发明名称 |
Process for the manufacture of a honeycomb panel made of a carbon/carbon or carbon/ceramic composite and structures fabricated with such a panel |
摘要 |
<p>Producing a carbon/carbon or carbon/ceramic composite honeycomb panel involves: (a) forming a honeycomb support by pyrolysis of a honeycomb structure (1) of carbon fabric pre-impregnated with a thermosetting resin; (b) forming one or more skins (2, 3) by draping carbon fabrics pre-impregnated with thermosetting resin; (c) assembling the support and the skin(s) with an interposed carbon fabric pre-impregnated with a thermosetting resin; (d) simultaneously polymerising and compacting the assembly; (e) pyrolysing the assembly; and (f) densifying and increasing the cohesion of the assembly by chemical vapour phase infiltration (CVI). Also claimed is a wall structure consisting of a sandwich formed by the above method. Preferably, the thermosetting resin, used in steps (a), (b) and (c), is selected from phenolic, polyimide, furan and polycyanate resins.</p> |
申请公布号 |
EP0796829(A1) |
申请公布日期 |
1997.09.24 |
申请号 |
EP19970450003 |
申请日期 |
1997.03.17 |
申请人 |
AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE |
发明人 |
ROUSSEAU, GERARD;PASQUET, JEAN CHRISTOPHE |
分类号 |
C04B35/83;B32B3/12;(IPC1-7):C04B35/83;B32B18/00;C04B35/80 |
主分类号 |
C04B35/83 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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