CN108463131A

CN108463131A - Brassiere

Info

Publication number: CN108463131A
Application number: CN201780006792.5A
Authority: CN
Inventors: 矢田和也; 小原和幸
Original assignee: Asahi Kasei Kogyo KK
Current assignee: Asahi Kasei Corp
Priority date: 2016-01-21
Filing date: 2017-01-20
Publication date: 2018-08-28
Anticipated expiration: 2037-01-20
Also published as: WO2017126684A1; CN108463131B

Abstract

The present invention provides a kind of i.e. damping excellent brassiere of effect that breast when mitigating movement shakes.A kind of brassiere (100), has：A pair of of cup parts (102)；Linking part (101), the preceding central side of the cup parts (102) is interconnected together；Alar part (103), it is adjacent with the oxter side of the cup parts (102)；And shoulder belt portion (110), its end is connected with a pair of cup parts (102) and the alar part (103), wherein, into exercise the linking part (101) transversely repeatedly stretching, extension 10% extension experiment, stretching, extension stress of the linking part (101) when third time stretches is 10N~30N, moreover, the brassiere has the more than one vibration damping portion chosen from comprising the structure group with lower structure, i.e.,：Upper limb high stress portion (104), lower edge high stress portion (105), shoulder belt portion (110) and aileron portion (109).

Description

Brassiere

Technical field

The present invention relates to a kind of brassiere, the shaking of breast when which can inhibit to be acted under wearing state.More In detail, the present invention relates to a kind of following such brassieres：Taste will not be destroyed, has and inhibits to carry out under wearing state When action breast shake effect, that is, have it is damping, also, dress pressure it is moderate, have wearing comfort sense.

Background technology

One of main purpose of brassiere be udder shape is adjusted so as to it is more beautiful, however, inhibit movement when breast shaking It is also one of the larger effect of brassiere.But in most cases, even if having on brassiere, one when walking or running, and breast still can shake Relatively acutely.In particular, in the case where breast size is larger, above-mentioned this shaking can become that very acutely, wearer can be caused Do not feel well and can also cause to bear to wearer, moreover, also results in mastoptosis.It is above-mentioned this as that can mitigate The method of shaking, dressing has the method for the brassiere of stronger wearing pressure more effective, still, can cause to wear using this method Comfort is worn obviously to be deteriorated.Moreover, following this problems are more increasingly prominent：Especially during exercise, the shaking of breast can become Must be more violent, therefore, wearer can be interfered to act, cause to bear to wearer.When therefore, as being moved for mitigating The brassiere that breast shakes, develops many movement brassieres (patent document 1 and patent document 2).But with regard to movement brassiere and Speech, the shaking of breast, is following this designs mostly when in order to inhibit movement：Area coverage is made larger, can block breast Ditch.Therefore, it is short of on taste mostly, it is unwelcome as routine use.

Accordingly, it is considered to routine use aspect, it is generally desirable to, a kind of following such brassieres of exploitation：Make the larger journey of cleavage The exposure of degree ground, it is ensured that taste, in this state, the shaking of breast when mitigating daily carry out light exercise, and dress pressure It is more moderate.

A kind of brassiere has been recorded in patent document 3, has been had：A pair of of cup parts；Linking part, in before the cup parts Heart side is interconnected together；Alar part；And shoulder belt portion, end are connected with a pair of cup parts and the alar part, wherein should At least there is cup parts liner, the liner to have liner high stress portion, which extends along liner upper limb or edge The extension of liner lower edge, or extend along liner upper limb and liner both lower edge, the stretching, extension stress S2 in liner high stress portion with It is 2/1~80/1 that the mammary areola of liner, which corresponds to the ratio between the stretching, extension stress S1 in portion S2/S1,.

In technology described in patent document 3, in the whole region until from cup parts to a part for alar part, in brassiere master Aileron portion is configured on body.By the fabric cloth and silk system for configuring the tensile stress for utilizing tensile stress to be different from brassiere main body cloth and silk At aileron, can be poor using the tensile stress between brassiere main body cloth and silk and aileron cloth and silk in the state of dressing brassiere, make It obtains and plays a role from the power pulled towards alar part with the joint portion in aileron portion on cup parts, effectiveness in vibration suppression can be played.

For above-mentioned brassiere, using the effect realized by aileron portion, although cleavage is made largely to expose, energy The shaking of breast when enough inhibiting to be acted with not destroying comfort.But although just for the brassiere, under wearing state For rolling is dynamic and the subjective assessment of comfort, be to increase, and shaking value is also dropped compared with common brassiere Low, still, there is also following situations：Because of the difference of wearer, for comfort, someone produces a little sense of discomfort.

Existing technical literature

Patent document

Patent document 1：Japanese Unexamined Patent Publication 2005-23497 bulletins

Patent document 2：Japanese Unexamined Patent Publication 2011-179144 bulletins

Patent document 3：Japanese Unexamined Patent Publication 2014-163018 bulletins

Invention content

Problems to be solved by the invention

Thus, it is i.e. damping excellent that the problem to be solved in the present invention is to provide a kind of effect mitigating breast shaking when moving Brassiere, it is preferred that provide it is a kind of in addition to it is damping it is excellent other than taste and comfort also more excellent brassiere.

The solution to the problem

The present inventors using accelerometer measure and find：The suppression as the brassiere as shown in patent document 3 In the product of the shaking of breast entirety processed, actually there is also following situations：Breast is in cup to the subtle shaking of three-dimensional. From the point of view of acceleration, although the shaking that the product of the shaking of breast entirety can inhibit breast more violent can be inhibited, Because the acceleration that delicate variations generate has generation, breast always can be by rushing caused by acceleration in all directions It hits.Although the above, which is considered, can make the shaking of breast under wearing brassiere state restrain oneself but can cause to dress Person generates the reason of sense of discomfort.Accordingly, it is believed that for wearing comfort is further increased, need to alleviate the acceleration The generation of degree.

Also, it has been found that：Sometimes, because of the difference of wearer, wearer can be allowed to generate sense of discomfort to cup parts.Find ：In the case where aileron portion is arranged as vibration damping portion, it is especially using set on the aileron portion of cup parts and brassiere main body cloth and silk Tensile stress between alar part is poor so that the power pulled from the joint portion in aileron portion towards alar part plays a role to play vibration damping effect Fruit, so, to cup parts apply only brassiere main body cloth and silk the case where more than power, make sometimes breast generate sense of discomfort.Especially Be, in order to adjust udder shape and in the brassiere that the lower part of cup parts is equipped with metal wire for, sometimes, will produce and allow wearing Person feels that metal wire is caught in sense of discomfort as breast lower part.Accordingly, it is believed that for wearing comfort is further increased Property, it needs to reduce the sense of discomfort caused by metal wire is caught in skin.

To solve the above-mentioned problems, the present inventors has carried out deep research, and experiment has been repeated, as a result, it has been found that： A kind of brassiere with opening portion and specific vibration damping portion, the physical property by the linking part for making to link up cup parts are specified value, So as to acceleration when inhibition acts in the case where not improving wearing pressure.Further, it was found that a kind of have as vibration damping The brassiere in the aileron portion in portion is particular value by making the physical property in aileron portion, also, makes brassiere main body cloth and silk especially alar part cloth and silk The physical property of physical property and aileron portion cloth and silk be in specific ratios, so as to inhibit metal wire to be caught in breast lower part, further, it is possible to carry High damping, the characteristic for the acceleration that this is damping when also including inhibition action, until complete the present invention.That is, the present invention Content is as follows.

[1] a kind of brassiere, has：A pair of of cup parts；The preceding central side of the cup parts is interconnected by linking part Together；Alar part, it is adjacent with the oxter side of the cup parts；And shoulder belt portion, end and a pair of cup parts and the wing Portion is connected, wherein into the linking part is exercised, transversely the extension experiment of stretching, extension 10%, the linking part are stretched in third time repeatedly When stretching, extension stress be 10N~30N, moreover,

The brassiere is more than one with being chosen from the structure group comprising structure below (I)~structure (III) Vibration damping portion,

Structure (I) is any one of upper limb high stress portion and lower edge high stress portion or both, the upper limb high stress portion edge The cup upper limb for the cup parts extends, the ratio between the stretching, extension stress S1 of stretching, extension the stress S2 and cup central portion in upper limb high stress portion S2/S1 is 2/1~400/1, which extends along the cup lower edge of the cup parts, the stretching, extension in lower edge high stress portion The ratio between stress S3 and the stretching, extension stress S1 of cup central portion S3/S1 are 2/1~400/1,

Structure (II) is shoulder belt portion, averga cross section area 20mm²~120mm²,

Structure (III) is aileron portion, the whole region until the part a to part for the alar part from the cup parts In be configured in brassiere main body, using extended to from the mammary areola portion of correspondence of the cup parts alar part center back line segment as longest Mode configure brassiere, and provide the plane of the normal with direction identical with the extending direction of the line segment, in this case, It is on the line segment, corresponded to using the mammary areola portion as starting point go count 0%~25% and 50% towards the center back~ In the plane at 100% position, there are the joint portions between the aileron portion and the brassiere main body, moreover, the aileron portion has There is the region not engaged with the brassiere main body.

[2] according to the brassiere described in [1], wherein

The brassiere has the vibration damping portion in the vibration damping portion and the structure (II) of the structure (I).

[3] according to the brassiere described in [1], wherein

The brassiere has the vibration damping portion of the structure (III).

[4] according to the brassiere described in [3], wherein

The brassiere has the vibration damping portion of the structure (I).

[5] according to the brassiere described in [3], wherein

The brassiere has the vibration damping portion of the structure (II).

[6] according to the brassiere described in [4], wherein

The brassiere has the vibration damping portion of the structure (II).

[7] brassiere according to any one of [1]~[6], wherein

By the distance between the endpoint of the preceding central side by cup parts in shoulder belt portion be it is maximum in a manner of configure brassiere when, Link the midpoint for the line segment for linking up cup lowest point and by the endpoint of the preceding central side by cup parts in shoulder belt portion The line segment that the midpoint of the line segment come links up is line segment L3, and the line segment corresponding with the position of linking part on line segment L3 is The length of line segment L4, line segment L4 are 0.10~0.50 with the length ratio L4/L3 of line segment L3.

[8] according to the brassiere described in [1], wherein

Cross direction elongation E1 when the wearing in the aileron portion meets

× 100 (1) E1={ (1+E2/100) × (m2/m1) -1 }

100/YR1≤E1≤1000/YR1 (2),

When dressing brassiere, meet in the lateral stress σ 1 that the aileron portion generates

1≤1000cN/inch of 100cN/inch≤σ (3),

The ratio between the lateral Young's modulus YR1 in aileron portion and the lateral Young's modulus YR2 of alar part are

0.7≤YR1/YR2≤3 (4)。

(cross direction elongation of brassiere main body when wherein, E2 is wearing, m1 is the length in aileron portion, moreover, m2 is brassiere The length between joint portion in main body.)

[9] brassiere according to any one of [1]~[8], wherein

By the distance between the endpoint of the preceding central side by cup parts in shoulder belt portion be it is maximum in a manner of configure brassiere when, It links up the preceding center lower end point of the endpoint of the preceding central side by cup parts in shoulder belt portion and the linking part to form triangle, The ratio for not accounted for the area of the triangle by the area of the part of the member of formation of brassiere covering is 60% or more.

[10] brassiere according to any one of [1]~[9], wherein

Maximum wearing pressure is 50hPa or less.

The effect of invention

The brassiere of the present invention includes the linking part for having regulation physical property, and thereby, it is possible to reduce the acceleration generated in all directions Degree can reduce the sense of discomfort (shaking dynamic) when being acted.Moreover, by the way that above-mentioned linking part and specific vibration damping portion group are closed Come, even if upper and lower dynamic (dynamic along Y-direction), the left and right moving of breast when movement can be inhibited if in the case where cup sizes are larger The violent shaking of breast entirety as (moving in X direction) and front and back dynamic (being moved along Z-direction), also, breast can also be inhibited Subtle shaking in cup, is capable of providing the brassiere for feeling relatively comfortable.

Moreover, for the brassiere as the aileron portion in vibration damping portion, by making the physical property in aileron portion be in particular value, and And brassiere main body cloth and silk, particularly alar part and the physical property in aileron portion is made to be in specific ratios, metal wire can be inhibited to be caught under breast Portion, further, it is possible to improve damping, it includes also the acceleration for inhibiting to generate when being acted that this is damping, is capable of providing feeling More comfortable brassiere.

Description of the drawings

Fig. 1 is the schematic diagram of an example for indicating the brassiere construction of the present invention.

Fig. 2 is the schematic diagram of an example for indicating the brassiere construction of the present invention.

Fig. 3 is the schematic diagram of an example for indicating the brassiere construction of the present invention.

Fig. 4 is the schematic diagram of an example for indicating the brassiere construction of the present invention.

Fig. 5 is the schematic diagram of an example for indicating the brassiere construction of the present invention.

Fig. 6 is the schematic diagram of an example for indicating the brassiere construction of the present invention.

Specific implementation mode

In the following, explaining the example of the exemplary embodiment of the present invention in detail.

One embodiment of the present invention provides a kind of brassiere, has：A pair of of cup parts；Linking part, by the cup parts Preceding central side it is interconnected together；Alar part, it is adjacent with the oxter side of the cup parts；And shoulder belt portion, end Be connected with a pair of cup parts and the alar part, into exercise the linking part transversely repeatedly stretching, extension 10% extension experiment, the company Stretching, extension stress of the knot when third time stretches is 10N~30N, moreover, the brassiere has specific vibration damping portion.By making linking part It is existed simultaneously with specific vibration damping portion, effectiveness in vibration suppression more more obvious than the case where there is only linking parts can be obtained.

Referring to Fig.1, the brassiere 100 of one embodiment of the present invention has：A pair of of cup parts 102 (in attached drawing, a pair of of cup Cup parts in portion with enclosed with dashed lines come region indicate)；Linking part 101, by the preceding central side of the cup parts It is interconnected together；And alar part 103 (it is configured in the oxter side (i.e. the oxter side of wearer) of cup parts 102).Also may be used To be, linking part 101 is, for example, lower sideband, extends along the lower edge of cup parts 102, forms the lower end of brassiere.103 court of alar part Extend to the back side of wearer.Alar part 103 can have base portion and lower edge (such as band).Each component is made of cloth and silk.Text Also there is chest shoulder belt portion 110, end and the alar part 103 and a pair of of cup parts 102 in the shoulder belt portion 110 to be connected.

For the brassiere of the present invention, it is assumed that be：The breast of wearer is accommodated by cup.Further it is assumed that being：Linking part The preceding central side of the cup parts is interconnected together.Further it is assumed that being：Shoulder belt portion extends since chest, and point Not Rao Guo wearer left shoulder and right shoulder be connected later with alar part in the back side of wearer.

In the present invention, " wearer side " is intended to refer to the inboard (i.e. that side of the concave shape of cup) of brassiere, " outside " Intention refers to that side opposite with above-mentioned wearer side.

In the present invention, " transverse direction " (such as the transverse direction of linking part) referred to about brassiere is intended to refer to the row of two cups Column direction, specifically, when placing brassiere in such a way that the mammary areola corresponding position of two cups is furthest away from each other, general The extending direction for the straight line that two mammary areola corresponding positions link up.In the present invention, " longitudinal direction " of brassiere be intended to refer to it is upper Laterally vertical direction is stated, and corresponding with the upper and lower directions of wearer's body.

In the present invention, " mammary areola corresponding position " intention refers to the position corresponding with the mammary areola of wearer when dressing brassiere It sets (position i.e. corresponding with the nipple of wearer).Mammary areola corresponding position is the top of the projecting shape (convex form) of cup. In the present invention, " the preceding center line " of brassiere and " back of the body center line " is to pass through the line for linking up two mammary areola corresponding positions respectively The midpoint of section and the line being longitudinally extended along brassiere, preceding center line are the lines positioned at chest, and center back is positioned at alar part Line.

In the present invention, the perimeter of brassiere intention refers in brassiere main body, with from preceding centerline by back The shortest length for the line that the mode of centerline is drawn before being again returned to after at the heart (still, has length adjustment machine in brassiere In the case of structure (such as length adjustment mechanism 106 in aftermentioned Fig. 4), the perimeter of brassiere refers to utilizing length adjustment mechanism will Value when perimeter is adjusted to maximum).

In the present invention, linking part 101 is interconnected together by the preceding central side of cup parts, into the enforcement linking part 101 transversely repeatedly stretching, extension 10% extension experiment, the linking part 101 third time stretch when stretching, extension stress be 10N~ 30N.Moreover, for the brassiere of the present invention, by combining more than one specific vibration damping portion, energy on the basis of the linking part The delicate variations of breast, can reduce the load that body is applied to when being acted, moreover, can have when enough inhibition are acted There is higher comfort.

In general it is assumed that being：The breast of wearer is accommodated by cup.But in fact, in cup, the incomplete edge of breast Cup, breast is not fixed by cup.Accordingly, it is believed that in the case that breast shakes when being acted, breast can be caused Delicate variations occur in cup for room.For the delicate variations, shaken even if not perceiving breast from the appearance, but It is that the delicate variations are still occurred on the directions such as X-direction, Y-direction, Z-direction.When dressing brassiere, brassiere is transversely Stretching, extension, at this point, the extending transversely power for being stretched to starting point with alar part plays a role so that the fabric of cup linking part stretches.Cause This, it is believed that linking part leaves skin, and gap is generated between linking part and skin.It is believed that due to producing between this Gap produces in cup close front the area of cup and breast is not arranged as a result, that is, produces the area that may be escaped for breast Domain reduces so as to cause the crystallized ability of cup.Thus it is speculated that be that the phenomenon is resulted in when dressing brassiere, even if from outer It sees that not perceiving breast is acutely shaking in sight, but still wearer can be allowed to generate and shake dynamic and sense of discomfort.

Transversely stretch 10% extension experiment, stretching, extension of the linking part when third time stretches repeatedly into enforcement linking part Stress is 10N~30N, this is advantageous in terms of inhibiting breast shaking.Above-mentioned stretching, extension stress is preferably 15N~25N.When upper When to state stretching, extension stress be 10N or more, linking part becomes to be not easy to stretch, and linking part becomes fixed point, will not leave to linking part Breast can be fixed on before cup to the region of cup side, can inhibit the delicate variations of breast by skin.Moreover, When above-mentioned stretching, extension stress is 30N or less, it will not feel that fabric is excessively stiff when dressing brassiere, therefore, it is possible to not destroy Inhibit the shaking of breast under the premise of comfort.

Moreover, about extending transversely stress, specifically measuring makes each position in the horizontal direction (such as in aftermentioned Fig. 3 Straight line L1 extending direction) stretching, extension when stress.Unless otherwise specified, elongation of the invention and stretching, extension stress be all with Measured value on the basis of strip coating method tension test in JIS L1096.8.12.1 A methods.

In addition, for physics value mentioned in the present invention, unless otherwise specified, just either, pass through handle The end at each position (such as linking part) of brassiere is held to measure, can also be, first cuts out piece of cloth silks from each position again The cloth and silk is measured, it is intended that refer to regarding the physics value measured by any means in the above method as the present invention's Physics value.

As long as linking part meets the cloth and silk of above-mentioned necessary condition, not by particular determination, but can exemplify by Following cloth and silks are constituted, i.e.,：Cotton woven, polyester tatting/knitted fabric, tatting/knitted fabric of polyamide raw materials or elastic network(s) group The knitted fabric of the yarn fibers containing spandex such as the knitted fabric of the knitted fabric, two-way tissue knitted.

By the way that aileron portion is arranged, cup upper limb high stress portion and/or cup lower edge high stress portion are set, and in shoulder belt portion Vibration damping portion is set, the more violent shaking perceived from the appearance can be also inhibited, meanwhile, with the linking part with specific physical property The effect for drawing breast over to one's side to trunk realized complements each other, thereby, it is possible to make cup and breast be close to securely, thus can also Enough further suppress the subtle shaking of breast.

In particular implementation, the upper limb high stress portion that there is brassiere the upper limb along cup to extend is (such as upper in Fig. 1 Edge high stress portion 104).

In particular implementation, brassiere have along cup lower edge extend lower edge high stress portion (such as in Fig. 1 under Edge high stress portion 105).

Referring specifically to Fig. 2, in certain embodiments, brassiere has the aileron portion 109 as vibration damping portion.Pass through brassiere quilt It dresses and the fabric in aileron portion is made to be extended in the range of from cup parts to alar part, thereby, it is possible to the trunk place side of human body To breast is drawn over to one's side, so as to improve the close property of cup and breast, make cup and the integrated excellent effect of breast, has anti- Breast leaves the effect of cup when only being acted.The breast perceived from the appearance when thereby, it is possible to inhibit to be acted compared with Violent shaking.

Aileron portion 109 is configured in the whole region until from a part for cup parts 102 to a part for alar part 103 In brassiere main body.Typical aileron portion 109 can be by the whole region until the oxter edge to alar part 103 from cup parts 102 The piece of cloth silks of configuration or polylith cloth and silk are constituted.Aileron portion 109 is not and brassiere main body on cup parts 102 and alar part 103 Integrally constitute, but by relative to the independent cloth and silk of brassiere main part in the way of being stacked on the brassiere main part shape At.

Aileron portion 109 and brassiere main body more typically have following two joint portions.

For the first joint portion, in the back that the mammary areola of each cup parts 102 is corresponded to portion H and the alar part corresponding to it The line segment I that heart C is linked up is that longest mode configures brassiere 100, and provides the extending direction phase Tongfang for having with the line segment To normal plane S, it is in this case, on line segment I, correspond to portion H using mammary areola and go to calculate towards center back C as starting point In the plane at 0%~25%, preferably 5%~25%, more preferably 8%~23% position risen, there is this First joint portion.It is to correspond to portion using mammary areola to go count 0% or more as starting point towards center back C in the position at the first joint portion Position in the case of, excessive pulling force will not be applied to the mammary areola portion of correspondence, advantageously.On the other hand, at the joint portion Position is to be corresponded in the case that portion goes to count 25% position below as starting point towards center back C using mammary areola, to bodyside The power for drawing breast over to one's side is easy to play a role, advantageously.

It is on line segment I, portion H is corresponded to using mammary areola as starting point direction about above-mentioned plane S for the second joint portion Center back C is gone at count 50%~100%, preferably 50%~85%, more preferably 55%~80% position The plane on, there are second joint portions.In the position at the second joint portion is to correspond to portion as starting point towards back using mammary areola In the case that the heart goes to the position of 50% or more counted, it is easy to apply pulling force to the mammary areola portion of correspondence, advantageously.On the other hand, It is that the case where portion goes to 100% position below counted as starting point towards center back is corresponded to using mammary areola in the position at the joint portion Under, the power for drawing breast over to one's side to bodyside is easy to play a role, advantageously.

For aileron portion 109 and the joint portion of brassiere main body, about defined plane S as described above, the joint portion Be present in it is on line segment I, corresponded to using mammary areola portion H as starting point go count 0%~25% and 50% towards center back C~ In the plane at 100% position, can also be, which is also present in the position other than above-mentioned plane.But From the viewpoint of the effectiveness in vibration suppression for obtaining more good aileron portion 109, it is further preferred that about above-mentioned plane S, in above-mentioned line It is on section I, to correspond to using mammary areola portion be that starting point is greater than 25% and less than 50% or 25% towards what center back C went to count Joint portion is not present in the plane at~55% or 28%~60% position.

Boundary between cup parts 102 and alar part 103 is generally in portion on line segment I, corresponding using mammary areola as starting point direction Center back C is gone on the plane S at the position of 25%~35% counted.Thus, it is present in above-mentioned 0% at joint portion~ In the case of in the plane at 25% position and 50%~100% position, aileron portion 109 can be made in cup parts 102 and alar part 103 it is respective, wish that the position of vibration damping is engaged with brassiere main body, therefore be advantageous.

Aileron portion 109 and the joint portion of brassiere main body, which can be formed as linear, (relatively typically has Rack It is band-like), it is dotted etc..For example, can be formed on left and right cup parts 102 and left and right alar part 103 linear along roughly vertical direction The joint portion of extension.In preferred embodiment, aileron portion 109 is in the partial zones of the regional area and alar part 103 of cup parts 102 The two regions of domain are engaged with brassiere main part, also, aileron portion 109 has the region not engaged with brassiere main part.It is excellent In the embodiment of choosing, aileron portion 109 is stacked in brassiere main part, a part as cup parts 102 region 107a and work The region being linked to be by the region 107b of a part for alar part 103.It includes region 107a and area that aileron portion 109 can be utilized, which to be formed, The oxter strengthening portion of domain 107b.That is, oxter strengthening portion is made of the engagement cloth and silk including brassiere main part and aileron portion 109 's.

In preferred embodiment, the both ends that include aileron portion of the aileron portion 109 in 103 side of 102 side of cup parts and alar part Region inside is engaged with brassiere main part.

In preferred embodiment, aileron portion 109 by between brassiere main part have space in a manner of with brassiere main body Portion engages.In the embodiment, aileron portion 109 at least covers brassiere main part, a part and the wing comprising cup parts 102 Region including at least part in portion 103.Moreover, it can be, aileron portion 109 is in the week for including the aileron portion 109 Region including at least part (such as positioned at end of 102 side of cup parts and positioned at this both ends of the end of 103 side of alar part) of edge with Brassiere main part engages, it is also possible that aileron portion 109 is merely with part other than periphery of the aileron portion 109 and text Chest main part engages.Aileron portion 109 engages in such a way that it is between brassiere main part there are space with brassiere main part. Here, space refer to by joint portion pick up Lai or say be fenced up by joint portion, aileron portion 109 and brassiere main part Unassembled region.In order to form above-mentioned such space, it is preferred that joint portion is with more than two points or two or more The shapes such as line are formed.Refer to more than one in the region of cup parts 102 for example, by taking more than two points as an example The combination of point and the more than one point in alar part 103.Refer to Fig. 2 institutes moreover, for example, by taking two or more lines as an example The combination of show, cup parts side engagement portion 107aS and alar part side engagement portion 107bS.For example, being formed as two dotted engagements In the case of portion, space is meant that the region that links up two points in aileron portion 109 and brassiere main part The region being unfolded between region that two points link up.In addition, at the space, aileron portion 109 and brassiere main part In unassembled state, can also be that aileron portion 109 and brassiere main part contact with each other.Using above-mentioned such structure, Can be poor using the tensile stress between the cloth and silk in aileron portion 109 and the cloth and silk of brassiere main part when dressing brassiere, make engagement Pulling force is generated between portion, therefore, it is possible to play effectiveness in vibration suppression.

With reference to Fig. 2, in particular implementation, aileron portion 109 at least positioned at 102 side of cup parts end and be located at alar part This both ends of the end of 103 sides include the end for being located at 102 side of cup parts and the region including this both ends of the end of 103 side of alar part It is engaged with brassiere main part, also, aileron portion 109 has the region not engaged with brassiere main part.Preferred embodiment In, as shown in Fig. 2, brassiere main part and aileron portion 109 are only in cup parts side engagement portion 107aS and alar part side engagement portion 107bS Place engages, and aileron portion 109 is in addition to this region at two other than is not engaged with brassiere main part.Utilize depositing for aileron portion 109 , it can be when dressing brassiere, power making aileron portion 109, being pulled from the end positioned at cup side towards flank plays a role, Thereby, it is possible to play effectiveness in vibration suppression.

With regard to the region not engaged with brassiere main part in aileron portion 109 area account for aileron portion 109, when dressing brassiere For the ratio of the area in the region of under tension, from the viewpoint of obtaining good effectiveness in vibration suppression, which is preferably 30% or more, more preferably 60% or more, further preferably 80% or more, from keeping aileron portion 109 and brassiere main part secured Ground engagement in this way from the perspective of, aforementioned proportion be preferably 99.5% hereinafter, more preferably 99% hereinafter, further preferably 98% or less.In addition, for the area in the region of the above-mentioned under tension when dressing brassiere, be related to same line segment I it is vertical and By the intersection on the surface in the face and aileron portion 109 at joint portion, be by away from the nearest intersection in preceding center and away from center back C most Close intersection picks up the area of aileron cloth and silk existing for the region come.

With reference to Fig. 3, by with brassiere bottom it is tangent in a manner of draw a straight line L1, and with from straight line L1 to following boundary point Pa Distance be shortest mode assume that a line segment L2, boundary point Pa are the boundaries between cup upper limb and the oxter edge of cup Point.Selection by line segment L2 and the plane vertical with line segment L2 with brassiere main part cloth and silk surface (from the point of view of wearer When outer surface) intersection in, the maximum intersection of length in the 107a of region, by the oxter edge of the intersection and cup Intersection point is set as M1, and the intersection point by the edge of oxter strengthening portion end side of the intersection and cup side engagement portion 107aS are set as M2, On the intersection line segment La will be set as in the line segment between M1 and M2.By the intersection with alar part side engagement portion 107bS by armpit The intersection point at the edge of lower strengthening portion end side is set as M3.On the intersection line segment Lb will be set as in the line segment between M1 and M3.

The length of alar part 103 is meant that：Center back from point M1 to alar part 103 (has at the end of alar part 103 Refer to the boundary between hook portion in the case of hook portion, if without hook portion, at center back when referring to wearing brassiere, Such as the point Pc in Fig. 4) until cloth and silk shortest length.

The length of above-mentioned alar part 103 is more moderate when being 5cm~15cm.

The length m1 in aileron portion 109 refers to by point M2 and point in the aileron portion 109, with the joint portion of brassiere main part The shortest length for the fabric that M3 is linked up.Moreover, the overall length of line segment La and line segment Lb on brassiere main part are set as brassiere Length m2 between joint portion on main part.In general, brassiere is worn with the state stretched.Preferably, aileron portion 109 Cross direction elongation E1 when wearing meets the two following conditions：

× 100 (1) E1={ (1+E2/100) × (m2/m1) -1 }

100/YR1≤E1≤1000/YR1 (2)。

Here, the transverse direction in aileron portion 109 refers to the length for the fabric for linking up point M2 and point M3 for most institute's structure in short-term At line segment extending direction.Here, the length m2 between joint portion on the length m1 in aileron portion 109, brassiere main part is The numerical value determined by the design of brassiere, face shaping, cross direction elongation E2 when the wearing of brassiere main body with (under bust girth)/ (perimeter of brassiere lowest part) × 100 } -100 (%) define, and elongation E2 is the numerical value determined by size.

Using these above-mentioned numerical value the cross direction elongation E1 in the aileron portion 109 when dressing brassiere is calculated according to (1) formula.It should If elongation E1 meets (2) formula, it will be able to give full play to it is damping, and when can inhibit when wearing and be acted not Suitable sense, is therefore preferred.(2) in formula, YR1 is the lateral Young's modulus in aftermentioned aileron portion 109.It is calculated according to (1) formula In the case that the elongation E1 gone out is unsatisfactory for (2) formula, change YR1 by changing the raw material in aileron portion 109, with satisfaction (2) formula. Alternatively, being further preferably changed in the following manner：By changing design, face shaping, size, by changing length m1, length Any one of m2, elongation E2 or combination thereof, to make elongation E1 meet (2) formula.

Preferably, according to above-mentioned elongation E1, meet in the lateral stress σ 1 that aileron portion 109 generates

100cN/inch≤σ1≤1000cN/inch (3)。

If σ 1 be 100cN/inch or more, can fully demonstrate it is damping, if σ 1 be 1000cN/inch hereinafter, if wear The wearing pressure worn at pressure especially shoulder and breast lower part would not be excessively high, can inhibit constraint sense, card voluptuousness.Preferably 1≤800cN/inch of 200cN/inch≤σ, particularly preferably 1≤600cN/inch of 300cN/inch≤σ.σ corresponding with E1 1 It can be determined according to the strain-stress relation of raw material in addition measuring, used in aileron portion 109.

Further it is preferred that the lateral Young's modulus YR2 of the lateral Young's modulus YR1 in aileron portion 109 and alar part 103 it Than meeting：

0.7≤YR1/YR2≤3 (4)。

Here, the transverse direction of alar part 103 refers to the direction along line segment Lb.If 0.7≤YR1/YR2, the length with alar part 103 Degree compares, and the length in aileron portion 109 would not seem extremely short, so as to obtain foot under the premise of keeping face shaping more U.S. Enough is damping, if YR1/YR2≤3, compares with the length of alar part, and the length in aileron portion 109, which would not seem, extremely stretches Exhibition embodies damping stress, further, it is possible to inhibit the feeling that breast lower part is clamped so as to obtain.Preferably 1≤ YR1/YR2≤2.5, particularly preferably 1.1≤YR1/YR2≤2.YR1, YR2 are used by conventional method according to JIS 0%~10% portion slope of the strain of strain-stress relation is obtained on the basis of strip coating method in L1096.8.12.1A methods Come the value calculated.

The shape in aileron portion 109, the determination method of physical property are as follows.According to the design, appearance, size of brassiere, length is determined M1, length m2, elongation E2, and according to (1) formula, calculate the cross direction elongation E1 in aileron portion 109.Use the cross in aileron portion 109 Confirm whether above-mentioned elongation E1 is in proper range to Young's modulus YR1, and according to (2) formula.At this point, also confirming aileron together Whether the ratio between the lateral Young's modulus of portion 109 and alar part 103 meets (4) formula.In elongation E1 not in the case of proper range, It is the cloth and silk changed used in aileron portion by changing Young's modulus YR1, is to change setting for brassiere by changing length m1, length m2 Meter, appearance are the size for changing brassiere by changing elongation E2, to make elongation E1 be in proper range.Then, according to pair The strain-stress relation of the cloth and silk of alar part 109 finds out the stress σ 1 corresponding to elongation E1, and confirms whether stress σ 1 meets (3) formula, so that it is determined that the shape in aileron portion 109, physical property.

In the case where the stress σ 1 in aileron portion 109 is unsatisfactory for (3) formula, i.e., in the case where σ 1 is less than 100cN/inch, The countermeasures such as following can be taken：Under the premise of satisfaction (2) formula and (4) formula, uses the larger cloth and silk of Young's modulus YR1 instead and make pair Alar part 109, and the length m1 in aileron portion 109 is changed into the shorter design of length, so as to increase cross when wearing brassiere To elongation E1.On the contrary, in the case where σ 1 is more than 1000cN/inch, the countermeasures such as following can be taken：In satisfaction (2) formula (4) it under the premise of formula, uses the smaller cloth and silk of Young's modulus YR1 instead and makes aileron portion 109, and by the length m1 in aileron portion 109 The longer design of length is changed into, so as to reduce cross direction elongation E1 when wearing brassiere.

The height in aileron portion 109 indicated using the length of line segment (not shown) in aileron portion, vertical with straight line L1, Height value is bigger, and effectiveness in vibration suppression is better.Thus it is preferred that 102 side engagement portion of cup parts is between the top and bottom of cup Entire scope extend, it is preferred that entire scope of 103 side engagement portion of alar part between the top and bottom of the wing extends.And And, it is preferred that the height of the part other than joint portion in aileron portion 109 be brassiere main part height it is same with On.

Aileron portion 109 helps to improve in the shaking in X-direction, Y-direction, Z-direction for breast, particularly X very much Shaking on direction and Z-direction it is damping.That is, aileron portion 109 can improve the close property of cup and breast, make cup and breast The integrated excellent effect in room, breast overflows brassiere when having the effect of preventing from being acted.In particular, using in Z-direction Damping, can more efficiently play the close property of raising cup and breast makes cup and the integrated effect of breast, especially It is, it is damping in the X-direction of pulling force using putting to good use, it can more efficiently play the effect for preventing breast from overflowing brassiere.

As long as aileron portion 109 meets the cloth and silk of above-mentioned necessary condition, not by particular determination, but can exemplify It is made of following cloth and silks：Cotton woven, polyester tatting/knitted fabric, tatting/knitted fabric of polyamide raw materials or elastic network(s) group The knitted fabric of the yarn fibers containing spandex such as the knitted fabric of the knitted fabric, two-way tissue knitted.The table side of brassiere main part cloth and silk Frictional force between the inboard of aileron cloth and silk may influence effectiveness in vibration suppression.Thus, for the frictional force, for example, utilizing The table side and aileron cloth and silk of the KES-SE friction tests equipment of カトーテッ Network society or equivalent devices to brassiere main part cloth and silk Inboard between frictional force evaluated, in this case, which is preferably 0.10~0.20, more preferably 0.12~ 0.18.The effect for making aileron cloth and silk be pressed on brassiere main body cloth and silk easily can be well played if frictional force is 0.10 or more, Friction will not be caused excessive if frictional force is 0.20 or less, from the point of view of this aspect, easy performance makes aileron cloth and silk be pressed on brassiere The effect of main body cloth and silk.Above-mentioned frictional force can pass through the combination of the cloth and silk of the cloth and silk and aileron portion 109 of change brassiere main part To be adjusted.

It aileron portion 109 can be by sewing, welding or other methods are engaged with brassiere main part.For example, in aileron portion 109 With the joint portion of brassiere main part be the aileron portion, positioned at the end of 102 side of cup parts and positioned at this both ends of the end of alar part side In the case of, it can be formed by the following method aileron portion 109, i.e.,：By the cloth and silk of brassiere main part and aileron portion 109 Cloth and silk stacks, and positioned at 102 side of cup parts end and at this both ends of the end of alar part side, by sewing, weld or Above-mentioned cloth and silk is fixed together by other methods.In the case where cup parts 102 are two layers or more, can also be, with wherein one Layer engagement, or can also be all to be engaged with all layers.In the smaller situation of the stretching, extension stress of the surface fabric of cup main part Under, if only being engaged with surface fabric, fabric can extend, and pull the effect unobvious of cup, it is preferred, therefore, that passing through seam The modes such as thread are engaged with cup parts main body, are extended to avoid only surface fabric.

It aileron portion, can be to trunk by rear ramp pulling cup (corresponding with the combinations of directions of X-direction and Z-direction) That layback holds together breast, so as to improve the close property of cup and breast.But while following trend are presented：With no aileron Brassiere is compared, and further can draw breast over to one's side to side.Therefore, meanwhile, for linking part, because pulling force caused by aileron can be to Left and right directions pulls linking part, and linking part can extend as a result,.Therefore, it compared with the brassiere of no aileron, is easy near linking part Gap is generated between cup and breast at (breast center).At this point, for the brassiere with aileron portion, by making linking part With regulation stress, it is fixed point that can make linking part, then generates the pulling force for drawing breast over to one's side to trunk, further, it is possible to inhibit to connect Knot leaves skin, subtle shaking when so as to inhibit to be acted.

Using another embodiment, high stress portion 104 is configured by the rising wood in cup, effectiveness in vibration suppression can be embodied. Upper limb high stress portion is configured to extend along cup rising wood.In addition, upper limb high stress portion constitutes the substantive peripheral part of cup parts At least part divided.

For cup parts, it is preferred that the stretching, extension stress S2 in upper limb high stress portion and the stretching, extension of cup central portion are answered The ratio between power S1 S2/S1 are 2/1~400/1.In the present invention, cup central portion be meant that cup containing top (i.e. with wearing The corresponding position of areola of breast of person) including, with it is single stretching, extension stress region.In the present invention, under stretching, extension stress refers to State such value：On the basis of the strip coating method tension test in JIS L1096.8.12.1A methods, measures cloth and silk and stretch along longitudinal direction Stress (N/2.5cm width, be only denoted as N below) when 10% and the stress (N) when transversely stretching 10%, calculate theirs Average value is used as stretching, extension stress (in the following, also referred to as averagely stretching stress in length and breadth, or simply referred to as stretching stress).

In the case where cup parts have two layers or more (such as Polyurethane Lining and cloth and silk this two layers), by two layers or more Stretching, extension stress is measured in the state of stacking.

As long as it is above-mentioned than S2/S1 be 2/1 or more, high stress portion inhibit breast shake effect it is more apparent.Another party As long as face than S2/S1 is 400/1 hereinafter, the stretching, extension stress in the high stress portion would not be excessively high above-mentioned, it will be able to avoid becoming deadlock It is not easy personal brassiere firmly.Above-mentioned than S2/S1 is preferably 3/1~100/1, more preferably 5/1~80/1, particularly preferably 10/1 ~60/1.

Upper limb high stress portion helps to improve in the shaking in X-direction, Y-direction, Z-direction for breast, special very much It is the damping of the shaking in X-direction and Y-direction.When into actions such as walking, races, human body can move up and down, and be contained Breast in cup relative to human body movement small delays carry out it is dynamic up and down.By the way that upper limb high stress portion, the feelings are arranged The shaking of breast upward under condition can be effectively suppressed.Moreover, into walking, run etc. actions when in addition to human body up and down Except movement, the side-to-side movement for making body rotate can be also generated simultaneously.Moreover, when being prolonged along cup upper limb with upper limb high stress portion When the upper limb high stress portion is arranged in the mode stretched, the side that usually can be relative to horizontal direction slightly tilted with upper limb high stress portion Formula installs the upper limb high stress portion.It, can thereby, it is possible to inhibit to make the shaking of breast inwardly because human body carries out side-to-side movement Enough inhibit the shaking of breast in the X direction.

Preferably, upper limb high stress portion is continuously configured for 0.5cm~5.0cm on the top of cup parts with width.More Preferably, above-mentioned width is 1.0cm~4.0cm.Moreover, above-mentioned width can be arbitrarily devised.For example, can be designed as： The width in upper limb high stress portion is relatively narrow in the preceding central side of the wearer's body of cup parts, wider in the oxter side of cup parts.

Moreover, using another embodiment, high stress portion 105 is configured by the lower edge in cup, vibration damping can be embodied Effect.Lower edge high stress portion is configured to extend along the lower edge of cup parts.In addition, lower edge high stress portion constitutes the reality of cup parts At least part of matter peripheral part.

For cup parts, it is preferred that the stretching, extension stress S3 in lower edge high stress portion and the stretching, extension of cup central portion are answered The ratio between power S1 S3/S1 are 2/1~400/1.As long as S3/S1 be 2/1 or more, high stress portion inhibit breast shake effect compared with Obviously.It on the other hand, can as long as above-mentioned than S3/S1 is 400/1 hereinafter, the stretching, extension stress in the high stress portion would not be excessively high Avoiding, which becomes stiff, is not easy personal brassiere.Above-mentioned than S3/S1 is preferably 3/1~100/1, and more preferably 5/1~80/1, especially Preferably 10/1~60/1.

Lower edge high stress portion helps to improve in being shaken in X-direction, Y-direction, Z-direction for breast, particularly Y very much Shaking on direction it is damping.When into actions such as walking, races, human body can move up and down, and be incorporated in cup Breast relative to human body movement small delays carry out it is dynamic up and down.By the way that lower edge high stress portion is arranged, in this case, downwards It pats such breast shaking and can effectively be suppressed in side.

Preferably, lower edge high stress portion is continuously configured for 0.5cm~4.0cm in the lower part of cup parts with width.More Preferably, above-mentioned width is 1.0cm~3.0cm.Moreover, above-mentioned width can be arbitrarily devised.For example, can be designed as： The width is relatively narrow in the preceding central side of the wearer's body of cup parts, wider in the oxter side of cup parts.

In the case of being equipped with upper limb high stress portion and lower edge high stress portion at the same time, it is preferred that upper limb high stress portion and The sum of the area in lower edge high stress portion account for the entire area of cup parts ratio be 10%~50%, particularly preferably 20%~ 40%.In the case where above-mentioned ratio is 10% or more, stiffening effect is more apparent, even if cup can obtain well if larger Inhibit breast shake effect.On the other hand, it is 50% below in above-mentioned ratio, can avoids dressing well When sense of discomfort.Area ratio shared by upper limb high stress portion and lower edge high stress portion is not by particular determination.Above-mentioned ratio can It is calculated by following methods：For example, thin paper is stacked in cup surface, the corresponding with the area of each section of cup of paper is found out Partial quality.

The stretching, extension stress S2 in upper limb high stress portion and the stretching, extension stress S3 in lower edge high stress portion are both preferably 20N~500N, More preferably 50N~400N, further preferably 100N~350N.In the case where above-mentioned stretching, extension stress is 20N or more, reinforce Effect is more apparent, is that 500N is below in above-mentioned elongation stress, can avoid sense of discomfort when wearing well.Upper limb The ratio of the stretching, extension stress in high stress portion and lower edge high stress portion is not by particular determination.Moreover, the stretching, extension stress of cup central portion Preferably 0.5N~50N, more preferably 1N~20N, further preferably 1.5N~15N, particularly preferably 2N~10N.Upper In the case of stretching, extension stress is stated as 0.5N or more, it is not easy to cause rupture etc. in wearing and when washing, in above-mentioned stretching, extension stress For 50N it is below in the case of, can avoid well wearing when sense of discomfort.

In the case where cup parts form upper limb high stress portion and/or lower edge high stress portion, can also be, in the rule of cup Positioning sets configuration knitting technology weave, improves the position of stretching, extension stress using yarn and by changing danier.Moreover, can use Following methods：It is configured by sewing or bonding way in the inside (that side for leaning on wearer skin surface) of brassiere and waits becoming upper The reinforcement cloth in edge high stress portion or lower edge high stress portion.Alternatively, in the case of using Polyurethane Lining in cup, can also make With following methods etc.：When carrying out processed molding etc. to Polyurethane Lining, the woven etc. in high stress portion to be become is clipped in it In, to pad local rigidity to improve.

In particular implementation, the averga cross section area in the shoulder belt portion as vibration damping portion is 20mm²~120mm².In the feelings Under condition, it can reach good damping.The averga cross section area is 25mm²~100mm²If more preferably.Area of section It is meant that the thickness (mm) of width (mm) × shoulder belt of shoulder belt.For averga cross section area, the both ends in shoulder belt portion are measured Area of section, also, measure by between the both ends part carry out 10 deciles after each section area of section, calculate institute The number average value of the area of section measured is as averga cross section area.In particular, averga cross section area can be by following Mode calculates.

Referring to Fig.1 and Fig. 4, the averga cross section area in shoulder belt portion are the arithmetic mean of instantaneous values of following areas of section：Shoulder belt portion The area of section that width W1 × thickness (not shown) positioned at the end (i.e. root) of cup parts side (i.e. front side) is calculated, shoulder belt The area of section that width W2 × thickness (not shown) of the end (i.e. root) for being located at alar part side (i.e. rear side) in portion is calculated, with And by the part positioned at the end of cup parts side and between the end of alar part side in shoulder belt portion along the length direction in shoulder belt portion 10 deciles are carried out, width × thickness (the not shown) (example for passing through each section for the section (i.e. nine sections) obtained after decile Such as, width W3 × thickness in Fig. 1) area of section that is calculated.In addition, width W1 refers between shoulder belt portion and cup parts For point of contact P1 by oxter to the shortest distance at the center of front in shoulder belt portion, width W2 refers between shoulder belt portion and alar part The shortest distance to shoulder belt portion at back side center of point of contact P2 by oxter.In addition, long with shoulder belt can be adjusted In the case of the adjuster of degree, shoulder belt length is transferred to after maximum using adjuster and measures and calculates again.

The weight of breast can largely be applied to strap portions, feelings especially larger in the cup sizes of wearer Under condition, which can become very large.Therefore, for movement brassiere and the larger brassiere of cup sizes, reality is needed Apply the design for the width for increasing shoulder belt portion.But in the case of the wider width in shoulder belt portion, sexuality is lost, taste is poor. Even if can be by the area of section in increase shoulder belt portion, to absorb vibration, and surely if in the case of the narrower width in shoulder belt portion Surely cup parts are supported.Averga cross section area in shoulder belt portion is less than 20mm²In the case of, it is unknown to there is the effect for absorbing and vibrating Aobvious trend.Averga cross section area in shoulder belt portion is more than 120mm²In the case of, although vibration can be absorbed, increasing Taste can be destroyed in the case of width, moreover, in the case where increasing thickness, exist cause the coarse senses of touch such as stiff and Influence the trend of housing.But as it is above-mentioned in this wise to other positions in brassiere implement reinforcement processing in the case of, As long as it is 20mm to make the averga cross section area in shoulder belt portion²For example, about 80% or more, it will be able to ensure the excellent damping of brassiere. For example, in the case where one or both of upper limb high stress portion, lower edge high stress portion and aileron portion or more is arranged, can make The averga cross section area in shoulder belt portion is 16mm²Above and it is 120mm²Below.

Preferably, shoulder belt portion back side connection center be present in towards cup parts side leave alar part center back away from 25%~60% position from the length for alar part, the more preferable distance are 30%~50% position of the length of alar part. In the case that the distance for linking the center back of centre-to-centre spacing alar part in the back side in shoulder belt portion is 25% or more of the length of alar part, tool Have the advantages that damping excellent, the distance that the back side in shoulder belt portion links the center back of centre-to-centre spacing alar part is the length of alar part In the case of 60% is below, have the advantages that shoulder belt portion is not easy to slide.In addition, the length of alar part can proceed as described above regulation. Moreover, for the back side connection center in shoulder belt portion, from the midpoint of line segment in Fig. 4, representing width W2, direction represents alar part Length line segment draw a vertical line, the shoulder belt portion back side connection center refer to the vertical line and represent the alar part length line segment Intersection point.

For the elongation (ability) in shoulder belt portion, by the length direction in shoulder belt portion with 0.5N/mm²It is aggravated When shoulder belt portion extend and measure and calculate the elongation, which is preferably 30%~80%, more preferably 40%~ 70%.Elongation can be measured on the basis of the strip coating method tension test in JIS L1096.8.12.1A methods, be held whole A shoulder belt portion simultaneously separates interval, and load when measurement is the load that averga cross section area is multiplied by that 0.5N is obtained.As long as shoulder belt portion Ability be 30% or more, would not be excessively stiff, vibration can be absorbed well.As long as the ability in shoulder belt portion be 80% with Under, it would not excessively extend, vibration can be absorbed well.

Preferably, locally there is low stress portion, the stretching, extension stress in the low stress portion to be less than shoulder belt portion in shoulder belt portion 110 The stretching, extension stress of other parts.By the way that above-mentioned such low stress portion is arranged, the concentration of wearing pressure can be prevented, can be improved Comfort.It is desirable that for example, referring to Fig. 1, there are other portions that stretching, extension stress is less than shoulder belt portion in the region of the 110a containing shoulder The low stress portion of the stretching, extension stress divided.

Shoulder belt portion helps to improve in the shaking in X-direction, Y-direction, Z-direction for breast, particularly Y-direction very much On shaking it is damping.When into actions such as walking, races, human body can move up and down, the breast being incorporated in cup It with small delays carries out moving up and down, but is hung from top by using the shoulder belt portion with area of section more than certain numerical value Cup, the upper and lower dynamic of breast can be inhibited.Moreover, by the way that shoulder belt portion to be arranged close at oxter, rather than be mounted on and lean on Nearly centre can help to improve in the shaking in the X-direction, Y-direction, Z-direction for breast, particularly X-direction very much On shaking it is damping.By the way that shoulder belt portion to be arranged close at oxter, the power for pulling cup to oblique upside can be made Play a role, therefore, it is possible to effectively inhibit because into walking, run etc. actions when human body spinning movement caused by breast shake It is dynamic.For the installation site in shoulder belt portion, it is preferred that the front in shoulder belt portion is mounted on cup, edge substantially X-direction away from cup Oxter end 3cm within position, the rear portion in shoulder belt portion be mounted on away from back side center and oxter center (i.e. preceding center with carry on the back Middle between the heart) between midpoint to the position within the 5cm of oxter side.Moreover, because shoulder belt portion can be towards human body rear side The cup of front is pulled, therefore, shoulder belt portion also contributes to damping in Z-direction.

As described above, for the brassiere of the present invention, the component in regulation physical property is used in cup linking part, and And vibration damping portion is aileron portion, cup upper limb high stress portion, cup lower edge high stress portion and with specific averga cross section area In the case of combination more than one of shoulder belt portion or in which the two, in particular, with aileron portion, especially It is that, in the case where aileron portion is in specific physical property ratio in specific physical property and alar part and aileron portion, can embody especially excellent Effectiveness in vibration suppression.In particular, by respectively combining the effectiveness in vibration suppression in X-direction, Y-direction or Z-direction, it can be further It improves damping.For example, by linking part, aileron portion, cup upper limb high stress portion, cup lower edge high stress portion, shoulder belt portion these The two combination of the above in position is got up, and the shaking in X-direction, Y-direction and Z-direction can be mitigated and disperse, the way right and wrong It is often preferred.Moreover, being aileron portion, cup upper limb high stress portion, cup lower edge high stress portion and with specific in vibration damping portion In the case of combination more than the two in the shoulder belt portion of averga cross section area, additionally it is possible to make each position characteristic value (in particular, The stretching, extension stress ratio in above-mentioned high stress portion and the averga cross section area in shoulder belt portion) the lower limiting value of preferred scope to reduce by 20% left It is right.For example, the averga cross section area in shoulder belt portion is 20mm²~120mm²In the case of, can obtain it is good damping, but Be, as described above also other positions be arranged vibration damping portion in the case of, be 16mm with averga cross section area²~120mm² It can obtain good damping.

Each component can both be formed with mutually cloth and silk is independent, and can also be formed with continuous monoblock cloth and silk, for In the case of monoblock cloth and silk, the boundary between component is divided according to shape.For the latter, in particular, with regard to cup For the outer rim in portion, if the edge of the projecting shape of cup is more apparent, the outer rim of cup parts is drawn into the edge in the projecting shape Position, if the edge unobvious of the projecting shape of cup, the outer rim of cup parts, which is drawn, can regard as according to projecting shape institute It is envisioned as the position of the edge come.

Can also be that vibration damping portion is configured to using the strengthening portion made relative to the independent cloth and silk of brassiere main body cloth and silk, For example, as described above, aileron portion by way of engagement be mounted on constitute brassiere main body fabric (present invention in, also referred to as based on Body fabric.).Compared with the case where being set to main body fabric by modes such as switching capabilities (stretch stress can by force can be weak), on The way of setting strengthening portion as stating has the advantages that make damping more good such.

Main body fabric can both be formed with mutually cloth and silk is independent, and can also be formed with continuous monoblock cloth and silk, In the case of for monoblock cloth and silk, the boundary between component is divided according to shape.For the latter, in particular, just covering For the outer rim of cup portion, if the edge of the projecting shape of cup is more apparent, the outer rim of cup parts is drawn into the edge in the projecting shape Position, if the edge unobvious of the projecting shape of cup, by the outer rim of cup parts draw can regard as according to projecting shape It is envisioned as the position of the edge come.

With reference to Fig. 5, in particular implementation, with the endpoint Q1 and endpoint Q2 of the preceding central side by cup parts in shoulder belt portion The distance between for maximum mode configure brassiere when, by endpoint Q1, the endpoint Q2 of the preceding central side by cup parts in shoulder belt portion It links up to form triangle T with the preceding center lower end point Q3 of linking part, not by the part 111 for constituting material for making clothes covering of brassiere The ratio that area accounts for the area of the triangle T is preferably 60% or more, more preferably 70% or more, further preferably 80% with On, most preferably 100%.So-called cleavage part is formd at the triangle.In the case where above-mentioned ratio is 60% or more, Cleavage can be prevented to be blocked, can realize good taste.For example, the brassiere of the present invention can be with by with specific Vibration damping portion is come realize, the specific shaking value as aftermentioned.For the brassiere of the present invention, even if being 60% in above-mentioned ratio It is damping also more excellent above in the state of i.e. so-called cleavage exposure, it is advantageous from the point of view of this aspect.

With reference to Fig. 6, for the vertical direction length of linking part, with the end of the preceding central side by cup parts in shoulder belt portion When the distance between point configures brassiere for maximum mode, being the line segment that links up of point B1, point B2 by cup lowest point Midpoint K and the midpoint R of the endpoint Q1 and endpoint Q2 of the preceding central side by cup parts in shoulder belt the portion line segment linked up is linked The line segment to get up is line segment L3, the length of the length and line segment L3 of the line segment L4 corresponding with the position of linking part on line segment L3 The ratio between L4/L3 be preferably 0.10~0.50, more preferably 0.15~0.45.In addition, the position phase with linking part on line segment L3 Corresponding line segment L4 refers to the set of the vertical line drawn from linking part on line segment L3 and the intersection point of line segment L3.By making above-mentioned ratio It is 0.10 or more, can ensures the setting area of enough linking parts, therefore, at cup central portion, cup and breast can It is close to, for being generated in wearing using alar part as starting point, stretching force to oxter direction, is fixed since linking part becomes Point can inhibit delicate variations thus, it is possible to which breast is secured firmly to before cup to the region of cup side.Moreover, logical Crossing makes above-mentioned than that hereinafter, the area of linking part can be prevented excessive, can keep sufficiently large breast exposed area for 0.50, has There is higher taste, meanwhile, it is capable to prevent linking part excessively stiff, therefore, wearing comfort will not be reduced.

The brassiere of the present invention is by with specific vibration damping portion, illustrating good damping.Thus, it is possible to inhibit breast It shakes, further, it is possible to make the wearing pressure at each position be 50hPa hereinafter, therefore, it is possible to make the maximum pressure of dressing of the present invention be 50hPa is hereinafter, can avoid not feeling well and fettering when wearing.It in general, mostly can be into order to inhibit the shaking of breast The stronger constraint of row, the very high brassiere of wearing pressure of especially shoulder are very common.But when the wearing at each position of brassiere When pressure is more than 50hPa, usually there is the trend that people does not feel well that allows.In the present invention, X-direction, Y-direction, the Z-direction of breast On activity be suppressed and scatter, it is thus possible to enough prevent wearing pressure concentration.In particular, above-mentioned is directed to shoulder belt portion Reinforcement processing can make dispersion wearing pressure excellent effect.Maximum wearing pressure is more preferably 45hPa hereinafter, further excellent It is selected as 40hPa or less.On the other hand, from the viewpoint of the offset of brassiere when inhibiting to dress and breast being inhibited to shake, for example, It is preferably 10hPa or more that can make maximum wearing pressure, more preferably 13hPa or more, further preferably 15hPa or more.

The raw material of each component (component for respectively constituting brassiere main body and strengthening portion) of the brassiere of the present invention is not by special It limits, it is recommended to use the synthetic fibers such as polyester fiber series fiber, perlon, artificial silk, copper ammonia fiber, acetate fiber etc. The natural fibers such as cellulose fibre, Yi Jimian, fiber crops.The construction of the cloth and silk of each component is constituted also not by particular determination, can be made With knitted fabric, woven, non-woven fabrics etc..Furthermore, it is also possible to use the fiber by processing of crispaturaing.In the present invention, for each structure Part configuration is more effective in the way of the cloth and silk of moderate stretch characteristics.For each component, it is recommended to use by by polyurethane Knitted fabric that elastomer friendship editorial afterword obtains, with extensibility.Moreover, the fabric of cup and alar part can use two-needle bar Round knitting (Japanese：ダ Block Le ball Knitting) fabric, Trico warp-knitting (Japanese：トリ U ット Knitting) fabric, La Sheer is through needle Knit (Japanese：ラッセ Le Knitting) fabric etc., it is recommended to use through suede-warp plain stitch's (Japanese：トリ U ットハー Off) fabric.Used The crochet needle of braider is away from preferably 20GG~40GG.Moreover, recommending high stress portion using woven or being inserted into the warp knit of warp thread The appearance design of knitted fabric etc., the materials such as lace with a little extensibility is also more excellent, recommends very much the materials such as lace Material.

Each component can be made of monofilament or multifilament.Can also be to contain delustering agents, the phosphoric acid such as titanium dioxide etc. in multifilament The crystallization nucleating agents such as the ultra-violet absorbers such as stabilizer, hydroxyl benzophenone derivant, talcum, fumed silica (AEROSIL) the easy antioxidants such as lubrication prescription, hindered phenol derivative, fire retardant, antistatic agent, pigment, fluorescent whitening agent, infrared such as Light absorbers, antifoaming agent etc..

The total fiber number for constituting the cloth and silk raw material of each component of the brassiere of the present invention can be in the commonly used model such as clothes It encloses.Wherein, from the viewpoint of intensity and pliability, total fiber number is preferably from about 22dtex~700dtex.

The weight per unit area of cloth and silk used in each component of brassiere is not by particular determination, but preferably from about 50g/m²~ 500g/m²。

It is desirable, moreover, that implementing absorbing sweat processing to the cloth and silk used in each component.

In the case of using Polyurethane Lining in cup, it is recommended to use thickness is the Polyurethane Lining of 2mm~15mm, but It is that stereoscopic knitwork is used in cup, gas permeability can be improved, which is also preferred.

Cloth and silk used in strengthening portion can be made of not by particular determination following cloth and silks：Cotton woven, polyester tatting/ Knitted fabric, the knitted fabric of tatting/knitted fabric of polyamide raw materials or elastic reticular tissue, two-way tissue knitted fabric etc. contain The cloth and silk etc. of polyurethane elastomeric fiber.

The present invention brassiere it is damping extremely excellent.In order to objectively evaluate breast shaking degree, can make In the following method.Allow five subjects that height is 160cm ± 8cm and the value of (upper bust-under bust girth) is 17.5cm or more The paces dressed brassiere, and subjects is allowed to step 150 steps with speed for 5.5km/h and with 1 minute on a treadmill, when landing The mode of single less touch with the ground is trotted.In this case, the reflection of a diameter of 2.0cm is installed in clavicle portion and areola of breast in advance Ball, and reflection sphere is shot 20 seconds using two high speed cameras.As by the shaking in clavicle portion for 13cm or so in a manner of carry out Breast when trotting shakes index, and it is each to calculate laterally (X-direction), longitudinal (Y-direction) and cup depth direction (Z-direction) these three directions From, (average value of maximum)-of (shaking of mammary areola)-(shaking of clavicle) (cm) in 20 seconds (minimum it is flat Mean value) (cm).Here, X-direction refers to the transverse direction of brassiere, Y-direction and Z-direction are vertical with X-direction respectively.By the value in three directions In maximum value as wearing when breast shaking value (cm), and the value divided by the value (cm) of (upper bust-under bust girth) are obtained Shaking value.When shaking value is 0.4 or less, breast shaking is smaller, advantageously.Shaking value is preferably 0.3 hereinafter, more preferably 0.2 or less.Shaking value is smaller more preferably, and still, from avoiding excessively oppressing, the viewpoint for being easy to get good wearing feeling goes out Hair, shaking value are for example preferably 0.03 or more.

In order to objectively evaluate subtle shaking degree of the invention, breast is in cup, can use following Method.When evaluating from the appearance the shaking of breast as described above, in advance by 3 axis accelerometers (SA12ZSCA：Ceramics Co., Ltd. of Fuji) (inside for being located at brassiere) is directly installed near the mammary areola of subject, make to be examined Person is on a treadmill 5.5km/h with speed and with the paces of 1 minute 150 step advanced in years, is carried out in a manner of list less touch with the ground when landing It trots.The situation is measured 20 seconds, wherein measure x direction (transverse direction) acceleration, the directions y (longitudinal direction) acceleration, the directions z (cup depth Direction) acceleration, and (minimum is averaged for the acceleration for calculating three directions respectively respective (average value of maximum)- Value) (m/s²).If acceleration is relatively low, indicate that subtle shaking of the breast in cup is less, thus, it is desirable that acceleration It is worth the smaller the better.In particular, acceleration is 50m/s²Below, delicate variations of the breast in cup can be inhibited, it can Reduce sense of discomfort when being acted under wearing state.

Embodiment

The present invention is specifically described below with embodiment.Certainly, the present invention is not limited to these embodiments.Separately Outside, the brassiere obtained in embodiment and comparative example is evaluated by following method.

(1) fabric of each component averagely stretches stress in length and breadth

On the basis of the strip coating method in JIS L1096.8.12.1 A methods, the stress of fabric sample is measured and calculated.It measures When stress characteristics when stretching 10%, measurement be along the first direction stretching, extension 10% arbitrarily set when stress and along and first The vertical second direction in direction stretches the stress (per width 2.5cm) when 10%, and calculates the average value of these above-mentioned stress.Poplar Family name's modulus uses the value calculated by following methods：0%~10% portion calculating the stress value of gained, straining The G-bar divided.

Test film width：2.5cm

Test film holds length：10cm

The rate of stretch：30cm/min

The fabric sample of each component is measured by above-mentioned condition, still, length is held sample can not be obtained In the case of, suitably change length.In the case where specimen width can not be obtained, width has been suitably changed, and by gained Stress value be converted into the numerical value of every 2.5cm width.

(2) the stretching, extension stress and elongation of the fabric of brassiere main body

On the basis of the strip coating method in JIS L1096.8.12.1A methods, measure and calculate the fabric of brassiere main body, applied It is added to the elongation until 22.1N, finds out elongation corresponding with the stress of setting.

(3) the extending transversely stress of the fabric of linking part is measured

The stretching, extension stress of the retractility knitted fabric of linking part is measured by following method.

Sample size：Length is 20mm (being free of handle part)

Test film width：25mm

Tensile test equipment：Tensilon tensile test equipments (ORIENTEC CORPORATION RTC-1210A)

Initial load：0.1N

Tensile speed：300mm/min

Tensile elongation and measurement：The fabric for transversely stretching linking part is allowed to stretch 10%, then is allowed to back with identical speed (recovery) arrives the original length after stretching, extension, and stretches, restores in triplicate by the condition, when finding out third time stretching, extension 10% Stretching, extension stress value.

It is measured by above-mentioned condition, still, in the case where sample holding length can not be obtained, is suitably changed Length.In the case where specimen width can not be obtained, width is suitably changed, and the stress value of gained is converted into often The numerical value of 2.5cm width.

(4) the extending transversely stress of the fabric in aileron portion is measured

The stretching, extension stress of retractility knitted fabric is measured by following method.

Sample size：Length is 100mm (being free of handle part)

Test film width：25mm

Initial load：0.1N

Tensile speed：300mm/min

Tensile elongation and measurement：The fabric for stretching aileron portion is allowed to stretch 30%, then is allowed to back (recovery) with identical speed It to the original length after stretching, extension, and stretches by the condition, restore in triplicate, find out stretching, extension when third time stretching, extension 30% Stress value.

(5) elongation in shoulder belt portion

On the basis of the strip coating method in JIS L1096.8.12.1A methods, measures and calculate stress of the shoulder belt portion in elongation Characteristic.Apply 0.5 (N) × area of section (mm on the length direction of shoulder belt²) load, and measure elongation (%).In addition, For shoulder belt with strengthening portion, the elongation of the elongation and shoulder belt strengthening portion of shoulder belt portion main body fabric is measured respectively Rate.

The holding length of test film：10cm

Extend speed：30cm/min

The fabric sample of each component is measured by above-mentioned condition, still, length is held sample can not be obtained In the case of, suitably change length.In the case where specimen width can not be obtained, width is suitably changed and has surveyed again later Amount.

(6) shaking when dressing

The brassiere size that height is 160cm ± 8cm and (upper bust-under bust girth) obtains is allowed to be 38DD (English size) (days If formula size be 85E) five subjects dress brassiere, and allow subjects on a treadmill with speed be 5.5km/h and 150 paces mended were stepped with 1 minute, are trotted in a manner of list less touch with the ground when landing.In this case, in advance in clavicle portion and Areola of breast installs the reflection sphere of a diameter of 2.0cm, and is shot 20 seconds to reflection sphere using two high speed cameras (200 frames/SEC). The shaking in clavicle portion is 13cm or so.Breast when as wearing brassiere shakes index, calculates (the rolling of mammary areola in 20 seconds It is dynamic)-(average value of maximum)-(average value of minimum) (cm) of (shaking of clavicle) (cm), will laterally (X-direction), Breast shaking value when longitudinal (Y-direction) and the value in the maximum direction of value in cup depth direction (Z-direction) are as wearing brassiere (cm), and by the value divided by (upper bust-under bust girth) (cm) shaking value is obtained.Calculate the average value of the result of five subjects.

(7) acceleration when brassiere is dressed

When measuring shaking when dressing brassiere, in advance by 3 axis accelerometer (SA12ZSCA：Ceramics Co., Ltd. of Fuji) The mammary areola of subject is directly installed on nearby (positioned at the inside of brassiere), to measure the case where testing similarly side with above-mentioned shaking Formula, the paces for allowing subjects to step 150 steps with speed for 5.5km/h and with 1 minute on a treadmill, list less touch with the ground when landing Mode trot.In this case, the directions x (transverse direction), the directions y (longitudinal direction), the directions z (the cup depth direction) in 20 seconds are measured Acceleration, and calculate (average value of maximum)-(average value of minimum) (m/s of the acceleration of all directions²).In addition, Acceleration is by being calculated after the acceleration value of all directions in the result of five subjects is averaged.

(8) the maximum wearing pressure dressed at pressure and cup lowest point

Using the Multi-contact pressure measuring instrument (AMI3037-10) of AMI Techno CO., LTD., in wearing brassiere When, sensor is inserted into measure wearing pressure in following positions between wearer and brassiere：The following band portion of alar part, alar part Central portion, the shoulder belt central portion in shoulder belt portion, the back root part in shoulder belt portion, cup top, cup oxter portion and cup lower part, by gained Value in maximum value as maximum wearing pressure (hPa).Moreover, as the standard for feeling metal line card meat, measurement is cover Wearing pressure at cup lowest point.

(9) comfort and rolling are dynamic

Comfort

When wearing test in progress (6), evaluated by following benchmark, and the evaluation of monitor is put down .

5：It is almost not felt by compressing, as snug as a bug in a rug

4：Constriction unobvious can be said to be comfortable

3：Feel slightly to have and a little oppress, but is not uncomfortable

2：Feel to oppress, it is uncomfortable

1：Feel compressing strongly, it is very uncomfortable

It shakes dynamic

5：Do not think that breast is shaking

4：Almost do not think that breast is shaking

3：Without special sensor

2：Think that breast is shaking

1：Think that breast shakes more violent

Taste

5：Breast appearance when dressing brassiere is very beautiful

4：Breast appearance when dressing brassiere is more beautiful

3：Without special sensor

2：Breast appearance when dressing brassiere is less beautiful

1：Breast appearance when dressing brassiere is not beautiful

Embodiment 1

Brassiere in shape shown in Fig. 2, that English size is 38DD is made in the following way (with Japanese size 85E is corresponding) (difference of upper bust and under bust girth is 20cm, is in longest with the shortest distance for corresponding to portion to center back from mammary areola Shortest distance when configuring brassiere of mode be 27cm).

The polyurethane formed production that average stretching, extension stress when being 6mm using thickness and stretching 10% in length and breadth is 3.0N Cup, and wrap up cup, the two-way trie which is the 28GG that nylon is 56dtex and polyurethane is 44dtex using fabric Section's warp-knitting fabric, and average stretching, extension stress when stretching 10% in length and breadth of the fabric is 0.4N, is made by the above process Cup parts 102.Whole average stretching, extension stress when stretching 10% in length and breadth of cup parts is 3.7N.Alar part 103 also use with it is above-mentioned Identical two-way Trico warp-knitting fabric, the width that lower sideband uses raschel to make are 1cm's Band, and the stress that averagely stretches in length and breadth of the band is 1.7N.

Linking part is made using the Trico warp knit fabric that nylon is 56dtex.It is transversely stretched repeatedly into the linking part is exercised The extension experiment of exhibition 10%, stretching, extension stress of the linking part in third time stretching, extension 10% is 19N.Moreover, the L4/L3 of linking part Value be 0.27.

Using elastic fabric formed aileron, the elastic fabric with 44dtex nylon and 44dtex polyurethane with And 310dtex as the polyurethane for being inserted into yarn, which goes to count corresponding to portion H using mammary areola as starting point towards center back C 15% position (being present on cup parts) have the first joint portion, the aileron using mammary areola corresponding to portion H be starting point towards the back of the body Portion center C goes to count 80% position to have the second joint portion (being present on the wing).The transversely stretching, extension of elastic fabric Stretching, extension stress when 30% is 2.70N.Moreover, the line segment Lb on aileron is formed as accounting for the 85% of chord.

Shoulder belt portion is made using woven, and in the woven, warp thread is by by a kind of following nylon of yarn and 155dtex Processing yarn by it is single it is alternate in a manner of be made into, wherein this kind of yarn be to be added the nylon of 70dtex by way of cable twisted netting twine The polyurethane of work yarn and 640dtex twist together with the yarn (gait 3.5) made, weft yarn uses the nylon of 155dtex to process Yarn.It is arranged to following such and is installed, i.e.,：At W1, width 1.0cm, thickness 2.0mm, moreover, at W2, it is wide Degree is 1.2cm, thickness 1.8mm, and at the W3 as intermediate point, width 1.8cm, thickness is 2.0cm (averga cross section areas For 27mm²).The elongated lengthwise rate in shoulder belt portion is 64% at shoulder belt central portion.

Width is sandwiched in the lower edge and rising wood of the cup of polyurethane and is the leno-marquisette woven of 2cm, and carries out mould Modeling is handled, to make leno-marquisette woven and cup be integrally formed.The vibration damping portion stretch 10% when average stretching, extension stress be 35N。

The preceding center lower end point Q3 of endpoint Q1, the endpoint Q2 of the preceding central side by cup parts in shoulder belt portion and linking part is connected Knot gets up to form triangle, and the 72% of the area of the triangle is not accounted for by the area that the composition material for making clothes of brassiere covers.

In the case of dressing the brassiere made, prevent the effectiveness in vibration suppression that breast shakes in wearing more apparent, moreover, wearing The maximum value for wearing pressure is suppressed smaller, and the absolute value of acceleration is also suppressed smaller, and comfort is also more excellent.Moreover, The preceding center lower end point P3 of endpoint P1, the endpoint P2 of the preceding central side by cup parts in shoulder belt portion and linking part is linked up into institute 72% in the area of the triangle of formation is not all covered by the composition material for making clothes of brassiere, between mammary areola also not from compared with Far, taste is also more excellent.

Embodiment 2

It is produced on the basis of the brassiere of embodiment 1 not in the brassiere in the rising wood of cup setting vibration damping portion, then implements Wearing test.

Embodiment 3

It is produced on the basis of the brassiere of embodiment 1 and the brassiere in vibration damping portion is not set in the lower edge of cup and rising wood, Then implement wearing test.

Embodiment 4

In the brassiere of embodiment 1, shoulder belt portion is made using woven, in the woven, warp thread is by by following one The nylon processing yarn of kind of yarn and 155dtex by it is single it is alternate in a manner of be made into, wherein this kind of yarn is the side by cable twisted netting twine Formula by the polyurethane of the nylon processing yarn of 70dtex and 640dtex twist together with the yarn (gait 3.5) made, weft yarn uses The nylon processing yarn of 155dtex.It is arranged to following such and is installed, i.e.,：At W1, width 1.0cm, thickness is 1.5mm, moreover, at W2, width 1.0cm, thickness 1.5mm, at the W3 as intermediate point, width 1.0cm, thickness For 1.5cm (averga cross section area 15mm²).The elongated lengthwise rate in shoulder belt portion is 68% at shoulder belt central portion.It uses The brassiere implements wearing test.

Embodiment 5

It is produced on the basis of the brassiere of embodiment 3 and the brassiere in vibration damping portion is not set in the lower edge of cup and rising wood, Then implement wearing test.

Embodiment 6

Make following brassieres：Based on the brassiere of embodiment 1, into linking part is exercised, transversely the stretching, extension of stretching, extension 10% tries repeatedly It tests, stretching, extension stress of the linking part in third time stretching, extension 10% is 19N, and the value of the L4/L3 of linking part is 0.60.Use this article Chest implements wearing test.

Embodiment 7

It is produced on the brassiere for not setting aileron on the basis of the brassiere of embodiment 1, then implements wearing test.

Comparative example 1

Linking part is made using the Trico warp knit fabric that nylon is 56dtex.It is transversely stretched repeatedly into the linking part is exercised The extension experiment of exhibition 10%, stretching, extension stress of the linking part in third time stretching, extension 10% is 5.2N.Moreover, the area of linking part I.e. the value of L4/L3 is 0.30.

Aileron is formed using elastic fabric, which has the polyurethane of the nylon and 310dtex of 78dtex, The aileron goes to count 15% position (being present on cup parts) to have corresponding to portion H using mammary areola as starting point towards center back C There is the first joint portion, which goes to count 70% position to have the corresponding to portion H using mammary areola as starting point towards center back C Two joint portions (are present on the wing).Stretching, extension stress when transversely stretching 30% of elastic fabric is 3.50N.Moreover, aileron On line segment Lb be formed as accounting for the 80% of chord.

Shoulder belt portion is made using woven, and in the woven, warp thread is by by a kind of following nylon of yarn and 155dtex Processing yarn by it is single it is alternate in a manner of be made into, wherein this kind of yarn be to be added the nylon of 70dtex by way of cable twisted netting twine The polyurethane of work yarn and 640dtex twist together with the yarn (gait 3.5) made, weft yarn uses the nylon of 155dtex to process Yarn.It is arranged to following such and is installed, i.e.,：At W1, width 1.0cm, thickness 2.0mm, moreover, at W2, it is wide Degree is 1.2cm, thickness 1.8mm, and at the W3 as intermediate point, width 1.8cm, thickness is 2.0cm (averga cross section areas For 21mm²).The elongated lengthwise rate in shoulder belt portion is 62% at shoulder belt central portion.

By use the plain weave object made of No. 40 cotton yarns that width is 2cm be stacked in polyurethane cup lower edge and Rising wood, and they are stitched together, to make the plain weave object be integrally formed with cup.The vibration damping portion is when stretching 10% Average stretching, extension stress be 170N.

The preceding center lower end point Q3 of endpoint Q1, the endpoint Q2 of the preceding central side by cup parts in shoulder belt portion and linking part is connected Knot gets up to form triangle, and the 80% of the area of the triangle is not accounted for by the area that the composition material for making clothes of brassiere covers.

In the case of dressing the brassiere made, acceleration is bigger, and shaking value is smaller, also, breast shake it is dynamic some not It is good.

Comparative example 2

It is produced on the basis of the brassiere of comparative example 1 and aileron cloth is not installed in the whole region until from cup parts to alar part Silks does not set cup vibration damping portion yet.

Shoulder belt portion is made using woven, and in the woven, warp thread is by by a kind of following nylon of yarn and 155dtex Processing yarn by it is single it is alternate in a manner of be made into, wherein this kind of yarn be to be added the nylon of 70dtex by way of cable twisted netting twine The polyurethane of work yarn and 640dtex twist together with the yarn (gait 3.5) made, weft yarn uses the nylon of 155dtex to process Yarn.It is arranged to following such and is installed, i.e.,：At W1, width 1.0cm, thickness 1.5mm, moreover, at W2, it is wide Degree is 1.0cm, thickness 1.5mm, and at the W3 as intermediate point, width 1.0cm, thickness is 1.5cm (averga cross section areas For 15mm²).The elongated lengthwise rate in shoulder belt portion is 68% at shoulder belt central portion.

Comparative example 3

It is produced on the basis of the brassiere of embodiment 1 and makes linking part using the Trico warp knit fabric that nylon is 56dtex And configure brassiere made of linking part.Into the linking part is exercised, transversely the extension experiment of stretching, extension 10%, the linking part exist repeatedly Stretching, extension stress when third time stretching, extension 10% is 5.2N.Moreover, area, that is, L4/L3 of linking part is 0.30.In addition to this, other Aspect is identical with the situation of embodiment 1.

Comparative example 4

It is produced on the basis of the brassiere of embodiment 7 and makes linking part using the Trico warp knit fabric that nylon is 56dtex And configure brassiere made of linking part.Into the linking part is exercised, transversely the extension experiment of stretching, extension 10%, the linking part exist repeatedly Stretching, extension stress when third time stretching, extension 10% is 5.2N.Moreover, area, that is, L4/L3 of linking part is 0.30.In addition to this, other The case where aspect is with embodiment 7 are identical.

Result according to examples and comparative examples is it is found that by making cup linking part have regulation stress, to linking part As fixed point, breast can be made to be close to cup in the region to cup side before cup, thereby, it is possible to reduce into Take action as when bring breast all directions acceleration.Therefore, it is possible to obtain following such brassieres：It can mitigate and be acted When rolling it is dynamic, to which comfort is excellent.

According to 1~embodiment of embodiment 3, embodiment and comparative example：By having except defined linking part, also With vibration damping portion, so as to obtain following such brassieres：The violent shaking of breast entirety can be mitigated, also, can also The subtle shaking for reducing breast can reduce sense of discomfort and corresponding rolling innervation when dressing brassiere, have higher Comfort.

Moreover, by being compared to each embodiment and comparative example 1, comparative example 2 it is found that by configuring vibration damping portion, it can Obtain following such brassieres：Wearing pressure with higher damping, and when can also reduce wearing brassiere, feel compared with Comfortably.

Table 1

8~embodiment of embodiment 11

On the basis of embodiment 1, using nylon be 78dtex and polyurethane is 470dtex stretch knit fabric (poplar Family name's modulus YR1 is 2500cN, the Young's modulus YR2=1250cN, YR1/YR2=2 of alar part) aileron portion 109 is made, by the aileron Portion 109 is stacked in brassiere main body, they are joined together to brassiere by sewing.In this case, in embodiment 8, It is 13cm to make length m1, and it is 18cm to make length m2, and it is 10% to make elongation E2, and in embodiment 9, it is 16cm to make length m1, makes length Degree m2 is 18cm, and it is in 10%, embodiment 10 to make elongation E2, and it is 18cm to make length m1, and it is 18cm to make length m2, makes elongation E2 is 10%, in embodiment 11, make length m1 be 19.5cm, make length m2 be 18cm, make elongation E2 be 10%, except this with Outside, other aspects are identical with the situation of embodiment 1, and then implement wearing test.Table 2 indicates result.

Embodiment 12

Aileron portion 109 is made using following plain weave objects, in the plain weave object, warp thread uses gathering for 84dtex Ester, weft yarn use 110dtex polyester (Young's modulus YR1 be 5000cN, the Young's modulus YR2=1250cN of alar part, YR1/YR2=4), in addition to this, the case where in terms of other with embodiment 9, makes brassiere identically, then implements wearing test. Table 2 indicates result.

Table 2

According to 8~embodiment of embodiment 12 it is found that on the basis of in the linking part for providing physical property, also have in rule The aileron portion of earnest, in particular, aileron portion and alar part embody following the description in the case of specific physical property ratio：Have It is damping, more particularly to reduce the acceleration that breast generates in cup, the wearing pressure generated in breast lower part can be inhibited, Taste is also more excellent.

Industrial availability

The present invention can recommend to be applied to commonly use brassiere as the opening portion that front has O-level.

Reference sign

100, brassiere

101, linking part

102, cup parts

103, alar part

104, upper limb high stress portion

105, lower edge high stress portion

106, length adjustment mechanism

107aS, cup side engagement portion

107bS, alar part side engagement portion

109, aileron portion

110, shoulder belt portion

111, the area not covered by cloth and silk in cup front

C, center back

H, mammary areola corresponds to portion

I, mammary areola is corresponded to the line segment linked up at portion and center back

K, the midpoint for the line segment for linking up cup lowest point

The point of contact by oxter between P1, shoulder belt portion and cup parts

The point of contact by oxter between P2, shoulder belt portion and alar part

Q1, shoulder belt portion the preceding central side by cup parts endpoint

Q2, shoulder belt portion the preceding central side by cup parts endpoint

The preceding center lower end point of Q3, linking part

R, the midpoint for the line segment for linking up the endpoint of the preceding central side by cup parts in shoulder belt portion

S, plane

T, triangle

Claims

1. a kind of brassiere, has：A pair of of cup parts；The preceding central side of the cup parts is interconnected one by linking part It rises；Alar part, it is adjacent with the oxter side of the cup parts；And shoulder belt portion, end and a pair of cup parts and the alar part phase Connection, wherein

Into the linking part is exercised, transversely the extension experiment of stretching, extension 10%, stretching, extension of the linking part when third time stretches are answered repeatedly Power is 10N~30N, moreover,

The brassiere has the more than one vibration damping chosen from the structure group comprising structure below (I)~structure (III) Portion,

Structure (I) is any one of upper limb high stress portion and lower edge high stress portion or both, and the upper limb high stress portion is along this The cup upper limb of cup parts extends, the ratio between the stretching, extension stress S2 and the stretching, extension stress S1 of cup central portion in upper limb high stress portion S2/ S1 is 2/1~400/1, which extends along the cup lower edge of the cup parts, and the stretching, extension in lower edge high stress portion is answered The ratio between power S3 and the stretching, extension stress S1 of cup central portion S3/S1 are 2/1~400/1,

Structure (III) is aileron portion, is matched in the whole region until the part a to part for the alar part from the cup parts Be placed in brassiere main body, with extended to from the mammary areola portion of correspondence of the cup parts alar part center back line segment be longest side Formula configures brassiere, and provides the plane of the normal with direction identical with the extending direction of the line segment, in this case, at this It is on line segment, correspond to portion using the mammary areola and go count 0%~25% and 50%~100% towards the center back as starting point In the plane at position, there are the joint portions between the aileron portion and the brassiere main body, moreover, the aileron portion have not with this The region of brassiere main body engagement.

2. brassiere according to claim 1, wherein

3. brassiere according to claim 1, wherein

The brassiere has the vibration damping portion of the structure (III).

4. brassiere according to claim 3, wherein

The brassiere has the vibration damping portion of the structure (I).

5. brassiere according to claim 3, wherein

The brassiere has the vibration damping portion of the structure (II).

6. brassiere according to claim 4, wherein

The brassiere has the vibration damping portion of the structure (II).

7. according to brassiere according to any one of claims 1 to 6, wherein

By the distance between the endpoint of the preceding central side by cup parts in shoulder belt portion be it is maximum in a manner of configure brassiere when, general The midpoint for the line segment that cup lowest point links up and the endpoint of the preceding central side by cup parts in shoulder belt portion linked up The line segment that the midpoint of line segment links up is line segment L3, and the line segment corresponding with the position of linking part on line segment L3 is line segment The length of L4, line segment L4 are 0.10~0.50 with the length ratio L4/L3 of line segment L3.

8. brassiere according to claim 1, wherein

Cross direction elongation E1 when the wearing in the aileron portion meets

× 100 (1) E1={ (1+E2/100) × (m2/m1) -1 }

100/YR1≤E1≤1000/YR1 (2),

1≤1000cN/inch of 100cN/inch≤σ (3),

0.7≤YR1/YR2≤3 (4)。

(cross direction elongation of brassiere main body when wherein, E2 is wearing, m1 is the length in aileron portion, moreover, m2 is brassiere main body On joint portion between length.)

9. according to brassiere according to any one of claims 1 to 8, wherein

By the distance between the endpoint of the preceding central side by cup parts in shoulder belt portion be it is maximum in a manner of configure brassiere when, by shoulder The endpoint of the preceding central side by cup parts of band portion and the preceding center lower end point of the linking part link up to form triangle, not by The ratio for the area that the area of the part of the member of formation covering of brassiere accounts for the triangle is 60% or more.

10. according to brassiere according to any one of claims 1 to 9, wherein

Maximum wearing pressure is 50hPa or less.