发明名称 AIRCRAFT HEATED FLOOR PANEL
摘要 An aircraft heated floor panel (10/110/210) including a support level (40/140/142), a heater level (42/142/242) and a protective cover layer (16/116/216). The support level and the heater level are formed as a composite structure (18/118/218), such as by curing a series of layers together to form the structure. A thermal conductor (62) may be provided to more evenly distribute a generated heat pattern. Alternatively, a metal sheet (116/216) may be used for the cover layer which performs a heat distributing function. If a metal sheet (216) is used, an elastic-after-bonding adhesive (266) may be used to secure the metal sheet (216) to the heater level (242) to accommodate different rates of thermal expansion.
申请公布号 WO0117850(A1) 申请公布日期 2001.03.15
申请号 WO2000US24874 申请日期 2000.09.11
申请人 BFGOODRICH COMPANY 发明人 GIAMATI, MICHAEL, J.;SCHRAMM, KEVIN, C.
分类号 B32B15/04;B64C1/18;B64C1/40;B64D13/08;F24D13/02;H05B3/22 主分类号 B32B15/04
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