Patent ID: 11881754
Assignee: SAFRAN AIRCRAFT ENGINES
Field: Electrical machinery, apparatus, energy (Electrical engineering)
Classification: CPC H  F  Y | IPC F  H

Claim 0:
1. An assembly for an aircraft turbomachine, comprising:
an electric machine of annular shape,
at least one electrically conductive rigid bar (80) for electrically connecting the electric machine comprising:
a body made of an electrically conductive material with an elongated shape and a polygonal cross-section greater than or equal to 50 mm2, and
an electrical insulation sheath which surrounds said body,

at least one of the longitudinal ends of the body not being covered by the sheath and comprising a through orifice in which is mounted a bolt for attaching and electrically connecting this end, and
an electric harness for connecting a stator of the machine to the bar, the electric harness comprising an end equipped with a lug which is applied and tightened on said end of the bar, by means of said bolt.