发明名称 Light Weight Thermoplastic Flex Foam and Hybrid Duct System
摘要 An aerospace vessel including a fuselage, a means for causing the fuselage to fly coupled to the fuselage, and an environmental control system within the fuselage. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.
申请公布号 US2013276959(A1) 申请公布日期 2013.10.24
申请号 US201313922246 申请日期 2013.06.20
申请人 THE BOEING COMPANY 发明人 FRANTZ WALTER FORREST;PATEL JAYANT D.;MABEN DOUGLAS DEAN;WHITMAN BRUCE;FREEMAN DOUGLAS E.
分类号 B29D23/00 主分类号 B29D23/00
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