Abstract: A lightweight ballistic resistant rigid structural panel especially for use in aircraft interiors is disclosed. The rigid structural panel is made up of a core layer including a plurality of sheets of flexible, high-tensile strength fabric interleaved with a plurality of sheets of a thermal-fusible film adhesive, and a sheet of cushioning material adhered to the plurality of sheets of flexible, high-tensile strength fabric. Fiber-reinforced face skins are adhered to exterior surfaces of the panel core for structural strength and rigidity. The rigid structural panel is capable of resisting ballistic attack from handguns and like weapons, while maintaining a high degree of strength and rigidity.
Abstract: The explosion resistant cargo container includes a frame including a main section and an angled projecting section, and is formed from a plurality of support members. The frame is covered with one or more explosion resistant sheets to form the explosion resistant side panels. The explosion resistant panels comprise a plurality of layers of explosion resistant sheets. The explosion resistant panels may also include a sheet of polycarbonate, and may also include padding or insulation placed between layers of the explosion resistant sheets. The side panels and flexible door comprise one or more of explosion resistant sheets, with one or more of the sheets of the plurality of explosion resistant sheets have edges wrapped around and secured to one or more mounting strips, with the edges of the plurality of explosion resistant sheets and mounting strips being bonded together. The mounting strips are currently preferably formed of metal, such as aluminum.
Type:
Grant
Filed:
June 26, 2002
Date of Patent:
June 15, 2004
Assignee:
Telair International Incorporated
Inventors:
Solomon M. Fingerhut, Richard L. Fingerhut