Patent ID: 9067684
Filing Date: 2015-06-30
Classification: B64C,B64D,H02K

Abstract:
1. An electrical power supply device for powering at least one piece of equipment of an aircraft rotor driven by a mast, said device comprising a removable pole suitable for being reversibly secured to said mast, said pole having a rotary casing provided with fastener means for fastening to said mast, and a non-rotary casing secured to link means suitable for being fastened to a reference member of said aircraft, wherein said pole comprises: a non-rotary converter fastened to the non-rotary casing and provided with an inlet suitable for being fed with electricity coming from an electricity network of said aircraft, said non-rotary converter being an electrical converter that generates AC at a frequency higher than one kilohertz from said electricity fed to the inlet; and a rotary transformer incorporated in the pole, said transformer having a primary member secured to the non-rotary casing and a secondary member secured to the rotary casing, the primary member being connected to the non-rotary converter to receive said AC, and the secondary member being suitable for electrically powering equipment of a rotor.