Verfahren und Maschine für die Fabrikation einer blockförmigen Armierung für ein Teil aus Verbundmaterial
摘要
The composite framework structure is a block (B) formed by a continuous succession of plates (30), to be embedded in a hardened matrix. Each plate has layers of filament grids overlaid in parallel in each layer and partially parallel and at an angle to other layers, held together by a locking filament (Fl) which also holds the plates (30) together. <IMAGE>
申请公布号
DE69500716(T2)
申请公布日期
1998.02.19
申请号
DE1995600716T
申请日期
1995.04.03
申请人
AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE, PARIS, FR
发明人
FANTINO, LUCIEN, F-33700 MERIGNAC, FR;CAHUZAC, GEORGES, F-33110 LE BOUSCAT, FR