| CPC B64D 13/06 (2013.01) [B64D 2013/0603 (2013.01)] | 13 Claims |

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1. A humidification system for aircrafts comprising:
a first duct configured to guide a first air stream;
a second duct configured to guide a second air stream, said second duct comprising a humidifier for humidifying the air in the second duct;
a first conduit for directing a part of the second air stream to the first duct, said first conduit comprising a first conduit inlet leading into the first duct and a first conduit outlet extending from the second duct; and
a second conduit for directing a part of the first air stream to the second duct, said second conduit comprising a second conduit inlet leading into the second duct and a second conduit outlet extending from the first duct, wherein the first conduit outlet is arranged downstream of the humidifier, the second conduit inlet is arranged separate from the first conduit outlet and wherein the first conduit inlet is arranged separate from the second conduit outlet, wherein the first duct and the second duct each carry humidified air downstream the first conduit inlet and downstream the second conduit inlet, respectively, when the humidification system is in use.
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