dual laminate composite 121 and second dual laminate composite 122 fig2 a through 26c depict another optional aspect of the invention wherein following the lamination of a cut material to two substrate layers that is first substrate layer 30 and second substrate layer 31 the resulting dual laminate composite material is mechanically stretched along one or two horizontal axis co planar with the substrate layers the purpose behind this optional procedure is to cause the plurality of resilient elements bonded to the substrate layers to move apart from each other and thereby break any residual or excess glue or adhesive such as traces of first joining element 3 or second joining element 4 that may have seeped out from the surface of the resilient materials and seeped into the various material cutting lines defining the resilient elements partially bonding the resilient elements to each other by way of example only and without limitations fig2 a depicts a double laminate composite which may be in this example first dual laminate composite 121 or second dual laminate composite 122 fabricated by means of the pressing or heat pressing operation described above fig2 b depicts a partial cutaway view of the double laminate composite fig2 c and 24d depict lateral and side views of the same double laminate composite fig2 b 24 c and 24 d also depict the individual resilient elements which may be in this example first resilient element 15 a or third resilient element.