Process for manufacturing a gas turbine engine case out of...

B - Operations – Transporting – 29 – C

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B29C 70/28 (2006.01) B29C 70/24 (2006.01) F01D 25/24 (2006.01)

Patent

CA 2621729

Un carter en matériau composite d'épaisseur variable, notamment pour une soufflante de turbine à gaz est réalisé par formation d'un renfort fibreux et densification du renfort par une matrice. Le renfort fibreux est formé par un enroulement en couches superposées sur un mandrin (40) d'une texture fibreuse (30) réalisée par tissage tridimensionnel avec épaisseur évolutive. Figure 7

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