| CPC B64D 47/06 (2013.01) [B64C 11/00 (2013.01); B64D 41/00 (2013.01); F21S 9/04 (2013.01); H02G 1/06 (2013.01); H02G 3/22 (2013.01); H02K 99/10 (2016.11); B64D 2203/00 (2013.01); F21W 2107/30 (2018.01)] | 16 Claims |

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1. A contactless power generation system for an aircraft lighting arrangement, the power generation system comprising: at least one magnet configured on a stationary aircraft structure; at least one coil mounted on an aircraft apparatus, the coil generating an electrical current using the magnet upon rotation of the aircraft apparatus; an electrical connection electrically connecting the coil to a lighting arrangement existing on a portion of the aircraft apparatus; a first socket formed into a forward facing surface of a blade tip of the aircraft apparatus, and a second socket formed into a rear facing surface of the blade tip, wherein the lighting arrangement includes a first lighting component incorporated into the first socket and a second lighting component incorporated into the second socket.
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