IMPROVEMENTS IN OR RELATING TO FABRICS

Abstract

A composite fabric including a textile support layer which has one or more support members arranged thereupon is provided, particularly for use in clothing garments for sportspersons. Each support member defines a plurality of mutually spaced support formations. Respective pairs of support formations have a flexible membrane portion extending therebetween. Each flexible membrane portion is selectively moveable between a passive configuration, in which it leaves unchanged a fluid flow passing thereover, and an active configuration, in which it initiates turbulent flow in a fluid flow passing thereover.

Claims

1. A composite fabric, for use in clothing garments for sportspersons, comprising a textile support layer having one or more support members arranged thereupon, the or each support member defining a plurality of mutually spaced support formations, respective pairs of support formations having a flexible membrane portion extending therebetween, each flexible membrane portion being selectively moveable between a passive configuration in which it leaves unchanged a fluid flow passing thereover and an active configuration in which it initiates turbulent flow in a fluid flow passing thereover.

2. A composite fabric according to claim 1 wherein one or more membrane portions is arranged to move between its passive and active configurations in response to a change in the flow characteristics of the fluid flow passing thereover.

3. A composite fabric according to claim 2 wherein one or more membrane portions is arranged to move from its passive configuration to its active configuration as the fluid flow begins to separate from the composite fabric.

4. A composite fabric according to claim 2 wherein one or more membrane portions is arranged to move from its active configuration to its passive configuration as the fluid flow begins to reattach to the composite fabric.

5. A composite fabric according to claim 1 wherein each membrane portion in its active configuration creates a perturbation in the flow path of the fluid flow passing thereover.

6. A composite fabric according to claim 5 wherein the perturbation created by one or more of the membrane portions deviates from the position of the corresponding membrane portion in its passive configuration by not more than 5 mm.

7. A composite fabric according to claim 5 wherein each membrane portion creates a perturbation by one of: adopting a convex form; adopting a concave form; and oscillating between convex and concave forms.

8. A composite fabric according to claim 1 wherein one or more of the membrane portions is elastic.

9. A composite fabric according to claim 1 wherein the membrane portions are formed from a single unitary membrane.

10. A clothing garment formed from or including a composite fabric according to claim 1.

11.-12. (canceled)

Description

[0031] There now follows a brief description of preferred embodiments of the invention, by way of non-limiting example, with reference being made to the following figures in which:

[0032] FIG. 1 shows a schematic cross-sectional view from one side of a composite fabric according to a first embodiment of the invention;

[0033] FIGS. 2(a) to 2(c) illustrate schematically respective manners in which a membrane portion forming a part of the composite fabric shown in FIG. 1 may create a perturbation; and

[0034] FIG. 3 illustrates how the drag coefficient of a sphere enveloped in the composite fabric shown in FIG. 1 varies with Reynolds number compared to other spherical bodies with differing surface configurations.

[0035] A composite fabric according to a first embodiment of the invention is designated generally by reference numeral 10, as shown in FIG. 1.

[0036] The composite fabric 10 includes a textile support layer 12 which has a plurality of discrete support members 14 arranged thereupon. The textile support layer 12 is, by way of example, formed from an elastomeric material such as spandex or elastane, which exhibits a desired degree of elasticity, although other textile materials, elastic or otherwise, may also be used. In the embodiment shown each support member 14 is an elongate, substantially straight, ridge 16 that is applied onto the textile support layer 12 in the form of a fusible component which, by way of example, is a silicone.

[0037] In other embodiments of the invention (not shown) one or more of the discrete support members may instead be an elongate, curved ridge, or a respective pillar or other support structure. Such other embodiments of the invention may also include a single, unitary support member that takes the form, for example, of a square or triangular lattice.

[0038] Such other support members may similarly be applied onto the support layer in the form of a fusible component, which could also be or include an adhesive.

[0039] Any one or more of the support members may also be integrally formed within the textile support layer, e.g. by knitting, weaving or embroidering.

[0040] In any event the or each support member, and more particularly the support members 14 shown in FIG. 1, define a plurality of mutually spaced support formations 18. The support formations 18 are uniformly spaced from one another by approximately 10 mm, although this need not necessarily be the case and may, for example range between 2 mm and 30 mm.

[0041] In addition, each of the support formations 18 extends beyond the support layer 12 by a height of approximately 0.2 mm. In further embodiments of the invention such protrusion of one or more of the support formations 18 beyond the support layer 12 may differ from 0.2 mm, and may for example instead extend beyond the support layer 12 by a height of between 0.1 mm and 4 mm.

[0042] Returning to the embodiment shown in FIG. 1, respective pairs of support formations 18 have a flexible membrane portion 20a, 20b, 20c, 20d, 20e, 20f, 20g, 20h, 20i, 20j, 20k, 20l, 20m, 20n, 20o extending therebetween. In the FIG. 1 embodiment of the invention, pairs of adjacent support formations 18 have a membrane portion 20a-20o extending therebetween, although in other embodiments of the invention one or more of the membrane portions may extend between pairs of support formations which are interposed by one or more other support formations.

[0043] Each membrane portion 20a-20o is elastic, and the plurality of elastic membrane portions 20a-20o are all formed from a single, unitary membrane 22 which lies over each of the support formations 18. The unitary membrane 22 is a textile membrane which, by way of example is formed from a spandex or elastane material. Other membranes and indeed individual membrane portions may be used, however, and such other membranes or portions thereof may or may not be elastic.

[0044] In all instances, each membrane portion 20a-20o is selectively moveable between a passive configuration, as shown in FIG. 1, in which it leaves unchanged a fluid flow 24 passing thereover, and an active configuration in which it initiates turbulent flow in the said fluid flow 24. Typically the fluid flow 24 is air, although this need not necessarily be the case.

[0045] Each membrane portion 20a-20o is arranged to move between its passive and active configurations in response to a change in the flow characteristics of the fluid flow 24 passing thereover. More particularly, each membrane portion 20a-20o is arranged to move from its passive configuration to its active configuration as the fluid flow 24 begins to separate from the composite fabric 10. In other words, each membrane portion 20a-20o will move from its passive configuration to its active configuration if the fluid flow 24 passing thereover begins to separate from the said membrane portion 20a-20o, or at least a segment of a given membrane portion 20a-20o will move into an active configuration if the fluid flow 24 immediately overhead is separating, or is about to separate from the said segment of membrane portion 20a-20o.

[0046] Moreover, each membrane portion 20a-20o is arranged to move from its active configuration to its passive configuration as the fluid flow 24 passing thereover begins to reattach to the composite fabric 10, i.e. each membrane portion 20a-20o will move from its active configuration to its passive configuration if the fluid flow 24 passing thereover begins to reattach to the said membrane portion 20a-20o, or at least a segment of a given membrane portion 20a-20o which has previously adopted an active configuration will return to a completely passive configuration if the fluid flow 24 immediately overhead is reattaching, or is about to reattach, to the said segment of membrane portion 20a-20o.

[0047] Each membrane portion 20a-20o, when in its passive configuration, lies essentially taught between the corresponding pair of support formations 18, i.e. as shown in FIG. 1.

[0048] Meanwhile, each membrane portion 20a-20o, when in its active configuration, creates a perturbation 26 in the flow path 28 of the fluid flow 24 which passes over the said membrane portion 20a-20o.

[0049] Each membrane portion 20a-20o is able to create a perturbation 26 in each of three manners, as described below.

[0050] In a first manner a given membrane portion 20a-20o creates a perturbation 26 by adopting a convex form 30, as shown schematically in FIG. 2(a).

[0051] In use, such a convex form 30 is generated by low pressure arising in the fluid flow 24 above the said given membrane portion 20a-20o as a result of the fluid flow 24 separating or being about to separate from the membrane portion 20a-20o. The convex form 30 causes a separation bubble (not shown) to form in the fluid flow 24 adjacent to the given membrane portion 20a-20o. Such a separation bubble efficiently initiates a transition to turbulent flow within the fluid flow 24. The turbulent flow within the fluid flow 24 then reattaches at a downstream portion of the composite fabric 10.

[0052] In a second manner, a given membrane portion 20a-20o creates a perturbation 26 by adopting a concave form 32, as shown schematically in FIG. 2(b).

[0053] In use, such a concave form 32 is generated as a result of the boundary layer of the fluid flow 24 separating from the membrane portion 20a-20o and thereby depressing the membrane portion 20a-20o inwards. The concave form 32 captures and holds in a controlled manner a separation bubble (not shown) which forms within the fluid flow 24. Such a separation bubble, as indicated above, efficiently initiates a transition to turbulent flow within the fluid flow 24. The turbulent flow within the fluid flow 24 then again reattaches at a downstream portion of the composite fabric 10.

[0054] In a third manner, a given membrane portion 20a-20o oscillates between the convex and concave forms 30, 32, as shown schematically in FIG. 2(c). In this regard, the main illustration in FIG. 2(c) shows a given membrane portion 20a-20o oscillating at a fundamental harmonic frequency. One or more of the membrane portions 20a-20o may, however, oscillate instead at other harmonic frequencies, e.g. as also shown schematically in FIG. 2(c).

[0055] In use, such oscillation between convex and concave forms 30, 32 arises as a consequence of the boundary layer of the fluid flow 24 beginning to separate from the said membrane portion 20a-20o and in doing so creating an instability in the membrane portion 20a-20o which causes a closed feedback vibration of the said membrane portion 20a-20o. The frequency of the vibration, i.e. oscillation, in turn gives rise to Tollmien-Schlicting waves or other instabilities which initiate turbulent flow in the fluid flow 24.

[0056] With respect to each of the three foregoing manners in which a given membrane portion 20a-20o may create a perturbation 26 when it its active configuration, the resulting perturbation 26 does not deviate from the position 34 of the corresponding membrane portion 20a-20o in its passive configuration (i.e. as shown by thin dashed line in each of FIGS. 2(a) to 2(c)) by a distance 36 of more than approximately 5 mm.

[0057] In use, the individual membrane portion 20a-20o, or group of membrane portions 20a-20o, that moves from its passive configuration to its active configuration can vary according to the characteristics of the fluid flow passing immediately over the or each membrane portion 20a-20o.

[0058] Such an ability to vary in real time which individual membrane portion 20a-20o, or group of membrane portions 20a-20o, moves into its active configuration permits the composite fabric 10 of the invention to exhibit a low drag coefficient C.sub.D irrespective of the orientation of the fluid flow 24 relative to the composite fabric 10, and more particularly irrespective of the orientation of the support members 14 within the composite fabric 10 relative to the direction of fluid flow 24.

[0059] In addition, in use the real time varying nature of the membrane portions 20a-20o which adopt an active configuration allows different areas of the composite fabric 10 to experience reduced drag at different fluid flow 24 speeds, and so the composite fabric 10 of the invention is able to exhibit a reduced overall drag coefficient C.sub.D over a wide range of Reynolds number R.sub.e.

[0060] For example, FIG. 3 illustrates how the drag coefficient C.sub.D of a sphere 60 enveloped in the composite fabric 10 of the invention varies with Reynolds number compared to other spherical bodies with differing surface configurations.

[0061] When natural, unforced transition to turbulent flow occurs on a smooth sphere 42 the drag coefficient C.sub.D drops to about 0.08 but only at a specific Reynolds number R.sub.e and then gradually increases with increasing Reynolds number R.sub.e.

[0062] A first dimpled sphere 42, such as a golf ball, has omnidirectional drag characteristics but is only able to achieve a reduction in drag coefficient C.sub.D from 0.5 to about 0.23, and only over a relatively small range of Reynolds number R.sub.e. A second dimpled sphere 44 is encumbered with similar limitations.

[0063] A first roughened sphere 46 is, like the dimpled spheres 42, 44 similarly insensitive to the direction of the fluid flow 24 passing over it. It is however able to achieve a lower drag coefficient C.sub.D than both of the dimpled spheres 42, 44 but only at a very specific Reynolds number R.sub.e. A second roughened sphere 48 is able to achieve an even lower drag coefficient C.sub.D but again, only at a very specific Reynolds number R.sub.e.

[0064] In the meantime a first tripped sphere 50, i.e. a sphere having a first trip formation arranged on the surface thereof to disrupt fluid flow thereacross, is able to achieve a lower drag coefficient C.sub.D than the first dimpled sphere 42 but it is costly in terms of lost energy and so achievable over only a short range of Reynolds number R.sub.e. A second tripped sphere 52 is similarly able to achieve a lower drag coefficient C.sub.D than the second dimpled sphere 42, but again only over a short range of Reynolds number R.sub.e. Such tripped spheres 52, 52 are also both only effective at reducing the drag coefficient when orientated in a specific manner relative to the fluid flow and so they have limited usefulness in situations where the direction of fluid flow relative to a body is likely to change over time.

[0065] In contrast to each of the above, a composite fabric sphere 60, i.e. a sphere with a surface covered by the composite fabric 10 of the invention, exhibits a low drag coefficient C.sub.D commensurate with the lowest drag coefficient achievable by natural, unforced transition to turbulent flow on a smooth sphere 42 but over a much wider range of Reynolds number R.sub.e than either the smooth sphere 42 or than is possible with any of the other surface configurations mentioned above.

[0066] The composite fabric 10 of the invention therefore enables, e.g. when incorporated into a sportswear garment, such a garment to exhibit a low drag coefficient both when worn on body parts with a range of varying diameters, such as relatively narrow wrists through to much wider torsos, and also when used at a range of different speeds, e.g. from running to tobogganing.

[0067] More particularly, modification of the support formations 18, i.e. in terms of the relative spacing, height and patterning of the or each support member 14 that defines the support formations 18 can be used to tune the low drag performance of the composite fabric 10 according to the size and shape of the body part around which it is to be used as well as the speed at which the body part will likely move, e.g. in the course of a particular sporting event.