发明名称 Composite material structure with integral fire protection
摘要 PCT No. PCT/US84/00023 Sec. 371 Date Jan. 9, 1984 Sec. 102(e) Date Jan. 9, 1984 PCT Filed Jan. 9, 1984.A load-bearing composite material structure (2, 2') has a plurality of layers of composite material. Each layer includes a matrix material (4) that maintains its structural integrity at 1200 DEG F. for at least five minutes. Preferred matrix materials are polyimide resins. Outer layers that will be directly exposed to a fire are reinforced with a woven fabric (8) that is sufficiently flame resistant and has a sufficiently fine weave to prevent flame penetration at 2000 DEG F. for at least fifteen minutes. The woven fabric (8) is preferably ceramic. The rest of the layers are reinforced with a fibrous material (6) to provide the necessary structural strength. The layers may be laminate cured together to form a single, integral structure (2) or such laminates adhesively bonded to a honeycomb (12).
申请公布号 US4767656(A) 申请公布日期 1988.08.30
申请号 US19840573976 申请日期 1984.01.09
申请人 THE BOEING COMPANY 发明人 CHEE, WAN T.;MCLAREN, DOUGLAS;THERRIEN, KEITH E.
分类号 B32B3/12;B64C1/40;E04B1/94;(IPC1-7):B32B3/12 主分类号 B32B3/12
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