发明名称 Composite material structure with integrated insulating blanket and method of manufacture
摘要 A load-bearing composite material structure (2) includes a first ply (10) of fiber reinforced composite material, and an integral blanket (20) for thermal and flame protection. Blanket (20) includes an outer flame resistant face sheet (28), an intermediate layer of insulation fill (26), and an inner face sheet (22). Sheet (22) is formed by a second ply of fiber reinforced composite material. Preferably, a thin film (24) is provided between ply (22) and fill (26) to prevent absorption of matrix material into fill (26). The layers (22, 24, 26, 28) of blanket (20) are stitched together with flame resistant thread (30). Plies (10, 22) are cured together to bond them together and integrate blanket (20) into structure (2).
申请公布号 US4567076(A) 申请公布日期 1986.01.28
申请号 US19840592539 申请日期 1984.03.23
申请人 THE BOEING COMPANY 发明人 THERRIEN, KEITH E.
分类号 B32B7/02;E04C2/284;E04C2/36;(IPC1-7):B32B3/06 主分类号 B32B7/02
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