Elastic ground plane

Abstract
An elastic ground plane (50) has an environmental coating (58) attached to a surface of a fabric (54) having a plurality of fibers. A conductive substance (56) is applied to the fabric (54) to coat the fabric (54).
Description




FIELD OF THE INVENTION




The present invention relates generally to the field of stretchable fabrics and more particularly to an elastic ground plane and method.




BACKGROUND OF THE INVENTION




Continuous moldline technology using reinforced elastomers presents an opportunity to improve upon many of the performance characteristics of aircraft and missiles.

FIG. 1

shows a side view of a rod reinforced elastomer of the prior art.

FIG. 2

is a top view of the rod reinforced elastomer of FIG.


1


. The rod reinforced elastomer


10


has a pair of rod blocks


12


. A plurality of rods


14


anchored to one of the pair of rod blocks


12


slide inside an elastomer panel


16


. The rod reinforced elastomer


10


is capable of both elongation and deflection, as shown in FIG.


3


. The rod reinforced elastomer has resting length


22


that can be stretched to an elongated length


24


and deflected a distance


26


. These products can be used in applications such as control surfaces and in expandable bays to provide cleaner airflow and reduced drag. However, these products so far have been limited to nonmetallic elastomeric compounds that provide little to no protection against electromagnetic interference (EMI). EMI can cause aircraft instruments to malfunction and can result in navigational errors and even the loss of the aircraft.




Conventional EMI shields have been designed as highly conductive metal strips, sprays, and panels that do not possess the ability to flex or elongate repeatedly without material degradation. Recent advances have produced foils that allow a continuous metallic surface with the ability to flex to various shapes. Unfortunately, these foils are limited to applications where elongation is less 10%.




Thus there exists a need for a material that can easily and significantly elongate in all directions, is highly conductive in all states of elongation, can withstand repeated elongations with no degradation in shielding effectiveness or material properties, is thin and light weight, and which is tough enough to withstand severe aerospace environments.




SUMMARY OF THE INVENTION




An elastic ground plane that overcomes these and other problems has an environmental coating attached to a surface of a fabric having a plurality of fibers. A conductive substance is applied to the fabric to coat the fabric.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a side view of a prior art rod reinforced elastomer;





FIG. 2

is a top view of the rod reinforced elastomer of

FIG. 1

;





FIG. 3

is a side view of the rod reinforced elastomer of

FIG. 1

in an elongated and deflected state;





FIG. 4

is a side view of an embodiment of an elastic ground plane;





FIG. 5

is a side view of another embodiment of the elastic ground plane; and





FIG. 6

is a side view of another embodiment of the elastic ground plane.











DETAILED DESCRIPTION OF THE DRAWINGS




An embodiment of an elastic ground plane (elastic conductive material)


50


attached to a surface


52


is shown in FIG.


4


. The surface


52


could be the rod reinforced elastomer discussed above. Alternatively, the surface could be any surface needing EMI shielding, particularly any surface that tends to stretch or elongate. The elastic ground plane


50


has a fabric


54


containing a plurality of fibers. In one embodiment the fabric is a warp knit fabric (warp knit style weave) made from polyamide NYLON fibers. In addition the fabric may contain a small amount of elastic polyurethane fiber (e.g., approximately 10%). The polyurethane or other elastic fiber assists in the recovery of the material after stretching. Note that the invention is not limited to NYLON or to warp knit weave as other materials and weaves are available. For instance, tubular knit weaves or other weaves that permit reversible elongation without permanent deformation or fabric damage can be used and higher temperature resistant materials such as super polyamide, glass, and quartz fibers can be knit when necessary for increased thermal performance. The fabric


54


is coated with a conductive substance by electrolessly plating the fabric


54


in one embodiment. The electroless plating deposits from five to forty percent (by weight) silver, nickel, copper, tin or other metal or combination of metals


56


on the fabric


54


. In another embodiment each of the plurality of fibers forming the fabric (plane)


54


are electrolessly plated and then woven. An environmental coating


58


is then applied over the fabric


54


. The environmental coating


58


is an elastomeric coating (elastomer) which can be in the form of fluorosilicones, fluoroelastomers, silicones, thermoplastic elastomers, urethanes or other viable elastic materials. An elastomeric adhesive (adhesive)


60


is applied to a side of the environmental coating


58


to attach the elastic ground plane to the surface


52


.




Tests have shown that the elastic ground plane is capable of a minimum of 100% elongation in all directions at the required operating temperature (operating range) (e.g., −65° to 250° Fahrenheit). The elastic ground plane has a resistance of less than 0.8 Ohms per square, even when elongated and after repeated high strain loading conditions, providing an excellent ground plane. The tensile moduli for the material is less than 1,000 pounds per square inch (PSI) over the operating conditions. A low tensile moduli is important when the elastic ground plane is placed on a rod reinforced elastomer. The low tensile moduli allows the rod reinforced elastomer to be elongated and deflected without requiring a large force to drive the rod reinforced elastomer. Placing the elastic ground plane over the rod reinforced elastomer also increases the tear resistance of the elastomer by two and half times.





FIG. 5

shows an alternative embodiment of the elastic ground plane


50


. In this embodiment the fabric (plurality of fibers)


54


only has the environmental coating


58


on the top surface of the fabric


54


(as opposed to encasing the fabric as in FIG.


4


). The elastomeric adhesive is applied to a second surface of the fabric


54


or to the surface


52


, to attach the elastic ground plane to the surface


52


.

FIG. 6

shows a third embodiment of a process for making and applying the elastic ground plane


50


. In this embodiment the conductive fabric


54


,


56


is prepared first. Next, the conductive fabric


54


,


56


is cleaned with a solvent. Then an elastomeric adhesive


60


is applied to a surface


52


and the fabric


54


is placed on the adhesive


60


. Last, the environmental elastomeric coating is applied by a sprayer


62


.




Thus there has been described an elastic ground plane that can easily and significantly elongate in all direction, is highly conductive in all states of elongation, can withstand repeated elongations with no degradation in shielding effectiveness or material properties, is thin and light weight and which is tough enough to withstand severe aircraft environments.




While the invention has been described in conjunction with specific embodiments thereof, it is evident that many alterations, modifications, and variations will be apparent to those skilled in the art in light of the foregoing description. Accordingly, it is intended to embrace all such alterations, modifications, and variations in the appended claims.



Claims
  • 1. An elastic ground plane comprising:an environmental coating; a fabric having a plurality of fibers capable of a minimum of 100% elongation, the fabric attached on a first surface thereof the environmental coating; and a conductive substance coating the fabric.
  • 2. The elastic ground plane of claim 1, further including an adhesive applied to a second side of the fabric.
  • 3. The elastic ground plane of claim 2, wherein the adhesive is an elastomer.
  • 4. The elastic ground plane of claim 2, further including a reinforced elastomer attached to the adhesive.
  • 5. The elastic ground plane of claim 1, wherein the environmental coating is an elastomer.
  • 6. The elastic ground plane of claim 1, wherein the environmental coating is an elastomeric coating selected from the group of fluorosilicones, fluoroelastomers, silicones, thermoplastic elastomers and urethanes.
  • 7. The elastic ground plane of claim 1, wherein the plurality of fibers include an elastic fiber.
  • 8. The elastic ground plane of claim 1, wherein the fabric has a warp knit style weave.
  • 9. The elastic ground plane of claim 1, wherein the conductive substance is a metal.
  • 10. The elastic ground plane of claim 9, wherein the conductive substance is between 5 and 40 weight percent of the fabric.
  • 11. An elastic conductive material, comprising:a plurality of fibers forming a plane wherein the plane is capable of 100% elongation; a conductive substance coating the plurality of fibers; and an elastomeric coating attached to a surface of the plane.
  • 12. The elastic conductive material of claim 11, wherein a tensile moduli of the plane is less than 1000 pounds per square inch.
  • 13. The elastic conductive material of claim 12, wherein a resistance is less than 0.8 Ohms per square throughout an operating range.
  • 14. The elastic conductive material of claim 11, further including an elastomeric adhesive covering a side of the elastomeric coating.
  • 15. An elastic ground plane adapted to be secured to a stretchable surface, the elastic ground plane comprising:a fabric having a plurality of fibers, the fabric being adapted to be secured to said stretchable surface and capable of elongation; a conductive substance coating the plurality of fibers; an environmental coating applied to at least a portion of a first surface of the fabric; and wherein the elastic ground plane is capable of a minimum of 100% elongation and is in accordance with that of the stretchable surface to which it is secured.
  • 16. The elastic ground plane of claim 15, further including an adhesive applied to a second side of the fabric for securing the fabric to the stretchable surface.
  • 17. The elastic ground plane of claim 16, wherein the adhesive is an elastomer.
  • 18. The elastic ground plane of claim 15, wherein the environmental coating is an elastomeric coating selected from the group of fluorosilicones, fluoroelastomers, silicones, thermoplastic elastomers and urethanes.
  • 19. The elastic ground plane of claim 15, wherein the plurality of fibers include an elastic fiber.
  • 20. The elastic ground plane of claim 15, wherein the fabric has a warp knit style weave.
  • 21. The elastic ground plane of claim 15, wherein the conductive substance is a metal.
  • 22. The elastic ground plane of claim 21, wherein the conductive substance is between 5 and 40 weight percent of the fabric.
  • 23. An elastic conductive material, comprising:a plurality of fibers forming a plane, capable of 100% elongation; a conductive substance coating the plurality of fibers; and an elastomeric coating attached to a surface of the plane and capable of elongation.
  • 24. The elastic conductive material of claim 23, wherein a tensile moduli of the plane is less than 1000 pounds per square inch.
  • 25. The elastic conductive material of claim 24, wherein a resistance is less than 0.8 Ohms per square throughout an operating range.
  • 26. The elastic conductive material of claim 23, further including an elastomeric adhesive covering an other side of the elastomeric coating.
  • 27. An elastomeric structure incorporating electromagnetic shielding, the structure comprising:an elastomeric substrate capable of a minimum of 100% elongation; a fabric having a plurality of fibers forming a panel, the fabric being securable to the elastomeric substrate and further being capable of a same degree of elongation in accordance with that of the elastomeric substrate; and a conductive substance coating the plurality of fibers such that the fibers provide an electromagnetic shielding effect to the elastomeric structure without impeding elongation of the fabric.
  • 28. The elastomeric structure of claim 27, further comprising an environmental coating applied to at least a portion of a surface of the fabric.
  • 29. The elastomeric structure of claim 27, further comprising an adhesive for securing the fabric to the elastomeric substrate.
  • 30. The elastomeric structure of claim 28, wherein the environmental coating is comprised of an elastomeric coating of material from the group of fluorosilicones, fluoroelastomers, silicones, thermoplastic elastomers and urethanes.
Parent Case Info

This application is a divisional application of Ser. No. 08/718,771, filed on Sep. 24, 1996, now U.S. Pat. No. 6,048,581.

US Referenced Citations (46)
Number Name Date Kind
1942867 Leguillon Jan 1934 A
2152029 Cone Mar 1939 A
2173262 Monegan et al. Sep 1939 A
2368702 Bourne Feb 1945 A
2504684 Harper Apr 1950 A
2716460 Young Aug 1955 A
2731221 Holton Jan 1956 A
3586267 Ingelman-Sundberg Jun 1971 A
4296900 Krall Oct 1981 A
4427169 Brown Jan 1984 A
4429844 Brown et al. Feb 1984 A
4461611 Michel Jul 1984 A
4706913 Cole Nov 1987 A
4892626 Covey Jan 1990 A
4966802 Hertzberg Oct 1990 A
5094412 Narramore Mar 1992 A
5222699 Albach et al. Jun 1993 A
5288039 DeLaurier et al. Feb 1994 A
5326050 Zell Jul 1994 A
5367970 Beauchamp et al. Nov 1994 A
5374011 Lazarus et al. Dec 1994 A
5481184 Jacobsen Jan 1996 A
5487351 Nedderman, Jr. Jan 1996 A
5639215 Yamakawa et al. Jun 1997 A
5662294 MacLean et al. Sep 1997 A
5700337 Jacobs et al. Dec 1997 A
5794893 Diller et al. Aug 1998 A
5803405 Ellis et al. Sep 1998 A
5806808 O'Neil Sep 1998 A
5839700 Nedderman, Jr. Nov 1998 A
5892877 Meyerhoefer Apr 1999 A
5896191 Beier et al. Apr 1999 A
5918834 Sommer et al. Jul 1999 A
5927651 Geders et al. Jul 1999 A
5947417 Cameron Sep 1999 A
5947422 Wille Sep 1999 A
5958803 Geiger Sep 1999 A
5975463 Gruensfelder et al. Nov 1999 A
5979828 Gruensfelder et al. Nov 1999 A
6027074 Cameron et al. Feb 2000 A
6048581 Waldrop, III Apr 2000 A
6068215 Gruensfelder et al. May 2000 A
6076766 Gruensfelder Jun 2000 A
6079667 Gruensfelder Jun 2000 A
6089505 Gruensfelder et al. Jul 2000 A
6092764 Gruensfelder et al. Jul 2000 A