CN201199933Y - Sheet-shaped stable side-pulling structure of brassiere - Google Patents

Sheet-shaped stable side-pulling structure of brassiere Download PDF

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Publication number
CN201199933Y
CN201199933Y CNU2008201140574U CN200820114057U CN201199933Y CN 201199933 Y CN201199933 Y CN 201199933Y CN U2008201140574 U CNU2008201140574 U CN U2008201140574U CN 200820114057 U CN200820114057 U CN 200820114057U CN 201199933 Y CN201199933 Y CN 201199933Y
Authority
CN
China
Prior art keywords
lateral
lateral margin
top flat
brassiere
cup
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CNU2008201140574U
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Chinese (zh)
Inventor
黄玉茹
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MODE MARIE INTERNATIONAL CO Ltd
Original Assignee
MODE MARIE INTERNATIONAL CO Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by MODE MARIE INTERNATIONAL CO Ltd filed Critical MODE MARIE INTERNATIONAL CO Ltd
Priority to CNU2008201140574U priority Critical patent/CN201199933Y/en
Application granted granted Critical
Publication of CN201199933Y publication Critical patent/CN201199933Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model provides a bra laminated stable side-push structure. The bra is provided with two cups, a vest is arranged at one side of each cup, a side seam is arranged at the other side of the cup, and the cup comprises a stable side-push structure with a stabilizing part and a side-push part; the stabilizing part is provided with an apical plate, the apical plate is arranged at the lower side of the cup, the side-push part is provided with a lateral plate, the lateral plate is arranged at one side of the cup, the lateral plate of the side-push part is combined with the apical plate of the stabilizing part, and an included angle is formed between the lateral plate and the apical plate; by adopting the structure, the bra can ensure that the breasts are stably supported high and centralized from down to up and from outside to inside through the strap-shaped thickness generated by the stabilizing part and the side-push part.

Description

The brassiere sheet is stablized the thruster structure
Technical field
The utility model is about a kind of brassiere, is meant that especially a kind of brassiere sheet stablizes the thruster structure.
Background technology
Liking to be beautiful is people's nature, yet the women promptly is beautiful Crazy Talk, in numerous commodity at women's release, brassiere promptly is that the women pursues one of most popular commodity of inner beauty, general brassiere drags chest except providing the women to be used for holding, reduces the heavy burdens, and the coating that is close to skin more provides moulding of chest profile external form, except stressing comfort level, has more increased women's confidence.
Learn according to further analysis of present market Bra structure of all kinds, still have following disappearance:
1. common brassiere is in the inboard design activity formula of cup liner, provide user's demand of being looked to adjust liner, but the user is when walking about, chest also can rock along with the rhythm of health, make the constantly displacement of movable liner along with rocking, not only can't effectively stablize rocking of chest, more order this movable liner can't provide chest from bottom to top, pushing and pressing from outside to inside, this brassiere is lost concentrate to hold in the palm high effectiveness;
2. common brassiere is in the inboard design activity formula of cup liner, under not located, cause the displacement arbitrarily between this brassiere and chest of this movable liner, make this movable liner cause extruding improperly to chest, make chest deflection produce sense of discomfort easily, the sensation of the comfortable wearing of women can't be provided, in the course of time will not favored by the consumer, reduce the sales volume of this brassiere relatively.
In view of this, this case designer thinks funiculus through detailed, satisfies with for many years experience and is designed, and through inquiring into and study sampling test in many ways, and repeatedly revises improvement, develops a kind of brassiere sheet and stablizes the thruster structure eventually.
Summary of the invention
The utility model is that a kind of brassiere sheet is stablized the thruster structure, and its purpose is to stablize moulding to chest and thruster is concentrated by stabilizers and thruster portion.
For reaching above-mentioned purpose, the technical scheme that the utility model adopted is:. a kind of brassiere sheet is stablized the thruster structure, and this brassiere has two cups, and this cup one side is provided with a ridge heart, and opposite side is provided with a side of body limit, and this cup comprises:
One stablizes the thruster structure, comprises a stabilizers and a thruster portion; Wherein, this stabilizers has a top flat, and this top flat is located at this cup downside; This thruster portion has a lateral plate, and this lateral plate is located at this cup one side, and this lateral plate one lateral margin stitches respectively on the side of body limit of the lower edge of being located at this cup and this cup; Lateral plate one side of this thruster portion changes mutually with top flat one side of this stabilizers or engages, and another lateral margin of this lateral plate and another lateral margin of this top flat is intersected form an angle.
The top flat of aforementioned this stabilizers is the integrated lunate shape structure of non-resilient material, and the lateral plate of this thruster portion is the lunate shape structure of non-resilient material.
The top flat of aforementioned this stabilizers is equipped with first lateral margin and second lateral margin, and first lateral margin seam of this top flat is located on the lower edge of this cup; And the lateral plate of this thruster portion is equipped with first lateral margin, second lateral margin and the 3rd lateral margin, first lateral margin seam of this lateral plate is located at the side of body limit place of lower edge one side of this cup near this brassiere, second lateral margin seam of this lateral plate is located on the side of body limit of this brassiere, and the 3rd lateral margin of this lateral plate and second lateral margin of this top flat intersect formation one angle.
First lateral margin of this top flat is that the camber line and second lateral margin are straight line, and first lateral margin of this lateral plate is a camber line, and second lateral margin of this lateral plate and the 3rd lateral margin are straight line.
The angle degree of the second lateral margin formation of the 3rd lateral margin of aforementioned this lateral plate and this top flat is obtuse angle or acute angle or right angle.
The lateral plate of this thruster portion repeatedly places on the top flat of this stabilizers.
The top flat of this stabilizers repeatedly places on the lateral plate of this thruster portion.
The top flat of aforementioned this stabilizers is equipped with first lateral margin and second lateral margin, and first lateral margin seam of this top flat is located on the lower edge of this cup; And the lateral plate of this thruster portion is equipped with first lateral margin, second lateral margin and the 3rd lateral margin, first lateral margin seam of this lateral plate is located at the side of body limit place of lower edge one side of this cup near this brassiere, and first lateral margin of this lateral plate engages with first lateral margin of this top flat, second lateral margin seam of this lateral plate is located on the side of body limit of this brassiere, and the 3rd lateral margin of this lateral plate engages formation one angle with second lateral margin of this top flat.
Can obtain following effect by aforementioned further analysis:
1. top flat and the lateral plate of the thruster portion sheet thickness that produce of this brassiere by stabilizers when the user avoids rocking the displacement that causes when walking about, makes this brassiere keep the chest type from bottom to top, from outside to inside, allows user's chest concentrate holder high more;
2. top flat and the lateral plate of the thruster portion sheet thickness that produce of this brassiere by stabilizers, when the user not only effectively is positioned between this brassiere and the chest when walking about, avoid displacement arbitrarily that chest is caused extruding improperly, the sensation of the comfortable wearing of women is provided, improve the user and use wish, and then promote the economic benefit of this brassiere.
The technology that the utility model adopted, means and other effect are lifted a preferred embodiment now, and cooperate diagram to be described in detail as follows.
Description of drawings
Fig. 1 is first an embodiment of the present utility model schematic diagram one repeatedly mutually.
Fig. 2 is first an embodiment of the present utility model schematic diagram two repeatedly mutually.
Fig. 3 is the second embodiment floor map of the present utility model.
[primary clustering symbol description]
[the utility model]
Brassiere A cup A1
Ridge heart A2 coerces limit A3
Stablize thruster structure 10
Stabilizers 11 top flats 111
First lateral margin, 112 second lateral margins 113
Thruster portion 12 lateral plates 121
First lateral margin, 122 second lateral margins 123
The 3rd lateral margin 124
Angle theta
Stablize thruster structure 20
Stabilizers 21 top flats 211
First lateral margin, 212 second lateral margins 213
Thruster portion 22 lateral plates 221
First lateral margin, 222 second lateral margins 223
The 3rd lateral margin 224
Angle theta
The specific embodiment
Embodiment 1
The utility model brassiere A (seeing also Figure 1 and Figure 2) has two cup A1, this cup A1 one side is provided with a ridge heart A2, this cup A1 opposite side is provided with a side of body limit A3, should stablize thruster structure 10 is the cup A1 inboards that are arranged at this brassiere A, and this cup A1 inboard is meant that relative user's chest pastes to the place;
Should stablize thruster structure 10 and comprise a stabilizers 11 and a thruster portion 12;
This stabilizers 11 has a top flat 111, this top flat 111 is one-body molded by non-resilient material, this top flat 111 is a lunate shape, this top flat 111 is located at this cup A1 downside, and this top flat 111 is equipped with first lateral margin 112 and second lateral margin 113, and this first lateral margin 112 is a camber line, this second lateral margin 113 is a straight line, first lateral margin, 112 seams of this top flat 111 are located on the lower edge of this cup A1, make the ridge heart A2 of adjacent this brassiere A of this top flat 111 Shu end, the side of body limit A3 of adjacent this brassiere of other end A;
This thruster portion 12 has a lateral plate 121, this lateral plate 121 is one-body molded by non-resilient material, this lateral plate 121 is a lunate shape, this lateral plate 121 is located at this cup A1 one side, this lateral plate 121 is equipped with first lateral margin 122, second lateral margin 123 and the 3rd lateral margin 124, this first lateral margin 122 is a camber line, this second lateral margin 123 is all straight line with the 3rd lateral margin 124, first lateral margin, 122 seams of this lateral plate 121 are located at the side of body limit A3 place of lower edge one side of this cup A1 near this brassiere A, second lateral margin, 123 seams of this lateral plate 121 are located on the side of body limit A3 of this brassiere A, make the lateral plate 121 of this thruster portion 12 partly change mutually with the top flat 111 of this stabilizers 11 by aforementioned structure, make second lateral margin, the 113 crossing angle theta that form of the 3rd lateral margin 124 with this top flat 111 of this lateral plate 121, aforementioned angle can be the obtuse angle, acute angle or right angle, the top flat 111 of aforementioned this stabilizers 11 (seeing also shown in Figure 1) can repeatedly place on the lateral plate 121 of this thruster portion 12, or the lateral plate 121 of this thruster portion 12 (seeing also shown in Figure 2) can repeatedly place on the top flat 111 of this stabilizers 11.
Embodiment 2
The utility model brassiere A (seeing also shown in Figure 3) has two cup A1, this cup A1 one side is provided with a ridge heart A2, this cup A1 opposite side is provided with a side of body limit A3, and this stable thruster structure 20 is the cup A1 inboards that are arranged at this brassiere A, and this cup A1 inboard is meant that relative user's chest pastes to the place;
Should stablize thruster structure 20 an one-body molded stabilizers 21 and thruster portions 22, this stabilizers 21 is all non-resilient material with this thruster portion 22;
This stabilizers 21 has a top flat 211, this top flat 211 is a lunate shape, this top flat 211 is located at this cup A1 downside, this top flat 211 is equipped with first lateral margin 212 and second lateral margin 213, this first lateral margin 212 is a camber line, and this second lateral margin 213 is a straight line, and first lateral margin, 212 seams of this top flat 211 are located on the lower edge of this cup A1, make the ridge heart A2 of adjacent this brassiere of these top flat 211 1 ends A, the side of body limit A3 of adjacent this brassiere of other end A;
This thruster portion 22 has a lateral plate 221, this lateral plate 221 is a lunate shape, this lateral plate 221 is located at this cup A1 one side, this lateral plate 221 is equipped with first lateral margin 222, second lateral margin 223 and the 3rd lateral margin 224, this first lateral margin 222 is a camber line, this second lateral margin 223 is all straight line with the 3rd lateral margin 224, first lateral margin, 222 seams of this lateral plate 221 are located at the side of body limit A3 place of lower edge one side of this cup A1 near this brassiere A, and first lateral margin 222 of this lateral plate 221 engages with first lateral margin 212 of this top flat 211 and forms a curved arc, second lateral margin, 223 seams of this lateral plate 221 are located on the side of body limit A3 of this brassiere A, and the 3rd lateral margin 224 of this lateral plate 221 engages with second lateral margin 213 of this top flat 211 and forms an angle theta, and aforementioned angle can be the obtuse angle, acute angle or right angle.
The sheet thickness that produced of stabilizers and the thruster portion of the cup of this brassiere by this stable thruster structure in sum, thickness stablizes that chest is avoided rocking and from top to bottom holder from outside to inside is high concentrates by this.For the women provides the brassiere of comfortable wearing, improve the user and use wish, and then increase economic efficiency.

Claims (7)

1. a brassiere sheet is stablized the thruster structure, and this brassiere has two cups, and this cup one side is provided with a ridge heart, and opposite side is provided with a side of body limit, it is characterized in that this cup comprises:
One stablizes the thruster structure, comprises a stabilizers and a thruster portion; Wherein, this stabilizers has a top flat, and this top flat is located at this cup downside; This thruster portion has a lateral plate, and this lateral plate is located at this cup one side, and this lateral plate one lateral margin stitches respectively on the side of body limit of the lower edge of being located at this cup and this cup; Lateral plate one side of this thruster portion changes mutually with top flat one side of this stabilizers or engages, and another lateral margin of this lateral plate and another lateral margin of this top flat is intersected form an angle.
2. brassiere sheet according to claim 1 is stablized the thruster structure, it is characterized in that, the top flat of this stabilizers is the integrated lunate shape structure of non-resilient material, and the lateral plate of this thruster portion is the lunate shape structure of non-resilient material.
3. brassiere sheet according to claim 1 is stablized the thruster structure, it is characterized in that:
The top flat of this stabilizers is equipped with first lateral margin and second lateral margin, and first lateral margin seam of this top flat is located on the lower edge of this cup; And
The lateral plate of this thruster portion is equipped with first lateral margin, second lateral margin and the 3rd lateral margin, first lateral margin seam of this lateral plate is located at the side of body limit place of lower edge one side of this cup near this brassiere, second lateral margin seam of this lateral plate is located on the side of body limit of this brassiere, and the 3rd lateral margin of this lateral plate and second lateral margin of this top flat intersect formation one angle.
4 brassiere sheets according to claim 3 are stablized the thruster structure, it is characterized in that, first lateral margin of this top flat is that the camber line and second lateral margin are straight line, and first lateral margin of this lateral plate is a camber line, and second lateral margin of this lateral plate and the 3rd lateral margin are straight line.
5. brassiere sheet according to claim 3 is stablized the thruster structure, it is characterized in that, the angle degree of the second lateral margin formation of the 3rd lateral margin of this lateral plate and this top flat is obtuse angle or acute angle or right angle.
6. brassiere sheet according to claim 3 is stablized the thruster structure, it is characterized in that, the lateral plate of this thruster portion repeatedly places on the top flat of this stabilizers.
7. brassiere sheet according to claim 3 is stablized the thruster structure, it is characterized in that, the top flat of this stabilizers repeatedly places on the lateral plate of this thruster portion.
8. brassiere sheet according to claim 1 is stablized the thruster structure, it is characterized in that:
The top flat of this stabilizers is equipped with first lateral margin and second lateral margin, and first lateral margin seam of this top flat is located on the lower edge of this cup; And the lateral plate of this thruster portion is equipped with first lateral margin, second lateral margin and the 3rd lateral margin, first lateral margin seam of this lateral plate is located at the side of body limit place of lower edge one side of this cup near this brassiere, and first lateral margin of this lateral plate engages with first lateral margin of this top flat, second lateral margin seam of this lateral plate is located on the side of body limit of this brassiere, and the 3rd lateral margin of this lateral plate engages formation one angle with second lateral margin of this top flat.
CNU2008201140574U 2008-05-06 2008-05-06 Sheet-shaped stable side-pulling structure of brassiere Expired - Fee Related CN201199933Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNU2008201140574U CN201199933Y (en) 2008-05-06 2008-05-06 Sheet-shaped stable side-pulling structure of brassiere

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNU2008201140574U CN201199933Y (en) 2008-05-06 2008-05-06 Sheet-shaped stable side-pulling structure of brassiere

Publications (1)

Publication Number Publication Date
CN201199933Y true CN201199933Y (en) 2009-03-04

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Family Applications (1)

Application Number Title Priority Date Filing Date
CNU2008201140574U Expired - Fee Related CN201199933Y (en) 2008-05-06 2008-05-06 Sheet-shaped stable side-pulling structure of brassiere

Country Status (1)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2477390A (en) * 2010-01-27 2011-08-03 Mjm Internat Ltd Foundation garments
CN104886791A (en) * 2015-06-18 2015-09-09 张植强 3T intelligent wearable bra

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2477390A (en) * 2010-01-27 2011-08-03 Mjm Internat Ltd Foundation garments
CN104886791A (en) * 2015-06-18 2015-09-09 张植强 3T intelligent wearable bra
CN104886791B (en) * 2015-06-18 2017-01-25 张植强 Intelligent wearable bra

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C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20090304

Termination date: 20140506