| 摘要 |
The present invention relates to an aircraft, comprising an actuator and/or comprising a brake having desiccant for absorbing liquid, in particular condensate, and/or having heating means for heating the actuator/the brake in order to evaporate liquid in or on the actuator/the brake and/or in order to de-ice the actuator/the brake, wherein the heating means are formed by one or more existing components of the actuator/the brake. |
