| 摘要 |
<p>The method involves drawing out a part of stream of cold air with temperature ranging from minus 1 degree Celsius to 5 degree Celsius. The part of the stream of cold air is heated to form a stream of hot air, at temperature ranging from 10 degree Celsius to 60 degree Celsius, using a heating element selected from a group formed by electric resistance heating elements and heating elements by heat exchange, and heat sources of an aircraft (13). The stream of hot air is introduced into a crown (19) of the aircraft. The heat sources are selected from a group formed by primary heat exchangers in a non-pressurized zone, secondary heat exchangers, recirculation lines in a pressurized zone, avionic extraction lines, and hot parts of liquid loops of the aircraft. An independent claim is also included for an anti-condensation device for an aircraft.</p> |
