Metallisation of a housing of an aeronautic engine made of electrically insulating material
View Patent ↗The invention relates to an aeronautic engine ( 1 ), comprising: a housing ( 10 ), made of electrically insulating material, a first metal piece ( 2, 3 ), and electrical equipment ( 30 ), fixed to the housing ( 10 ) and connected to the first metal piece ( 2, 3 ) by means of an electrically conductive connection path ( 16, 18 ) and a first connecting flange ( 12, 14 ) of the housing ( 10 ).
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.
2. The aeronautic engine according to claim 1 , wherein the connection path comprises at least one of the following elements: a metal-metal contact, a ground braid.
3. The aeronautic engine according to claim 2 , wherein the metal-metal contact comprises a metal support fixed both to the electrical equipment and also to the first connecting flange.
4. The aeronautic engine according to claim 3 , wherein:
the electrically insulating material of the housing comprises a composite material, said composite material comprising a fibrous reinforcement densified by a polymer matrix,
at the level of the contact between the metal support of the electrical equipment and the housing, the fibres of the composite material of the housing are at least partially exposed to improve metal-metal contact between the metal support and the first connecting flange and improve contact between the connection path and the first connecting flange.
5. The aeronautic engine according to claim 1 , wherein the electrical equipment comprises at least one of the elements of the following group: a computer, a sensor.