Abstract: A heater panel includes a face layer. A heater/dielectric layer includes a heater layer between a pair of dielectric layers. The face layer is bonded to a first one of the dielectric layers. A ballistic structure is bonded to a second one of the dielectric layers. The face layer can be bonded directly to the first one of the dielectric layers with a film adhesive. The ballistic structure can be bonded directly to the second one of the dielectric layers with a film adhesive. The ballistic structure can be configured to withstand at least a 5.56 mm bullet impact.

Abstract: A heater panel includes a face layer. A heater/dielectric layer includes a heater layer between a pair of dielectric layers. The face layer is bonded to a first one of the dielectric layers. A ballistic structure is bonded to a second one of the dielectric layers. The face layer can be bonded directly to the first one of the dielectric layers with a film adhesive. The ballistic structure can be bonded directly to the second one of the dielectric layers with a film adhesive. The ballistic structure can be configured to withstand at least a 5.56 mm bullet impact.

Abstract: A socket is described for use with a partial prosthesis of the hand. The socket includes a base layer molded to encapsulate and conform to the contours of a natural hand. The base layer has a dorsal portion and a palmar portion. The palmar portion has a distal edge positioned, in use, proximal to the transverse metacarpal arch of a natural hand, and the dorsal portion having a distal edge positioned, in use, along a transverse span along a mid-portion of the dorsum of the natural hand in an area proximal to the area of the second through fifth metacarpals of a natural hand. The palmar portion of the base layer defines a first open area around the hypo-thenar eminence and a second open area surrounding on the palmar portion the thenar eminence and extending to the radial side of the second metacarpal on the dorsal portion.

Abstract: An aircraft wing (12) comprising a fixed wing (14), a slat (16) movable relative to the fixed wing (14) between a retracted position and an extended position, electrical lines (36, 38) extending between the fixed wing (14) and an electrical system (34) on the slat (16), and a linkage (40). The linkage (40) houses the electrical lines (36, 38) and is convertible between a retracted condition when the slat (16) is in the retracted position and an extended condition when the slat (16) is in the extended position.