A heated floor panel for an airborne vehicle and an airborne vehicle having at least one heated floor panel are described. The floor panel includes a controller housing, a first heated panel configured to heat the floor panel, a panel connector arranged in a wall of the controller housing, at least one power line coupled between the panel connector and the first heated panel and configured to supply electric power, which is input to the panel connector, to the first heated panel, a switch connected in one of the power lines, and a microcontroller connected to the switch and configured to actuate the switch for interrupting the electric power supply to the first heated panel in case of an electric fault in the floor panel.
Heated floor panel for an aircraft and aircraft having a heated floor panel
2020-05-19
Patent
Electronic Resource
English