F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 1/48 (2006.01) F02K 1/38 (2006.01)
Patent
CA 2721227
The invention relates to a dual-flow turbine engine for an aircraft with low noise emission, wherein the opening (6) for the cold flow (9) of the turbine engine is provided with short, narrow, and spaced chevrons (15) that penetrate deeply, like claws, into said cold flow (9).
Turbomoteur à double flux pour aéronef à émission de bruit réduite. - Selon l'invention, l'orifice (6) du flux froid (9) du turbomoteur est équipé de chevrons (15) courts, étroits et espacés, pénétrant fortement dans ledit flux froid (9) à la manière de griffes.
Debatin Klaus
Huber Jerome
Pelagatti Olivier
Sylla Amadou Andre
Airbus (sas)
Airbus Operations (sas)
Robic
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