| 摘要 |
A heated floor panel system for an aircraft, the floor panel system comprising a floor panel element including a panel structure and a panel heater device, a temperature sensor device for detecting the temperature at the floor panel element, and a connector device connected to the floor panel element, wherein the connector device comprises a power link for providing an electric power connection between the panel heater device and an electric power supply, and a data link for providing a data connection between the temperature sensor device and a control unit. An object of the present disclosure, to provide a floor panel system including a floor panel element which has a possibly simple construction and which can be used independently from the connector device, is achieved in that the temperature sensor device is located in the connector device and connected to the floor panel element via a thermal conductor element. |
