发明名称 COMPOSITE TURBOMACHINERY BLADE.
摘要 A turbomachine blade comprises a central core (1) covered by a plurality of layers (3) of composite material, and an outer sleeve (4) of woven composite material. A network of transverse seams (5) pass through the layers of composite material, and preferably also the core and the outer sleeve. The core may be formed from for example a layer of carbon or glass fibres impregnated with resin. The layers are made from a woven composite material comprising, for example, carbon fibres, ceramic fibres or metallic fibres which may be impregnated with epoxy resin. The seams may be made from fibres of the same type. Such a construction is particularly applicable to large diameter turbine blades. <IMAGE>
申请公布号 GB2262315(A) 申请公布日期 1993.06.16
申请号 GB19920023581 申请日期 1992.11.11
申请人 SOCIETE * NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "S.N.E.C.M.A." 发明人 JOEL MICHEL DANIEL * BENOIT;BRUNO JACQUES GERARD * DAMBRINE;LAURENT JEAN PIERRE * DAVID;PATRICK * FOUCHE;DANIEL GEORGES * GIRAULT;CHRISTOPHE GERARD REGIS * GROSBOIS;CATHERINE LAURENCE FRANCOISE * GUET
分类号 B29C70/54;B29D99/00;B32B7/08;B64C3/20;D03D25/00;F01D5/28;F01D9/02 主分类号 B29C70/54
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