Sound attenuating aircraft reactor nacelle

Details Sound attenuating aircraft reactor nacelle Sound attenuating aircraft reactor nacelle

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/24 (2006.01) F02C 7/045 (2006.01)

Patent

CA 2441058

According to the invention, the acoustic attenuation internal tubular piece (10) covering the air intake (6) has no internal assembly fishplate and the tubular transition part (17) between the air intake (6) and the fan casing (16) is acoustically homogeneous.

Selon l'invention, la pièce tubulaire interne d'atténuation acoustique (10) revêtant l'entrée d'air (6) ne comporte aucune éclisse d'assem- blage interne et la partie tubulaire (17) de transition entre l'entrée d'air (6) et le carter de soufflante ( 16) est acoustiquement homogène.

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