 0.000003cm2；Use roll make-up machine
Fitting, laminating parameter is: temperature: 165 DEG C, pressure: 4kg, rotating speed: 350RPM.Remaining condition is constant, obtains high recovery
Bra flank.
Embodiment 6
Repeating embodiment 5, difference is, laminating parameter is changed into: temperature: 175 DEG C, pressure: 3.5kg, rotating speed:
400RPM.Remaining condition is constant, obtains high recovery bra flank.
Embodiment 7
Repeating embodiment 1, difference is, adhesive layer 4 material changes into thermoplastic polyurethane elastic micelle, uses thermoplasticity
Micelle make-up machine is fitted.Laminating parameter is: temperature: 120 DEG C, pressure: 6kg, time: 80s.Remaining condition is constant, obtains
High recovery bra flank.
Embodiment 8
Repeating embodiment 7, difference is, laminating parameter is changed into: temperature: 145 DEG C, pressure: 5kg, time: 60s.Remaining
Condition is constant, obtains high recovery bra flank.
Embodiment 9
Repeating embodiment 1, difference is, adhesive layer 4 material changes into thermoplastic polyurethane adhesive, uses concora crush laminating
Machine is fitted.Laminating parameter is: pressure: 6kg.Remaining condition is constant, obtains high recovery bra flank.
Embodiment 10
Repeating embodiment 9, difference is, laminating parameter is: pressure: 4kg.Remaining condition is constant, obtains high recovery literary composition
Breast flank.
Comparative example 1
A kind of bra flank, is made up of flank surface layer and flank nexine, and wherein, flank surface layer and flank nexine are by bonding
Material thermoplastic polyurethane elastic glued membrane uses the laminating of concora crush make-up machine to form, laminating parameter and flank surface layer and flank nexine face
Material is all with embodiment 1.
Bra flank above-described embodiment and comparative example obtained carries out elasticity and elastic recovery rate test
Method of testing is:
1. the flank made according to above example and comparative example is intercepted mid portion, length 10cm；
2. using CRE tensile strength test instrunment to be fixed at two ends, fixture takes 10cm*5cm；
3. flank being at the uniform velocity stretched to 15cm and takes now tensile strength A, draw speed is 300mm/min, and now strength is surveyed
Examination instrument is static, flank persistently keeps extended state 8 hours；
4. measure length after taking off flank and calculate response rate B.
Test result is as shown in table 1 below:
Table 1 bra flank response rate result
| Embodiment is numbered | Tensile strength A (N) | Response rate B |
| Embodiment 1 | 4.3 | 91% |
| Embodiment 2 | 4.5 | 93% |
| Embodiment 3 | 4.5 | 94% |
| Embodiment 4 | 4.2 | 97% |
| Embodiment 5 | 4.0 | 95% |
| Embodiment 6 | 3.8 | 95% |
| Embodiment 7 | 3.6 | 94% |
| Embodiment 8 | 3.8 | 96% |
| Embodiment 9 | 3.7 | 96% |
| Embodiment 10 | 3.9 | 95% |
| Comparative example 1 | 9 | 60% |
Obviously, the above embodiment of the present invention is only for clearly demonstrating example of the present invention, and is not right
The restriction of embodiments of the present invention, for those of ordinary skill in the field, the most also may be used
To make other changes in different forms, cannot all of embodiment be given exhaustive here, every belong to this
What bright technical scheme was extended out obviously changes or changes the row still in protection scope of the present invention.
Claims (9)
- The highest recovery bra flank, comprises flank surface layer and flank nexine, it is characterised in that: also comprise flank intermediate layer, institute State flank intermediate layer to select by the Fabric of 100% spandex fibre weaving.
- High recovery bra flank the most according to claim 1, it is characterised in that described flank surface layer, flank intermediate layer Fit the most successively with flank nexine.
- High recovery bra flank the most according to claim 1, it is characterised in that described bra flank also comprises bonding Layer；Preferably, described flank surface layer is fitted by adhesive layer with flank intermediate layer comprehensively or locally；Preferably, in described flank Layer and flank intermediate layer are by adhesive layer comprehensively or local laminating.
- High recovery bra flank the most according to claim 1, it is characterised in that the material of described adhesive layer is selected from thermoplastic One in property elastic polyurethane glued membrane, thermoplastic polyurethane elastic micelle, thermoplastic polyurethane binding agent.
- 5. according to the high recovery bra flank described in Claims 2 or 3, it is characterised in that described laminating uses heat bonding work Skill is fitted, and bonding temperature is 80 DEG C～200 DEG C.
- High recovery bra flank the most according to claim 5, it is characterised in that the mode of described laminating is for selecting concora crush Make-up machine, roll make-up machine, thermoplasticity micelle make-up machine or glue spraying bonder are fitted.
- High recovery bra flank the most according to claim 1, it is characterised in that the outward appearance of described Fabric is screen cloth Or the mesh fabric of punching；Preferably, when the most non-stretched, the area of mesh is 0.000001～0.01cm2。
- High recovery bra flank the most according to claim 7, it is characterised in that the shape of described mesh comprise circle, One or more in rhombus, rectangle.
- 9. a bra, it is characterised in that comprise high recovery bra flank as claimed in claim 1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610749631.2A CN106213597A (en) | 2016-08-29 | 2016-08-29 | High recovery bra flank and application thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610749631.2A CN106213597A (en) | 2016-08-29 | 2016-08-29 | High recovery bra flank and application thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106213597A true CN106213597A (en) | 2016-12-14 |
Family
ID=57555754
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610749631.2A Pending CN106213597A (en) | 2016-08-29 | 2016-08-29 | High recovery bra flank and application thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106213597A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107173893A (en) * | 2017-06-05 | 2017-09-19 | 昆山腾飞内衣科技股份有限公司 | The dress ornament and its manufacture method dressed suitable for different building shape crowd |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20080016296A (en) * | 2006-08-18 | 2008-02-21 | 임성식 | Brassiere a wing structure |
| CN201967655U (en) * | 2010-09-02 | 2011-09-14 | 胡煦芸 | Novel side wing bra |
| CN102406247A (en) * | 2011-12-01 | 2012-04-11 | 普宁市仙宜岱时装有限公司 | Waterproof stable prosthesis bra |
| CN105407752A (en) * | 2012-12-28 | 2016-03-16 | 英威达技术有限公司 | Garments including elastic composite fabric |
| CN206137242U (en) * | 2016-08-29 | 2017-05-03 | 深圳汇洁集团股份有限公司 | High resilience brassiere flank |
-
2016
- 2016-08-29 CN CN201610749631.2A patent/CN106213597A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20080016296A (en) * | 2006-08-18 | 2008-02-21 | 임성식 | Brassiere a wing structure |
| CN201967655U (en) * | 2010-09-02 | 2011-09-14 | 胡煦芸 | Novel side wing bra |
| CN102406247A (en) * | 2011-12-01 | 2012-04-11 | 普宁市仙宜岱时装有限公司 | Waterproof stable prosthesis bra |
| CN105407752A (en) * | 2012-12-28 | 2016-03-16 | 英威达技术有限公司 | Garments including elastic composite fabric |
| CN206137242U (en) * | 2016-08-29 | 2017-05-03 | 深圳汇洁集团股份有限公司 | High resilience brassiere flank |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107173893A (en) * | 2017-06-05 | 2017-09-19 | 昆山腾飞内衣科技股份有限公司 | The dress ornament and its manufacture method dressed suitable for different building shape crowd |
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