Turbine engine for aircraft

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 7/04 (2006.01) F02K 3/06 (2006.01)

Patent

CA 2656137

According to the invention, the internal wall of the air intake (2) and the housing of the fan (3) form a single tubular piece (30) made from a fibre/resin composite material.

- Selon l'invention, la paroi interne de l'entrée d'air (2) et le carter de la soufflante (3) forment une unique pièce tubulaire (30) réalisée en une matière composite fibres/résine.

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