Patent ID: 9595774
Date: 2017-03-14
CPC Classifications: F01D,F02C,H01R,H02G

Claim:
1. An aeronautic engine, comprising: a housing, a first metal piece, a second metal piece, and electrical equipment, fixed on the housing and connected to the first metal piece with an electrically conductive connection path, wherein the housing is made of electrically insulating material, and the housing comprises a first connecting flange on a downstream of the engine, adapted to fix the housing to the first metal piece, the electrically conductive connection path being connected to the first metal piece through said first connecting flange; and the electrically conductive connection path further adapted to electrically connect the electrical equipment to an air inlet sleeve comprising the second metal piece, through a second connecting flange located on an upstream of the engine and adapted to fix the second metal piece to the housing.