Title:
航空機の外装保護のための環境的に安定したハイブリッド織物システム
Document Type and Number:
Japanese Patent JP4964245
Kind Code:
B2
Abstract:
A method of forming an exterior surface protective structure (12) 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 a structure 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).
Inventors:
Brown, Arlene M
Application Number:
JP2008537860A
Publication Date:
June 27, 2012
Filing Date:
October 24, 2006
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64C1/00; B64C1/12; D03D1/00; D03D15/00; D03D15/02; D03D15/12
Domestic Patent References:
| JP2003147103A |
Foreign References:
| WO2004000643A1 |
Attorney, Agent or Firm:
Sonoda Yoshitaka
Kobayashi Yoshinori
Kobayashi Yoshinori