| 摘要 |
A method for at least partially de-icing an aircraft by applying a de-icing fluid through a nozzle (10) is disclosed. The method involves the steps of : measuring a distance to an outside surface of the aircraft, applying the distance in an evaluation, controlling the position and/or the orientation of the nozzle (10) according to the evaluation, and applying the de-icing fluid to at least a part of the outside surface trough the nozzle. In addition, a system for performing the de-icing method is also revealed. |
