The present invention relates to a brassiere. More particularly this invention concerns a back closure or fastener for a brassiere.
A standard brassiere comprises a pair of rearwardly open cups adapted to fit over the wearer's breasts and having inner edges that are connected together and outer edges from which extend wing straps that pass under the wearer's arms and around to the wearer's back where they overlay and are releasably joined together at a closure. A strap normally extends from the top of each cup over the respective shoulder of the wearer and is connected at the wearer's back to a top edge of the respective wing.
The standard closure is formed as a plurality of horizontally spaced vertical rows of eyes provided on an outer or back face of an end of one of the wings and a complementary vertical row of hooks on a front or inner face of the end of the other of the wings. The hooks are engaged in the eyes of one of the rows to fasten the two wing ends together. For comfort, the wings are typically made of an elastic textile, but the ends carrying the hooks and eyes are somewhat stiffer.
While the standard hook/eye closure is effective, it has several problems. The metallic hooks are themselves hard and can dig into the back of the wearer and get caught on other garments when the brassiere is laundered. The closure is also bulky so that it can be seen underneath tight clothing, creating an unattractive bump in the middle of the wearer's back. Finally, when longitudinal stress is applied pulling the two wing ends apart, the entire closure can curl, projecting out at its upper and lower edges and also at the outer edge of the back. Such curling deformation increases with tension and makes the already existing unattractive bump in the middle of the wearer's back even bigger.
Manufacture of the closure from various elements involves several assembly and fastening steps that increase the cost of the closure. They are typically stitched together and it is very difficult to provide stitching that perfectly matches the textile elements of the fastener, normally contrasting somewhat when the garment is new and always contrasting after some use.
It is therefore an object of the present invention to provide an improved brassiere back closure.
Another object is the provision of such an improved brassiere back closure that overcomes the above-given disadvantages, in particular that is extremely flat so that it can be worn under tight clothing without being visible, and that does not curl outward when the wings are tensioned.
A further object is to provide an improved and simplified method of making such a closure, one that in particular avoids the use of unattractive stitching.
A closure for connection between ends of two back wings of a brassiere has according to the invention an inelastic textile patch having a back face turned away from a wearer of the brassiere and an opposite front face. The patch is attached to the end of one of the wings and carries a plurality of transversely extending and longitudinally spaced rows each having at least two transversely spaced first closure elements made of plastic on the back face. A flat body has an inner end attached to the end of the other of the wings, an opposite outer end, a front face at least partially overlapping at the outer end the back face of the patch, and a back face opposite the body front face. Respective plastic second closure elements generally complementary to and matable with the first closure elements are fixed to the body front face at the outer end so as to align with and interfit with the first closure elements. A transversely rigid bar on or forming part of the body prevents transverse relative movement of the second closure elements and bending of the body at the second closure elements.
Such a closure can be made extremely thin measured front to back, in fact as thin as 4 mm, which is considerably thinner than the 6 mm of a standard closure. What is more, the construction is such that tension exerted on it by the wings does not cause it to curl or twist back, but in fact simply makes it flatter, so that it never presents an unattractive bump, even if worn, for instance, under a snug tee shirt. This closure can be wholly made without stitching, that is by welding, normally ultrasonically, so that there is never the problem of unattractive contrasting stitching.
The first closure elements are female and U-shaped and the second closure elements are male. They are both wholly made of plastic so as not to snag, for instance, in the laundry. What is more, such completely nonmetallic construction is quite simple and cheap, and avoids some of the skin-sensitivity and allergy problems of metallic parts.
The patch according to the invention is formed by congruous front and back textile layers and the first closure elements each include a front part sandwiched between the layers, a back part matable with a respective one of the second closure elements, and a peg or web extending through the back layer between the respective front and back parts. The pegs or webs can be formed integrally with the respective front and back parts or they can be formed integrally with one of the respective front and back parts and ultrasonically welded to the other of the respective front and back parts.
Each of the layers is generally rectangular and the closure further has ultrasonic welds extending around at least three sides of the layers and bonding same together immediately inward of outer edges thereof. These welds, according to a particularly advantageous form of the invention, only extend around the three sides and the layers are separate at a fourth side. The respective wing end is received between and fastened to the layers at the fourth side. Of course one or both of the layers can also in fact be formed as an integral part of the brassiere wing if the fastener is to be manufactured with the undergarment.
In accordance with the invention transverse bar welds are formed between the rows of first closure elements. These prevent the closure from curling and maintain an accurate spacing between the first closure elements.
The flat body according to the invention can also unitarily formed of plastic with the second closure elements and rigid bar. In this case at least one flexible textile flap is secured to the rigid bar and attached to the respective wing end, or more particularly two such textile flaps sandwich and are welded to the bar and also sandwich and are attached to the respective wing end.
The method according to the invention comprises the steps of fixing a plurality of first closure elements made of plastic to a front face of an inelastic textile patch having a back face turned away from a wearer of the brassiere and an opposite front face with the first closure elements are arrayed in a plurality of transversely extending and longitudinally spaced rows on the back face and also providing a flat body having an inner end attached to the end of the other of the wings and an opposite outer end and a front face at least partially overlapping the back face of the patch at the outer end and a back face opposite the body front face. Respective plastic second closure elements generally complementary to the first closure elements are fixed to the body front face at the outer end so as to align with and interfit with the first closure elements. A transversely rigid bar is formed on or as part of the body so as to prevent transverse relative movement of the second closure elements and bending of the body at the second closure elements.
As described above, the patch is formed by congruous front and back textile layers and the first closure elements each include a front part sandwiched between the layers, a back part matable with a respective one of the second closure elements, and a peg or web extending through the back layer between the respective front and back parts. These front and back parts can be unitarily formed with each other, with the pegs or web, and with the bar in a single shot by injection molding, or alternately the pegs or webs are formed integrally with one of the respective front and back parts and are welded to the other of the respective front and back parts.
The above and other objects, features, and advantages will become more readily apparent from the following description, reference being made to the accompanying drawing in which:
As seen in
The female part 10 is formed by front and back layers 11a and 11b of which at least one, here both, is made of a nonstretch textile, typically a tricot knit microfiber. These layers 11a and 11b are bonded together along their longitudinal edges and outer end at a U-shaped weld 11c. In addition crosswise welds 11d are longitudinally spaced along the ultrasonically welded-together layers 11a and 11b within the area defined by the weld 11c to further stabilize the assembly by eliminating stretch. The U-shaped edge weld 11c ends short of the inner ends of the layers 11a and 11b and the innermost crosswise weld 11d also is spaced outward from this inner end so that the two layers 11a and 11b are separate at the inner end of the female part 11, forming fastening lips. This allows the two layers 11a and 11b to be sandwiched to opposite inner and outer faces of the respective wing W and fastened thereto by welding or stitching in a manner providing a solid anchoring and smooth joint.
Three rows of two female butterfly elements 12 are secured to the back face of the back layer 11b in longitudinally spaced transversely extending rows. In principal each row could have more than two such elements 12 for brassieres with larger cup sizes, but in practice as described below it is often only necessary to increase the transverse spacing of the two elements 12, not the number, with an increase in the transverse dimension of the fastener to match wider wings W.
Each female element 12 comprises as better shown in
The male part 20 as better shown in
It would also be possible to make a system where the flaps 20a and 20b were not a single piece, and one of the pieces is made large to cover the entire back or outer face of the plastic part 20d so that nothing but textile is seen from the rear.
The front face of the outer part 20c is formed with a pair of hook elements 20h each having an enlarged head 20i and an inwardly extending ridge 20j. The heads 20i can fit underneath the overhangs 12e to lock the parts 10 and 20 together against separation in any direction but toward each other, that is by moving the part 20 in the direction of the “SHIFT” arrow of the indicia 20g. The ridges 20j that are inward of the heads 20i serve to guide the heads 20i into position by sliding between the arms 12c of the parts 12a.
The female part 10 of this closure is made as shown in
In a first step shown in
Then as shown in
In a final step an edge 11e is trimmed off the blanks 11a′ and 11b′ to turn them into the layers 11a and 11b. This trimming is done cold, immediately adjacent or slightly outside the ultrasonic weld 12c so that, as the fabric of the layers 11a and 11b frays slightly with use and laundering a soft edge is left.
The embodiment of
More particularly, the male part 30 here is not formed of two pieces, namely the textile element shown in
The blank 30b′ is then as shown in
Then as shown in
Finally a cold cut is formed around the weld 30j, that is spaced slightly outward from it, to cut off an edge 30m to form front and back layers 30a and 30b with a soft edge and a pair of lips between which the respective wing W can be anchored.
The female part of the second embodiment is formed as shown in
More particularly as shown in
The blank 40b′ is then, like the blank 30b′, clamped between two die halves into which plastic is injected to form parts 50a and 50b essentially identical to the parts 12a and 12b, except that they are unitarily formed with each other and connected together by tiny integral pegs extending though the holes 40c. This is shown in
The steps shown at 6E and 6F are identical to those of