发明名称 Method and apparatus for forming airfoil structures
摘要 An assemblage for bonding the skin of an airfoil to the core of the airfoil includes a hybrid caul plate assembly for covering the surface of the airfoil assembly which is exposed to bonding pressure. The hybrid caul plate includes a central elastomeric component and peripheral semi-rigid metal components. The semi-rigid metal components are formed from a steel sinusoidal mesh and are axially elongated. The mesh is flexible in the direction of elongation, but are rigid in the transverse direction. The peripheral semi-rigid caul componnents will thus closely conform to the contours of the core in the axial direction, and will, at the same time, provide support for the edges of the core so that the core edges will not be crushed or deformed by bonding pressure applied to the assemblage during the skin-to-core bonding process. The result of using the hybrid caul plate assembly is an improved skin-to-core bond wherein bridging or voids in the bond line at the periphery of the airfoil are avoided.
申请公布号 US6197146(B1) 申请公布日期 2001.03.06
申请号 US19980217305 申请日期 1998.12.21
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 SUCIC STEVE;SUCIC LORI ANN M.
分类号 B29C43/18;B29C43/36;B29C65/70;B29D24/00;(IPC1-7):B29C33/18 主分类号 B29C43/18
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