| 摘要 |
The panel has a heat producing layer (22), and an upper layer (24) resisting impacts provoked by circulation of object e.g. trailed luggage, on the panel in a heated zone of an aircraft. The upper layer has a heat conducting layer having units providing solidity in a die and has an average energy value required for breaking insulation resistance and penetration in surface, where upper layer supports 90 percent of the value. An independent claim is also included for a method for fabricating an aircraft floor panel. |
