Abstract: One embodiment of a topper for a bed includes a liner assembly 40 having a top liner 42, a bottom liner 44 and a slip liner 70 underneath the bottom liner. The slip liner is of relatively lower friction than the top liner. An apron 62, with openings 76 therein, extends from the perimeter of the liners. Another embodiment includes a liner assembly having a top liner, a bottom liner and a slip liner underneath the bottom liner. The slip liner is of relatively lower friction than the top liner. Bridge straps 98, or 98? having a working length of at least the width of a host mattress minus the arm length of a fifth percentile female extend from the liner assembly.

Abstract: One embodiment of a topper for a bed includes a liner assembly 40 having a top liner 42, a bottom liner 44 and a slip liner 70 underneath the bottom liner. The slip liner is of relatively lower friction than the top liner. An apron 62, with openings 76 therein, extends from the perimeter of the liners. Another embodiment includes a liner assembly having a top liner, a bottom liner and a slip liner underneath the bottom liner. The slip liner is of relatively lower friction than the top liner. Bridge straps 98, or 98? having a working length of at least the width of a host mattress minus the arm length of a fifth percentile female extend from the liner assembly.

Abstract: An occupant transfer device 34 for use on a host mattress 20 having a top side 22 and a flank 24 is in the form of a fitted sheet. The device has a top 36 for covering the top side of the mattress and a skirt 38 extending from the top. The top and skirt each have an occupant side 40, 44 and a mattress side 42, 46. Substantially all of the mattress side of the top exhibits relatively low friction; the occupant side of at least the top exhibits relatively higher friction.

Abstract: A system for fabricating a free form structure of a composite material including carbon nanotubes. The system includes a discharge assembly and a composite formation device operatively linked with the discharge assembly. The discharge assembly dispenses a fusing agent such as for example a high energy density emission, a laser emission or a particle beam emission. The composite formation device includes a composite generator and an arranger in operative engagement with a composite generator. The composite generator engages with the fusing agent so as to create a composite nodal element. The composite nodal element includes a matrix and a multiplicity of fibers formed of carbon nanotubes dispersed throughout the matrix. The arranger positions one node relative to another to define the free form structure.

Abstract: A structure arrangement and method for the protection of a host system against an impacting ballistic element and for providing ease of mobility. The structure arrangement includes a composite. The composite includes a matrix and a multiplicity of single-walled carbon nanotubes. The single-walled carbon nanotubes are arranged with respect to the matrix so as to define an array for engagement with an impacting ballistic element.