Magnetic perimeter attachment for an aircraft flooring section
A magnetic perimeter attachment for an interior space of a vehicle, such as an aircraft or other such vehicle. The vehicle flooring section includes a magnetic tape attached to the structural floor of a vehicle and a spacer panel magnetically coupled to the magnetic tape, where the spacer panel is located on the perimeter of the vehicle flooring section. The magnetic tape includes a carrier layer having an acrylic or rubber adhesive material, which is for bonding to a structural floor panel of the vehicle. The tape also includes a magnetic material deposited in the carrier layer. The magnetic material and the adhesive material are located on opposite sides of the carrier layer.
1. A magnetic perimeter attachment system for an aircraft flooring section, comprising:
a magnetic tape attached to a structural floor of an aircraft and near a monument adjacent to an edge of the structural floor; and
a spacer panel laterally adjacent to the monument and to a flooring panel of an aircraft flooring section, wherein the spacer panel is magnetically coupled to the magnetic tape, wherein the spacer panel provides a magnetic connection between the flooring section and the structural floor and wherein the spacer panel is located on the perimeter of the aircraft flooring section.
2. The magnetic perimeter attachment system of claim 1 , wherein the magnetic tape comprises:
a carrier layer having, on one side, an acrylic or rubber adhesive which is bonded to the structural floor of the aircraft; and
a magnetic material deposited on the opposite side of the carrier layer.
3. The magnetic perimeter attachment system of claim 1 , wherein the spacer panel includes a complementary magnetic tape attached to its bottom face, wherein the complementary magnetic tape is magnetically coupled to the magnetic tape attached to the structural floor of the aircraft.
4. The magnetic perimeter attachment system of claim 1 , wherein the spacer panel includes an embedded magnetic material to be magnetically coupled to the magnetic tape attached to the structural floor of the aircraft.
5. The magnetic perimeter attachment system of claim 1 , wherein the spacer panel includes a magnetic coating applied to a lower face of the spacer panel, wherein the magnetic coating is to be magnetically coupled to the magnetic tape attached to the structural floor of the aircraft.
6. The magnetic perimeter attachment system of claim 1 , wherein the spacer panel includes, in an upper face and on an edge contiguous to a structural monument located on the perimeter of the aircraft flooring section, a first cut section that allows the spacer panel to be inserted into a recessed cavity of the structural monument.
7. The magnetic perimeter attachment system of claim 6 , wherein the upper face of the spacer panel includes:
a second cut section located on an edge contiguous to a flooring panel, wherein the second cut section is connected to the flooring panel by an adhesive material.
8. The magnetic perimeter attachment system of claim 7 , wherein the adhesive material comprises one or more of a silicone adhesive, a polymer adhesive, an acrylonitrile, an acrylic adhesive, a cyanoacrylate, an epoxy resin, an epoxy putty, an ethylene-vinyl acetate (EVA), a polyvinyl butyral (PVB), a polyvinyl acetate (PVA), a polyester resin, a polysulfide, a polyurethane, a polyvinyl alcohol, a polyvinyl chloride (PVC), a polyurethane tape, a butyl rubber tape, a neoprene adhesive, or a urethane adhesive.
9. The magnetic perimeter attachment system of claim 7 , wherein the first cut section and the second cut section are a same shape.
10. The magnetic perimeter attachment system of claim 7 , wherein the first cut section and the second cut section are a different shape.
11. The magnetic perimeter attachment system of claim 1 , wherein the spacer panel is positioned laterally adjacent to the flooring panel.
12. The magnetic perimeter attachment system of claim 1 , wherein the flooring section comprises at least one floating attachment points that allow for horizontal displacement of the floor panel caused by a movement of the aircraft.