发明名称 |
BURN THROUGH RESISTANT SYSTEMS FOR TRANSPORTATION, ESPECIALLY AIRCRAFT |
摘要 |
An encapsulated insulation composite system for increasing the bum through resistance of an aircraft fuselage includes: an insulation layer of glass fiber or foam insulation and a coating or interleaf barrier layer of a high temperature resistant material and/or a coating or barrier layer of a high temperature resistant material on an outer major surface of the insulation layer of the composite and a film encapsulating the composite. Preferably, the barrier layer or layers include a reflective mineral, such as a reflective mineral containing coating carried on a sheet material. Preferably, the encapsulating film is a polymeric film such as a~ polyimide film.
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申请公布号 |
CA2326314(C) |
申请公布日期 |
2006.07.11 |
申请号 |
CA19992326314 |
申请日期 |
1999.11.16 |
申请人 |
JOHNS MANVILLE INTERNATIONAL, INC. |
发明人 |
WULLIMAN, REBECCA SUE;FAY, RALPH MICHAEL;STACY, JAMES WALTER;TOWNSEND, JEFFREY CANON;VOLENEC, STEVEN N. |
分类号 |
B64C1/40;B32B3/00;B32B5/22;B32B5/26;B32B17/10;B32B27/00;B32B27/12;B32B27/20;B64C1/12 |
主分类号 |
B64C1/40 |
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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