发明名称 |
Hybrid composite articles and missile components, and their fabrication |
摘要 |
<p>A surface-protected composite article (40), such as a component of a missile (20), is prepared with a heat-sink substrate (42), a first composite layer (44) of an pre-ceramic-matrix structural composite material, and a second composite layer (46) of a reinforced silicone pre-ceramic material. The silicone material is co-curable with the organic matrix of the first composite layer (44). The silicone at the surface (48) of the article (40) is thereafter converted to a silica refractory by an appropriate treatment such as exposure to an oxygen-rich plasma or a high-surface temperature. The silica protects the surface of the composite material. <IMAGE></p> |
申请公布号 |
EP0747661(A3) |
申请公布日期 |
1997.12.03 |
申请号 |
EP19960303655 |
申请日期 |
1996.05.22 |
申请人 |
HUGHES MISSILE SYSTEMS COMPANY |
发明人 |
BROWN, JANIS M.;ALLRED, RONALD E.;DUNCAN, TOM;FACCIANO, ANDREW B.;KIRBY, KEVIN W. |
分类号 |
F42B15/34;B32B18/00;F42B12/76;(IPC1-7):F42B12/76 |
主分类号 |
F42B15/34 |
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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