Patent ID: 11858643
Assignee: AIRBUS HELICOPTERS
Field: Transport (Mechanical engineering)
Classification: CPC B  H | IPC B  H

Claim 11:
12. AAn aerial vehicle drone comprising:
a body; and
at least one rotor carried by the body, the at least one rotor including a piece of rotary equipment having a rotary assembly for the aerial vehicle drone, the rotary assembly having a rotary wing blade and including a skin having an outside face having a furrow extending from a first end to a second end and having at least one change of direction, the skin comprising a composite material provided with a laser activated organic metal, the rotary equipment including a deicer comprising an electrically conductive track extending in the furrow from a first terminal to a second terminal,
the at least one furrow being a laser formed furrow on an external surface of the skin,
the electrically conducting track of the deicer being formed in the at least one laser formed furrow and being a catalyzed anchored electrically conducting track comprising the laser activated composite material, and
wherein the electrically conducting track is covered with the protective layer.