Environmentally stable hybrid fabric system for exterior...

Details Environmentally stable hybrid fabric system for exterior... Environmentally stable hybrid fabric system for exterior...

2008-07-22

2008-07-22

Huson, Monica A (Department: 1791)

Plastic and nonmetallic article shaping or treating: processes

Mechanical shaping or molding to form or reform shaped article

To produce composite, plural part or multilayered article

C156S273900

Reexamination Certificate

active

07402269

ABSTRACT:
A method of forming an exterior surface protective structure (12) for an aircraft (10) includes uniting a loaded surfacer (52) having a carrier (51) to a hybrid prepreg substrate (32). The prepreg substrate (32) includes a carbon fabric (44) with an integral conductive component (48) having conductivity with in a metal conductivity range and is united to a base substrate (30). The loaded surfacer (52) and the prepreg substrate (32) are cured, which includes interfacially adhering matter between the loaded surfacer (52) and the prepreg substrate (32). A protective fabric system (12) for an exterior (14) of an aircraft (10) includes the base substrate (30). The hybrid prepreg substrate (32) is coupled to the base substrate (30). The loaded surfacer (52) with the carrier (51) is interfacially adhered to the prepreg substrate (32).

REFERENCES:
patent: 5225265 (1993-07-01), Prandy et al.
patent: 5370921 (1994-12-01), Cedarleaf

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