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 |
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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