Abstract A composition is disclosed for forming an EMI shielding gasket for instalion against a metal object, such as an aluminum frame member of an aircraft, wherein the composition is comprised of a mixture of a prepolymer composition of a flexible polyurethane material, a sacrificial metallic material which provides electrical conductivity and anodic protection against corrosion of the metal object, and a curing agent for curing the prepolymer composition. The sacrificial metallic material can be a metal salt selected from the group consisting of water soluble zinc and cadmium salts. Water can also be present to serve two functions, as a curing agent for the polyurethane and as a foaming agent, producing carbon dioxide. A method is also providing for installing an EMI shielding gasket on an aircraft between a graphite skin panel and a metal frame member. The composition for forming the EMI shielding gasket on a metal surface can also include an agent that cleans the metal surface to which the gasket is applied.
A method of installing a removable EMI shielding gasket between a graphite skin panel and a metallic frame component in an aircraft, comprising the steps of: loosening means for connecting the graphite skin panel and the metallic frame component; separating the graphite skin panel and the metallic frame component to provide a space therebetween; introducing into said space a liquid composition capable of polymerizing to form a gasket, said liquid composition comprising: a prepolymer composition of a polyurethane present in a range of from 75-92% by weight, from 2 to 10% by weight of zinc chloride, and from 6 to 15% by weight of water; permitting the composition to at least partially polymerize whereby a gasket is formed between the graphite skin panel the metallic frame component, said gasket being removable from said metallic frame component by peeling.
Claim 2
Independent Claim
138 words
A method of installing a removable EMI shielding gasket between a graphite skin panel and a metallic frame component in an aircraft, comprising the steps of: loosening means for connecting the graphite skin panel and the metallic frame component; separating the graphite skin panel and the metallic frame component to provide a space therebetween; introducing into said space a liquid composition capable of polymerizing to form a gasket, said liquid composition comprising: a prepolymer composition of a polyurethane present in a range of from 75-92% by weight, from 2 to 10% by weight of zinc chloride, and from 6 to 15% by weight of water; permitting the composition to at least partially polymerize whereby a gasket is formed between the graphite skin panel the metallic frame component, said gasket being removable from said metallic frame component by peeling.
Claim 3
Dependent Claim
25 words
The method described in claim 1 comprising the additional step of tightening the means for connecting the graphite skin panel and the metallic frame component.
Claim 4
Dependent Claim
15 words
The method described in claim 1 wherein the metallic frame component is made from aluminum.