Elastomeric gel body gasket having a substantially incompressible skeleton, a method of making and using the same
Gaskets, including aircraft gaskets, are disclosed, the gaskets having an elastomeric gel body and substantially incompressible skeletons. The bodies may be pliable and deformable and, in one example, may be comprised of a two-part chemically cured polyurethane that sets up as a gel after mixing with the web so that it is fully integral with the web and so that there is substantially no air bubbles or air pockets left in the web. The web may be a regular shaped web and made of nylon.
1. An assembly for use with an aircraft, the assembly comprising:
an aircraft base;
a workpiece for removably engaging the base; and
a gasket or gasket tape for interposition between the aircraft workpiece and the aircraft base, the gasket or gasket tape comprising:
a pliable, elastomeric gel body having an upper surface, a lower surface, and a perimeter; and
a non-metallic, non-fibrous, non-conductive, non-woven molded or extruded skeletal web having an upper surface, a lower surface, a perimeter and a multiplicity of strands meeting at and integral with a multiplicity of joints, the strands and joints defining a multiplicity of open pores;
wherein the elastomeric gel body is the same size or thicker than and substantially encapsulates the skeletal web, including filling the pores thereof, and is integral therewith;
and wherein an x and y dimension is much greater than the z (thickness) dimension;
and wherein the skeletal web is crimped.
2. The assembly in claim 1 , wherein the skeletal web is comprised of nylon.
3. The assembly of claim 1 , further including a skin.
4. The assembly of claim 3 , wherein the skin is semi-permeable by the gel of the gel body.
5. The assembly of claim 3 , wherein the skin is impermeable.
6. An assembly for use with an aircraft, the assembly comprising:
an aircraft base;
a workpiece for removably engaging the base; and
a gasket or gasket tape for interposition between the workpiece and the aircraft base, the gasket comprising:
a pliable, elastomeric gel body having an upper surface, a lower surface, and a perimeter; and
a non-metallic, non-fibrous, non-conductive, non-woven skeletal web having an upper surface, a lower surface, a perimeter and a multiplicity of strands meeting at and integral with a multiplicity of joints, the strands and joints defining a multiplicity of open pores;
wherein the elastomeric gel body is the same size or thicker than and substantially encapsulates the skeletal web, including filling the pores thereof, and is integral therewith; and
wherein the x and y dimensions are much greater than the z (thickness) dimension; and
wherein there is only a single layer of skeletal web and gel between the upper and lower surfaces of the elastomeric gel body and wherein the gasket is configured for lateral gel flow under compression between the workpiece and base, such compression in the range of about 50-500 psi, wherein such compression fails to cause substantial permanent deformation of the web.
7. The assembly of claim 6 , wherein the workpiece is a fuel access door panel.
8. The assembly of claim 6 , wherein the workpiece is an aircraft antenna.
9. The assembly of claim 6 , wherein the workpiece is an aircraft floor panel.
10. The assembly of claim 6 , wherein the body and skeletal web have similar perimeters in size and shape to that of the workpiece.
11. The assembly of claim 6 , wherein the body is a tacky polyurethane gel and has a hardness about 40-150 on cone penetrometer.
12. The assembly of claim 6 , wherein the skeletal web resists compression and exhibits structural and dimensional stability following compression at the stated psi range.
13. The assembly of claim 6 , wherein the skeletal web is comprised of nylon.
14. The assembly of claim 6 , wherein the thickness of the elastomer gel body is between 0.020 inches and 0.250 inches, and the thickness of the skeletal web is between 0.010 inches and 0.125 inches.
15. The assembly of claim 6 , wherein the multiplicity of strands include some strands in a machine direction and other strands in a cross direction, and the strands in the machine direction are thicker than the strands in the cross direction.
16. The assembly of claim 6 , wherein the joints are thicker than any of the multiplicity of strands.
17. The assembly of claim 6 , wherein the web has a tensile strength of between 10 MPa and 150 MPa.
18. The assembly of claim 6 , wherein the joint is square or rectangular in cross section.
19. The assembly of claim 6 , wherein the joint is substantially circular in cross section.
20. The assembly of claim 6 , wherein the assembly comprises a fillet seal at its edges.
21. The assembly of claim 6 , wherein the compression of the skeletal web is less than about five percent.
22. The assembly of claim 6 , wherein the compression of the skeletal web is less than one percent.
23. The assembly of claim 6 , wherein the compression of the skeletal web fails to cause the skeletal web to exceed its elastic limit.
24. The assembly of claim 6 , further including a skin.
25. The assembly of claim 24 , wherein the skin is semi-permeable by the gel of the gel body.
26. The assembly of claim 24 , wherein the skin is impermeable.