发明名称 Verfahren zur Herstellung einer kohlenfaserverstärkte Wabenstruktur
摘要 A method for preparing a carbon honeycomb structure comprises the steps of alternately stacking a plurality of corrugated sheets, each of which is produced by corrugating a supporting base of carbon fibers impregnated with an epoxy resin prepolymer and then curing the prepolymer, and a plurality of flat sheets, each of which is prepared by curing a supporting base of carbon fibers impregnated with an epoxy resin prepolymer, through a node bond adhesive; curing the adhesive to form a honeycomb structure; dipping the resulting honeycomb structure in a phenolic resin prepolymer solution; evaporating the solvent; then curing the phenolic resin prepolymer; repeating these dip, evaporation and curing processes to coat the honeycomb structure with a predetermined amount of the phenolic resin; and cutting the coated honeycomb structure to a predetermined thickness. The method permits the use of a dipping solution having a high concentration and as a result, the number of steps required for dipping may substantially be reduced. Moreover, the dipping solution is never repelled even if the dipping steps are repeatedly carried out. In addition, only a small quantity of burrs are formed when cutting the honeycomb structure. The honeycomb structure shows only slight reduction in the strength under high humidity conditions.
申请公布号 DE69504001(T2) 申请公布日期 1999.02.25
申请号 DE1995604001T 申请日期 1995.10.13
申请人 SHOWA AIRCRAFT INDUSTRY CO.,LTD., TOKIO/TOKYO, JP 发明人 KOMINE, TAKAYA, C/O SHOWA AIRCRAFT IND. CO., LTD., TOKYO, JP;KATOH, KIMITOSHI, C/O SHOWA AIRCRAFT IND.CO., LTD., TOKYO, JP
分类号 B29B15/10;B29D99/00;(IPC1-7):B29D31/00 主分类号 B29B15/10
代理机构 代理人
主权项
地址