发明名称 AIRCRAFT INSULATION SYSTEMS AND METHODS WITH FIRE PENETRATION RESISTANT COVERING
摘要 In one of the embodiments of the disclosure, there is provided an aircraft insulation system and method for providing fire penetration resistance and/or thermal and acoustic protection. The aircraft insulation system comprises one or more insulation blankets, each having an inboard side and an outboard side. The aircraft insulation system further comprises a fire penetration resistant cover material having a heat seal adhesive, wherein the fire penetration resistant cover material covers the outboard side of the one or more insulation blankets. The aircraft insulation system further comprises an insulation cover film having a heat seal adhesive, wherein the insulation cover film covers the inboard side of the one or more insulation blankets. The aircraft insulation system further comprises a thermal heat seal that joins the fire penetration resistant cover material and the insulation cover film together to form a continuous insulation blanket assembly.
申请公布号 CA2697797(A1) 申请公布日期 2010.09.30
申请号 CA20102697797 申请日期 2010.03.24
申请人 THE BOEING COMPANY 发明人 HOSSAIN, ZAHID;BORUMAND, KHASHAYAR;SHARMA, NEHA;COUILLIARD, KEITH;KUMAR, GAURAV;FINERTY, SEAN M.;WALTER, SARA LYNN
分类号 B64C1/40;B64C1/38 主分类号 B64C1/40
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